CN106761123A - A kind of gas spring assembly with auto-lock function - Google Patents
A kind of gas spring assembly with auto-lock function Download PDFInfo
- Publication number
- CN106761123A CN106761123A CN201710008849.7A CN201710008849A CN106761123A CN 106761123 A CN106761123 A CN 106761123A CN 201710008849 A CN201710008849 A CN 201710008849A CN 106761123 A CN106761123 A CN 106761123A
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- CN
- China
- Prior art keywords
- locking member
- gas spring
- auto
- block
- locking
- 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.)
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Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05F15/00—Power-operated mechanisms for wings
- E05F15/50—Power-operated mechanisms for wings using fluid-pressure actuators
- E05F15/53—Power-operated mechanisms for wings using fluid-pressure actuators for swinging wings
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
- E05Y2201/00—Constructional elements; Accessories therefor
- E05Y2201/40—Motors; Magnets; Springs; Weights; Accessories therefor
- E05Y2201/47—Springs
- E05Y2201/478—Gas springs
Landscapes
- Lock And Its Accessories (AREA)
- Fluid-Damping Devices (AREA)
Abstract
A kind of gas spring assembly with auto-lock function, belongs to aircraft door technical field.It is two including gas spring, is symmetrical arranged side by side, one end is connected on the hatch door mouthful auxiliary frame of frame, other end connection self-locking device；Bearing, one end is connected on self-locking device, and the other end is affixed with hatch door mouthful frame eyebrow beam；Pull bar, one end is connected on self-locking device, other end connection hatch door；Self-locking device, difference connects bearing, the gentle spring of pull bar, thereon with the locking member and block for cooperating, when hatch door is opened in final state, the block is locked with the locking member being connected on bearing.The gas spring assembly of connecting cabin doorway of the present invention frame carries auto-lock function so that oneself locking when hatch door opens final position, prevents resilience from crushing discrepancy personnel.Locking device of the invention, by mechanical structure mating reaction auto lock, during unblock, is unlocked when hatch door is opened by pulling the spanner for exposing, and simple structure is easy to operate.
Description
Technical field
The invention belongs to cabin technical field, more particularly to a kind of gas spring assembly with auto-lock function.It is applied to
With the upper-turn-type hatch door that gas spring is outwardly opened as power.
Background technology
The existing upper-turn-type hatch door outwardly opened as opening power by the use of gas spring, at hatch door completely opening, gas
The stroke maximum of spring, and gas spring load minimum now, hatch door easily return hatch door by wind load or other external actions
Operating personnel are damaged by bullet.And such hatch door of existing type, strut is generally relied on the connection of doorway frame to prevent cabin
The resilience of door.The weight of this class formation is big, high cost, cumbersome.
The content of the invention
For above-mentioned technical problem, the present invention provides a kind of gas spring assembly with auto-lock function, in hatch door
Open position self can lock, and prevent the resilience of hatch door.
The purpose of the present invention is achieved through the following technical solutions：
A kind of gas spring assembly with auto-lock function of the present invention, including：
Gas spring, is two, is symmetrical arranged side by side, and one end is connected on the hatch door mouthful auxiliary frame of frame, is hinged with auxiliary frame, the other end
Connection self-locking device；
Bearing, one end is connected on self-locking device, and the eyebrow beam on the other end and hatch door mouthful frame is affixed；
Pull bar, one end is connected on self-locking device, other end connection hatch door；
Self-locking device, difference connects bearing, the gentle spring of pull bar, thereon with the locking member and block for cooperating,
Hatch door is opened during in final state, and the block is locked with the locking member being connected on bearing.
Further, the self-locking device includes：
Connecting crank, is triangular frame structure, and one jiao of end is hinged on two gas springs, one jiao of end cylinder lever connecting rod, another angle
End connection rotating shaft, bearing is nested with the rotating shaft, and the outward flange near rotating shaft end carries block；
Locking member, on lock shaft, in bearing, contacts with connecting crank, is rotated in opened door connecting crank
When axle is rotated, locking member along connecting crank surface pivots, when hatch door is opened in final state, locking member just be connected song
Block on handle is locked, and realizes self-locking.
Further, opposition F1 and both contact points and the lock shaft line of centres of the connecting crank to locking member
Folded sharp angle α is more than 30 °.
