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CN108725752A - A kind of efficient electrically controlled latch gear - Google Patents

A kind of efficient electrically controlled latch gear Download PDF

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Publication number
CN108725752A
CN108725752A CN201810671006.XA CN201810671006A CN108725752A CN 108725752 A CN108725752 A CN 108725752A CN 201810671006 A CN201810671006 A CN 201810671006A CN 108725752 A CN108725752 A CN 108725752A
Authority
CN
China
Prior art keywords
circuit board
pin shaft
coil
coil assembly
interface
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201810671006.XA
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Chinese (zh)
Inventor
陈永红
贺新华
杨志伏
罗天
茹毅
韦泽波
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Guizhou Aerospace Control Technology Co Ltd
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Guizhou Aerospace Control Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by Guizhou Aerospace Control Technology Co Ltd filed Critical Guizhou Aerospace Control Technology Co Ltd
Priority to CN201810671006.XA priority Critical patent/CN108725752A/en
Publication of CN108725752A publication Critical patent/CN108725752A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lock And Its Accessories (AREA)

Abstract

本发明公开了一种高效电控锁销装置,包括外壳(2);外壳(2)上设有线圈组件供电接口(1)和电路板接口(7);外壳(2)内设有导磁架(3)和电路板(4);导磁架(3)上设有线圈组件(9);线圈组件(9)与线圈供电接口(1)电气连接;线圈组件(9)内设有销轴(5),销轴(5)一端设有双极性磁钢组件(6),销轴(5)另一端伸出外壳(2);电路板(4)上设有霍尔传感器(10),电路板(4)与电路板接口(7)电气连接。本发明锁定和解锁效率高、锁定力矩大、体积小,结构简单。本发明采用霍尔开关器件输出电压的高低来判断锁销的状态,具有较强的通用性。The invention discloses a high-efficiency electronically controlled locking device, which comprises a casing (2); the casing (2) is provided with a coil component power supply interface (1) and a circuit board interface (7); the casing (2) is provided with a magnetically conductive frame (3) and circuit board (4); the coil assembly (9) is provided on the magnetic frame (3); the coil assembly (9) is electrically connected to the coil power supply interface (1); the coil assembly (9) is provided with a pin shaft (5), one end of the pin shaft (5) is provided with a bipolar magnetic steel assembly (6), and the other end of the pin shaft (5) extends out of the shell (2); the circuit board (4) is provided with a Hall sensor (10 ), the circuit board (4) is electrically connected with the circuit board interface (7). The invention has high locking and unlocking efficiency, large locking torque, small volume and simple structure. The present invention uses the level of the output voltage of the Hall switch device to judge the state of the lock pin, and has strong versatility.

Description

一种高效电控锁销装置A high-efficiency electronically controlled locking device

技术领域technical field

本发明涉及一种高效电控锁销装置,属于伺服控制技术领域。The invention relates to a high-efficiency electronically controlled locking device, which belongs to the technical field of servo control.

背景技术Background technique

对于正常式布局的飞行器系统,舵机位于飞行器的尾部,由于飞行器舵面受外部铰链力矩的影响,在飞行过程中一般都不能稳定在零位,而会随着载机的机动在空中偏摆,从而会影响舵机的关键部件及传感器的使用寿命,同时,舵面不在零位时若飞行器应急发射会导致严重的发射安全,所以一般均需要将舵面锁定在零位,正常发射时再将舵面解锁,而且舵面锁定与解锁的可靠性决定了整机系统的飞行可靠性。For an aircraft system with a normal layout, the steering gear is located at the tail of the aircraft. Because the aircraft's rudder surface is affected by the external hinge moment, it generally cannot be stabilized at zero position during flight, but will deflect in the air with the maneuvering of the carrier aircraft. , which will affect the service life of the key components and sensors of the steering gear. At the same time, if the aircraft is launched in an emergency when the rudder surface is not at zero position, it will cause serious launch safety. Unlock the rudder surface, and the reliability of the rudder surface locking and unlocking determines the flight reliability of the whole aircraft system.

