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TWI768257B - Wind power plant and wind power system - Google Patents

Wind power plant and wind power system Download PDF

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TWI768257B
TWI768257B TW108139611A TW108139611A TWI768257B TW I768257 B TWI768257 B TW I768257B TW 108139611 A TW108139611 A TW 108139611A TW 108139611 A TW108139611 A TW 108139611A TW I768257 B TWI768257 B TW I768257B
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yaw
wind power
actuators
actuator
wind
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TW108139611A
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TW202018180A (en
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佐伯満
東石良治
宮田隆弘
浅川雄一
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日商日立製作所股份有限公司
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

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  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

本發明提供一種能夠儘早地判定偏航致動器之異常之風力發電裝置及風力發電系統。 風力發電裝置2具備:支持受風而旋轉之葉輪之機艙22、將機艙22可旋動地支持之塔架21、使機艙22相對於塔架21旋動之複數個偏航致動器10、及檢測偏航致動器10之異常之異常檢測裝置30。異常檢測裝置30將各偏航致動器10之輸出之合計值與規定之第1閾值進行比較,若上述輸出之合計值超過規定之第1閾值,則判定為偏航致動器10之異常。The present invention provides a wind power generation device and a wind power generation system capable of early determination of an abnormality of a yaw actuator. The wind power generator 2 includes a nacelle 22 that supports an impeller that is rotated by wind, a tower 21 that rotatably supports the nacelle 22, a plurality of yaw actuators 10 that rotate the nacelle 22 relative to the tower 21, And the abnormality detection device 30 which detects the abnormality of the yaw actuator 10. The abnormality detection device 30 compares the total value of the outputs of the yaw actuators 10 with a predetermined first threshold value, and determines that the yaw actuator 10 is abnormal when the total value of the outputs exceeds the predetermined first threshold value. .

Description

風力發電裝置及風力發電系統Wind power plant and wind power system

本發明係關於一種風力發電裝置、及具備包括複數架風力發電裝置之風電場之風力發電系統,尤其關於一種具備偏航致動器異常檢測功能之風力發電裝置及風力發電系統。The present invention relates to a wind power generation device and a wind power generation system including a wind farm including a plurality of wind power generation devices, and more particularly, to a wind power generation device and a wind power generation system with a function of detecting abnormality of a yaw actuator.

近年來,就保護地球環境之觀點而言,利用風力進行發電之風力發電裝置備受關注。一般而言,風力發電裝置具有將複數個葉片安裝於輪轂而成之葉輪,藉由受風而旋轉之葉輪之旋轉能量來驅動發電機。 通常,風力發電裝置所受之風之條件根據地形等之影響而不同。若實際之風之條件比設計假定更嚴苛,則風力發電機所受之變動負荷增大。因此,有可能風力發電裝置之各構成零件(例如葉片、機艙、塔架及輔助設備等)較設計時所假定之時期更早受到損傷,而讓更換時期提前。於產生未曾預料之損傷之情形時,更換零件之準備或更換工程之準備等需耗費時間,因此有產生停工時間,而發電企業或製造商之損失增大之顧慮。In recent years, from the viewpoint of protecting the global environment, a wind power generating apparatus that generates power using wind power has attracted attention. Generally speaking, a wind power generator has an impeller formed by attaching a plurality of blades to a hub, and the generator is driven by the rotational energy of the impeller rotated by the wind. Generally, the wind conditions to which the wind turbine generator is subjected are different depending on the influence of the terrain and the like. If the actual wind conditions are more severe than the design assumptions, the variable load on the wind turbine will increase. Therefore, it is possible that the constituent parts of the wind power plant (such as blades, nacelles, towers and auxiliary equipment, etc.) are damaged earlier than the period assumed in the design, so that the replacement period is advanced. In the event of unforeseen damage, preparation for replacement of parts or preparation for replacement work takes time, so there is a concern that downtime will occur and the loss of power generation companies or manufacturers will increase.

例如,作為藉由發現減速機之異常並進行有計劃之修繕而可縮短發電運轉之停止時間之風力發電裝置,提出有專利文獻1中所記載之技術。於專利文獻1中揭示有如下內容:具備構成偏航驅動裝置之複數個減速機、及連結於減速機之馬達,判定減速機之異常之異常判定部將由各個電量計所測得之各馬達之累計消耗電量進行比較,於至少兩個馬達之累計消耗電量之差為規定值以上之情形時,判定與累計消耗電量較小之馬達對應之減速機處於異常狀態。又,於專利文獻1中記載有如下內容:於存在三個以上之馬達之情形時,針對所有馬達,以循環方式取每兩個累計消耗電量之差量,於所有差量中只要有一個超過規定之閾值之情形時,便判定為異常。 [先前技術文獻] [專利文獻]For example, the technology described in Patent Document 1 has been proposed as a wind power generator capable of shortening the stop time of the power generation operation by discovering the abnormality of the reduction gear and carrying out planned repairs. Patent Document 1 discloses that a plurality of speed reducers constituting a yaw drive device and a motor connected to the speed reducers are provided, and an abnormality determination unit for judging an abnormality of the speed reducer uses the values of the motors measured by the respective electricity meters. The cumulative power consumption is compared, and when the difference between the cumulative power consumption of at least two motors is greater than or equal to a predetermined value, it is determined that the reducer corresponding to the motor with the smaller cumulative power consumption is in an abnormal state. In addition, Patent Document 1 describes the following: when there are three or more motors, the difference between every two accumulated power consumption is cyclically obtained for all the motors, and only one of the differences exceeds the When the specified threshold is reached, it is judged as abnormal. [Prior Art Literature] [Patent Literature]

[專利文獻1]日本專利特開2015-74998號公報[Patent Document 1] Japanese Patent Laid-Open No. 2015-74998

[發明所欲解決之問題][Problems to be Solved by Invention]

然而,於專利文獻1中所揭示之構成中,由於基於兩個馬達之累計消耗電量之差量來判定減速機之異常,故而為了獲得累計消耗電量而需要時間,因此難以儘早地判定減速機之異常。 對此,本發明提供一種能夠儘早地判定偏航致動器之異常之風力發電裝置及風力發電系統。 [解決問題之技術手段]However, in the configuration disclosed in Patent Document 1, since the abnormality of the reducer is determined based on the difference between the accumulated power consumption of the two motors, it takes time to obtain the accumulated power consumption, so it is difficult to determine the speed reducer as soon as possible. abnormal. In view of this, the present invention provides a wind power generation device and a wind power generation system capable of early determination of an abnormality of a yaw actuator. [Technical means to solve problems]

為了解決上述問題,本發明之風力發電裝置之特徵在於具備:機艙,其支持受風而旋轉之葉輪;塔架,其將上述機艙可旋動地支持;複數個偏航致動器,其使上述機艙相對於上述塔架旋動;及異常檢測裝置,其檢測上述偏航致動器之異常;且上述異常檢測裝置將各偏航致動器之輸出之合計值與規定之第1閾值進行比較,若上述輸出之合計值超過上述規定之第1閾值,則判定為偏航致動器之異常。 又,本發明之風力發電系統之特徵在於:具備複數架風力發電裝置,並且具備異常檢測裝置,該風力發電裝置具有支持受風而旋轉之葉輪之機艙、將上述機艙可旋動地支持之塔架、及使上述機艙相對於上述塔架旋動之複數個偏航致動器,該異常檢測裝置檢測上述偏航致動器之異常,且上述異常檢測裝置將各偏航致動器之輸出之合計值與規定之第1閾值進行比較,若上述輸出之合計值超過上述規定之第1閾值,則判定為偏航致動器之異常。 又,本發明之另一風力發電系統之特徵在於:具備複數架風力發電裝置,並且具備異常檢測裝置,該風力發電裝置具有支持受風而旋轉之葉輪之機艙、將上述機艙可旋動地支持之塔架、及使上述機艙相對於上述塔架旋動之複數個偏航致動器,該異常檢測裝置檢測上述偏航致動器之異常,且上述異常檢測裝置至少將鄰接之2架風力發電裝置所具備之各偏航致動器之輸出之合計值或2架風力發電裝置所具備之各偏航致動器之輸出之曲線進行比較,於上述鄰接之2架風力發電裝置中之上述各偏航致動器之輸出之合計值或上述各偏航致動器之輸出之曲線產生變動之情形時,判定為一架風力發電裝置所具備之偏航致動器之異常。 [發明之效果]In order to solve the above-mentioned problems, the wind power generator of the present invention is characterized by comprising: a nacelle for supporting the impeller that is rotated by the wind; a tower for rotatably supporting the nacelle; and a plurality of yaw actuators for enabling The nacelle rotates relative to the tower; and an abnormality detection device detects an abnormality of the yaw actuator; and the abnormality detection device compares the sum of the outputs of the yaw actuators with a predetermined first threshold value. By comparison, if the total value of the above-mentioned outputs exceeds the above-mentioned predetermined first threshold value, it is determined that the yaw actuator is abnormal. Furthermore, the wind power generation system of the present invention is characterized by comprising a plurality of wind power generators including a nacelle for supporting an impeller that is rotated by the wind, and a tower for rotatably supporting the nacelle, and an abnormality detection device. A frame, and a plurality of yaw actuators for rotating the nacelle relative to the tower, the abnormality detection means detects the abnormality of the yaw actuator, and the abnormality detection means outputs the output of each yaw actuator The total value is compared with a predetermined first threshold value, and if the total value of the output exceeds the predetermined first threshold value, it is determined that the yaw actuator is abnormal. Further, another wind power generation system according to the present invention is characterized by comprising a plurality of wind power generators including a nacelle supporting an impeller that is rotated by wind, and supporting the nacelle in a rotatable manner, and an abnormality detection device. The tower, and a plurality of yaw actuators for rotating the nacelle relative to the tower, the abnormality detection device detects the abnormality of the yaw actuator, and the abnormality detection device at least two adjacent to the wind The total value of the output of the yaw actuators provided in the power generation device or the curves of the outputs of the yaw actuators provided by the two wind power generation devices are compared, and the above-mentioned two adjacent wind power generation devices are compared. When the total value of the output of each yaw actuator or the curve of the output of each yaw actuator described above changes, it is determined that the yaw actuator provided in one wind power generator is abnormal. [Effect of invention]

根據本發明,可提供一種能夠儘早地判定偏航致動器之異常之風力發電裝置及風力發電系統。 上述以外之課題、構成及效果係藉由以下實施形態之說明而明確。According to the present invention, it is possible to provide a wind power generation device and a wind power generation system capable of early determination of an abnormality of a yaw actuator. Problems, configurations, and effects other than those described above will be clarified by the description of the following embodiments.

於本說明書中,作為構成本發明之實施形態之風力發電系統之風力發電裝置,將順風型風力發電裝置作為一例進行說明,但亦可同樣地應用於逆風型風力發電裝置。又,構成本發明之實施形態之風力發電系統之風力發電裝置亦可設置於海洋上、山嶽部及平原部中之任一場所。 以下,使用圖式對本發明之實施例進行說明。 [實施例1]In this specification, the downwind type wind turbine generator is described as an example as the wind turbine generator constituting the wind turbine generator system according to the embodiment of the present invention, but the same can be applied to the downwind type wind turbine generator. Moreover, the wind power generator which comprises the wind power generation system of embodiment of this invention may be installed in any place of the ocean, a mountain part, and a plain part. Hereinafter, embodiments of the present invention will be described with reference to the drawings. [Example 1]

<風力發電系統> 圖1係本發明之一實施例之風力發電系統之整體概略構成圖。如圖1所示,風力發電系統1包括:風力發電裝置2、設置於運轉管理中心3內之電子終端5、設置於詳情下文敍述之風力發電裝置2內之控制裝置29、及將電子終端5與控制裝置29可相互通信地連接之通信網路6。此處,通信網路6不限為有線、或無線。<Wind power generation system> FIG. 1 is an overall schematic configuration diagram of a wind power generation system according to an embodiment of the present invention. As shown in FIG. 1 , the wind power generation system 1 includes: a wind power generation device 2 , an electronic terminal 5 provided in the operation management center 3 , a control device 29 provided in the wind power generation device 2 described in detail below, and the electronic terminal 5 The communication network 6 is connected to the control device 29 so as to be able to communicate with each other. Here, the communication network 6 is not limited to wired or wireless.

<風力發電裝置> 如圖1所示,風力發電裝置2具備:受風而旋轉之葉片24、支持葉片24之輪轂23、機艙22、及將機艙22可旋動地支持之塔架21。於機艙22內具備:連接於輪轂23且與輪轂23一起旋轉之主軸25、連接於主軸25且使旋轉速度增速之增速機26、及以經增速機26增速之旋轉速度使轉子旋轉而進行發電運轉之發電機27。將葉片24之旋轉能量傳遞至發電機27之部位被稱為動力傳遞部,於本實施例中,動力傳遞部包含主軸25及增速機26。又,藉由葉片24及輪轂23構成葉輪。如圖1所示,於塔架21內之底部(下部)配置有轉換電力頻率之電力轉換器28、進行電流之開閉之開關用開閉器及變壓器(未圖示)、以及控制裝置29等。<Wind power generator> As shown in FIG. 1 , the wind power generator 2 includes blades 24 that are rotated by wind, a hub 23 that supports the blades 24 , a nacelle 22 , and a tower 21 that rotatably supports the nacelle 22 . The nacelle 22 includes: a main shaft 25 connected to the hub 23 and rotating together with the hub 23, a speed-up gear 26 connected to the main shaft 25 and increasing the rotational speed, and a rotor for increasing the rotational speed by the speed-up gear 26. A generator 27 that rotates to generate power. The part that transmits the rotational energy of the blades 24 to the generator 27 is called a power transmission part. In this embodiment, the power transmission part includes a main shaft 25 and a speed increaser 26 . In addition, the impeller is constituted by the blades 24 and the hub 23 . As shown in FIG. 1 , a power converter 28 for converting electric power frequency, a switch for switching and a transformer (not shown) for switching current, and a control device 29 are arranged at the bottom (lower part) of the tower 21 .

