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CN201687662U - Large wind turbine nacelle cover with airflow guides and airflow channels inside - Google Patents

Large wind turbine nacelle cover with airflow guides and airflow channels inside Download PDF

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Publication number
CN201687662U
CN201687662U CN2009202460269U CN200920246026U CN201687662U CN 201687662 U CN201687662 U CN 201687662U CN 2009202460269 U CN2009202460269 U CN 2009202460269U CN 200920246026 U CN200920246026 U CN 200920246026U CN 201687662 U CN201687662 U CN 201687662U
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China
Prior art keywords
airflow
air
guide plate
nacelle cover
channel
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Expired - Fee Related
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CN2009202460269U
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Chinese (zh)
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奚国防
许磊
蔡尧军
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Beijing Zhongxinturui Science & Technology Co Ltd
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Beijing Zhongxinturui Science & Technology Co Ltd
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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

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  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

本实用新型涉及一种内部带有气流导板及气流通道的大型风力发电机组机舱罩,包括机舱罩本体(1),机舱罩内部安装有气流入口通道(2)、四段式的气流导板(3)、气流出口通道(4),机舱罩本体(1)尾部安装有百叶窗(5)、后顶罩安装有后阻流板(6)。所述气流入口通道(2)安装在机舱罩前顶罩下部;所述气流出口通道(4)与机舱罩后阻流板(6)连接,通过后阻流板(6)内置风扇进行强制排风;所述百叶窗(5)进行自然吸风;所述气流入口通道(2)、四段式气流导板(3)及气流出口通道(4)之间均采用软连接。本实用新型由内置在后阻流板内的风扇进行强制吸风,通过机舱罩内部设置的气流导板及气流通道,使机舱罩内的气流按图示设计流向与外界进行循环,带走舱内热量。

Figure 200920246026

The utility model relates to a large-scale wind turbine nacelle cover with an airflow guide plate and an airflow channel inside, comprising a nacelle cover body (1), an airflow inlet channel (2) and a four-stage airflow guide plate (3) installed inside the nacelle cover ), the air outlet channel (4), the louvers (5) are installed at the rear of the nacelle cover body (1), and the rear spoiler (6) is installed on the rear top cover. The air inlet channel (2) is installed at the lower part of the front top cover of the nacelle cover; the air outlet channel (4) is connected with the rear spoiler (6) of the nacelle cover, and the built-in fan of the rear spoiler (6) performs forced exhaust. wind; the louvers (5) carry out natural suction; the airflow inlet channel (2), the four-stage airflow guide plate (3) and the airflow outlet channel (4) all adopt soft connections. The utility model uses the fan built in the rear baffle to carry out forced air suction, and through the airflow guide plate and airflow channel set inside the nacelle cover, the airflow in the nacelle cover is circulated with the outside according to the design flow direction shown in the diagram, and the airflow in the cabin is taken away. heat.

Figure 200920246026

Description

内部带有气流导板及气流通道的大型风力发电机组机舱罩 Large-scale wind turbine nacelle cover with airflow guide plate and airflow channel inside

技术领域technical field

本实用新型涉及一种大型风力发电机组的机舱罩,尤其是功率在2MW以上风力发电机组的机舱罩。属风力发电机技术领域。 The utility model relates to a nacelle cover of a large-scale wind power generating set, in particular to a nacelle cover of a wind power generating set with power above 2MW. It belongs to the technical field of wind power generators. the

背景技术Background technique

大型风力发电机组内部的轴承转动、刹车系统、齿轮箱、发电机及变流柜的正常工作均会产生较高的温升,且目前的机舱罩本体各部件连接紧密,密封性较好。为了将机舱罩内部热量排出机舱,以往的兆瓦级风力发电机组,一种只在机舱罩顶部或底部设置通风口,此种方式受到实时风速的影响,且机舱罩内部空气流向不固定,散热效果很差;一种虽在机舱顶部和底部设了通风口和排风口,但由于内部没有设置合理的气流通道,机舱罩内气流只是进行了局部交换,散热效果也不甚理想。 The normal operation of the bearing rotation, braking system, gearbox, generator and converter cabinet inside the large-scale wind turbine will generate a high temperature rise, and the current nacelle cover body is tightly connected and sealed. In order to discharge the heat inside the nacelle cover, the previous megawatt-level wind turbines only provided vents on the top or bottom of the nacelle cover. This method is affected by the real-time wind speed, and the air flow inside the nacelle cover is not fixed. The effect is very poor; one type has vents and exhaust outlets at the top and bottom of the cabin, but because there is no reasonable airflow channel inside, the airflow in the cabin cover is only partially exchanged, and the heat dissipation effect is not ideal. the