Further, the locking member is made up of homonymy on axle sleeve with two symmetrical stopper blocks, the stopper block termination
It is the block cooperation in arc transition, with connecting crank.
Further, the block on the connecting crank is two, is symmetrical arranged in connecting crank edge side, the gear
Block is in contact with stopper block termination, mutually stops, forms self-locking.
Further, in the locked state, maximal clearance is 1-2mm between connecting crank block and locking member termination.
Further, in the locked condition, when gas spring occurs resilience, connecting crank is contacted with locking member, connecting crank
To the directed force F 2 of locking member 5 ° are less than with the angle β of both contact points and the lock shaft line of centres.
Further, torsion spring is also set with the lock shaft, release lever is arranged on lock shaft, and torsion spring two ends connect respectively
Bearing and release lever, torsion spring make release lever have the trend for rotating down, and pull handle during unblock upwards, drive locking member to turn
It is dynamic, locking member is bypassed the stop location of connecting crank, release locking.
A kind of aircraft door of the present invention, is provided with the above-mentioned gas spring assembly with auto-lock function.
A kind of aircraft of the present invention, with described aircraft door.
Beneficial effects of the present invention are：
1. the gas spring assembly of connecting cabin doorway of the present invention frame carries auto-lock function so that during hatch door opening final position certainly
Oneself locks, and prevents resilience from crushing discrepancy personnel.
2. locking device of the invention is when being opened by hatch door, to be locked automatically by mechanical structure mating reaction of the present invention
Tightly, during unblock, unlocked by pulling the spanner for exposing, simple structure is easy to operate.
Brief description of the drawings
Fig. 1 is that the present invention uses the structural representation for installing
Fig. 2 is dimensional structure diagram of the invention.
Fig. 3 is the planar structure schematic diagram of Fig. 2.
Fig. 4 is working state schematic representation of the present invention.
Fig. 5 is self-locking state schematic diagram of the present invention.
Fig. 6 is the structural representation of connecting crank of the present invention and locking member locking state.
Fig. 7 is lock shaft attachment structure schematic diagram of the present invention.
Fig. 8 is the dimensional structure diagram of connecting crank of the present invention.
Fig. 9 is the planar structure schematic diagram of Fig. 8.
In figure：1. eyebrow beam, 2. auxiliary frame, 3. gas spring, 4. connecting crank, 5. bearing, 6. locking member, 7. rotating shaft, 8. handle,
9. lock shaft, 10. pull bar, 11. torsion springs, 12. blocks, 13. bearing pins.
Specific embodiment
The present invention will be described in detail with reference to the accompanying drawings and examples.
Embodiment：As shown in Figure 1-Figure 3, a kind of gas spring assembly with auto-lock function of the present invention, positioned at hatch door top,
The eyebrow beam 1 of mouth frame and the junction of auxiliary frame 2；Including：
Gas spring 3, is symmetrical arranged side by side by two, and one end is connected on the hatch door mouthful auxiliary frame 2 of frame, is hinged with auxiliary frame 2, another
End connection self-locking device；
Bearing 5, one end is connected on self-locking device, and the other end is affixed with hatch door mouthful frame eyebrow beam 1, play fixed supporting role；
Pull bar 10, one end is connected on self-locking device, other end connection hatch door；
Self-locking device, difference connects bearing 5, the gentle spring 3 of pull bar 10, thereon with the locking member 6 and gear for cooperating
Block 12, when hatch door is opened in final state, the block 12 is locked with the locking member 6 being connected on bearing 5.
As Figure 4-Figure 7, the self-locking device includes：
Shown, connecting crank 4 is triangular frame structure, and one jiao of end is connected on two gas springs, and the angle end carries two points
Not Lian Jie gas spring 3 adapter sleeve hole, be sleeved on gas spring 3；One jiao of end cylinder lever connecting rod 10, the angle end is with connection bearing pin 13
Two connecting holes, between pull bar 10 is placed in two connecting holes, connected by bearing pin 13；Another angle end connection rotating shaft 7, the angle end is with company
Switch through the mounting hole of axle 7, bearing 5 is nested with the rotating shaft 7, positioned at the outside of connecting crank 4, near the connecting crank 4 at the end of rotating shaft 7
Outward flange carries block 12；Connecting crank 4 keeps contacting with locking member 6 in unlocked timing instant, and connecting crank 4 is to locking member
6 opposition F1 and both contact points are more than 30 ° with sharp angle α folded by the line of centres of lock shaft 9, it is ensured that hatch door opening or
Stuck situation will not occur in closing process.