作為控制裝置29,例如使用控制台或SCADA(Supervisory Control And Data Acquisition,監督控制及資料獲取)。 於本實施例中,示出利用3片葉片24及輪轂23構成葉輪之例,但並不限於此,葉輪亦可包括輪轂及至少1片葉片24。As the control device 29, for example, a console or SCADA (Supervisory Control And Data Acquisition) is used. In the present embodiment, an example in which the impeller is constituted by three blades 24 and the hub 23 is shown, but the impeller is not limited thereto, and the impeller may also include a hub and at least one blade 24 .

設置於風力發電裝置2之感測器4例如包括:設置於機艙22之上部之風向風速計、設置於葉片24之根部且量測葉片24之槳距角之槳距角感測器、量測機艙22之方位角之偏航角感測器、及量測對葉片24施加之應力之應變感測器。再者,雖未圖示,但作為感測器4,例如亦可設為包括設置於機艙22之上部且量測外部大氣溫度之溫度計、量測機艙22內之溫度之溫度計、及量測機艙22內之濕度之濕度計等之構成。又,進而亦可設為包括未圖示之量測發電機27之轉數、發電量等之感測器之構成。再者,並不限於設置上述所有感測器之構成。The sensor 4 provided in the wind power generation device 2 includes, for example: a wind direction anemometer provided on the upper part of the nacelle 22, a pitch angle sensor provided at the root of the blade 24 and measuring the pitch angle of the blade 24, a measuring A yaw angle sensor for the azimuth of the nacelle 22 , and a strain sensor for measuring the stress applied to the blades 24 . Furthermore, although not shown, the sensor 4 may include, for example, a thermometer disposed on the upper part of the engine room 22 and measuring the temperature of the outside air, a thermometer measuring the temperature in the engine room 22, and a measuring engine room. 22. The composition of the hygrometer, etc. for the humidity within. In addition, it is also possible to further include a sensor that measures the number of revolutions of the generator 27, the amount of power generation, and the like, which are not shown. Furthermore, it is not limited to the configuration in which all the above-mentioned sensors are provided.

控制裝置29自上述風向風速計、槳距角感測器、偏航角感測器、及上述各種感測器4經由信號線獲取量測資料,基於該所獲取之量測資料而適當地控制槳距角、機艙方位角、發電機旋轉速度等,並且將所獲得之量測資料經由通信網路6向設置於運轉管理中心3內之電子終端5發送。The control device 29 acquires measurement data from the above-mentioned wind direction anemometer, the pitch angle sensor, the yaw angle sensor, and the above-mentioned various sensors 4 via the signal line, and appropriately controls based on the acquired measurement data The pitch angle, the nacelle azimuth, the rotation speed of the generator, etc., and the obtained measurement data are sent to the electronic terminal 5 installed in the operation management center 3 via the communication network 6 .

圖2係表示圖1所示之風力發電裝置之塔架頂部附近之立體圖,圖3係表示圖1所示之風力發電裝置之塔架頂部附近之側視圖。於圖2及圖3中,以透視機艙22之形式進行圖示,以便容易瞭解塔架21之頂部附近之情況。於塔架21與機艙22之連結部分設置有偏航軸承齒輪9及複數個偏航致動器10,作為對機艙22與葉輪即輪轂23及複數個葉片24相對於塔架21之位置進行控制之偏航驅動裝置(偏航角控制機構)發揮功能。偏航軸承齒輪9設置於塔架21之頂部,偏航致動器10於機艙22內設置有複數個。偏航致動器10之設置數量取決於風力發電裝置2之種類或規模,例如於發電量(輸出)為2 MW左右時,設置有4個左右,於5 MW左右之規模時,以圍繞塔架21之頂部之方式設置8個左右。以下,將設置8個偏航致動器10之情形作為一例進行說明。 如圖3所示,偏航致動器10係將成為偏航驅動(偏航回轉)之動力源之驅動馬達13、將驅動馬達13之驅動力傳遞至小齒輪11之減速機12、及以與偏航軸承齒輪9嚙合之方式設置之小齒輪11連結而構成。FIG. 2 is a perspective view showing the vicinity of the top of the tower of the wind power generator shown in FIG. 1 , and FIG. 3 is a side view of the vicinity of the top of the tower of the wind power generator shown in FIG. 1 . In FIGS. 2 and 3 , a perspective view of the nacelle 22 is shown for easy understanding of the situation near the top of the tower 21 . A yaw bearing gear 9 and a plurality of yaw actuators 10 are arranged at the connecting part of the tower 21 and the nacelle 22 to control the position of the nacelle 22 and the impeller, that is, the hub 23 and the plurality of blades 24 relative to the tower 21 The yaw drive device (yaw angle control mechanism) functions. The yaw bearing gear 9 is arranged on the top of the tower 21 , and a plurality of yaw actuators 10 are arranged in the nacelle 22 . The installed number of the yaw actuators 10 depends on the type or scale of the wind power generator 2. For example, when the power generation (output) is about 2 MW, about 4 are provided, and when the scale is about 5 MW, around the tower About 8 are arranged on the top of the frame 21 . Hereinafter, a case where eight yaw actuators 10 are provided will be described as an example. As shown in FIG. 3 , the yaw actuator 10 is a drive motor 13 that becomes a power source for yaw drive (yaw rotation), a reducer 12 that transmits the driving force of the drive motor 13 to the pinion 11 , and The pinion gear 11 provided so as to mesh with the yaw bearing gear 9 is connected.

圖4係本實施例之偏航致動器及異常檢測裝置之方塊線圖。於8個偏航致動器10分別連接有偏航動力控制部14及動力阻斷機構部15。偏航動力控制部14係對偏航致動器10輸出運轉信號之裝置,包括變流器。變流器例如具備未圖示之全橋電路,全橋電路根據自PWM(Pulse Width Modulation,脈衝寬度調變)控制部(未圖示)輸入之驅動信號將直流電壓源(未圖示)開關,而向構成偏航致動器10之驅動馬達13輸出電流。全橋電路具備4個開關元件,構成具備串聯連接之2個開關元件之第一上下臂(U相)、及具備2個開關元件之第二上下臂(V相)。開關元件可基於PWM控制部所產生之驅動信號,根據閘極驅動器電路(未圖示)所輸出之脈衝狀之閘極信號進行開關動作。FIG. 4 is a block diagram of the yaw actuator and the abnormality detection device of the present embodiment. A yaw power control unit 14 and a power blocking mechanism unit 15 are connected to the eight yaw actuators 10 , respectively. The yaw power control unit 14 is a device for outputting an operation signal to the yaw actuator 10, and includes an inverter. The converter includes, for example, a full-bridge circuit not shown. The full-bridge circuit switches a DC voltage source (not shown) on and off according to a drive signal input from a PWM (Pulse Width Modulation) control unit (not shown). , and output current to the drive motor 13 constituting the yaw actuator 10 . The full-bridge circuit includes four switching elements, and constitutes a first upper and lower arm (U-phase) including two switching elements connected in series, and a second upper and lower arm (V-phase) including two switching elements. The switching element can perform switching operations according to the pulsed gate signal output from the gate driver circuit (not shown) based on the driving signal generated by the PWM control unit.

詳情下文敍述之動力阻斷機構部15係使內置於偏航致動器10之離合器機構動作之裝置,包括油壓單元。具有如下功能:藉由利用油壓單元來控制油壓,而阻斷偏航致動器10之動力。輸出量測部16量測作為偏航動力控制部14之變流器之電流值。再者,亦可構成為例如量測轉矩、振動、應變等其他參數來代替量測變流器之電流值。 輸出運算部31將由各輸出量測部16量測所得之電流值輸入,求出其合計值,並向異常判定部32輸出。詳情下文敍述之異常判定部32基於自輸出運算部31輸入之合計值,對偏航動力控制部14及動力阻斷機構部15輸出控制信號。利用輸出運算部31及異常判定部32構成異常檢測裝置。Details The power blocking mechanism portion 15 described below is a device for operating the clutch mechanism built in the yaw actuator 10, and includes a hydraulic unit. It has the function of blocking the power of the yaw actuator 10 by controlling the oil pressure with the oil pressure unit. The output measurement unit 16 measures the current value of the inverter serving as the yaw power control unit 14 . Furthermore, other parameters such as torque, vibration, strain, etc. can be measured instead of measuring the current value of the current transformer. The output calculation unit 31 inputs the current values measured by the respective output measurement units 16 , obtains a total value thereof, and outputs the result to the abnormality determination unit 32 . The abnormality determination unit 32 described in detail below outputs a control signal to the yaw power control unit 14 and the power interruption mechanism unit 15 based on the total value input from the output calculation unit 31 . An abnormality detection device is constituted by the output calculation unit 31 and the abnormality determination unit 32 .

此處,對偏航致動器10及動力阻斷機構部15進行說明。 <偏航致動器及動力阻斷機構部> 圖6係表示圖4所示之偏航致動器10及動力阻斷機構部15之局部剖視圖。如圖6所示,偏航致動器10具備:具有動力軸44之驅動馬達13、及連結於動力軸44及小齒輪11之各者且自動力軸44向小齒輪11傳遞動力之減速機12。 動力阻斷機構部15具備被自詳情下文敍述之異常判定部32輸入控制信號之離合器控制部90、及由油壓馬達252驅動之離合器油壓源94。離合器控制部90具有壓力調整閥90a及通電控制器90b。又,動力阻斷機構部15具有經由油壓供給路93依序連接於離合器油壓源94之泄放閥98、積蓄器95、及排水閥99。將離合器油壓源94與泄放閥98連結之油壓供給路93於中途分支,該分支之油壓供給路93連接於壓力調整閥(電磁閥)90a,經由該分支之油壓供給路93將離合器油壓源94與壓力調整閥90a連結。於壓力調整閥90a之下游側之油壓供給路93設置有排水閥199。Here, the yaw actuator 10 and the power interruption mechanism unit 15 will be described. <Yaw actuator and power blocking mechanism> FIG. 6 is a partial cross-sectional view showing the yaw actuator 10 and the power blocking mechanism portion 15 shown in FIG. 4 . As shown in FIG. 6 , the yaw actuator 10 includes a drive motor 13 having a power shaft 44 and a speed reducer that is connected to each of the power shaft 44 and the pinion gear 11 and that transmits power from the power shaft 44 to the pinion gear 11 . 12. The power interruption mechanism unit 15 includes a clutch control unit 90 to which a control signal is input from the abnormality determination unit 32 described in detail below, and a clutch hydraulic pressure source 94 driven by a hydraulic motor 252 . The clutch control unit 90 includes a pressure regulating valve 90a and an energization controller 90b. Further, the power shut-off mechanism portion 15 includes a relief valve 98 , an accumulator 95 , and a drain valve 99 connected to the clutch hydraulic pressure source 94 via the hydraulic pressure supply passage 93 in this order. The hydraulic pressure supply path 93 connecting the clutch hydraulic pressure source 94 and the relief valve 98 is branched in the middle, the branched hydraulic pressure supply path 93 is connected to the pressure regulating valve (solenoid valve) 90a, and the branched hydraulic pressure supply path 93 passes through the branch. The clutch hydraulic pressure source 94 is connected to the pressure regulating valve 90a. A drain valve 199 is provided in the hydraulic pressure supply passage 93 on the downstream side of the pressure regulating valve 90a.

[減速機] 減速機12具備:連結於驅動馬達13之動力軸44之輸入齒輪43、與輸入齒輪43嚙合之複數個正齒輪53、固定於複數個正齒輪53之各者之複數個曲軸50、及經由離合器作動部89連結於輸出軸66之小齒輪11。又,減速機12具有:於內周側(內周面)具有內齒42之殼體40、具有與殼體40之內齒42嚙合之外齒46之外齒輪45、保持外齒輪45之載體60、及經由離合器作動部89及輸出軸66連結於載體60之小齒輪11。殼體40形成為筒狀,於內側收容輸入齒輪43、複數個正齒輪53、複數個曲軸50(桿身本體51)、外齒輪45及載體60。外齒輪45經由外齒用軸承(未圖示)將複數個曲軸50可旋轉地保持,作為根據輸入齒輪43及複數個正齒輪53之旋轉而由複數個曲軸50擺動之擺動齒輪發揮功能。載體60將各曲軸50可旋轉地保持,並且經由複數個之曲軸50保持外齒輪45。[Reducer] The reducer 12 includes an input gear 43 connected to a power shaft 44 of the drive motor 13, a plurality of spur gears 53 meshing with the input gear 43, a plurality of crankshafts 50 fixed to each of the plurality of spur gears 53, and a clutch The actuating portion 89 is connected to the pinion 11 of the output shaft 66 . In addition, the speed reducer 12 includes a housing 40 having internal teeth 42 on the inner peripheral side (inner peripheral surface), an external gear 45 having external teeth 46 meshing with the internal teeth 42 of the housing 40 , and a carrier holding the external gear 45 60 , and the pinion 11 connected to the carrier 60 via the clutch actuating portion 89 and the output shaft 66 . The casing 40 is formed in a cylindrical shape, and accommodates the input gear 43 , the plurality of spur gears 53 , the plurality of crankshafts 50 (shaft body 51 ), the external gear 45 , and the carrier 60 inside. The external gear 45 holds the plurality of crankshafts 50 rotatably via bearings for external teeth (not shown), and functions as a swing gear that swings by the plurality of crankshafts 50 according to the rotation of the input gear 43 and the plurality of spur gears 53 . The carrier 60 holds each crankshaft 50 rotatably, and holds the external gear 45 via the plurality of crankshafts 50 .

於減速機12中,自驅動馬達13輸入至輸入齒輪43之旋轉動力被旋轉減速,自小齒輪11輸出。小齒輪11以與偏航軸承齒輪9嚙合之方式配置。因此,經由輸入齒輪43及減速機12傳遞至小齒輪11之旋轉動力於轉矩增大之狀態下作為偏航驅動力輸出至偏航軸承齒輪9。In the speed reducer 12 , the rotational power input from the drive motor 13 to the input gear 43 is rotationally reduced and output from the pinion gear 11 . The pinion gear 11 is arranged to mesh with the yaw bearing gear 9 . Therefore, the rotational power transmitted to the pinion gear 11 via the input gear 43 and the speed reducer 12 is output to the yaw bearing gear 9 as a yaw driving force in a state where the torque is increased.