实用新型内容Utility model content

本实用新型目的在于,提供一种能使机舱罩内部空气按照设计流向进行规则流动,并通过气流导板、气流通道等结构将机舱罩内的热空气排出舱外,达到理想温降效果的大型风力发电机组机舱罩。 The purpose of the utility model is to provide a large-scale wind power system that can make the air inside the nacelle cover flow regularly according to the design flow direction, and discharge the hot air in the nacelle cover out of the cabin through the airflow guide plate, airflow channel and other structures to achieve the ideal temperature drop effect. Generator set nacelle cover. the

本实用新型的目的是这样实现的:内部带有气流导板及气流通道的大型风力发电机组机舱罩,包括机舱罩本体,所述机舱罩本体尾部安装有百叶窗,机舱罩顶部安装气流导板、气流入口通道及气流出口通道,尾部的后阻流板内设置有风扇。其特征在于,所述气流导板、气流入口通道及气流出口通道紧贴于前顶罩和后顶罩安装;气流导板与气流入口通道、气流出口通道间进行软连接;气流入口通道设有导风口;气流出口通道与后阻流板连接;所述气流入口通道、气流导板及气流出口通道在机舱罩内部形成一段风道。The purpose of this utility model is achieved in that the large-scale wind turbine nacelle cover with airflow guide plate and airflow channel inside includes a nacelle cover body, a shutter is installed at the tail of the nacelle cover body, an airflow guide plate and an airflow inlet are installed on the top of the nacelle cover channel and air outlet channel, and a fan is arranged in the rear spoiler at the tail. It is characterized in that the airflow guide plate, the airflow inlet channel and the airflow outlet channel are installed close to the front top cover and the rear top cover; the airflow guide plate is softly connected with the airflow inlet channel and the airflow outlet channel; the airflow inlet channel is provided with an air guide port The air outlet channel is connected with the rear spoiler; the air inlet channel, the air guide plate and the air outlet channel form a section of air duct inside the nacelle cover.

其工作原理是,由内置在后阻流板内的风扇进行强制吸风,通过机舱罩内部设置的气流导板及气流通道,使机舱罩内的气流按图示设计流向与外界进行循环,带走舱内热量。而设置在机舱罩尾部的百叶窗将外界新鲜空气补充进机舱罩内,以起到换风散热的效果。 Its working principle is that the fan built in the rear spoiler performs forced air suction, and through the airflow guide plate and airflow channel set inside the nacelle hood, the airflow in the nacelle hood circulates with the outside according to the flow direction shown in the diagram, and takes away Cabin heat. The louvers arranged at the tail of the nacelle cover will supplement the fresh air from the outside into the nacelle cover to achieve the effect of exchanging wind and dissipating heat. the

由于利用上述技术方案,本实用新型机舱罩散热效果甚佳。 Owing to utilizing above-mentioned technical scheme, the utility model nacelle cover heat dissipation effect is very good. the

附图说明Description of drawings

图1为本实用新型机舱罩结构图; Fig. 1 is the structural diagram of the utility model nacelle cover;

图2为本实用新型气流入口通道结构图; Fig. 2 is the structural diagram of the air inlet channel of the utility model;

图3为本实用新型气流导板结构图; Fig. 3 is the structural diagram of the air flow guide plate of the present utility model;

图4为本实用新型气流出口通道结构图。 Fig. 4 is a structural diagram of the air outlet channel of the utility model. the

附图符号说明 Description of reference symbols

机舱罩本体1、气流入口通道2、导风口7、气流导板3、气流出口通道4、百叶窗5、后阻流板6。 The nacelle cover body 1, the air inlet channel 2, the air guide port 7, the air guide plate 3, the air outlet channel 4, the louver 5, and the rear spoiler 6. the

具体实施方式Detailed ways

以下参照附图对本实用新型进行说明。 The utility model is described below with reference to accompanying drawing. the

图1是本实用新型机舱罩结构图,如图1所示,本实用新型涉及的内部带有气流导板及气流通道的大型风力发电机组机舱罩,包括机舱罩本体1;安装在所述机舱罩本体1尾部的百叶窗5;安装在机舱罩本体1前顶罩下部的气流入口通道2;用软连接连接在气流入口通道2上的气流导板3;安装在机舱罩本体1后顶罩下部、用软连接连接在气流导板3上的气流出口通道4;连接在气流出口通道4上的后阻流板6。连接气流入口通道2、气流导板3、气流出口通道4,在机舱罩上部形成了一个从前至后的气流通道。 Fig. 1 is the structural diagram of the nacelle cover of the present utility model, as shown in Fig. 1, the large-scale wind turbine nacelle cover that the interior of the utility model relates to has the airflow guide plate and the air flow channel, comprises the nacelle cover body 1; The louvers 5 at the rear of the body 1; the air inlet channel 2 installed on the lower part of the front top cover of the nacelle body 1; the air flow guide plate 3 connected to the air inlet channel 2 with a soft connection; The flexible connection is connected to the airflow outlet channel 4 on the airflow guide plate 3 ; the rear spoiler 6 connected to the airflow outlet channel 4 . Connecting the airflow inlet channel 2, the airflow guide plate 3, and the airflow outlet channel 4, a front-to-back airflow channel is formed on the upper part of the nacelle cover. the

