CN108146619A - A kind of control draw ring for the holder function that rises and falls with emergency extension - Google Patents

A kind of control draw ring for the holder function that rises and falls with emergency extension Download PDF

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Publication number
CN108146619A
CN108146619A CN201611097530.8A CN201611097530A CN108146619A CN 108146619 A CN108146619 A CN 108146619A CN 201611097530 A CN201611097530 A CN 201611097530A CN 108146619 A CN108146619 A CN 108146619A
Authority
CN
China
Prior art keywords
draw ring
bar assembly
protection cap
ring bar
spring
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.)
Granted
Application number
CN201611097530.8A
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Chinese (zh)
Other versions
CN108146619B (en
Inventor
程起兴
梅宇飞
傅劲翔
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.)
Shanghai Aviation Electric Co Ltd
Original Assignee
Shanghai Aviation Electric 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 Shanghai Aviation Electric Co Ltd filed Critical Shanghai Aviation Electric Co Ltd
Priority to CN201611097530.8A priority Critical patent/CN108146619B/en
Publication of CN108146619A publication Critical patent/CN108146619A/en
Application granted granted Critical
Publication of CN108146619B publication Critical patent/CN108146619B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18Operating mechanisms
    • B64C25/26Control or locking systems therefor
    • B64C25/30Control or locking systems therefor emergency actuated

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  • Engineering & Computer Science (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Driving Mechanisms And Operating Circuits Of Arc-Extinguishing High-Tension Switches (AREA)
  • Switches Operated By Changes In Physical Conditions (AREA)

Abstract

It rises and falls the control draw ring of holder function with emergency extension the present invention provides a kind of; it is characterized in that; including protection cap (1), microswitch (10), spring (3), draw ring box (4), draw ring bar assembly, guide pressing plate (8), draw ring bar assembly can be moved up along guide pressing plate (8);The first end of draw ring bar assembly is mounted in draw ring box (4); spring (3) is sleeved on the first end of draw ring bar assembly; spring (3) upper end is fixed in the first end of draw ring bar assembly; spring (3) lower end is pressed in draw ring box (4) bottom; opening above draw ring box (4) is sealed by protection cap (1); protection cap (1) sets shaft; it can rotate around the axis after protection cap (1) stress; during off working state, the upper end of the first end of draw ring bar assembly is withstood in protection cap (1);The lower part of the first end of draw ring bar assembly is pierced by downwards from the hole of draw ring box (4).

