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CN201137336Y - Cabin door locking apparatus - Google Patents

Cabin door locking apparatus Download PDF

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Publication number
CN201137336Y
CN201137336Y CNU2007203105208U CN200720310520U CN201137336Y CN 201137336 Y CN201137336 Y CN 201137336Y CN U2007203105208 U CNU2007203105208 U CN U2007203105208U CN 200720310520 U CN200720310520 U CN 200720310520U CN 201137336 Y CN201137336 Y CN 201137336Y
Authority
CN
China
Prior art keywords
rotating shaft
connecting rod
lock
locking
latch hook
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.)
Expired - Lifetime
Application number
CNU2007203105208U
Other languages
Chinese (zh)
Inventor
梁应军
赵那斯图
汪海清
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.)
Xi'an aircraft, international aviation manufacturing, Limited by Share Ltd, Hanzhoung aircraft branch
Original Assignee
AVIC Shaanxi Aircraft Industry Group Corp 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 AVIC Shaanxi Aircraft Industry Group Corp Ltd filed Critical AVIC Shaanxi Aircraft Industry Group Corp Ltd
Priority to CNU2007203105208U priority Critical patent/CN201137336Y/en
Application granted granted Critical
Publication of CN201137336Y publication Critical patent/CN201137336Y/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

The utility model relates to a compartment door locking device, which comprises a shifting claw torsion spring, a shifting claw, a lock hook, a lock pillar, a lock hook torsion spring and a support stand, wherein the lock pillar is connected with a device body, an L-shaped locking arm is installed on the shifting claw through a rotation shaft which is arranged on the peak of the L-shaped locking arm, one end of the L-shaped locking arm is connected with a steel rope with a locking spring, and the other end is connected with a connecting rod through a connecting rotation shaft, the other end of the connecting rod is connected on a fixed rotation shaft on the support stand, and the rotation shafts are all in one line when the L-shaped locking arm and the connecting rod are in the locking state. Compared with the prior art, the compartment door locking device has the advantages that firstly the locking and lockup (secure) are firm and reliable, secondly a secure device is naturally provided, thirdly larger impact which is generated through closing the compartment door can be effectively absorbed, and finally the structure is simple, and the financial resource and labor resource can be saved.