As shown in Fig. 2, Fig. 7, locking member 6 on lock shaft 9, between connecting crank 4 and bearing 5, is opening cabin
During 7 rotation around the shaft of door connecting crank 4, locking member 6 is slided along the surface of connecting crank 4, when hatch door is opened in final state,
Locking member 6 is just locked with the block 12 on connecting crank 4, realizes self-locking.In the locked state, the termination of locking member 6 with
Maximal clearance between the block 12 of connecting crank 4 is 1mm -2mm；When there is resilience in gas spring 3, locking member 6 and connecting crank
4 block 12 is contacted, directed force F 2 and both contact points and the angle β of lock shaft 9 line of centres of the connecting crank 4 to locking member 6
Less than 5 °, as shown in fig. 6, force direction is on the lower side for both lines above-mentioned, so ensure the security of self-locking.
As shown in fig. 7, the locking member 6 is made up of homonymy on axle sleeve with two symmetrical stopper blocks, the stopper block end
Head coordinates for the block 12 in arc transition, with connecting crank 4, convenient unblock.
As Figure 4-Figure 7, the block 12 on the connecting crank 4 is two, is symmetrically set in the edge side of connecting crank 4
Put, in the locked condition, the block 12 is in contact with stopper block termination, mutually stop, form self-locking.
Torsion spring 11 is also set with the lock shaft 9, release lever 8 is fixedly mounted on lock shaft 9, the two ends of torsion spring 11 connect respectively
Bearing 5 and release lever 8 are connect, and torsion spring 11 makes release lever 8 have the trend for rotating down.Handle 8 is pulled during unblock, lock is driven
Tight part 6 is rotated, and locking member 6 is bypassed the position of block 12 of connecting crank 4, releases locking.
Operation principle of the invention：
When hatch door is opened, gas spring 3 extends, and gas spring 3 promotes connecting crank 47 to rotate around the shaft, and I is moved in such as Fig. 4
It is shown, enable connecting crank 4 to drive locking member 6 to be slided along the surface of connecting crank 4, this motion makes locking member 6 drive lock
Axle 7 is rotated, and II is moved as shown in Figure 4；When hatch door is in opens final position, locking member 6 just bypasses the gear of connecting crank 4
The position of block 12, completes locking, as shown in Figure 5.
When needing to unlock, release lever 8 (as shown in Fig. 5 motions III) must be rotated up, release lever 8 drives lock shaft
9 rotate, and lock shaft 9 drives locking member 6 to be turned out (as shown in Fig. 5 motions IV), makes locking
Part 6 can bypass the position of block 12 of connecting crank 4, unlock, and can now close hatch door.
Claims (10)
1. a kind of gas spring assembly with auto-lock function, it is characterised in that including：
Gas spring, is two, is symmetrical arranged side by side, and one end is connected on the hatch door mouthful auxiliary frame of frame, is hinged with auxiliary frame, other end connection
Self-locking device；
Bearing, one end is connected on self-locking device, and the eyebrow beam on the other end and hatch door mouthful frame is affixed；
Pull bar, one end is connected on self-locking device, other end connection hatch door；
Self-locking device, difference connects bearing, the gentle spring of pull bar, thereon with the locking member and block for cooperating, in hatch door
Open during in final state, the block is locked with the locking member being connected on bearing.
2. the gas spring assembly of auto-lock function is carried according to claim 1, it is characterised in that：The self-locking device includes：
Connecting crank, is triangular frame structure, and one jiao of end is hinged on two gas springs, one jiao of end cylinder lever connecting rod, and another angle end connects
Switch through axle, bearing is nested with the rotating shaft, the outward flange near rotating shaft end carries block；
Locking member, on lock shaft, in bearing, contacts with connecting crank, turns around the shaft in opened door connecting crank
When dynamic, locking member along connecting crank surface pivots, when hatch door is opened in final state, locking member just with connecting crank on
Block lock, realize self-locking.
