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
coil block
axis pin
shell
electrically controlled
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
Other languages
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
Original Assignee
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.)
Filing date
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

Landscapes

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

Abstract

The invention discloses a kind of efficient electrically controlled latch gears, including shell(2);Shell(2)It is equipped with coil block power supply interface(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 block(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.The present invention lock and unlock it is efficient, locking torque it is big, small, it is simple in structure.The present invention judges the state of lock pin using the height of Hall switch device output voltage, has stronger versatility.

Description

A kind of efficient electrically controlled latch gear
Technical field
The present invention relates to a kind of efficient electrically controlled latch gears, belong to technical field of servo control.
Background technology
For the aerocraft system of normal configuration, steering engine is located at the tail portion of aircraft, since vehicle rudder is by outside The influence of hinge moment generally cannot all stablize in zero-bit in flight course, and can with the motor-driven beat in the air of carrier aircraft, So that the critical component of steering engine and the service life of sensor can be influenced, meanwhile, if rudder face not in zero-bit the emergent hair of aircraft Serious emission security can be led to by penetrating, so general be required to rudder face being locked in zero-bit, when normal transmission again unlocks rudder face, And rudder face locking determines the flight reliability of machine system with the reliability of unlock.
Current rudder face locking mode has the electromagnetic brake of lock out motor axis, electromagnetic system latch mechanism, pneumatic lockmaking mechanism Shear pin mechanism etc. with rudder face, it is most reliable for can not be reverse pneumatic lockmaking mechanism or shear mode, but pneumatic lockmaking mechanism Or shear mode is used in the aircraft of part and is limited, and is not suitable for needing highly reliable aircraft rudder system.
Invention content
It is an object of the invention to be directed to aircraft rudder system provide it is a kind of locking and unlock it is efficient, locking torque it is big, The high efficient electrically controlled latch gear of reliability, to meet requirement of the aircraft rudder system to latch gear, to overcome existing skill The deficiency of art.
To achieve the above object, the present invention adopts the following technical scheme that:
A kind of efficient electrically controlled latch gear of the present invention, including shell;Shell is equipped with coil block power supply interface and circuit board Interface;Magnetic guiding frame and circuit board are equipped in shell;Magnetic guiding frame is equipped with coil block;Coil block and coil power supply Interface Electrical Connection;Axis pin is equipped in coil block, axis pin one end is equipped with bipolarity magnetic steel component, and the axis pin other end stretches out shell;Circuit board It is equipped with Hall sensor, circuit board is electrically connected with circuit board interface.
In aforementioned efficient electrically controlled latch gear, it is attached that the Hall sensor on the circuit board is located at bipolarity magnetic steel component Closely;Hall sensor uses hall ic.
In aforementioned efficient electrically controlled latch gear, set between the signal output end Uout on the circuit board and ground terminal GND There are RC filter circuits.
In aforementioned efficient electrically controlled latch gear, the axis pin is located in the centre bore of coil block, and with coil block Centre bore is slidably connected;The armature of axis pin and coil block connects.
By adopting the above-described technical solution, compared with prior art, the present invention the present invention locks and unlocks efficient, lock It is big, small to determine torque, it is simple in structure.The present invention judges the shape of lock pin using the height of Hall switch device output voltage State has stronger versatility.
Description of the drawings
Fig. 1 is the structural schematic diagram of the present invention.
It is marked in figure as follows:1- coil blocks power supply interface, 2- shells, 3- magnetic guiding frames, 4- circuit boards, 5- axis pins, 6- are bis- Polarity magnetic steel component, 7- Hall sensors interface, 8-RC filter circuits, 9- coil blocks, 10- Hall sensors, 11- springs.
Specific implementation mode
The present invention is described in further detail with reference to the accompanying drawings and examples.