目前的舵面锁定模式有锁定电机轴的电磁制动器、电磁制锁机构、气动制锁机构和舵面剪切销机构等,最可靠的为不可逆向的气动制锁机构或剪切模式,但气动制锁机构或剪切模式在部分飞行器中使用受限,不适用于需要高可靠的飞行器舵系统。The current rudder surface locking modes include electromagnetic brakes for locking the motor shaft, electromagnetic locking mechanisms, pneumatic locking mechanisms and rudder surface shear pin mechanisms, etc. The most reliable is the irreversible pneumatic locking mechanism or shearing mode, but the pneumatic locking mechanism The locking mechanism or shear mode has limited use in some aircraft, and is not suitable for aircraft rudder systems that require high reliability.

发明内容Contents of the invention

本发明的目的在于针对飞行器舵系统提供一种锁定和解锁效率高、锁定力矩大,可靠性高的高效电控锁销装置,以满足飞行器舵系统对锁销装置的要求,从而克服现有技术的不足。The purpose of the present invention is to provide a kind of high-efficiency locking and unlocking efficiency, large locking torque, high reliability electronically controlled locking device for the aircraft rudder system, so as to meet the requirements of the aircraft rudder system for the locking device, thereby overcoming the prior art lack of.

为实现上述目的,本发明采用如下技术方案:To achieve the above object, the present invention adopts the following technical solutions:

本发明的一种高效电控锁销装置,包括外壳;外壳上设有线圈组件供电接口和电路板接口;外壳内设有导磁架和电路板;导磁架上设有线圈组件;线圈组件与线圈供电接口电气连接;线圈组件内设有销轴,销轴一端设有双极性磁钢组件,销轴另一端伸出外壳;电路板上设有霍尔传感器,电路板与电路板接口电气连接。A high-efficiency electronically controlled locking device of the present invention comprises a casing; the casing is provided with a coil assembly power supply interface and a circuit board interface; a magnetic frame and a circuit board are arranged inside the casing; a coil assembly is provided on the magnetic frame; Electrically connected with the coil power supply interface; there is a pin shaft in the coil assembly, a bipolar magnetic steel assembly is provided at one end of the pin shaft, and the other end of the pin shaft protrudes from the shell; a Hall sensor is provided on the circuit board, and the interface between the circuit board and the circuit board Electrical connections.

前述高效电控锁销装置中,所述电路板上的霍尔传感器位于双极性磁钢组件附近;霍尔传感器采用霍尔开关集成电路。In the aforementioned high-efficiency electronically controlled locking device, the Hall sensor on the circuit board is located near the bipolar magnetic steel assembly; the Hall sensor adopts a Hall switch integrated circuit.

前述高效电控锁销装置中,所述电路板上的信号输出端Uout与接地端GND之间设有RC滤波电路。In the aforementioned high-efficiency electronically controlled locking device, an RC filter circuit is provided between the signal output terminal Uout and the ground terminal GND on the circuit board.

前述高效电控锁销装置中,所述销轴位于线圈组件的中心孔内,并与线圈组件的中心孔滑动连接;销轴与线圈组件的衔铁连接。In the aforementioned high-efficiency electronically controlled locking device, the pin shaft is located in the central hole of the coil assembly and is slidingly connected with the central hole of the coil assembly; the pin shaft is connected with the armature of the coil assembly.

由于采用了上述技术方案,本发明与现有技术相比,本发明锁定和解锁效率高、锁定力矩大、体积小,结构简单。本发明采用霍尔开关器件输出电压的高低来判断锁销的状态,具有较强的通用性。Due to the adoption of the above technical solution, compared with the prior art, the present invention has high locking and unlocking efficiency, large locking torque, small volume and simple structure. The present invention uses the level of the output voltage of the Hall switch device to judge the state of the lock pin, and has strong versatility.

附图说明Description of drawings

图1是本发明的结构示意图。Fig. 1 is a schematic structural view of the present invention.