Description

A kind of hatch door locking device
Technical field
The utility model is a kind of hatch door locking device, belongs to the frame for movement technical field.
Background technology
Locking device such as Fig. 1 of aircraft door use at present show, be to rotate pusher dog 2 by pusher dog torsion spring 1 to block latch hook 3, latch hook 3 hooks lock 4 and the device of realization locking, and the weak point of this device is: do not have insurance institution, locking is unreliable concerning some important hatch doors; Can not effectively absorb the impact force that produces when closing hatch door, particularly impact force and destroy locking device when big easily.
Summary of the invention
The defective that the present invention exists at above-mentioned existing apparatus just and design a kind of hatch door locking device is provided its objective is the improvement existing apparatus, and a kind of locking device that carries insurance institution is provided.
The purpose of this utility model realizes by following measure:
This kind hatch door locking device, comprise the pusher dog torsion spring, pusher dog, latch hook, lock, latch hook torsion spring and bearing, lock and body link together, its structural design features is: by rotating shaft a L shaped lock arm is installed on pusher dog, rotating shaft is arranged on L shaped lock arm point place, one end of L shaped lock arm connects a firm rope of deciding spring with lock, its other end connects rotating shaft by one and is connected with connecting rod, the other end of connecting rod is connected on the fixed rotating shaft on the bearing, L shaped lock arm and connecting rod when lock-out state, rotating shaft, rotating shaft and rotating shaft are in a straight line.In addition, the indent of the junction of latch hook and pusher dog is the transition region of one section circular arc.
The structure design of the utility model device has solved following problem in the existing mechanism:
(a) locking state: the utility model and hatch door connect as one, and during locking, latch hook hooks lock (lock is fixed on the body), hatch door is closed put in place, and pusher dog blocks latch hook in the other direction, and latch hook can not be rotated towards the direction of unblanking, and keep firm locking state;
(b) locking (insurance) state: the utility model design has the insurance institution of a cover by connecting rod, lock arm and locking spring, by the self-locking action of connecting rod, lock arm itself, provides a kind of locking (insurance) device;
(c) the greater impact power that is produced when effectively hatch door is closed in absorption by the arc transition district on the latch hook.
Description of drawings
The hatch door locking device that Fig. 1 uses at present
Fig. 2 is that hatch door locking state, insurance institution are in insurance (self-locking) status architecture schematic diagram
Fig. 3 is that insurance institution is in open mode, status architecture schematic diagram when hatch door is about to open
Fig. 4 is hatch door status architecture schematic diagram when opening moment
Status architecture schematic diagram when Fig. 5 is the hatch door turn-off transient
Status architecture schematic diagram when Fig. 6 is the impact force that produces when effectively absorbing hatch door and closing
Fig. 7 is the arc transition district signal of latch hook
The specific embodiment
Below with reference to accompanying drawing and embodiment the utility model is described in further detail:
Shown in accompanying drawing 2~7, this kind hatch door locking device, comprise pusher dog torsion spring 1, pusher dog 2, latch hook 3, lock 4, latch hook torsion spring 5 and bearing 6, lock 4 links together with body, on pusher dog 2, a L shaped lock arm 9 is installed by rotating shaft 11, rotating shaft 11 is arranged on place, L shaped lock arm 9 pinnacles, one end of L shaped lock arm 9 connects a firm rope 7 of deciding spring 10 with lock, its other end connects rotating shaft 12 by one and is connected with connecting rod 8, the other end of connecting rod 8 is connected on the fixed rotating shaft 13 on the bearing 6, L shaped lock arm 9 and connecting rod 8 when lock-out state, rotating shaft 11, rotating shaft 12 and rotating shaft 13 are in a straight line.In addition, latch hook 3 is the transition region of one section circular arc with the indent of the junction of pusher dog 2.
The course of work of the utility model device is:
As shown in Figure 2, the hatch door locking state, this moment, latch hook 3 hooked lock 4, and pusher dog 2 blocks latch hook 3, and latch hook 3 can not be rotated towards the direction of unblanking; Connecting rod 8 and lock arm are in self-locking state 9 this moments, and its active force conllinear guarantees that pusher dog 2 can not rotate on same straight line, play safety effect.
As shown in Figure 3, when opening hatch door, only need the firm rope 7 of pulling, open safeties, pusher dog 2 is thrown off latch hooks 3 at this moment, and hatch door is about to open.
Behind pusher dog 2 complete latch hooks 3, latch hook 3 rotates towards the direction of unblanking under the effect of latch hook torsion spring 5, throws off lock 4, and hatch door is opened, and Fig. 4 opens moment for hatch door.
When closing hatch door, when latch hook 3 is run into lock 4, under the effect of door closing force, overcome the elastic force of latch hook torsion spring 5, latch hook 3 is rotated, as shown in Figure 5 towards shutting direction.After latch hook 3 forwarded the position to, pusher dog 2 rotated under the effect of pusher dog torsion spring 1 and locking spring 10 and blocks latch hook 3, and connecting rod 8 and lock arm 9 are in self-locking state again, play safety effect again, and at this moment, hatch door is locked fully, locks.
Shown in Fig. 6,7, if in closing the hatch door process, produce bigger impact force, can effectively absorb by the arc transition district on the latch hook 3, promptly be that latch hook 3 rotates along the impact force direction in this process, and pusher dog 2 is owing to be to contact with arc transition district on the latch hook 3, then pusher dog 2 can not rotate, thus the impact force that produces when effectively absorbing hatch door and closing, and can not damage body, hatch door and the utility model.Impact force returns to hatch door locking state as shown in Figure 2 after disappearing under the effect of latch hook torsion spring 5.
Through verification experimental verification, the utility model locking puts in place, and safeties are solid and reliable.
The utility model is compared with existing apparatus, and its advantage is:
(a) locking, the locking (insurance) solid and reliable;
(b) carry safeties;
(c) can effectively absorb the greater impact power that hatch door produces of closing;
(d) simple in structure, save financial resources, manpower.