於圖6中,符號「L1」表示小齒輪11之中心軸。殼體40之設置內齒42之內周面之中心軸與中心軸L1位於同一軸上。於以下說明中,僅表示為「軸向」之方向意指在中心軸L1上延伸之方向或與中心軸L1平行之方向。又,將與中心軸L1正交之方向稱為「徑向」,將繞中心軸L1之方向稱為「圓周方向」。 殼體40具有:形成為筒狀且兩端部打開之主殼體部41a、及固定於主殼體部41a之一端部側之副殼體部41b。於本實施例中,利用螺栓(未圖示)將主殼體部41a之緣部與副殼體部41b之緣部固定,藉此將主殼體部41a與副殼體部41b連結。輸出軸66自與主殼體部41a中之安裝副殼體部41b之一端部相反側之另一端部突出。In FIG. 6 , the symbol “ L1 ” represents the central axis of the pinion gear 11 . The central axis of the inner peripheral surface of the housing 40 on which the inner teeth 42 are provided is located on the same axis as the central axis L1. In the following description, a direction only expressed as "axial" means a direction extending on the central axis L1 or a direction parallel to the central axis L1. In addition, the direction orthogonal to the central axis L1 is referred to as a "radial direction", and the direction around the central axis L1 is referred to as a "circumferential direction". The case 40 has a main case portion 41a formed in a cylindrical shape with both ends opened, and a sub case portion 41b fixed to one end side of the main case portion 41a. In this embodiment, the main case portion 41a and the sub case portion 41b are connected by fixing the edge portion of the main case portion 41a and the edge portion of the sub case portion 41b with bolts (not shown). The output shaft 66 protrudes from the other end portion on the opposite side to the one end portion of the main case portion 41a to which the sub case portion 41b is attached.

內齒42包括形成為銷狀之複數個內齒銷。該等內齒銷被嵌入至銷槽,該銷槽係跨及主殼體部41a之輸入側部分111之內周面之全域沿著圓周方向等間隔地形成有複數個,且該等內齒銷以各內齒銷之長度方向變得與中心軸L1平行之方式配置。具有此種構成之內齒42以與外齒輪45之外齒46嚙合之方式配置。 於殼體40之副殼體部41b安裝有驅動馬達13。驅動馬達13所具有之動力軸44朝向副殼體部41b之內側延伸,與配置於副殼體部41b內之輸入齒輪43固定地連接,從而將藉由驅動馬達13而產生之旋轉動力經由動力軸44傳遞至輸入齒輪43。The inner teeth 42 include a plurality of inner teeth pins formed in a pin shape. These internally toothed pins are fitted into pin grooves formed in plural at equal intervals in the circumferential direction across the entire area of the inner peripheral surface of the input side portion 111 of the main housing portion 41a, and the internally toothed pins The pins are arranged so that the longitudinal direction of each inner tooth pin becomes parallel to the central axis L1. The internal teeth 42 having such a configuration are arranged so as to mesh with the external teeth 46 of the external gear 45 . The drive motor 13 is attached to the sub-casing portion 41 b of the casing 40 . The power shaft 44 of the drive motor 13 extends toward the inner side of the sub-housing portion 41b, and is fixedly connected to the input gear 43 disposed in the sub-housing portion 41b, so that the rotational power generated by the drive motor 13 is passed through the power The shaft 44 is transmitted to the input gear 43 .

載體60具有:將曲軸50之一端部(輸入齒輪43及正齒輪53側之端部)可旋轉地保持之第1保持部61、將曲軸50之另一端部(小齒輪11突出之側之端部)可旋轉地保持之第2保持部62、將第1保持部61與第2保持部62連結之支柱63、及用以將載體60與輸出軸66連結之結合筒部64。再者,為了便於說明,於圖6中利用二點鏈線表示支柱63。The carrier 60 has a first holding portion 61 that rotatably holds one end portion of the crankshaft 50 (the end portion on the input gear 43 and the spur gear 53 side), and the other end portion of the crankshaft 50 (the end on the side where the pinion gear 11 protrudes) part) a second holding part 62 rotatably held, a strut 63 connecting the first holding part 61 and the second holding part 62 , and a coupling cylinder part 64 for connecting the carrier 60 and the output shaft 66 . In addition, for convenience of description, the support|pillar 63 is shown by the two-dot chain line in FIG.

第1保持部61及第2保持部62分別形成為圓環狀,第1保持部61與第2保持部62係於沿著軸向隔開之位置處相互對向而配置。支柱63以橫跨第1保持部61之徑向之大致中央區域與第2保持部62之徑向之大致中央區域之間之方式設置,而將第1保持部61與第2保持部62連結。結合筒部64以橫跨第1保持部61之內周緣與第2保持部62之內周緣之間之方式設置,具有圓筒形狀,於內周面形成有載體側花鍵部65。 於第1保持部61形成第1端部用貫通孔71,曲軸50之一端部經由第1曲軸用軸承73可旋轉地保持於第1端部用貫通孔71。又,於第2保持部62形成第2端部用貫通孔72,曲軸50之另一端部經由第2曲軸用軸承74可旋轉地保持於第2端部用貫通孔72。The first holding portion 61 and the second holding portion 62 are each formed in an annular shape, and the first holding portion 61 and the second holding portion 62 are arranged to face each other at positions spaced apart in the axial direction. The struts 63 are provided so as to straddle between the substantially central region in the radial direction of the first holding portion 61 and the substantially central region in the radial direction of the second holding portion 62 , and connect the first holding portion 61 and the second holding portion 62 . The coupling cylindrical portion 64 is provided so as to straddle between the inner peripheral edge of the first holding portion 61 and the inner peripheral edge of the second holding portion 62 , has a cylindrical shape, and has a carrier-side spline portion 65 formed on the inner peripheral surface. A first end portion through hole 71 is formed in the first holding portion 61 , and one end portion of the crankshaft 50 is rotatably held in the first end portion through hole 71 via a first crankshaft bearing 73 . Further, a second end portion through hole 72 is formed in the second holding portion 62 , and the other end portion of the crankshaft 50 is rotatably held in the second end portion through hole 72 via a second crankshaft bearing 74 .

本實施例之載體60於軸向上被分成兩個部分,包括配置於副殼體部41b側之第1半體60a、及配置於小齒輪11突出之側之第2半體60b。第1半體60a具有:上述第1保持部61、構成支柱63之一部分之第1支柱半部、及構成結合筒部64之一部分之第1筒半部64a。另一方面,第2半體60b具有:上述第2保持部62、構成支柱63之一部分之第2支柱半部、及構成結合筒部64之一部分之第2筒半部64b。The carrier 60 of this embodiment is divided into two parts in the axial direction, including a first half body 60a disposed on the side of the auxiliary housing portion 41b and a second half body 60b disposed on the side where the pinion gear 11 protrudes. The first half body 60 a includes the above-described first holding portion 61 , a first column half portion constituting a part of the support column 63 , and a first cylindrical half portion 64 a constituting a part of the coupling cylindrical portion 64 . On the other hand, the second half body 60b includes the above-mentioned second holding portion 62 , a second column half portion constituting a part of the support column 63 , and a second cylindrical half portion 64b constituting a part of the coupling cylindrical portion 64 .

[離合器機構] 如圖6所示,離合器機構具備離合器作動部89及離合器驅動體91,且於構成動力阻斷機構部15之離合器控制部90之控制下作動。離合器控制部90可藉由空壓方式及油壓方式等任意動力對離合器作動部89及離合器驅動體91進行驅動控制。例如,於圖6所示之偏航致動器10中,藉由油壓方式之動力對離合器作動部89及離合器驅動體91進行驅動控制。於圖6所示之例中,離合器油壓源94及離合器控制部90等與偏航致動器10分開設置,藉由裝滿油等液狀傳遞介質之油壓供給路93,將離合器油壓源94及離合器控制部90與離合器驅動體91相連。離合器驅動體91設置為被液狀傳遞介質推壓而可沿軸向移動,離合器驅動體91相對於離合器作動部89之抵接狀態(推壓狀態)根據離合器驅動體91之軸向位置而改變。離合器控制部90可藉由調整油壓供給路93內(尤其是離合器控制部90與離合器驅動體91之間)之液狀傳遞介質之壓力來改變離合器驅動體91對離合器作動部89之推壓力,而據以控制離合器作動部89之離合器之離合。[Clutch Mechanism] As shown in FIG. 6 , the clutch mechanism includes a clutch actuating portion 89 and a clutch driving body 91 , and operates under the control of a clutch control portion 90 constituting the power interruption mechanism portion 15 . The clutch control unit 90 can drive and control the clutch actuating unit 89 and the clutch driving body 91 by any power such as an air pressure system or a hydraulic system. For example, in the yaw actuator 10 shown in FIG. 6 , the clutch actuating portion 89 and the clutch driving body 91 are driven and controlled by hydraulic power. In the example shown in FIG. 6, the clutch hydraulic pressure source 94, the clutch control unit 90, etc. are provided separately from the yaw actuator 10, and the clutch hydraulic The pressure source 94 and the clutch control unit 90 are connected to the clutch driving body 91 . The clutch driving body 91 is provided so as to be movable in the axial direction by being pressed by the liquid transmission medium, and the contact state (pressing state) of the clutch driving body 91 with respect to the clutch actuating portion 89 is changed according to the axial position of the clutch driving body 91 . The clutch control part 90 can change the pressing force of the clutch driving body 91 to the clutch actuating part 89 by adjusting the pressure of the liquid transmission medium in the oil pressure supply path 93 (especially between the clutch control part 90 and the clutch driving body 91 ). , and the clutch clutch of the clutch actuating portion 89 is controlled accordingly.

離合器作動部89具有:藉由花鍵聯接連結於輸出軸66之第1摩擦板89a、及藉由花鍵聯接連結於小齒輪11之第2摩擦板89b。第1摩擦板89a及第2摩擦板89b設置為:關於繞中心軸L1之旋轉方向之舉動分別受輸出軸66及小齒輪11約束,但關於中心軸L1方向可不受輸出軸66及小齒輪11約束而移動。然而,第1摩擦板89a及第2摩擦板89b之中心軸L1方向之舉動受設置於第1摩擦板89a及第2摩擦板89b之下方之離合器驅動體91及第1連結構件107約束,防止第1摩擦板89a及第2摩擦板89b之脫落。 第1連結構件107經由螺絲構件107a安裝於輸出軸66之前端部,且配置於離合器驅動體91之內側。第1連結構件107之外周部係於與中心軸L1垂直之方向上較輸出軸66稍微突出而配置於第1摩擦板89a及第2摩擦板89b之下方。該第1連結構件107之外周部配置於如下位置,即,由第1連結構件107支持之第1摩擦板89a及第2摩擦板89b彼此間不相互推壓而不於第1摩擦板89a與第2摩擦板89b之間產生摩擦力的位置。The clutch actuating portion 89 includes a first friction plate 89a connected to the output shaft 66 by a spline connection, and a second friction plate 89b connected to the pinion 11 by a spline connection. The first friction plate 89a and the second friction plate 89b are provided so that their behavior in the rotational direction around the central axis L1 is constrained by the output shaft 66 and the pinion gear 11, respectively, but may not be affected by the output shaft 66 and the pinion gear 11 in the direction of the central axis L1 move within constraints. However, the movement in the direction of the central axis L1 of the first friction plate 89a and the second friction plate 89b is restricted by the clutch driving body 91 and the first connecting member 107 provided below the first friction plate 89a and the second friction plate 89b, preventing the The first friction plate 89a and the second friction plate 89b come off. The first connecting member 107 is attached to the front end portion of the output shaft 66 via the screw member 107 a, and is disposed inside the clutch driving body 91 . The outer peripheral portion of the first connecting member 107 slightly protrudes from the output shaft 66 in the direction perpendicular to the central axis L1, and is disposed below the first friction plate 89a and the second friction plate 89b. The outer peripheral portion of the first coupling member 107 is arranged at a position where the first friction plate 89a and the second friction plate 89b supported by the first coupling member 107 do not press against each other and do not overlap the first friction plate 89a and the second friction plate 89b. A position where frictional force is generated between the second friction plates 89b.

離合器驅動體91設置為可於小齒輪11之內側在較離合器作動部89(第1摩擦板89a及第2摩擦板89b)更靠近下方處向中心軸L1方向移動。離合器驅動體91之下部之一部分被切除,於該離合器驅動體91之切除部插入有彈性構件92。圖6所示之彈性構件92包括板彈簧,且由經由螺絲構件109a安裝於小齒輪11之下部之第2連結構件109及離合器驅動體91所保持。彈性構件92利用自身之彈性力,以將離合器驅動體91壓抵於離合器作動部89(第1摩擦板89a及第2摩擦板89b)之方式,於中心軸L1方向上對離合器驅動體91施加推壓力。再者,彈性構件92亦可利用碟形彈簧而非板彈簧構成。The clutch driving body 91 is provided inside the pinion 11 so as to be movable in the direction of the central axis L1 below the clutch actuating portion 89 (the first friction plate 89 a and the second friction plate 89 b ). A part of the lower part of the clutch driving body 91 is cut out, and the elastic member 92 is inserted in the cut-out part of the clutch driving body 91 . The elastic member 92 shown in FIG. 6 includes a leaf spring, and is held by the second connecting member 109 and the clutch driving body 91 attached to the lower part of the pinion 11 via the screw member 109a. The elastic member 92 applies its own elastic force to the clutch driving body 91 in the direction of the central axis L1 so as to press the clutch driving body 91 against the clutch actuating portion 89 (the first friction plate 89a and the second friction plate 89b ). push pressure. Furthermore, the elastic member 92 can also be constituted by a disc spring instead of a plate spring.

油壓作用部93b係藉由設置於小齒輪11與離合器驅動體91之間之O形環等密封構件而具有液密構造,但與形成於小齒輪11內之油壓供給路93連通。形成於小齒輪11內之油壓供給路93與形成於第2連結構件109內之油壓供給路93連通,形成於第2連結構件109內之油壓供給路93經由旋轉接頭與自壓力調整閥90a延伸之油壓供給路93連通。因此,離合器油壓源94與油壓作用部93b經由油壓供給路93連通。The hydraulically acting portion 93b has a liquid-tight structure by a sealing member such as an O-ring provided between the pinion 11 and the clutch driving body 91 , but communicates with the hydraulic supply passage 93 formed in the pinion 11 . The hydraulic pressure supply passage 93 formed in the pinion gear 11 communicates with the hydraulic pressure supply passage 93 formed in the second connection member 109, and the hydraulic pressure supply passage 93 formed in the second connection member 109 is adjusted by the self-pressure via the rotary joint The oil pressure supply path 93 extending from the valve 90a is communicated. Therefore, the clutch hydraulic pressure source 94 communicates with the hydraulic pressure acting portion 93 b via the hydraulic pressure supply passage 93 .