图中标记如下: 1-线圈组件供电接口、2-壳体、3-导磁架、4-电路板、5-销轴、6-双极性磁钢组件、7-霍尔传感器接口、8-RC滤波电路、9-线圈组件、10-霍尔传感器、11-弹簧。The marks in the figure are as follows: 1-coil assembly power supply interface, 2-housing, 3-magnetic frame, 4-circuit board, 5-pin shaft, 6-bipolar magnetic steel assembly, 7-Hall sensor interface, 8 -RC filter circuit, 9-coil assembly, 10-Hall sensor, 11-spring.

具体实施方式Detailed ways

下面结合附图和实施例对本发明作进一步的详细说明。The present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

本发明的一种高效电控锁销装置,如图1所示:包括外壳2;外壳2上设有线圈组件供电接口1和电路板接口7;外壳2内设有导磁架3和电路板4;导磁架3上设有线圈组件9;线圈组件9与线圈供电接口1电气连接;线圈组件9内设有销轴5,销轴5一端设有双极性磁钢组件6,销轴5另一端伸出外壳2;电路板4上设有霍尔传感器10,电路板4与电路板接口7电气连接。电路板4上的霍尔传感器10位于双极性磁钢组件6附近;霍尔传感器10采用霍尔开关集成电路。电路板4上的信号输出端Uout与接地端GND之间设有RC滤波电路8。销轴5位于线圈组件9的中心孔内,并与线圈组件9的中心孔滑动连接;销轴5与线圈组件9的衔铁连接。A high-efficiency electronically controlled locking device of the present invention, as shown in Figure 1: includes a casing 2; the casing 2 is provided with a coil assembly power supply interface 1 and a circuit board interface 7; the casing 2 is provided with a magnetic frame 3 and a circuit board 4. The magnetic frame 3 is provided with a coil assembly 9; the coil assembly 9 is electrically connected to the coil power supply interface 1; the coil assembly 9 is provided with a pin shaft 5, and one end of the pin shaft 5 is provided with a bipolar magnetic steel assembly 6, and the pin shaft 5 The other end protrudes from the shell 2; the Hall sensor 10 is provided on the circuit board 4, and the circuit board 4 is electrically connected to the circuit board interface 7. The Hall sensor 10 on the circuit board 4 is located near the bipolar magnetic steel assembly 6; the Hall sensor 10 adopts a Hall switch integrated circuit. An RC filter circuit 8 is provided between the signal output terminal Uout on the circuit board 4 and the ground terminal GND. The pin shaft 5 is located in the central hole of the coil assembly 9 and is slidably connected with the central hole of the coil assembly 9 ; the pin shaft 5 is connected with the armature of the coil assembly 9 .

实施例Example

本例的高效电控锁销装置,用于伺服系统的锁定与解锁。本例包括一个线圈组件,销轴置于线圈中央,销轴上安装一个双极性磁钢,通过霍尔传感器及处理电路检测解锁信号。The high-efficiency electronically controlled locking device of this example is used for locking and unlocking of the servo system. This example includes a coil assembly, the pin shaft is placed in the center of the coil, a bipolar magnet is installed on the pin shaft, and the unlocking signal is detected by the Hall sensor and the processing circuit.

具体如图1所示,由线圈组件供电接口1、壳体2、导磁架3、电路板4、销轴5、双极性磁钢组件6、电路板接口7、RC滤波电路8、线圈组件9、霍尔传感器10和弹簧11组成。Specifically as shown in Figure 1, the power supply interface 1 of the coil assembly, the shell 2, the magnetic frame 3, the circuit board 4, the pin shaft 5, the bipolar magnetic steel assembly 6, the circuit board interface 7, the RC filter circuit 8, the coil Assembly 9, Hall sensor 10 and spring 11.