Description

A kind of control draw ring for the holder function that rises and falls with emergency extension
Technical field
Patent of the present invention is related to a kind of control draw ring for the holder function that rises and falls with emergency extension, is opened for original undercarriage Closing increases the function of emergency extension undercarriage.
Technical background
Landing gear switch is very important switch on aircraft, but at present on landing gear switch and useless good emergent Drop function using the architecture basics of original landing gear switch maturation, increases emergency extension and rises and falls the control of holder function Draw ring takes reliable and stable mechanism to press microswitch, so as to connect emergency extension undercarriage signal.
Invention content
The purpose of patent of the present invention, is solved when aircraft is in state of flight and landing gear switch is in disabler, has been assisted It rises and falls holder function into emergency extension.In order to realize the purpose, the present invention provides one kind, and there is emergency extension to rise and fall holder function Control draw ring, which is characterized in that including protection cap (1), microswitch (10), spring (3), draw ring box (4), tab lever group Part, guide pressing plate (8), draw ring bar assembly can be moved up along guide pressing plate (8);The first end of draw ring bar assembly is mounted on draw ring In box (4), spring (3) is sleeved on the first end of draw ring bar assembly, and spring (3) upper end is fixed on the first end of draw ring bar assembly On, lower end is pressed in draw ring box (4) bottom, and the opening above draw ring box (4) is sealed by protection cap (1), and protection cap (1) setting turns Axis can rotate around the axis after protection cap (1) stress, and during off working state, the upper end of the first end of draw ring bar assembly withstands on protection It covers on (1);The lower part of the first end of draw ring bar assembly is pierced by downwards from the hole of draw ring box (4), microswitch (10) and draw ring The second end cooperation of bar assembly, draw ring bar assembly press microswitch (10) after moving upward to certain distance.
Preferably:Draw ring bar assembly includes tab lever (5) and draw ring guide rail (6), and tab lever (5) is the draw ring bar assembly First end, draw ring guide rail (6) is the second end of the draw ring bar assembly, and tab lever (5) led by rivet (7) mounted on draw ring On rail (6), rivet (7) is fixed on tab lever (5) lower end, and guide groove is set on draw ring guide rail (6), and rivet (7) is upper and lower in guide groove It is mobile.Using tab lever (5) and draw ring guide rail (6) slidable structure, but so that total is compact, so as to save Space.
Preferably:Further include reed (9), reed (9) is set in guide pressing plate (8), be provided on draw ring guide rail (6) with The limit hole of reed (9) cooperation, reed (9) are pressed on draw ring guide rail (6) in off working state, are inserted in working condition Enter in limit hole.Increase reed (9) mainly with providing feedback when draw ring bar assembly is from off working state to working condition to be made With.
The advantages of patent of the present invention:Increase emergency extension in landing gear switch to rise and fall holder function, be lost in landing gear switch It can ensure that undercarriage is put down safely, and simple in structure during effect, connection is reliable, and assembly technology is easy to operate.
Description of the drawings
Fig. 1 is patent structure schematic diagram of the present invention.
Fig. 2 is structure of the present invention schematic diagram when connecting model.
Specific embodiment
Fig. 1, a kind of control draw ring of shown holder function that rises and falls with emergency extension are referred to, one kind has emergency extension Rise and fall the control draw ring of holder function, which is characterized in that including protection cap 1, microswitch 10, spring 3, draw ring box 4, tab lever group Part, guide pressing plate 8, draw ring bar assembly can be moved up along guide pressing plate 8;The first end of draw ring bar assembly is mounted on draw ring box 4 Interior, spring 3 is sleeved on the first end of draw ring bar assembly, and 3 upper end of spring is fixed in the first end of draw ring bar assembly, and lower end is pressed in 4 bottom of draw ring box, the opening of 4 top of draw ring box are sealed by protection cap 1, and protection cap 1 sets shaft, can after 1 stress of protection cap It rotates around the axis, during off working state, the upper end of the first end of draw ring bar assembly is withstood in protection cap 1;The of draw ring bar assembly The lower part of one end is pierced by downwards from the hole of draw ring box 4, and microswitch 10 and the second end of draw ring bar assembly coordinate, tab lever group Part presses microswitch 10 after moving upward to certain distance.
Preferably:Draw ring bar assembly includes tab lever 5 and draw ring guide rail 6, and tab lever 5 is the first of the draw ring bar assembly End, draw ring guide rail 6 are the second end of the draw ring bar assembly, and tab lever 5 is mounted on by rivet 7 on draw ring guide rail 6, rivet 7 5 lower end of tab lever is fixed on, guide groove is set on draw ring guide rail 6, rivet 7 moves up and down in guide groove.
When aircraft is in state of flight and landing gear switch disabler, need to pull open protection cap 1, tab lever 5 at this time Certain distance is popped up under the action of spring 3, tab lever 5 is then continued up into pull-out, tab lever 5 is in draw ring guide rail 6 Guide groove vertex is inside marched to, drives draw ring guide rail 6 is whole to move up under the action of rivet, when draw ring guide rail 6 moves upwards Realize the function of pressing microswitch.
Preferably:Reed 9 is further included, reed 9 is set in guide pressing plate 8, is provided on draw ring guide rail 6 and the reed The limit hole of 9 cooperations, reed 9 are pressed in off working state on draw ring guide rail 6, are inserted into limit hole in working condition.