圖7係表示自圖6所示之輸出軸向小齒輪之旋轉動力之傳遞狀態之概略圖,圖8係表示自圖6所示之輸出軸向小齒輪之旋轉動力之非傳遞狀態之概略圖。再者,於圖7及圖8中,為了容易理解作動機制,而簡化各要素之顯示,省略一部分要素之圖示。 於自輸出軸66向小齒輪11傳遞旋轉動力時,圖6所示之壓力調整閥90a關閉而阻斷油壓供給路93內之液狀傳遞介質之流通,將自壓力調整閥90a至小齒輪11內之油壓供給路93內之壓力保持得較低。於該情形時,如圖7所示,離合器驅動體91被彈性構件92向上推,第1摩擦板89a及第2摩擦板89b被夾於離合器驅動體91與小齒輪11之間,在中心軸L1方向上相互推壓。藉此,第1摩擦板89a及第2摩擦板89b彼此摩擦卡合,將來自輸出軸66之旋轉動力傳遞給小齒輪11,小齒輪11經由第1摩擦板89a及第2摩擦板89b而與輸出軸66一體地旋轉。FIG. 7 is a schematic diagram showing the transmission state of the rotational power from the output shaft pinion shown in FIG. 6 , and FIG. 8 is a schematic diagram showing the non-transmission state of the rotational power from the output shaft pinion shown in FIG. 6 . In addition, in FIG. 7 and FIG. 8 , in order to facilitate the understanding of the operation mechanism, the display of each element is simplified, and the illustration of some elements is omitted. When the rotational power is transmitted from the output shaft 66 to the pinion gear 11, the pressure regulating valve 90a shown in FIG. 6 is closed to block the flow of the liquid transmission medium in the oil pressure supply path 93, and the pressure regulating valve 90a to the pinion gear is closed. The pressure in the oil pressure supply passage 93 in 11 is kept low. In this case, as shown in FIG. 7 , the clutch driving body 91 is pushed up by the elastic member 92, the first friction plate 89a and the second friction plate 89b are sandwiched between the clutch driving body 91 and the pinion 11, and the center shaft Push each other in the L1 direction. Thereby, the first friction plate 89a and the second friction plate 89b are frictionally engaged with each other, and the rotational power from the output shaft 66 is transmitted to the pinion gear 11, and the pinion gear 11 is connected to the pinion gear 11 via the first friction plate 89a and the second friction plate 89b. The output shaft 66 integrally rotates.

另一方面,於不自輸出軸66向小齒輪11傳遞旋轉動力時,壓力調整閥90a打開而容許油壓供給路93內之液狀傳遞介質之流通,將高壓之液狀傳遞介質自離合器油壓源94送往小齒輪11內之油壓供給路93。然後,高壓之液狀傳遞介質自小齒輪11內之油壓供給路93流入至油壓作用部93b,離合器驅動體91抵抗彈性構件92之彈性力,向自第1摩擦板89a及第2摩擦板89b離開之方向移動。藉此,第1摩擦板89a及第2摩擦板89b彼此間之推壓力減少,而解除第1摩擦板89a與第2摩擦板89b之間之摩擦卡合,從而不再將輸出軸66之旋轉動力傳遞至小齒輪11。因此,即便輸出軸66及第1摩擦板89a繞中心軸L1旋轉,第2摩擦板89b及小齒輪11亦基本上不會旋轉。On the other hand, when the rotational power is not transmitted from the output shaft 66 to the pinion gear 11, the pressure regulating valve 90a is opened to allow the circulation of the liquid transmission medium in the hydraulic pressure supply passage 93, and the high pressure liquid transmission medium is released from the clutch oil. The pressure source 94 is sent to the oil pressure supply passage 93 in the pinion 11 . Then, the high-pressure liquid transmission medium flows from the hydraulic supply passage 93 in the pinion 11 to the hydraulically acting portion 93b, and the clutch driving body 91 resists the elastic force of the elastic member 92, and moves toward the first friction plate 89a and the second friction plate 89a. The plate 89b moves in the direction away from it. As a result, the pressing force between the first friction plate 89a and the second friction plate 89b is reduced, and the frictional engagement between the first friction plate 89a and the second friction plate 89b is released, and the rotation of the output shaft 66 is stopped. The power is transmitted to the pinion gear 11 . Therefore, even if the output shaft 66 and the first friction plate 89a rotate around the central axis L1, the second friction plate 89b and the pinion 11 basically do not rotate.

<控制裝置> 其次,對圖1所示之控制裝置29進行說明。圖5係圖1所示之控制裝置29之功能方塊圖。如圖5所示,控制裝置29具備輸出運算部31、異常判定部32、記憶部33、機器控制部34、通信I/F36、輸入I/F37、及輸出I/F38,該等以彼此可利用內部匯流排39進行存取之方式連接。輸出運算部31、異常判定部32、及機器控制部34例如利用未圖示之CPU(Central Processing Unit,中央處理單元)等處理器、供儲存各種程式之ROM(read only memory,唯讀記憶體)、暫時儲存運算過程之資料之RAM(Random Access Memory,隨機存取記憶體)、外部記憶裝置等記憶裝置來實現,並且CPU等處理器讀出ROM中所儲存之各種程式並執行,將作為執行結果之運算結果儲存於RAM或外部記憶裝置。<Control device> Next, the control apparatus 29 shown in FIG. 1 is demonstrated. FIG. 5 is a functional block diagram of the control device 29 shown in FIG. 1 . As shown in FIG. 5 , the control device 29 includes an output calculation unit 31 , an abnormality determination unit 32 , a memory unit 33 , a device control unit 34 , a communication I/F 36 , an input I/F 37 , and an output I/F 38 , which are mutually compatible. The connection is made by means of the internal bus bar 39 for access. The output calculation unit 31 , the abnormality determination unit 32 , and the machine control unit 34 use a processor such as a CPU (Central Processing Unit), not shown, and a ROM (read only memory) for storing various programs, for example. ), RAM (Random Access Memory), an external memory device and other memory devices that temporarily store the data of the operation process, and the CPU and other processors read out various programs stored in the ROM and execute them, which will be used as The operation result of the execution result is stored in RAM or an external memory device.

機器控制部34經由輸入I/F37及內部匯流排39,獲取作為感測器4之例如風向風速計、槳距角感測器、偏航角感測器、及應變感測器之量測資料。機器控制部34基於所獲取之量測資料控制風力發電裝置2之運轉。例如,一面基於風速資料控制葉片24之朝向或轉數等參數,一面繼續運轉。具體而言,基於由風向風速計量測所得之風向資料,經由輸出I/F38向構成偏航角控制機構之偏航動力控制部14輸出偏航角控制信號,以使包括葉片24及輪轂23之葉輪與風向正對,及/或,基於由風向風速計量測所得之風速資料,經由輸出I/F38向槳距角控制機構17輸出作為葉片24之傾斜角之槳距角控制信號。又,機器控制部34基於由感測器4量測所得之發電機27之發電量,經由輸出I/F38向增速機26輸出控制發電機旋轉速度之轉速控制信號。The machine control unit 34 acquires the measurement data of the sensors 4 such as the wind direction anemometer, the pitch angle sensor, the yaw angle sensor, and the strain sensor through the input I/F 37 and the internal bus bar 39 . The equipment control unit 34 controls the operation of the wind power generator 2 based on the acquired measurement data. For example, while controlling parameters such as the orientation of the blade 24 or the number of revolutions based on the wind speed data, the operation is continued. Specifically, based on the wind direction data measured by the wind direction anemometer, the yaw angle control signal is output to the yaw power control unit 14 constituting the yaw angle control mechanism through the output I/F 38, so that the blades 24 and the hub 23 are included. The impeller is directly opposite to the wind direction, and/or, based on the wind speed data measured by the wind direction anemometer, the pitch angle control signal as the pitch angle of the blade 24 is output to the pitch angle control mechanism 17 via the output I/F 38. Furthermore, the device control unit 34 outputs a rotational speed control signal for controlling the rotational speed of the generator to the gearbox 26 via the output I/F 38 based on the power generation amount of the generator 27 measured by the sensor 4 .

輸出運算部31經由輸入I/F37及內部匯流排39獲取由與各偏航致動器10對應之輸出量測部16量測所得之作為偏航動力控制部14之變流器之電流值。輸出運算部31將所獲取之與各偏航致動器10對應之變流器之電流值進行相加,以輸出之合計值形式經由內部匯流排39向異常判定部32傳送。 異常判定部32將自輸出運算部31傳送之輸出之合計值與規定之第1閾值進行比較,判定偏航致動器10之異常之有無。又,異常判定部32於詳情下文敍述之處理中,於檢測出偏航致動器10之異常之情形時,為了使特定之偏航致動器10停止,而經由輸出I/F38向與應停止之偏航致動器10對應之動力阻斷機構部15輸出控制信號。於該情形時,動力阻斷機構部15如上所述,藉由構成動力阻斷機構部15之通電控制器90b將壓力調整閥90a設為打開狀態,而容許油壓供給路93內之液狀傳遞介質之流通,從而將高壓之液狀傳遞介質自離合器油壓源94送至小齒輪11內之油壓供給路93。然後,如圖8所示,離合器機構動作,解除第1摩擦板89a與第2摩擦板89b之間之摩擦卡合,而不再將輸出軸66之旋轉動力傳遞至小齒輪11。換言之,動力阻斷機構部15阻斷應停止之偏航致動器10之動力。再者,異常判定部32經由通信I/F36及通信網路6向設置於運轉管理中心3內之電子終端5發送偏航致動器10之異常判定之結果。 藉由輸出運算部31及異常判定部32構成異常檢測裝置30。The output computing unit 31 acquires the current value of the inverter serving as the yaw power control unit 14 measured by the output measuring unit 16 corresponding to each yaw actuator 10 through the input I/F 37 and the internal bus bar 39 . The output calculation unit 31 adds the acquired current values of the current transformers corresponding to the yaw actuators 10 , and transmits the output sum to the abnormality determination unit 32 via the internal bus 39 . The abnormality determination unit 32 compares the total value of the outputs transmitted from the output calculation unit 31 with a predetermined first threshold value, and determines the presence or absence of an abnormality in the yaw actuator 10 . In addition, the abnormality determination unit 32 detects the abnormality of the yaw actuator 10 in the processing described in detail below, and sends the output I/F 38 to the corresponding response in order to stop the specific yaw actuator 10 . The power blocking mechanism 15 corresponding to the stopped yaw actuator 10 outputs a control signal. In this case, as described above, the power shut-off mechanism portion 15 allows the liquid state in the hydraulic pressure supply passage 93 to be allowed to open by the energization controller 90b constituting the power shut-off mechanism portion 15 to open the pressure regulating valve 90a. The circulation of the transmission medium sends the high-pressure liquid transmission medium from the clutch oil pressure source 94 to the oil pressure supply passage 93 in the pinion 11 . Then, as shown in FIG. 8 , the clutch mechanism operates to release the frictional engagement between the first friction plate 89 a and the second friction plate 89 b , and the rotational power of the output shaft 66 is no longer transmitted to the pinion 11 . In other words, the power blocking mechanism portion 15 blocks the power of the yaw actuator 10 to be stopped. Furthermore, the abnormality determination unit 32 transmits the abnormality determination result of the yaw actuator 10 to the electronic terminal 5 installed in the operation management center 3 via the communication I/F 36 and the communication network 6 . The abnormality detection device 30 is constituted by the output calculation unit 31 and the abnormality determination unit 32 .

記憶部33將經由輸入I/F37及內部匯流排39獲取之作為感測器4之例如風向風速計、槳距角感測器、偏航角感測器、及應變感測器之量測資料儲存於規定之記憶區域。又,記憶部33將異常檢測裝置30所使用之詳情下文敍述之規定之第1閾值及規定之第2閾值儲存於規定之記憶區域。The memory section 33 will obtain the measurement data of the sensor 4, such as the wind direction anemometer, the pitch angle sensor, the yaw angle sensor, and the strain sensor, which are obtained through the input I/F 37 and the internal bus bar 39. Stored in the specified memory area. Moreover, the memory|storage part 33 memorize|stores the predetermined 1st threshold value and the predetermined 2nd threshold value which are used in the abnormality detection apparatus 30 in the predetermined memory area|region which are mentioned later in detail.

經由輸入I/F37及內部匯流排39所獲取之作為感測器4之例如風向風速計、槳距角感測器、偏航角感測器、及應變感測器之量測資料,視需要經由通信I/F36及通信網路6向設置於運轉管理中心3內之電子終端5發送。Measurement data such as wind direction anemometer, pitch angle sensor, yaw angle sensor, and strain sensor as sensor 4 obtained through input I/F 37 and internal bus bar 39, as needed It is transmitted to the electronic terminal 5 installed in the operation management center 3 via the communication I/F 36 and the communication network 6 .

再者,於本實施例中,設為將圖5所示之控制裝置29配置於塔架21內之底部(下部)之構成,但並不限於此。例如,亦可設為如下構成:於機艙22內配置控制台,安裝作為上述機器控制部34所具備之功能之一部分之偏航角指令運算部及槳距角指令運算部、及/或異常檢測裝置30。Furthermore, in this embodiment, the control device 29 shown in FIG. 5 is arranged at the bottom (lower part) of the tower 21, but it is not limited to this. For example, a configuration may be adopted in which a console is arranged in the nacelle 22, and a yaw angle command calculation unit and a pitch angle command calculation unit, and/or abnormality detection, which are part of the functions of the above-mentioned machine control unit 34 are installed. device 30.