销轴5为活动销轴,霍尔传感器10使用霍尔开关集成电路作为位置检测元器件安装在电路板4上,双极性磁钢组件6安装在销轴5上。当线圈组件9通过线圈组件供电接口1接通电源时,线圈组件9磁化衔铁,被磁化的衔铁和导磁架3产生较大电磁吸合力带动销轴5运动,销轴5带动双极性磁钢组件6移动,使双极性磁钢组件6覆盖或脱离霍尔传感器10,实现锁销5吸合或锁定,同时霍尔传感器10输出反馈信号。本发明具有结构简单的特点。采用霍尔开关器件输出电压的高低来判断锁销的状态,具有较强的通用性。The pin shaft 5 is a movable pin shaft, and the Hall sensor 10 is installed on the circuit board 4 using a Hall switch integrated circuit as a position detection component, and the bipolar magnetic steel assembly 6 is installed on the pin shaft 5 . When the coil assembly 9 is powered on through the coil assembly power supply interface 1, the coil assembly 9 magnetizes the armature, and the magnetized armature and the magnetic frame 3 generate a large electromagnetic attraction force to drive the pin shaft 5 to move, and the pin shaft 5 drives the bipolar magnet. The steel component 6 moves, so that the bipolar magnetic steel component 6 covers or separates from the Hall sensor 10, and the locking pin 5 is attracted or locked, and the Hall sensor 10 outputs a feedback signal at the same time. The invention has the characteristics of simple structure. The state of the lock pin is judged by using the output voltage of the Hall switch device, which has strong versatility.

本发明的工作过程及原理Working process and principle of the present invention

本发明的装置通过销轴5的伸缩干涉固定于电机轴上的凸台锁制盘,进行锁定和开锁。断电时销轴5在弹簧11作用下伸出,插到两个凸台之间,阻止电机转动;而通电时销轴5收回,与凸台互不干涉,电机可以自由转动。当线圈组件9不通电时,弹簧11处于放松状态,弹簧11产生的轴向压力将推动衔铁向弹簧11伸长的方向移动,与衔铁连接的销轴5与制动盘上的槽对位准确的情况下,销轴5会对应落入相应的槽内,此时若转动电机轴,由于制动盘固定在电机轴上,并且销轴5卡在制动盘内,因此电机轴能转动的角度范围只是制动盘槽所限制的范围。通过销轴5限位的方式,电磁锁制器能将电机轴及舵面锁定在允许零位误差范围内,实现该电磁锁制器的锁定功能。The device of the present invention performs locking and unlocking by the expansion and contraction of the pin shaft 5 interfering with the boss locking disc fixed on the motor shaft. When the power is off, the pin shaft 5 stretches out under the action of the spring 11, and is inserted between the two bosses to prevent the motor from rotating; when the power is turned on, the pin shaft 5 retracts without interfering with the bosses, and the motor can rotate freely. When the coil assembly 9 is not energized, the spring 11 is in a relaxed state, and the axial pressure generated by the spring 11 will push the armature to move in the direction of spring 11 elongation, and the pin shaft 5 connected with the armature is aligned with the slot on the brake disc accurately In the case of , the pin shaft 5 will fall into the corresponding groove. If the motor shaft is rotated at this time, since the brake disc is fixed on the motor shaft and the pin shaft 5 is stuck in the brake disc, the motor shaft can rotate The angular range is only limited by the disc slots. The electromagnetic lock can lock the motor shaft and the rudder surface within the allowable zero error range by means of the pin shaft 5 to realize the locking function of the electromagnetic lock.

Claims (4)