A kind of efficient electrically controlled latch gear of the present invention, as shown in Figure 1:Including shell 2;Shell 2 is equipped with coil block Power supply interface 1 and circuit board interface 7;Magnetic guiding frame 3 and circuit board 4 are equipped in shell 2;Magnetic guiding frame 3 is equipped with coil block 9;Line Coil assembly 9 is electrically connected with coil power supply interface 1;Axis pin 5 is equipped in coil block 9,5 one end of axis pin is equipped with bipolarity magnet steel group Part 6,5 other end of axis pin stretch out shell 2;Circuit board 4 is equipped with Hall sensor 10, and circuit board 4 electrically connects with circuit board interface 7 It connects.Hall sensor 10 on circuit board 4 is located near bipolarity magnetic steel component 6;Hall sensor 10 uses Hall switch collection At circuit.RC filter circuits 8 are equipped between signal output end Uout on circuit board 4 and ground terminal GND.Axis pin 5 is located at coil In the centre bore of component 9, and it is slidably connected with the centre bore of coil block 9;Axis pin 5 is connect with the armature of coil block 9.
Embodiment
The efficient electrically controlled latch gear of this example is used for the locking and unlock of servo-drive system.This example includes a coil block, Axis pin is placed in coil center, and a bipolarity magnet steel is installed on axis pin, passes through Hall sensor and processing circuit detection unlock letter Number.
Specifically as shown in Figure 1, by coil block power supply interface 1, shell 2, magnetic guiding frame 3, circuit board 4, axis pin 5, bipolarity Magnetic steel component 6, circuit board interface 7, RC filter circuits 8, coil block 9, Hall sensor 10 and spring 11 form.
Axis pin 5 is active pin shaft, and Hall sensor 10 uses hall ic to pacify as position detection component On the circuit board 4, bipolarity magnetic steel component 6 is mounted on axis pin 5 dress.When coil block 9 is connect by coil block power supply interface 1 When energization source, coil block 9 magnetizes armature, and the armature being magnetized and magnetic guiding frame 3 generate larger electromagnetism the suction-combining force and axis pin 5 driven to transport Dynamic, axis pin 5 drives bipolarity magnetic steel component 6 to move, and so that bipolarity magnetic steel component 6 is covered or be detached from Hall sensor 10, realizes Lock pin 5 is attracted or locking, while Hall sensor 10 exports feedback signal.The present invention has the characteristics that simple in structure.Using suddenly The height of your switching device output voltage judges the state of lock pin, has a stronger versatility.
The course of work and principle of the present invention
The device of the invention is fixed on the boss locking disk on motor shaft by the flexible interference of axis pin 5, is locked and is unlocked. Axis pin 5 stretches out under the effect of spring 11 when power-off, is inserted between two boss, and motor is prevented to rotate;And axis pin 5 is received when being powered It returns, non-interference with boss, motor can be freely rotated.When 9 no power of coil block, spring 11 is in relaxation state, bullet The axial compressive force that spring 11 generates moves the direction for pushing armature to be extended to spring 11, the axis pin 5 and brake disc being connect with armature On slot contraposition accurately in the case of, axis pin 5, which can correspond to, to be fallen into corresponding slot, if rotary electric machine axis at this time, due to brake disc It is fixed on motor shaft, and axis pin 5 is stuck in brake disc, therefore the angular range that motor shaft can rotate only brakes dish groove institute The range of limitation.In such a way that axis pin 5 limits, motor shaft and rudder face can be locked in by electromagnetism locking device allows error of zero model In enclosing, the lock function of the electromagnetism locking device is realized.

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)

Priority Applications (1)

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

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
CN108725752A true CN108725752A (en) 2018-11-02

Family

ID=63930909

Family Applications (1)

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

Country Status (1)

Country Link
CN (1) CN108725752A (en)

Cited By (3)

* 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 kind of big depth underwater plotting board guard box
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

Cited By (6)

* 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 kind of big depth underwater plotting board guard box
CN110017882B (en) * 2019-05-16 2020-12-08 武昌理工学院 Big degree of depth underwater surveying and mapping device guard box
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 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
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

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