其次,對異常檢測裝置30之動作進行說明。以下,對如下情形進行說明,即,將8個偏航致動器10於偏航軸承齒輪9之外周側在圓周方向上以規定之間隔隔開而設置。換言之,各致動器自偏航軸承齒輪9之中心起在其圓周方向上以45°間隔設置。雖未圖示,但設為偏航致動器10a、偏航致動器10b、偏航致動器10c、偏航致動器10d、偏航致動器10e、偏航致動器10f、偏航致動器10g、及偏航致動器10h例如沿順時針方向依序設置。Next, the operation of the abnormality detection device 30 will be described. Hereinafter, the case where eight yaw actuators 10 are provided at predetermined intervals in the circumferential direction on the outer peripheral side of the yaw bearing gear 9 will be described. In other words, the respective actuators are arranged at intervals of 45° in the circumferential direction from the center of the yaw bearing gear 9 . Although not shown, yaw actuator 10a, yaw actuator 10b, yaw actuator 10c, yaw actuator 10d, yaw actuator 10e, yaw actuator 10f, The yaw actuator 10g and the yaw actuator 10h are arranged in this order, for example, in the clockwise direction.

[異常檢測裝置之動作] 圖9係圖5所示之異常檢測裝置30之流程圖。 於步驟S11中,當異常檢測裝置30偵測偏航回轉異常時,進入步驟S12。此處,所謂「偏航回轉異常」係指例如偏航角相對於偏航角控制指令之跟蹤誤差、或作為對構成偏航致動器之驅動馬達13進行驅動之偏航動力控制部14之變流器之異常等。[Operation of the abnormality detection device] FIG. 9 is a flowchart of the abnormality detection device 30 shown in FIG. 5 . In step S11, when the abnormality detection device 30 detects an abnormality in the yaw rotation, the process proceeds to step S12. Here, the "abnormal yaw rotation" refers to, for example, a tracking error of the yaw angle with respect to the yaw angle control command, or the yaw power control unit 14 that drives the drive motor 13 constituting the yaw actuator. The abnormality of the converter, etc.

於步驟S12中,構成異常檢測裝置30之異常判定部32將藉由構成異常檢測裝置30之輸出運算部31所求出之輸出之合計值(與偏航致動器10a~10h對應之變流器之電流值之合計值)、與記憶部33中所儲存之規定之第1閾值進行比較。於比較結果為輸出之合計值為規定之第1閾值以下之情形時,進入步驟S18,異常判定部32判定產生了偏航致動器以外之異常。然後,於步驟S19中停止風車、即風力發電裝置2,結束處理。另一方面,於比較結果為輸出之合計值超過規定之第1閾值之情形時,進入步驟S13。 此處,作為規定之第1閾值,例如設定在工廠內之試運轉時之各偏航致動器10a~10h之輸出(變流器之電流值)之合計值、或安設風力發電裝置2時之試運轉時之各偏航致動器10a~10h之輸出之合計值。再者,並不限於此,亦可基於儲存於未圖示之資料庫中之實際資料、即偏航致動器之更換等維護記錄,將較維護時更早之規定期間之各偏航致動器之輸出之合計值之平均變更為規定之第1閾值,進而,亦可設為基於實際資料對如上所述般預先設定之第1閾值進行修正之構成。In step S12, the abnormality determination unit 32 constituting the abnormality detection device 30 calculates the total value of the outputs (converted currents corresponding to the yaw actuators 10a to 10h) calculated by the output calculation unit 31 constituting the abnormality detection device 30. The total value of the current value of the device) is compared with the predetermined first threshold value stored in the memory unit 33 . When the result of the comparison is that the total value of the outputs is equal to or less than the predetermined first threshold value, the process proceeds to step S18, and the abnormality determination unit 32 determines that an abnormality other than the yaw actuator has occurred. Then, in step S19, the windmill, that is, the wind turbine generator 2 is stopped, and the process is terminated. On the other hand, when the result of the comparison is that the total value of the outputs exceeds the predetermined first threshold value, the process proceeds to step S13. Here, as the predetermined first threshold value, for example, the total value of the outputs (current values of the converters) of the yaw actuators 10a to 10h during the trial operation in the factory is set, or the wind power generator 2 is installed. The total value of the outputs of the yaw actuators 10a to 10h during the trial operation. Furthermore, it is not limited to this, and the actual data stored in the database (not shown), that is, the maintenance records such as the replacement of the yaw actuator, can also be used to make each yaw cause earlier than the maintenance time. The average of the total value of the output of the actuator is changed to the predetermined first threshold value, and further, the first threshold value previously set as described above may be corrected based on actual data.

於步驟S13中,異常判定部32判定偏航致動器10a~10h中之至少一者產生異常。 於步驟S14中,異常判定部32執行偏航致動器異常部位檢測序列。再者,關於偏航致動器異常部位檢測序列之詳細內容將於下文敍述。In step S13, the abnormality determination unit 32 determines that at least one of the yaw actuators 10a to 10h is abnormal. In step S14, the abnormality determination unit 32 executes the yaw actuator abnormality part detection sequence. Furthermore, the details of the abnormal part detection sequence of the yaw actuator will be described below.

於步驟S15中,異常判定部32判定是否於步驟S14中檢測出偏航致動器異常部位。於判定結果為未檢測出偏航致動器異常部位之情形時,進入上述步驟S18。另一方面,於判定結果為檢測出偏航致動器異常部位之情形時,進入步驟S16。In step S15, the abnormality determination unit 32 determines whether or not an abnormal part of the yaw actuator has been detected in step S14. When the determination result is that the abnormal part of the yaw actuator is not detected, the process proceeds to the above-mentioned step S18. On the other hand, when the determination result is that the abnormal part of the yaw actuator is detected, the process proceeds to step S16.

於步驟S16中,異常判定部32阻斷異常偏航致動器之動力。具體而言,如上所述,異常判定部32經由輸出I/F38向與異常偏航致動器對應之動力阻斷機構部15輸出控制信號。動力阻斷機構部15藉由構成動力阻斷機構部15之通電控制器90b將壓力調整閥90a設為打開狀態,而容許油壓供給路93內之液狀傳遞介質之流通,從而將高壓之液狀傳遞介質自離合器油圧源94送至小齒輪11內之油壓供給路93。然後,如圖8所示,離合器機構動作,解除第1摩擦板89a與第2摩擦板89b之間之摩擦卡合,而不再將輸出軸66之旋轉動力輸出至小齒輪11。藉此,動力阻斷機構部15阻斷異常偏航致動器之動力。再者,異常判定部32經由通信I/F36及通信網路6將所檢測出之異常偏航致動器之資訊發送至設置於運轉管理中心3內之電子終端5。由於在電子終端5之顯示畫面(未圖示)顯示異常偏航致動器之資訊,故而作業人員(操作員)可迅速地進行該異常偏航致動器之維護之需要與否、或用以維護之零件之置辦準備等。In step S16, the abnormality determination unit 32 blocks the power of the abnormal yaw actuator. Specifically, as described above, the abnormality determination unit 32 outputs the control signal to the power blocking mechanism unit 15 corresponding to the abnormal yaw actuator via the output I/F 38 . The power shut-off mechanism portion 15 opens the pressure regulating valve 90a by the energization controller 90b constituting the power shut-off mechanism portion 15 to allow the flow of the liquid transmission medium in the hydraulic pressure supply passage 93, thereby reducing the high-pressure The liquid transmission medium is sent from the clutch oil pressure source 94 to the oil pressure supply path 93 in the pinion 11 . Then, as shown in FIG. 8 , the clutch mechanism operates to release the frictional engagement between the first friction plate 89 a and the second friction plate 89 b , and the rotational power of the output shaft 66 is not output to the pinion gear 11 . Thereby, the power blocking mechanism part 15 blocks the power of the abnormal yaw actuator. Furthermore, the abnormality determination unit 32 transmits the detected information of the abnormal yaw actuator to the electronic terminal 5 installed in the operation management center 3 via the communication I/F 36 and the communication network 6 . Since the information of the abnormal yaw actuator is displayed on the display screen (not shown) of the electronic terminal 5, the operator (operator) can quickly check whether the maintenance of the abnormal yaw actuator is necessary or not, or use the To prepare for the purchase of maintenance parts, etc.

於步驟S17中,異常判定部32利用已阻斷動力以外之偏航致動器繼續運轉,結束處理。換言之,異常判定部32利用除異常偏航致動器以外之偏航致動器進行降級運轉。In step S17, the abnormality determination unit 32 continues the operation of the yaw actuators other than the power cut off, and ends the process. In other words, the abnormality determination unit 32 performs the degraded operation using the yaw actuator other than the abnormal yaw actuator.

圖10係表示圖9所示之偏航致動器異常部位檢測序列之詳細流程之流程圖。 於步驟S141中,異常判定部32自n個(總數)偏航致動器選定m個偏航致動器。此處,作為一例,自n=8、即8個偏航致動器10a~10h選定m個偏航致動器。於該情形時,較理想為設為1≦m≦3。再者,總數n不限於8個,只要適當設定即可,該情形時之m之可獲取範圍例如只要設為(1/8×n)≦m≦(3/8×n)即可。以下,將設為m=3之情形作為一例進行說明。FIG. 10 is a flowchart showing a detailed flow of the abnormal part detection sequence of the yaw actuator shown in FIG. 9 . In step S141, the abnormality determination unit 32 selects m yaw actuators from the n (total) yaw actuators. Here, as an example, m yaw actuators are selected from n=8, that is, eight yaw actuators 10a to 10h. In this case, it is preferable to set it as 1≦m≦3. In addition, the total number n is not limited to 8, and may be appropriately set, and the obtainable range of m in this case may be, for example, (1/8×n)≦m≦(3/8×n). Hereinafter, the case where m=3 is set as an example will be described.

於步驟S142中,異常判定部32停止m個偏航致動器,利用(n-m)個偏航致動器進行偏航運轉。即,藉由阻斷作為3個偏航致動器之偏航致動器10a~10c之動力而使之停止,藉由自異常判定部32向與剩餘5個偏航致動器10d~10h對應之作為偏航動力控制部14之變流器輸出控制信號來進行偏航運轉。In step S142, the abnormality determination unit 32 stops m yaw actuators, and performs yaw rotation with (n-m) yaw actuators. That is, the yaw actuators 10a to 10c, which are the three yaw actuators, are stopped by interrupting the power of the three yaw actuators. The yaw rotation is performed by correspondingly outputting a control signal of the inverter as the yaw power control unit 14 .

於步驟S143中,輸出運算部31經由輸入I/F37及內部匯流排39獲取由與偏航致動器10d~10h對應之輸出量測部16量測所得之作為偏航動力控制部14之變流器之電流值。然後,輸出運算部31將所獲取之與偏航致動器10d~10h對應之變流器之電流值進行相加,以輸出之合計值形式經由內部匯流排39向異常判定部32傳送。In step S143 , the output computing unit 31 obtains, through the input I/F 37 and the internal bus bar 39 , the variables measured by the output measuring units 16 corresponding to the yaw actuators 10 d to 10 h as the variation of the yaw power control unit 14 . The current value of the current transformer. Then, the output calculation unit 31 adds the acquired current values of the current transformers corresponding to the yaw actuators 10d to 10h, and transmits the output sum to the abnormality determination unit 32 via the internal bus 39 .

於步驟S144中,異常判定部32將由輸出運算部31所求出之輸出之合計值(與偏航致動器10d~10h對應之變流器之電流值之合計值)、與記憶部33中所儲存之規定之第2閾值進行比較,於比較結果為輸出之合計值超過規定之第2閾值之情形時,結束處理。即,進入上述圖9之步驟S15。 另一方面,於比較結果為輸出之合計值為規定之第2閾值以下之情形時,進入步驟S145。此處,作為規定之第2閾值,例如設定(5/8)×(規定之第1閾值)。In step S144 , the abnormality determination unit 32 compares the total value of the outputs obtained by the output calculation unit 31 (the total value of the current values of the current transformers corresponding to the yaw actuators 10 d to 10 h ) with the storage unit 33 . The stored predetermined second threshold value is compared, and when the result of the comparison is that the total output value exceeds the predetermined second threshold value, the process ends. That is, the process proceeds to step S15 of FIG. 9 described above. On the other hand, when the result of the comparison is that the total value of the outputs is equal to or less than the predetermined second threshold value, the process proceeds to step S145. Here, as the predetermined second threshold value, for example, (5/8)×(the predetermined first threshold value) is set.

於步驟S145中,異常判定部32選定不同之m個偏航致動器,返回至步驟S142。具體而言,選定偏航致動器10d~10f作為不同之3個偏航致動器。於步驟S142中,異常判定部32藉由阻斷偏航致動器10d~10f之動力而使之停止,藉由自異常判定部32向與剩餘之5個偏航致動器10a~10c及偏航致動器10g~10h對應之作為偏航動力控制部14之變流器輸出控制信號來進行偏航運轉。藉由如此反覆執行步驟S142~S145之處理,而執行偏航致動器異常部位檢測序列。 再者,於本實施例中,示出了於總數n=8時設定為m=3之情形,因此可能會產生於步驟S145中選定偏航致動器10g~10h作為2個致動器之情形。於該情形時,利用作為剩餘之6個偏航致動器之偏航致動器10a~10f進行偏航運轉,於步驟S144中與輸出之合計值進行比較之規定之第2閾值例如設定為(6/8)×(規定之第1閾值)。In step S145, the abnormality determination part 32 selects m different yaw actuators, and returns to step S142. Specifically, the yaw actuators 10d to 10f are selected as three different yaw actuators. In step S142 , the abnormality determination unit 32 stops the yaw actuators 10d to 10f by blocking the power of the yaw actuators 10d to 10f. The yaw actuators 10g to 10h corresponding to the yaw power control unit 14 output a control signal to the inverter to perform yaw rotation. By repeating the processing of steps S142 to S145 in this manner, the yaw actuator abnormality part detection sequence is executed. Furthermore, in this embodiment, the case where m=3 is set when the total number n=8 is shown, so it may occur that the yaw actuators 10g-10h are selected as one of the two actuators in step S145. situation. In this case, the yaw rotation is performed by the yaw actuators 10a to 10f as the remaining six yaw actuators, and the predetermined second threshold value to be compared with the total value of the outputs in step S144 is set, for example, as (6/8)×(prescribed first threshold value).