Claims (3)

1. a kind of control draw ring for the holder function that rises and falls with emergency extension, which is characterized in that including protection cap (1), microswitch (10), spring (3), draw ring box (4), draw ring bar assembly, guide pressing plate (8), draw ring bar assembly can be along guide pressing plates (8) to moving up It is dynamic;The first end of draw ring bar assembly is mounted in draw ring box (4), and spring (3) is sleeved on the first end of draw ring bar assembly, spring (3) upper end is fixed in the first end of draw ring bar assembly, and spring (3) lower end is pressed in draw ring box (4) bottom, draw ring box (4) top Opening sealed by protection cap (1), protection cap (1) setting shaft can rotate around the axis after protection cap (1) stress, inoperative During state, the upper end of the first end of draw ring bar assembly is withstood in protection cap (1);The lower part of the first end of draw ring bar assembly is from draw ring It is pierced by downwards in the hole of box (4), microswitch (10) and the second end of draw ring bar assembly coordinate, and draw ring bar assembly moves upward to Microswitch (10) is pressed after certain distance.
2. the control draw ring of the holder function according to claim 1 that rises and falls with emergency extension, which is characterized in that tab lever group Part includes tab lever (5) and draw ring guide rail (6), and tab lever (5) is the first end of the draw ring bar assembly, and draw ring guide rail (6) is The second end of the draw ring bar assembly, by rivet (7) on draw ring guide rail (6), rivet (7) is fixed on tab lever (5) Tab lever (5) lower end sets guide groove on draw ring guide rail (6), and rivet (7) moves up and down in guide groove.
3. the control draw ring of the holder function according to claim 2 that rises and falls with emergency extension, which is characterized in that further include spring Piece (9), reed (9) are set in guide pressing plate (8), and the limiting coordinated with the reed (9) is provided on draw ring guide rail (6) Hole, reed (9) are pressed in off working state on draw ring guide rail (6), are inserted into limit hole in working condition.
CN201611097530.8A 2016-12-02 2016-12-02 Control pull ring with emergency landing gear laying-down function Active CN108146619B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611097530.8A CN108146619B (en) 2016-12-02 2016-12-02 Control pull ring with emergency landing gear laying-down function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611097530.8A CN108146619B (en) 2016-12-02 2016-12-02 Control pull ring with emergency landing gear laying-down function

Publications (2)

Publication Number Publication Date
CN108146619A true CN108146619A (en) 2018-06-12
CN108146619B CN108146619B (en) 2022-07-15

Family

ID=62470167

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611097530.8A Active CN108146619B (en) 2016-12-02 2016-12-02 Control pull ring with emergency landing gear laying-down function

Country Status (1)

Country Link
CN (1) CN108146619B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2930114Y (en) * 2006-06-29 2007-08-01 武汉电信器件有限公司 Photoelectric module pull ring type de-locking device
CN202258955U (en) * 2011-07-19 2012-05-30 吕宗伟 Improved pull switch structure
CN202526791U (en) * 2012-04-26 2012-11-14 中汽客汽车零部件(厦门)有限公司 Fire emergency escape device
US20150151832A1 (en) * 2013-12-02 2015-06-04 Embraer S.A. Emergency gravity free-fall deployment systems for retractable aircraft landing gear assemblies
CN205049358U (en) * 2015-10-10 2016-02-24 陕西飞机工业(集团)有限公司 Emergent testing tool of putting undercarriage
CN105667808A (en) * 2014-11-19 2016-06-15 中国航空工业集团公司西安飞机设计研究所 Emergency manual releaser

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2930114Y (en) * 2006-06-29 2007-08-01 武汉电信器件有限公司 Photoelectric module pull ring type de-locking device
CN202258955U (en) * 2011-07-19 2012-05-30 吕宗伟 Improved pull switch structure
CN202526791U (en) * 2012-04-26 2012-11-14 中汽客汽车零部件(厦门)有限公司 Fire emergency escape device
US20150151832A1 (en) * 2013-12-02 2015-06-04 Embraer S.A. Emergency gravity free-fall deployment systems for retractable aircraft landing gear assemblies
CN105667808A (en) * 2014-11-19 2016-06-15 中国航空工业集团公司西安飞机设计研究所 Emergency manual releaser
CN205049358U (en) * 2015-10-10 2016-02-24 陕西飞机工业(集团)有限公司 Emergent testing tool of putting undercarriage

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Publication number Publication date
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