3. the gas spring assembly of auto-lock function is carried according to claim 2, it is characterised in that：The connecting crank is to locking
The opposition F1 of part and both contact points are more than 30 ° with sharp angle α folded by the lock shaft line of centres.
4. the gas spring assembly of auto-lock function is carried according to claim 2, it is characterised in that：The locking member is by axle sleeve
Homonymy is constituted with two symmetrical stopper blocks, and the stopper block termination is that the block in arc transition, with connecting crank coordinates.
5. the gas spring assembly of auto-lock function is carried according to claim 4, it is characterised in that：Gear on the connecting crank
Block is two, is symmetrical arranged in connecting crank edge side, and the block is in contact with stopper block termination, is mutually stopped, is formed
Self-locking.
6. the gas spring assembly of auto-lock function is carried according to claim 5, it is characterised in that：In the locked state, connect
Maximal clearance is 1-2mm between crank block and locking member termination.
7. the gas spring assembly of auto-lock function is carried according to claim 5, it is characterised in that：In the locked condition, gas bullet
When spring occurs resilience, connecting crank is contacted with locking member, directed force F 2 and both contact point and lock of the connecting crank to locking member
The angle β of the axle line of centres is less than 5 °.
8. the gas spring assembly of auto-lock function is carried according to claim 2, it is characterised in that：Also it is set with the lock shaft
Torsion spring, release lever is arranged on lock shaft, and torsion spring two ends difference connects bearing and release lever, torsion spring make release lever have downwards
The trend of rotation, pulls handle upwards during unblock, drive locking member to rotate, and locking member is bypassed the block position of connecting crank
Put, release locking.
9. a kind of aircraft door, is provided with the gas spring assembly with auto-lock function described in claim any one of 1-8.
10. a kind of aircraft, with the aircraft door described in claim 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710008849.7A CN106761123B (en) | 2017-01-06 | 2017-01-06 | A kind of gas spring assembly with auto-lock function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710008849.7A CN106761123B (en) | 2017-01-06 | 2017-01-06 | A kind of gas spring assembly with auto-lock function |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106761123A true CN106761123A (en) | 2017-05-31 |
| CN106761123B CN106761123B (en) | 2018-02-02 |
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ID=58949712
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710008849.7A Active CN106761123B (en) | 2017-01-06 | 2017-01-06 | A kind of gas spring assembly with auto-lock function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106761123B (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110657324A (en) * | 2019-10-29 | 2020-01-07 | 深圳市科曼医疗设备有限公司 | A rocker device |
| CN110748758A (en) * | 2019-10-29 | 2020-02-04 | 深圳市科曼医疗设备有限公司 | A rocker device |
| CN110748757A (en) * | 2019-10-29 | 2020-02-04 | 深圳市科曼医疗设备有限公司 | Rocker arm device |
| CN110748759A (en) * | 2019-10-29 | 2020-02-04 | 深圳市科曼医疗设备有限公司 | Rocker arm device |
| CN111803305A (en) * | 2020-08-11 | 2020-10-23 | 烟台宏远载人压力舱工程技术研究院有限公司 | Wedged pre-tightening cabin door of pressure cabin |
| EP4535086A1 (en) * | 2023-10-03 | 2025-04-09 | Canon Kabushiki Kaisha | Opening and closing device, image forming apparatus including opening and closing device, and gas spring unit for image forming apparatus |
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| DE2914469A1 (en) * | 1979-04-10 | 1980-10-23 | Messerschmitt Boelkow Blohm | ARRANGEMENT OF A FLAP DRIVED BY AN ACTUATOR, IN PARTICULAR ON AN AIRPLANE CELL, A SPACE VEHICLE OR THE LIKE, IN PARTICULAR A FLAP FOR CLOSING AN AIR SUCTION OPENING FOR THE STARTING TURBINE ENGINE |