藉由如本實施例般設為m=3,可儘早地判定出包含處於異常狀態之偏航致動器之組(群),於特定處於異常狀態之偏航致動器之情形時,藉由將構成被判定為異常之組(群)之m個偏航致動器依序逐個停止,進行相同之判定,可特定出處於異常狀態之偏航致動器。亦可設為如下構成:於以規定間隔隔開而配置之偏航致動器中,選擇在偏航軸承齒輪9之圓周方向上設置於成為對稱之位置之致動器代替如上所述般連續鄰接之3個偏航致動器並使之停止。 再者,於m=1之情形時,藉由反覆進行最多8次上述步驟S142~步驟S145之處理,可特定出處於異常狀態之偏航致動器。By setting m=3 as in the present embodiment, the group (group) including the yaw actuator in the abnormal state can be determined as soon as possible, and when the situation of the yaw actuator in the abnormal state is specified, the By sequentially stopping the m yaw actuators constituting the group (group) judged to be abnormal, and performing the same judgment, the yaw actuator in the abnormal state can be identified. It is also possible to have a configuration in which, among the yaw actuators arranged at predetermined intervals, the actuators arranged at symmetrical positions in the circumferential direction of the yaw bearing gear 9 are selected instead of continuous as described above. Adjacent 3 yaw actuators and stop them. Furthermore, in the case of m=1, by repeating the above-mentioned steps S142 to S145 at most 8 times, the yaw actuator in the abnormal state can be identified.

又,嚴密而言,關於對在偏航軸承齒輪9之外周側在圓周方向上以規定間隔隔開而設置之複數個偏航致動器施加之負荷,根據風力狀況(風向及風速)而每個偏航致動器不同。然而,如圖9及圖10所示,藉由使用偏航運轉中之偏航致動器之輸出之合計值(與偏航致動器對應之變流器之電流值之合計值),可吸收因風力狀況帶來之影響並且判定偏航致動器之異常。換言之,藉由設為利用偏航致動器之輸出之合計值進行異常判定之構成,即便於對各偏航致動器施加不同之負荷之情形時,亦可不考慮其影響而進行判定。Strictly speaking, the load applied to a plurality of yaw actuators provided at predetermined intervals in the circumferential direction on the outer peripheral side of the yaw bearing gear 9 varies depending on the wind conditions (wind direction and wind speed). Each yaw actuator is different. However, as shown in FIGS. 9 and 10 , by using the total value of the outputs of the yaw actuators in the yaw rotation (the total value of the current values of the current transformers corresponding to the yaw actuators), it is possible to Absorbs the influence of wind conditions and determines the abnormality of the yaw actuator. In other words, by using the total value of the outputs of the yaw actuators for abnormality determination, even when different loads are applied to the respective yaw actuators, the determination can be made without considering the influence.

於本實施例中,於圖9所示之流程圖中,設為當於步驟S11中偵測偏航回轉異常時進入步驟S12之構成,但未必需要「偵測偏航回轉異常」之步驟,亦可取而代之,設為以規定週期執行步驟S12~步驟S19之處理之構成。In this embodiment, in the flowchart shown in FIG. 9 , it is assumed that the step S12 is entered when the abnormal yaw rotation is detected in the step S11, but the step of “detecting the abnormal yaw rotation” is not necessarily required, Instead, it may be set as the structure which performs the process of step S12 - step S19 in predetermined cycle.

又,本實施例之風力發電裝置及風力發電系統亦可同樣地應用於具備複數架風力發電裝置之風電場。In addition, the wind power generation apparatus and the wind power generation system of the present embodiment can be similarly applied to a wind farm including a plurality of wind power generation apparatuses.

如上所述,根據本實施例,可提供一種能夠儘早地判定偏航致動器之異常之風力發電裝置及風力發電系統。 又,根據本實施例,即便於因風力狀況(風向及風速)而對各偏航致動器施加不同之負荷之情形時,亦可不考慮其影響而進行判定。 [實施例2]As described above, according to the present embodiment, it is possible to provide a wind power generation device and a wind power generation system capable of early determination of the abnormality of the yaw actuator. Furthermore, according to the present embodiment, even when different loads are applied to the yaw actuators due to wind conditions (wind direction and wind speed), the determination can be made without considering the influence. [Example 2]

圖11係本發明之另一實施例之實施例2之風力發電系統之整體概略構成圖。於實施例1中,設為將一架風力發電裝置2中所設置之複數個偏航致動器之輸出之合計值與規定之第1閾值進行比較而判定異常之構成,相對於此,本實施例與實施例1之不同點在於:以設置複數架風力發電裝置之風電場為對象,將風電場內鄰接之2架風力發電裝置之各者中所設置之複數個偏航致動器之輸出相對地進行比較,藉此判定異常。對與實施例1相同之構成要素標註相同符號,以下,省略與實施例1重複之說明。FIG. 11 is an overall schematic configuration diagram of the wind power generation system according to the second embodiment of the present invention. In the first embodiment, the total value of the outputs of the plurality of yaw actuators installed in one wind turbine generator 2 is compared with the predetermined first threshold value to determine the abnormality. In contrast to this, this The difference between Example 1 and Example 1 is that a wind farm where a plurality of wind power generators are installed is taken as an object, and the difference between the plurality of yaw actuators installed in each of the two adjacent wind power generators in the wind farm is compared. The outputs are compared relative to each other, thereby determining the abnormality. The same reference numerals are assigned to the same components as those of the first embodiment, and the descriptions overlapping those of the first embodiment will be omitted below.

如圖11所示,本實施例之風力發電系統1a包括:複數架風力發電裝置(2a、2b、…2n)、設置於運轉管理中心3內之電子終端5、設置於各風力發電裝置(2a、2b、…2n)內之控制裝置29a、及將電子終端5與控制裝置29a可相互通信地連接之通信網路6。此處,通信網路6不限為有線、或無線。設置於各風力發電裝置(2a、2b、…2n)之感測器4、設置於塔架21與機艙22之連結部分之未圖示之偏航軸承齒輪9及複數個偏航致動器10與上述實施例1相同,故而省略說明。又,偏航動力控制部14及動力遮斷機構部15之構成亦與實施例1相同,故而省略說明。 一般而言,於風電場中,通過位於上風側之風力發電裝置之風受到構成處於上風側之風力發電裝置之葉輪之旋轉之影響,而風向、風速等風力狀況變化,並向處於下風側之風力發電裝置傳遞。如此,將向處於下風側之風力發電裝置傳遞之風力狀況已變化之風之流動稱為風車後流(亦稱為尾流)。再者,於通過處於上風側之風力發電裝置時變化之風力狀況不限於風向、風速,亦包括作為風之亂流方式之亂流特性或漩渦之形狀等。風車後流(尾流)於通過處於上風側之風力發電裝置後,一面擴大,一面向下風側流動。即,風車後流一面擴散,一面產生漩渦流(亂流),同時向下風側傳遞。As shown in FIG. 11, the wind power generation system 1a of this embodiment includes: a plurality of wind power generation devices (2a, 2b, . . . 2n), an electronic terminal 5 installed in the operation management center 3, and each wind power generation device (2a , 2b, . . . 2n) within the control device 29a, and the communication network 6 that connects the electronic terminal 5 and the control device 29a in a communicable manner. Here, the communication network 6 is not limited to wired or wireless. Sensors 4 installed in each wind power generator (2a, 2b, . . . 2n), yaw bearing gears 9 and a plurality of yaw actuators 10 not shown in the connecting portion of tower 21 and nacelle 22 It is the same as the above-mentioned Embodiment 1, so the description is omitted. In addition, the configuration of the yaw power control unit 14 and the power cutoff mechanism unit 15 is also the same as that of the first embodiment, so the description is omitted. Generally speaking, in a wind farm, the wind passing through the wind power generation device on the windward side is affected by the rotation of the impeller constituting the wind power generation device on the windward side, and the wind direction, wind speed and other wind conditions change, and the wind direction, wind speed and other wind conditions change, and the wind direction, wind speed, etc. Wind power transmission on the wind side. In this way, the flow of the wind with the changed wind condition transmitted to the wind power generating device on the leeward side is called a windmill backflow (also called a wake). Furthermore, the wind condition that changes when passing through the wind turbine generator on the windward side is not limited to the wind direction and wind speed, but also includes the turbulent flow characteristics and the shape of the vortex as the turbulent flow of the wind. After passing through the wind turbine on the windward side, the back flow (wake) of the windmill expands and flows on the leeward side. That is, while the windmill rear flow spreads, a vortex flow (turbulent flow) is generated, and it is transmitted to the leeward side.

圖12係圖11所示之控制裝置29a之功能方塊圖。此處,假定如下情形:圖12所示之控制裝置29a為設置於風力發電裝置2a之控制裝置。如圖12所示,控制裝置29a具備:輸出運算部31、異常判定部32、記憶部33、機器控制部34、正規化處理部35、通信I/F36、輸入I/F37、及輸出I/F38,該等以彼此可利用內部匯流排39進行存取之方式連接。輸出運算部31、異常判定部32、機器控制部34、及正規化處理部35例如利用未圖示之CPU(Central Processing Unit)等處理器、供儲存各種程式之ROM、暫時儲存運算過程之資料之RAM、外部記憶裝置等記憶裝置來實現,並且CPU等處理器讀出ROM中所儲存之各種程式並執行,將作為執行結果之運算結果儲存於RAM或外部記憶裝置。FIG. 12 is a functional block diagram of the control device 29a shown in FIG. 11 . Here, it is assumed that the control device 29a shown in FIG. 12 is a control device provided in the wind power generator 2a. As shown in FIG. 12, the control device 29a includes an output calculation unit 31, an abnormality determination unit 32, a memory unit 33, a device control unit 34, a normalization processing unit 35, a communication I/F 36, an input I/F 37, and an output I/F F38, these are connected in such a way that they are accessible to each other by means of the internal bus bar 39. The output calculation unit 31 , the abnormality determination unit 32 , the machine control unit 34 , and the normalization processing unit 35 use a processor such as a CPU (Central Processing Unit), not shown, for example, a ROM for storing various programs, and temporarily store the data of the calculation process. It is realized by a memory device such as RAM and an external memory device, and a processor such as a CPU reads out various programs stored in the ROM and executes it, and stores the operation result as the execution result in the RAM or the external memory device.

機器控制部34經由輸入I/F37及內部匯流排39獲取作為感測器4之例如風向風速計、槳距角感測器、偏航角感測器、及應變感測器之量測資料。機器控制部34基於所獲取之量測資料控制風力發電裝置2之運轉。例如,一面基於風速資料控制葉片24之朝向或轉數等參數,一面繼續運轉。具體而言,基於由風向風速計量測所得之風向資料,經由輸出I/F38向構成偏航角控制機構之偏航動力控制部14輸出偏航角控制信號,以使包括葉片24及輪轂23之葉輪與風向正對,及/或,基於由風向風速計量測所得之風速資料,經由輸出I/F38向槳距角控制機構17輸出作為葉片24之傾斜角之槳距角控制信號。又,機器控制部34基於由感測器4量測所得之發電機27之發電量,經由輸出I/F38向增速機26輸出控制發電機旋轉速度之轉速控制信號。The machine control unit 34 acquires measurement data such as anemometers, pitch angle sensors, yaw angle sensors, and strain sensors as the sensors 4 through the input I/F 37 and the internal bus bar 39 . The equipment control unit 34 controls the operation of the wind power generator 2 based on the acquired measurement data. For example, while controlling parameters such as the orientation of the blade 24 or the number of revolutions based on the wind speed data, the operation is continued. Specifically, based on the wind direction data measured by the wind direction anemometer, the yaw angle control signal is output to the yaw power control unit 14 constituting the yaw angle control mechanism through the output I/F 38, so that the blades 24 and the hub 23 are included. The impeller is directly opposite to the wind direction, and/or, based on the wind speed data measured by the wind direction anemometer, the pitch angle control signal as the pitch angle of the blade 24 is output to the pitch angle control mechanism 17 via the output I/F 38. Furthermore, the device control unit 34 outputs a rotational speed control signal for controlling the rotational speed of the generator to the gearbox 26 via the output I/F 38 based on the power generation amount of the generator 27 measured by the sensor 4 .

正規化處理部35經由輸入I/F37及內部匯流排39,獲取由與設置於風力發電裝置2a(第1風力發電裝置)之各偏航致動器10對應之輸出量測部16量測所得之作為偏航動力控制部14之變流器之電流值。進而,正規化處理部35經由通信網路6、輸入I/F37及內部匯流排39,獲取由與設置於和風力發電裝置2a鄰接之例如風力發電裝置2b(第2風力發電裝置)之各偏航致動器10對應的輸出量測部16量測所得之作為偏航動力控制部14之變流器之電流值。 如上所述,於彼此鄰接之風力發電裝置2a(第1風力發電裝置)及風力發電裝置2b(第2風力發電裝置)處,風力狀況變化,位於下風側之風力發電裝置2b(第2風力發電裝置)亦受到風車後流之影響。因此,設置於風力發電裝置2a(第1風力發電裝置)之各偏航致動器10受施加之負荷、與設置於位於下風側之風力發電裝置2b(第2風力發電裝置)之各偏航致動器10上受施加之負荷不同。表現出受施加之負荷越大,與偏航致動器10對應之變流器之電流之振幅變得越高之傾向。因此,正規化處理部35對所獲取之與風力發電裝置2a(第1風力發電裝置)之各偏航致動器10對應之變流器之電流值及與設置於鄰接之風力發電裝置2b(第2風力發電裝置)之各偏航致動器10對應之變流器之電流值,例如執行基於電流值之振幅之峰值位準之正規化處理。正規化處理部35經由內部匯流排39向輸出運算部31及異常判定部32傳送正規化處理後之風力發電裝置2a(第1風力發電裝置)之變流器之電流值及正規化處理後之鄰接之風力發電裝置2b(第2風力發電裝置)之變流器之電流值。The normalization processing unit 35 obtains, through the input I/F 37 and the internal bus bar 39, the measurement results obtained by the output measurement unit 16 corresponding to each yaw actuator 10 provided in the wind turbine generator 2a (first wind turbine generator). It is used as the current value of the current transformer of the yaw power control unit 14 . Further, the normalization processing unit 35 acquires the data of each offset from the wind turbine generator 2b (second wind turbine generator) installed adjacent to the wind turbine generator 2a via the communication network 6, the input I/F 37, and the internal busbar 39, for example. The current value of the current transformer of the yaw power control unit 14 is measured by the output measuring unit 16 corresponding to the yaw actuator 10 . As described above, in the adjacent wind power generators 2a (first wind power generators) and wind power generators 2b (second wind power generators), the wind conditions change, and the wind power generator 2b (second wind power generator) on the leeward side power generation units) are also affected by windmill backflow. Therefore, the load applied to each yaw actuator 10 installed in the wind power generator 2a (first wind power generator) and the yaw actuators 10 installed on the leeward side of the wind power generator 2b (second wind power generator) The loads applied to the aviation actuator 10 are different. It appears that the larger the applied load, the higher the amplitude of the current of the current transformer corresponding to the yaw actuator 10 becomes. Therefore, the normalization processing unit 35 compares the acquired current values of the converters corresponding to the yaw actuators 10 of the wind turbine generator 2a (first wind turbine generator) and the current values of the inverters provided in the adjacent wind turbine generator 2b ( The current value of the converter corresponding to each yaw actuator 10 of the second wind power generator) is, for example, normalized based on the peak level of the amplitude of the current value. The normalization processing unit 35 transmits the normalized current value of the inverter of the wind power generator 2a (first wind power generator) and the normalized value of the normalized value to the output calculation unit 31 and the abnormality determination unit 32 via the internal bus bar 39 . The current value of the converter of the adjacent wind turbine generator 2b (second wind turbine generator).