1. a kind of efficient electrically controlled latch gear, including shell(2);It is characterized in that:Shell(2)Coil block power supply is equipped with to connect Mouthful(1)And circuit board interface(7);Shell(2)It is interior to be equipped with magnetic guiding frame(3)And circuit board(4);Magnetic guiding frame(3)It is equipped with coil group Part(9);Coil block(9)With coil power supply interface(1)Electrical connection;Coil block(9)It is interior to be equipped with axis pin(5), axis pin(5)One End is equipped with bipolarity magnetic steel component(6), axis pin(5)The other end stretches out shell(2);Circuit board(4)It is equipped with Hall sensor (10), circuit board(4)With circuit board interface(7)Electrical connection.
2. efficient electrically controlled latch gear according to claim 1, it is characterised in that:The circuit board(4)On hall sensing Device(10)Positioned at bipolarity magnetic steel component(6)Near;Hall sensor(10)Using hall ic.
3. efficient electrically controlled latch gear according to claim 1, it is characterised in that:The circuit board(4)On signal output It is equipped with RC filter circuits between the Uout and ground terminal GND of end(8).
4. efficient electrically controlled latch gear according to claim 1, it is characterised in that:The axis pin(5)Positioned at coil block(9) Centre bore in, and and coil block(9)Centre bore be slidably connected;Axis pin(5)With coil block(9)Armature connection.
CN201810671006.XA 2018-06-26 2018-06-26 A kind of efficient electrically controlled latch gear Pending CN108725752A (en)

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Application Number Priority Date Filing Date Title
CN201810671006.XA CN108725752A (en) 2018-06-26 2018-06-26 A kind of efficient electrically controlled latch gear

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Application Number Priority Date Filing Date Title
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110017882A (en) * 2019-05-16 2019-07-16 武昌理工学院 A protection box for a large-depth underwater surveying and mapping device
CN111940819A (en) * 2020-08-07 2020-11-17 国网江苏省电力有限公司常州供电分公司 Universal interface convenient for replacing and locking
CN112173070A (en) * 2020-09-25 2021-01-05 兰州万里航空机电有限责任公司 Electric control surface lock mechanism
CN112537446A (en) * 2021-01-29 2021-03-23 绵阳空天科技有限公司 Locking device of rotor propeller of vertical take-off and landing fixed wing unmanned aerial vehicle

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102068822A (en) * 2010-12-31 2011-05-25 西安航天精密机电研究所 Self-locking electric steering engine
JP2012073135A (en) * 2010-09-29 2012-04-12 Nabtesco Corp Position detector for actuator
CN105270607A (en) * 2015-11-09 2016-01-27 湖北航天技术研究院总体设计所 Helm system locking device
CN106128820A (en) * 2016-07-04 2016-11-16 贵州航天控制技术有限公司 A kind of non-contact type Hall electromagnetic position detection device
CN208470098U (en) * 2018-06-26 2019-02-05 贵州航天控制技术有限公司 A kind of efficient electrically controlled latch gear

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012073135A (en) * 2010-09-29 2012-04-12 Nabtesco Corp Position detector for actuator
CN102068822A (en) * 2010-12-31 2011-05-25 西安航天精密机电研究所 Self-locking electric steering engine
CN105270607A (en) * 2015-11-09 2016-01-27 湖北航天技术研究院总体设计所 Helm system locking device
CN106128820A (en) * 2016-07-04 2016-11-16 贵州航天控制技术有限公司 A kind of non-contact type Hall electromagnetic position detection device
CN208470098U (en) * 2018-06-26 2019-02-05 贵州航天控制技术有限公司 A kind of efficient electrically controlled latch gear

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110017882A (en) * 2019-05-16 2019-07-16 武昌理工学院 A protection box for a large-depth underwater surveying and mapping device
CN110017882B (en) * 2019-05-16 2020-12-08 武昌理工学院 A protection box for a large-depth underwater surveying and mapping device
CN111940819A (en) * 2020-08-07 2020-11-17 国网江苏省电力有限公司常州供电分公司 Universal interface convenient for replacing and locking
CN111940819B (en) * 2020-08-07 2021-07-13 国网江苏省电力有限公司常州供电分公司 Universal interface for easy replacement of locking
CN112173070A (en) * 2020-09-25 2021-01-05 兰州万里航空机电有限责任公司 Electric control surface lock mechanism
CN112173070B (en) * 2020-09-25 2022-02-08 兰州万里航空机电有限责任公司 Electric control surface lock mechanism
CN112537446A (en) * 2021-01-29 2021-03-23 绵阳空天科技有限公司 Locking device of rotor propeller of vertical take-off and landing fixed wing unmanned aerial vehicle

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