| US20030132347A1 (en) * | 2001-12-14 | 2003-07-17 | Stefan Blum | Emergency opening cylinder of a passenger door for an airplane, a door system and a method of modifying a door system |
| CN102452475A (en) * | 2010-10-29 | 2012-05-16 | 中国商用飞机有限责任公司 | Aircraft cabin door stop device |
| CN103510783A (en) * | 2013-10-18 | 2014-01-15 | 青岛四方车辆研究所有限公司 | Opening-closing mechanism with self-locking devices |
| CN203638079U (en) * | 2013-12-31 | 2014-06-11 | 陕西中航气弹簧有限责任公司 | Middle self-locking type cabin door supporting rod |
| CN206397337U (en) * | 2017-01-06 | 2017-08-11 | 江苏美龙振华科技有限公司 | A kind of gas spring assembly with auto-lock function |
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2017
- 2017-01-06 CN CN201710008849.7A patent/CN106761123B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2914469A1 (en) * | 1979-04-10 | 1980-10-23 | Messerschmitt Boelkow Blohm | ARRANGEMENT OF A FLAP DRIVED BY AN ACTUATOR, IN PARTICULAR ON AN AIRPLANE CELL, A SPACE VEHICLE OR THE LIKE, IN PARTICULAR A FLAP FOR CLOSING AN AIR SUCTION OPENING FOR THE STARTING TURBINE ENGINE |
| US20030132347A1 (en) * | 2001-12-14 | 2003-07-17 | Stefan Blum | Emergency opening cylinder of a passenger door for an airplane, a door system and a method of modifying a door system |
| CN102452475A (en) * | 2010-10-29 | 2012-05-16 | 中国商用飞机有限责任公司 | Aircraft cabin door stop device |
| CN103510783A (en) * | 2013-10-18 | 2014-01-15 | 青岛四方车辆研究所有限公司 | Opening-closing mechanism with self-locking devices |
| CN203638079U (en) * | 2013-12-31 | 2014-06-11 | 陕西中航气弹簧有限责任公司 | Middle self-locking type cabin door supporting rod |
| CN206397337U (en) * | 2017-01-06 | 2017-08-11 | 江苏美龙振华科技有限公司 | A kind of gas spring assembly with auto-lock function |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110657324A (en) * | 2019-10-29 | 2020-01-07 | 深圳市科曼医疗设备有限公司 | A rocker device |
| CN110748758A (en) * | 2019-10-29 | 2020-02-04 | 深圳市科曼医疗设备有限公司 | A rocker device |
| CN110748757A (en) * | 2019-10-29 | 2020-02-04 | 深圳市科曼医疗设备有限公司 | Rocker arm device |
| CN110748759A (en) * | 2019-10-29 | 2020-02-04 | 深圳市科曼医疗设备有限公司 | Rocker arm device |
| CN110748759B (en) * | 2019-10-29 | 2021-07-27 | 深圳市科曼医疗设备有限公司 | Rocker arm device |
| CN110748758B (en) * | 2019-10-29 | 2022-01-25 | 深圳市科曼医疗设备有限公司 | Rocker arm device |
| CN110748757B (en) * | 2019-10-29 | 2022-03-22 | 深圳市科曼医疗设备有限公司 | Rocker arm device |
| CN110657324B (en) * | 2019-10-29 | 2022-04-26 | 深圳市科曼医疗设备有限公司 | A rocker device |
| CN111803305A (en) * | 2020-08-11 | 2020-10-23 | 烟台宏远载人压力舱工程技术研究院有限公司 | Wedged pre-tightening cabin door of pressure cabin |
| EP4535086A1 (en) * | 2023-10-03 | 2025-04-09 | Canon Kabushiki Kaisha | Opening and closing device, image forming apparatus including opening and closing device, and gas spring unit for image forming apparatus |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106761123B (en) | 2018-02-02 |
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| CB03 | Change of inventor or designer information |
Inventor after: You Xianghua Inventor after: Chen Xiaofeng Inventor after: Lv Peng Inventor after: Wu Di Inventor after: Xiao Chunhong Inventor after: Zhu Liang Inventor before: Chao Xiangfei Inventor before: Chen Xiaofeng Inventor before: Lv Peng Inventor before: Wu Di Inventor before: Xiao Chunhong Inventor before: Zhu Liang |
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| CB03 | Change of inventor or designer information |
Inventor after: You Zhenhua Inventor after: Chen Xiaofeng Inventor after: Lv Peng Inventor after: Wu Di Inventor after: Xiao Chunhong Inventor after: Zhu Liang Inventor before: Chao Xiangfei Inventor before: Chen Xiaofeng Inventor before: Lv Peng Inventor before: Wu Di Inventor before: Xiao Chunhong Inventor before: Zhu Liang |
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