輸出運算部31將自正規化處理部35傳送之正規化處理後之與風力發電裝置2a(第1風力發電裝置)之各偏航致動器10對應之變流器之電流值進行相加,以風力發電裝置2a(第1風力發電裝置)之各偏航致動器10之輸出之合計值形式經由內部匯流排39向異常判定部32傳送。又,輸出運算部31將自正規化處理部35傳送之正規化處理後之與鄰接之風力發電裝置2b(第2風力發電裝置)之各偏航致動器10對應之變流器之電流值進行相加,以風力發電裝置2b(第2風力發電裝置)之各偏航致動器10之輸出之合計值形式經由內部匯流排39向異常判定部32傳送。 異常判定部32將自正規化處理部35傳送之正規化處理後之與風力發電裝置2a(第1風力發電裝置)之各偏航致動器10對應之變流器之電流值之曲線(正規化處理後之風力發電裝置2a(第1風力發電裝置)之各偏航致動器之輸出之曲線)、與自正規化處理部35傳送之正規化處理後之與鄰接之風力發電裝置2b(第2風力發電裝置)之各偏航致動器10對應之變流器之電流值之曲線(正規化處理後之鄰接之風力發電裝置2b(第2風力發電裝置)之各偏航致動器之輸出之曲線)進行比較,於比較結果大致一致之情形時,判定為風力發電裝置2a(第1風力發電裝置)及鄰接之風力發電裝置2b(第2風力發電裝置)均為各偏航致動器10正常。另一方面,於比較結果有變動之情形時,特定出具有異常偏航致動器之風力發電裝置。The output calculation unit 31 adds the current values of the converters corresponding to the yaw actuators 10 of the wind turbine generator 2a (first wind turbine generator) after the normalization process transmitted from the normalization processing unit 35, The sum of the outputs of the yaw actuators 10 of the wind turbine generator 2a (first wind turbine generator) is transmitted to the abnormality determination unit 32 via the internal bus bar 39 . In addition, the output calculation unit 31 outputs the current value of the converter corresponding to each yaw actuator 10 of the adjacent wind turbine generator 2b (second wind turbine generator) after the normalization process transmitted from the normalization processing unit 35. The addition is performed, and the sum of the outputs of the yaw actuators 10 of the wind turbine generator 2b (second wind turbine generator) is sent to the abnormality determination unit 32 via the internal bus bar 39 . The abnormality determination unit 32 uses a curve (normalized) of the current value of the converter corresponding to each yaw actuator 10 of the wind turbine generator 2a (first wind turbine generator) after the normalization process transmitted from the normalization processing unit 35. The curve of the output of each yaw actuator of the wind power generator 2a (first wind power generator) after the normalization process), and the normalization process transmitted from the normalization processing unit 35 and the adjacent wind power generator 2b ( Curve of the current value of the converter corresponding to each yaw actuator 10 of the second wind turbine The output curves) are compared, and when the comparison results are substantially consistent, it is determined that the wind power generator 2a (first wind power generator) and the adjacent wind power generator 2b (the second wind power generator) are both yaw-induced Actuator 10 is normal. On the other hand, in the case where the comparison result varies, the wind power generation device having the abnormal yaw actuator is specified.

或,異常判定部32將自輸出運算部31傳送之風力發電裝置2a(第1風力發電裝置)之各偏航致動器10之輸出之合計值、與自輸出運算部31傳送之風力發電裝置2b(第2風力發電裝置)之各偏航致動器10之輸出之合計值進行比較,於比較結果大致一致之情形時,判定為風力發電裝置2a(第1風力發電裝置)及鄰接之風力發電裝置2b(第2風力發電裝置)均為各偏航致動器10正常。另一方面,於比較結果有變動之情形時,特定出具有異常偏航致動器之風力發電裝置。 再者,異常檢測裝置30a包括正規化處理部35、輸出運算部31、及異常判定部32。Alternatively, the abnormality determination unit 32 compares the total value of the outputs of the respective yaw actuators 10 of the wind turbine generator 2 a (first wind turbine generator) transmitted from the output calculation unit 31 to the wind turbine generator transmitted from the output calculation unit 31 . 2b (2nd wind power generator) The total value of the output of each yaw actuator 10 is compared, and when the comparison results are substantially the same, it is determined that the wind power generator 2a (1st wind power generator) and the adjacent wind power Each of the yaw actuators 10 was normal in the power generator 2b (second wind power generator). On the other hand, in the case where the comparison result varies, the wind power generation device having the abnormal yaw actuator is specified. Furthermore, the abnormality detection device 30 a includes a normalization processing unit 35 , an output calculation unit 31 , and an abnormality determination unit 32 .

圖13係圖12所示之異常檢測裝置30a之流程圖。以下,以構成設置於風力發電裝置2a之控制裝置29a之異常檢測裝置30a之動作作為一例進行說明。 於步驟S21中,異常檢測裝置30a設定風電場內之彼此相鄰之2架風力發電裝置(第1風力發電裝置及第2風力發電裝置)。此處,假定如下情形:所選定之第1風力發電裝置為風力發電裝置2a,第2風力發電裝置為風力發電裝置2b。FIG. 13 is a flowchart of the abnormality detection device 30a shown in FIG. 12 . Hereinafter, the operation|movement of the abnormality detection apparatus 30a which comprises the control apparatus 29a provided in the wind turbine generator 2a is demonstrated as an example. In step S21, the abnormality detection device 30a sets two wind turbines (a first wind turbine and a second wind turbine) adjacent to each other in the wind farm. Here, it is assumed that the selected first wind power generator is the wind power generator 2a, and the second wind power generator is the wind power generator 2b.

於步驟S22中,構成異常檢測裝置30a之正規化處理部35獲取由與所選定之第1風力發電裝置(風力發電裝置2a)及第2風力發電裝置(風力發電裝置2b)之各偏航致動器10對應之輸出量測部16量測所得之變流器之電流值。In step S22, the normalization processing unit 35 constituting the abnormality detection device 30a acquires the yaw correlation with each of the selected first wind power generator (wind power generator 2a) and the second wind power generator (wind power generator 2b). The output measurement unit 16 corresponding to the actuator 10 measures the current value of the converter.

於步驟S23中,正規化處理部35對所獲取之與第1風力發電裝置(風力發電裝置2a)之各偏航致動器10對應之變流器之電流值及與第2風力發電裝置(風力發電裝置2b)之各偏航致動器10對應之變流器之電流值,例如執行基於電流值之振幅之峰值位準之正規化處理。正規化處理部35經由內部匯流排39將正規化處理後之第1風力發電裝置(風力發電裝置2a)之變流器之電流值及正規化處理後之第2風力發電裝置(風力發電裝置2b)之變流器之電流值向異常判定部32傳送。In step S23, the normalization processing unit 35 compares the acquired current value of the converter corresponding to each yaw actuator 10 of the first wind power generator (wind power generator 2a) and the current value of the converter corresponding to the second wind power generator (wind power generator 2a). The current value of the converter corresponding to each yaw actuator 10 of the wind power generation device 2b) is, for example, normalized based on the peak level of the amplitude of the current value. The normalization processing unit 35 normalizes the current value of the inverter of the first wind power generator (wind power generator 2a) after the normalization process and the normalized second wind power generator (wind power generator 2b) through the internal bus bar 39 ), the current value of the current transformer is sent to the abnormality determination unit 32 .

於步驟S24中,異常判定部32於第1風力發電裝置(風力發電裝置2a)及第2風力發電裝置(風力發電裝置2b)間比較正規化後之各偏航致動器之輸出之曲線。於比較結果為有變動之情形時,進入步驟S25,特定出具有異常偏航致動器之風力發電裝置,結束處理。 另一方面,於比較結果為大致一致之情形時,進入步驟S26。In step S24, the abnormality determination unit 32 compares the normalized output curves of the yaw actuators between the first wind power generator (wind power generator 2a) and the second wind power generator (wind power generator 2b). When the comparison result shows that there is a change, the process proceeds to step S25, and the wind power generator with the abnormal yaw actuator is specified, and the process ends. On the other hand, when the comparison result is substantially the same, the process proceeds to step S26.

於步驟S26中,選定彼此鄰接之2架風力發電裝置,返回至步驟S22,對風電場內所有之風力發電裝置2n執行步驟S22~步驟S26之處理。In step S26, two adjacent wind power generators are selected, and the process returns to step S22, and the processes of steps S22 to S26 are performed on all the wind power generators 2n in the wind farm.

再者,代替步驟S24,由輸出運算部31將自正規化處理部35傳送之正規化處理後之與第1風力發電裝置(風力發電裝置2a)之各偏航致動器10對應之變流器之電流值進行相加,以第1風力發電裝置(風力發電裝置2a)之各偏航致動器10之輸出之合計值形式經由內部匯流排39向異常判定部32傳送。又,由輸出運算部31將自正規化處理部35傳送之正規化處理後之與鄰接之第2風力發電裝置(風力發電裝置2b)之各偏航致動器10對應之變流器之電流值進行相加,以第2風力發電裝置(風力發電裝置2b)之各偏航致動器10之輸出之合計值形式經由內部匯流排39向異常判定部32傳送。然後,亦可設為如下構成:異常判定部32對所傳送之第1風力發電裝置(風力發電裝置2a)之各偏航致動器10之輸出之合計值與第2風力發電裝置(風力發電裝置2b)之各偏航致動器10之輸出之合計值進行比較。In addition, instead of step S24, the output calculation unit 31 performs the normalization process transmitted from the normalization processing unit 35 to the variable current corresponding to each yaw actuator 10 of the first wind power generator (wind power generator 2a). The current values of the generators are added, and the sum of the outputs of the yaw actuators 10 of the first wind power generator (wind power generator 2 a ) is sent to the abnormality determination unit 32 via the internal bus bar 39 . Further, the current of the converter corresponding to each yaw actuator 10 of the adjacent second wind power generator (wind power generator 2b) after the normalization process transmitted from the normalization processing unit 35 is carried out by the output calculation unit 31 The values are added, and the sum of the outputs of the yaw actuators 10 of the second wind turbine generator (wind turbine generator 2 b ) is transmitted to the abnormality determination unit 32 via the internal bus bar 39 . Then, a configuration may be adopted in which the abnormality determination unit 32 transmits the sum of the outputs of the respective yaw actuators 10 of the first wind power generator (wind power generator 2a) and the second wind power generator (wind power generator 2a). The sum of the outputs of the yaw actuators 10 of the device 2b) is compared.

又,亦可設為如下構成:對於上述步驟S25中所特定出之具有異常偏航致動器之風力發電裝置執行上述實施例1中示於圖10之偏航致動器異常部位檢測序列之詳細流程。In addition, it can also be configured as follows: for the wind power generation device with the abnormal yaw actuator specified in the above step S25, the abnormal part detection sequence of the yaw actuator shown in FIG. 10 in the above-mentioned embodiment 1 is executed. Detailed process.

再者,於本實施例中,設為由構成設置於彼此鄰接之2架風力發電裝置中之一架風力發電裝置之控制裝置29a的異常檢測裝置30a執行圖13所示之流程之構成,但並不限於此。例如亦可設為如下構成:於設置於運轉管理中心3內之電子終端5安裝異常檢測裝置30a,而執行圖13所示之流程。Furthermore, in this embodiment, the abnormality detection device 30a constituting the control device 29a of one of the two wind turbine generators installed adjacent to each other executes the flow shown in FIG. 13, but It is not limited to this. For example, the following configuration may be employed: the abnormality detection device 30a is installed in the electronic terminal 5 installed in the operation management center 3, and the flow shown in FIG. 13 is executed.

如上所述,根據本實施例,除實施例1之效果以外,即便於設置複數架風力發電裝置之風電場中,亦可儘早地特定出具有已產生異常之偏航致動器之風力發電裝置。 又,根據本實施例,為藉由將風電場內鄰接之2架風力發電裝置之各者中所設置之複數個偏航致動器之輸出相對地進行比較來判定異常的構成,因此能夠以相對簡易之處理實現異常判定。As described above, according to the present embodiment, in addition to the effect of the first embodiment, even in a wind farm in which a plurality of wind turbines are installed, a wind turbine having a yaw actuator in which an abnormality has occurred can be identified as soon as possible . Furthermore, according to the present embodiment, the abnormality can be determined by relatively comparing the outputs of the plurality of yaw actuators installed in each of the two adjacent wind turbine generators in the wind farm. Relatively simple processing realizes abnormal judgment.

再者,本發明並不限於上述實施例,包括多種變化例。例如,上述實施例係為了容易理解地說明本發明而進行了詳細說明,但未必限於具備所說明之所有構成。又,可將某一實施例之構成之一部分置換成另一實施例之構成,又,亦可對某一實施例之構成添加另一實施例之構成。Furthermore, the present invention is not limited to the above-described embodiments, and includes various modifications. For example, the above-mentioned embodiments have been described in detail in order to explain the present invention in an easy-to-understand manner, but the present invention is not necessarily limited to having all the structures described. In addition, a part of the configuration of a certain embodiment may be replaced with the configuration of another embodiment, and the configuration of another embodiment may be added to the configuration of a certain embodiment.