由内置在后阻流板6内的风扇进行强制吸风,通过机舱罩内部设置的气流入口通道2、气流导板3、气流出口通道4形成的气流通道,机舱罩内的气流按图示设计流向与外界,带走舱内热量。而设置在机 舱罩尾部的百叶窗5将外界新鲜空气补充进机舱罩内,以起到换风散热的效果。 The fan built in the rear spoiler 6 is used for forced air suction, and through the airflow channel formed by the airflow inlet channel 2, the airflow guide plate 3 and the airflow outlet channel 4 inside the nacelle cover, the airflow in the nacelle cover is designed according to the diagram With the outside world, take away the cabin heat. And the louver 5 that is arranged on the nacelle cover afterbody supplements the fresh air from the outside into the nacelle cover, to play the effect of changing air and radiating heat. the

图2是本实用新型气流入口通道结构图,如图2所示,所述气流入口通道上设有导风口7。机舱内的热气流通过所述导风口7导入到气流入口通道2。 Fig. 2 is a structural diagram of the air inlet passage of the utility model, as shown in Fig. 2, the air inlet passage is provided with an air guide port 7. The hot air in the cabin is introduced into the air inlet channel 2 through the air guide opening 7 . the

图3是本实用新型气流导板结构图,如图3所示,气流导向板3为四段结构,从气流入口通道2进入的热气流通过气流导向板3流入气流出口通道4。 Fig. 3 is a structure diagram of the airflow guide plate of the present utility model, as shown in Fig. 3, the airflow guide plate 3 is a four-section structure, and the hot air entering from the airflow inlet channel 2 flows into the airflow outlet channel 4 through the airflow guide plate 3. the

图4是本实用新型气流出口通道结构图,如图4所示,气流出口通道4通过法兰与后阻流板6连接,机舱内的热气流通过所述导风口7导入到气流入口通道2后,通过气流导向板3与气流出口通道4向外排出。 Fig. 4 is a structure diagram of the air outlet channel of the utility model, as shown in Fig. 4, the air outlet channel 4 is connected with the rear spoiler 6 through the flange, and the hot air in the cabin is introduced into the air inlet channel 2 through the air guide port 7 After that, it is discharged outward through the airflow guide plate 3 and the airflow outlet channel 4. the

Claims (5)

1. an inside has the Large-scale Wind Turbines engine room cover of air-flow guide plate and air-flow path, it is characterized in that this structure comprises: engine room cover body, air-flow guide plate, air-flow path and venetian blind;
Described air-flow guide plate and air-flow path are installed on engine room cover inside, and are close to preceding overhead guard and back overhead guard.
2. inside as claimed in claim 1 has the Large-scale Wind Turbines engine room cover of air-flow guide plate and air-flow path, it is characterized in that, the air flow inlet passage communicates with engine room cover inside and is provided with air guide hole, and the flow outlet passage communicates with the back spoiler.
3. inside as claimed in claim 1 has the Large-scale Wind Turbines engine room cover of air-flow guide plate and air-flow path, it is characterized in that, uses between air-flow guide plate and air-flow path to be flexible coupling.
4. inside as claimed in claim 1 has the Large-scale Wind Turbines engine room cover of air-flow guide plate and air-flow path, it is characterized in that, at the engine room cover afterbody venetian blind is installed.
5. inside as claimed in claim 1 has the Large-scale Wind Turbines engine room cover of air-flow guide plate and air-flow path, it is characterized in that built-in fans in the spoiler of back.
CN2009202460269U 2009-09-25 2009-09-25 Large wind turbine nacelle cover with airflow guides and airflow channels inside Expired - Fee Related CN201687662U (en)

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CN201687662U true CN201687662U (en) 2010-12-29

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108661866A (en) * 2018-03-30 2018-10-16 北京金风科创风电设备有限公司 Wind generating set
CN112412715A (en) * 2020-12-09 2021-02-26 北京三力新能科技有限公司 Wind generating set cooling mode capable of effectively utilizing natural wind

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108661866A (en) * 2018-03-30 2018-10-16 北京金风科创风电设备有限公司 Wind generating set
CN108661866B (en) * 2018-03-30 2020-01-31 北京金风科创风电设备有限公司 Wind Turbine
CN112412715A (en) * 2020-12-09 2021-02-26 北京三力新能科技有限公司 Wind generating set cooling mode capable of effectively utilizing natural wind

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20101229

Termination date: 20150925

EXPY Termination of patent right or utility model