1:風力發電系統 1a:風力發電系統 2:風力發電裝置 2a:風力發電裝置 2b:風力發電裝置 2n:風力發電裝置 3:運轉管理中心 4:感測器 5:電子終端 6:通信網路 9:偏航軸承齒輪 10:偏航致動器 11:小齒輪 12:減速機 13:驅動馬達 14:偏航動力控制部 15:動力阻斷機構部 16:輸出量測部 17:槳距角控制機構 21:塔架 22:機艙 23:輪轂 24:葉片 25:主軸 26:增速機 27:發電機 28:電力轉換器 29:控制裝置 29a:控制裝置 30:異常檢測裝置 30a:異常檢測裝置 31:輸出運算部 32:異常判定部 33:記憶部 34:機器控制部 35:正規化處理部 36:通信I/F 37:輸入I/F 38:輸出I/F 39:內部匯流排 40:殼體 41a:主殼體部 41b:副殼體部 42:內齒 43:輸入齒輪 44:動力軸 45:外齒輪 46:外齒 50:曲軸 51:桿本體 53:正齒輪 60:載體 60a:第1半體 60b:第2半體 61:第1保持部 62:第2保持部 63:支柱 64:結合筒部 64a:第1筒半部 64b:第2筒半部 65:載體側花鍵部 66:輸出軸 71:第1端部用貫通孔 72:第2端部用貫通孔 73:第1曲軸用軸承 74:第2曲軸用軸承 89:離合器作動部 89a:第1摩擦板 89b:第2摩擦板 90:離合器控制部 90a:壓力調整閥 90b:通電控制器 91:離合器驅動體 92:彈性構件 93:油壓供給路 93b:油壓作用部 94:離合器油壓源 95:積蓄器 98:泄放閥 99:排水閥 107:第1連結構件 107a:螺絲構件 109:第2連結構件 109a:螺絲構件 111:輸入側部分 199:排水閥 252:油壓馬達 1: Wind power generation system 1a: Wind Power Systems 2: Wind power plant 2a: Wind Power Plants 2b: Wind Power Plants 2n: wind power plant 3: Operation Management Center 4: Sensor 5: Electronic terminal 6: Communication network 9: Yaw bearing gear 10: Yaw actuator 11: pinion gear 12: Reducer 13: drive motor 14: Yaw power control section 15: Power Blocking Mechanism Department 16: Output measurement section 17: Pitch angle control mechanism 21: Tower 22: Cabin 23: Wheels 24: Blades 25: Spindle 26: Speed up machine 27: Generator 28: Power Converter 29: Controls 29a: Controls 30: Abnormal detection device 30a: Abnormal detection device 31: Output operation part 32: Abnormal Determination Department 33: Memory Department 34: Machine Control Department 35: Normalization Processing Department 36: Communication I/F 37: Input I/F 38: Output I/F 39: Internal busbar 40: Shell 41a: main housing part 41b: Auxiliary housing part 42: Internal teeth 43: Input gear 44: Power shaft 45: External gear 46: External teeth 50: Crankshaft 51: Rod body 53: Spur Gear 60: Carrier 60a: 1st half body 60b: 2nd half body 61: 1st Retention Department 62: 2nd Retention Division 63: Pillar 64: Combined barrel 64a: 1st cylinder half 64b: 2nd barrel half 65: Spline part on carrier side 66: Output shaft 71: Through hole for the first end 72: Through hole for second end 73: Bearing for the first crankshaft 74: Bearing for the second crankshaft 89: Clutch Actuator 89a: 1st friction plate 89b: 2nd friction plate 90: Clutch control unit 90a: Pressure regulating valve 90b: Power On Controller 91: Clutch drive body 92: Elastic member 93: Hydraulic supply path 93b: Hydraulic action part 94: Clutch oil pressure source 95: Accumulator 98: Relief valve 99: Drain valve 107: 1st connecting member 107a: Screw components 109: Second link member 109a: Screw components 111: Input side part 199: Drain valve 252: hydraulic motor

圖1係本發明之一實施例之風力發電系統之整體概略構成圖。 圖2係表示圖1所示之風力發電裝置之塔架頂部附近之立體圖。 圖3係表示圖1所示之風力發電裝置之塔架頂部附近之側視圖。 圖4係實施例1之偏航致動器及異常檢測裝置之方塊線圖。 圖5係圖1所示之控制裝置之功能方塊圖。 圖6係表示圖4所示之偏航致動器及動力阻斷機構部之局部剖視圖。 圖7係表示自圖6所示之輸出軸向小齒輪之旋轉動力之傳遞狀態之概略圖。 圖8係表示自圖6所示之輸出軸向小齒輪之旋轉動力之非傳遞狀態之概略圖。 圖9係圖5所示之異常檢測裝置之流程圖。 圖10係表示圖9所示之偏航致動器異常部位檢測序列之詳細流程之流程圖。 圖11係本發明之另一實施例之實施例2之風力發電系統之整體概略構成圖。 圖12係圖11所示之控制裝置之功能方塊圖。 圖13係圖12所示之異常檢測裝置之流程圖。FIG. 1 is an overall schematic configuration diagram of a wind power generation system according to an embodiment of the present invention. FIG. 2 is a perspective view showing the vicinity of the top of the tower of the wind power generator shown in FIG. 1 . FIG. 3 is a side view showing the vicinity of the top of the tower of the wind power plant shown in FIG. 1 . 4 is a block diagram of the yaw actuator and the abnormality detection device of the first embodiment. FIG. 5 is a functional block diagram of the control device shown in FIG. 1 . FIG. 6 is a partial cross-sectional view showing the yaw actuator and the power blocking mechanism shown in FIG. 4 . FIG. 7 is a schematic view showing the transmission state of the rotational power of the pinion gear from the output shaft shown in FIG. 6 . FIG. 8 is a schematic view showing a non-transmission state of the rotational power from the output shaft shown in FIG. 6 to the pinion. FIG. 9 is a flowchart of the abnormality detection apparatus shown in FIG. 5 . FIG. 10 is a flowchart showing a detailed flow of the abnormal part detection sequence of the yaw actuator shown in FIG. 9 . FIG. 11 is an overall schematic configuration diagram of the wind power generation system according to the second embodiment of the present invention. FIG. 12 is a functional block diagram of the control device shown in FIG. 11 . FIG. 13 is a flowchart of the abnormality detection apparatus shown in FIG. 12 .

4:感測器 4: Sensor

6:通信網路 6: Communication network

14:偏航動力控制部 14: Yaw power control section

15:動力阻斷機構部 15: Power Blocking Mechanism Department

16:輸出量測部 16: Output measurement section

17:槳距角控制機構 17: Pitch angle control mechanism

29:控制裝置 29: Controls

30:異常檢測裝置 30: Abnormal detection device

31:輸出運算部 31: Output operation part

32:異常判定部 32: Abnormal Determination Department

33:記憶部 33: Memory Department

34:機器控制部 34: Machine Control Department

36:通信I/F 36: Communication I/F

37:輸入I/F 37: Input I/F

38:輸出I/F 38: Output I/F

39:內部匯流排 39: Internal busbar

Claims (11)

一種風力發電裝置,其特徵在於具備:機艙,其支持受風而旋轉之葉輪;塔架,其將上述機艙可旋動地支持;複數個偏航致動器,其使上述機艙相對於上述塔架旋動;及異常檢測裝置,其檢測上述偏航致動器之異常;上述異常檢測裝置將各偏航致動器之輸出之合計值與規定之第1閾值進行比較,若上述輸出之合計值超過上述規定之第1閾值,則判定為偏航致動器之異常,且上述異常檢測裝置具備異常判定部,該異常判定部於上述輸出之合計值超過上述規定之第1閾值之情形時,使上述複數個偏航致動器中之一部分偏航致動器停止,並基於動作中之偏航致動器之輸出之合計值判定存在異常之偏航致動器。 A wind power generator is characterized by comprising: a nacelle for supporting an impeller that is rotated by wind; a tower for rotatably supporting the nacelle; and a plurality of yaw actuators for making the nacelle relative to the tower Frame rotation; and abnormality detection means for detecting abnormality of said yaw actuator; said abnormality detection means compares the sum of the outputs of the respective yaw actuators with a prescribed first threshold value, and if the sum of said outputs is If the value exceeds the first threshold value specified above, it is determined that the yaw actuator is abnormal, and the abnormality detection device includes an abnormality determination unit that, when the total value of the outputs exceeds the first threshold value specified above, , a part of the yaw actuators among the plurality of yaw actuators is stopped, and the abnormal yaw actuator is determined based on the total value of the outputs of the yaw actuators in operation. 如請求項1之風力發電裝置,其中上述異常判定部使上述複數個偏航致動器中之一部分偏航致動器停止,於動作中之偏航致動器之輸出之合計值超過規定之第2閾值之情形時,將動作中之偏航致動器判定為異常。 The wind power generator according to claim 1, wherein the abnormality determination unit stops a part of the yaw actuators among the plurality of yaw actuators, and the total value of the outputs of the yaw actuators in operation exceeds a predetermined value In the case of the second threshold value, the operating yaw actuator is determined to be abnormal. 如請求項2之風力發電裝置,其中上述異常判定部使上述複數個偏航致動器中之一部分偏航致動器之每個依序停止,將動作中之偏航致動器之輸出之合計值與上述規定之第2 閾值進行比較,而特定出存在異常之偏航致動器。 The wind power generator according to claim 2, wherein the abnormality determination unit stops each of a part of the yaw actuators in sequence among the plurality of yaw actuators, and sets the output of the yaw actuator in operation to The total value and the 2nd of the above provisions Thresholds are compared to identify the abnormal yaw actuator. 如請求項2或3之風力發電裝置,其中上述規定之第2閾值小於上述規定之第1閾值。 The wind power generator according to claim 2 or 3, wherein the second threshold specified above is smaller than the first threshold specified above. 如請求項4之風力發電裝置,其中上述規定之第2閾值係藉由將上述複數個偏航致動器之總數中所占的要停止之一部分偏航致動器之數量的比率乘以上述規定之第1閾值而設定。 The wind power generator according to claim 4, wherein the second threshold specified above is obtained by multiplying the ratio of the number of partial yaw actuators to be stopped in the total number of the plurality of yaw actuators by the above A predetermined first threshold value is set. 如請求項5之風力發電裝置,其中上述規定之第1閾值至少為在工廠內之試運轉時之各偏航致動器之合計值、安設風力發電裝置時之試運轉時之各偏航致動器之輸出之合計值、及較基於包括偏航致動器之更換之維護記錄進行維護時更早之規定期間內之各偏航致動器之輸出之合計值之平均中之任一者。 The wind power generator according to claim 5, wherein the first threshold specified above is at least the total value of each yaw actuator during trial operation in the factory, and each yaw value during trial operation when the wind power generator is installed Either the total value of the outputs of the actuators, and the average of the total values of the outputs of the respective yaw actuators within a specified period earlier than when maintenance was performed based on the maintenance record including the replacement of the yaw actuator By. 一種風力發電系統,其特徵在於:具備複數架風力發電裝置,並且具備異常檢測裝置,該風力發電裝置具有支持受風而旋轉之葉輪之機艙、將上述機艙可旋動地支持之塔架、及使上述機艙相對於上述塔架旋動之複數個偏航致動器,該異常檢測裝置檢測上述偏航致動器之異常,上述異常檢測裝置將各偏航致動器之輸出之合計值與規定之第1閾值進行比較,若上述輸出之合計值超過上述規定之第1閾值,則判定為偏航致動器之異常,且 上述異常檢測裝置具備異常判定部,該異常判定部於上述輸出之合計值超過上述規定之第1閾值之情形時,使上述複數個偏航致動器中之一部分偏航致動器停止,並基於動作中之偏航致動器之輸出之合計值判定存在異常之偏航致動器。 A wind power generation system comprising: a plurality of wind power generation devices including a nacelle for supporting an impeller that is rotated by wind, a tower for rotatably supporting the nacelle, and an abnormality detection device; A plurality of yaw actuators for rotating the nacelle relative to the tower, the abnormality detection device detects the abnormality of the yaw actuator, and the abnormality detection device compares the sum of the outputs of the yaw actuators with the sum of the outputs of the yaw actuators. If the total value of the above-mentioned outputs exceeds the above-mentioned predetermined first threshold value, it is determined that the yaw actuator is abnormal, and The abnormality detection device includes an abnormality determination unit that stops a part of the yaw actuators among the plurality of yaw actuators when the total value of the outputs exceeds the predetermined first threshold value, and stops the yaw actuators. An abnormal yaw actuator is determined based on the total value of the outputs of the yaw actuators in operation. 如請求項7之風力發電系統,其中上述異常判定部使上述複數個偏航致動器中之一部分偏航致動器停止,於動作中之偏航致動器之輸出之合計值超過規定之第2閾值之情形時,將動作中之偏航致動器判定為異常。 The wind power generation system according to claim 7, wherein the abnormality determination unit stops a part of the yaw actuators among the plurality of yaw actuators, and the total value of the outputs of the yaw actuators in operation exceeds a predetermined value In the case of the second threshold value, the operating yaw actuator is determined to be abnormal. 如請求項8之風力發電系統,其中上述異常判定部使上述複數個偏航致動器中之一部分偏航致動器之每個依序停止,將動作中之偏航致動器之輸出之合計值與上述規定之第2閾值進行比較,而特定出存在異常之偏航致動器。 The wind power generation system of claim 8, wherein the abnormality determination unit stops each of a part of the yaw actuators in sequence among the plurality of yaw actuators, and changes the output of the yaw actuators in operation The total value is compared with the predetermined second threshold value, and the abnormal yaw actuator is identified. 如請求項8或9之風力發電系統,其中上述規定之第2閾值小於上述規定之第1閾值。 The wind power generation system of claim 8 or 9, wherein the second threshold specified above is smaller than the first threshold specified above. 如請求項10之風力發電系統,其中上述規定之第2閾值係藉由將上述複數個偏航致動器之總數中所占的要停止之一部分偏航致動器之數量的比率乘以上述規定之第1閾值而設定。The wind power generation system of claim 10, wherein the second threshold specified above is obtained by multiplying the ratio of the number of partial yaw actuators to be stopped in the total number of the plurality of yaw actuators by the above A predetermined first threshold value is set.
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