Claims (2)

1. hatch door locking device, comprise pusher dog torsion spring (1), pusher dog (2), latch hook (3), lock (4), latch hook torsion spring (5) and bearing (6), lock (4) links together with body, it is characterized in that: go up by rotating shaft (11) at pusher dog (2) a L shaped lock arm (9) is installed, rotating shaft (11) is arranged on place, L shaped lock arm (9) pinnacle, one end of L shaped lock arm (9) connects a firm rope (7) of deciding spring (10) with lock, its other end connects rotating shaft (12) by one and is connected with connecting rod (8), the other end of connecting rod (8) is connected on the fixed rotating shaft (13) on the bearing (6), L shaped lock arm (9) and connecting rod (8) when lock-out state, rotating shaft (11), rotating shaft (12) and rotating shaft (13) are in a straight line.
2. hatch door locking device according to claim 1 is characterized in that: latch hook (3) is the transition region of one section circular arc with the indent of the junction of pusher dog (2).
CNU2007203105208U 2007-12-13 2007-12-13 Cabin door locking apparatus Expired - Lifetime CN201137336Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2007203105208U CN201137336Y (en) 2007-12-13 2007-12-13 Cabin door locking apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2007203105208U CN201137336Y (en) 2007-12-13 2007-12-13 Cabin door locking apparatus

Publications (1)

Publication Number Publication Date
CN201137336Y true CN201137336Y (en) 2008-10-22

Family

ID=40038022

Family Applications (1)

Application Number Title Priority Date Filing Date
CNU2007203105208U Expired - Lifetime CN201137336Y (en) 2007-12-13 2007-12-13 Cabin door locking apparatus

Country Status (1)

Country Link
CN (1) CN201137336Y (en)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103132826A (en) * 2013-02-07 2013-06-05 玉环县天润航空机械制造厂 Locking mechanism of cockpit door
CN103527008A (en) * 2012-07-06 2014-01-22 哈尔滨飞机工业集团有限责任公司 Pulling and pressing type quick-release lock
CN103748303A (en) * 2011-08-22 2014-04-23 埃尔塞乐公司 Locking device with mechanical detection of closing and opening
CN104328948A (en) * 2013-07-22 2015-02-04 Eads飞机设计有限公司 System for monitoring state of two-part-cowl lock unit
CN104863421A (en) * 2015-05-27 2015-08-26 北京航空航天大学 Quick connecting, locking and unlocking mechanism
CN105133972A (en) * 2015-09-24 2015-12-09 江西洪都航空工业集团有限责任公司 Hook-type lock safety mechanism for aviation cockpit
CN105492319A (en) * 2013-08-30 2016-04-13 B/E航空公司 Mobile Kitchen Cart
CN105625839A (en) * 2014-10-31 2016-06-01 中国航空工业集团公司西安飞机设计研究所 Mechanism locking device
CN106527088A (en) * 2016-09-06 2017-03-22 江西亿铂电子科技有限公司 Photosensitive element box
CN109958347A (en) * 2019-04-04 2019-07-02 上海宇航系统工程研究所 A kind of retaining mechanism for tensing and pushing open
CN110700689A (en) * 2019-09-29 2020-01-17 中航通飞研究院有限公司 Cabin door latch mechanism
CN111114782A (en) * 2019-12-29 2020-05-08 宏光空降装备有限公司 Mooring and automatic release lock mounted on side wall
CN113229192A (en) * 2021-05-13 2021-08-10 厦门大学 Frame-type multilayer cultivation box and frame-type multilayer abalone cultivation box
CN115573631A (en) * 2022-10-09 2023-01-06 中国航空工业集团公司西安飞机设计研究所 Aircraft cabin door lock mechanism safety locking mechanism
CN115584897A (en) * 2022-10-09 2023-01-10 中国航空工业集团公司西安飞机设计研究所 A drop-type aircraft cabin door lock mechanism
WO2024178776A1 (en) * 2023-02-28 2024-09-06 玉环天润航空机械制造有限公司 Locking mechanism for landing gear door of unmanned aerial vehicle, and door system

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103748303A (en) * 2011-08-22 2014-04-23 埃尔塞乐公司 Locking device with mechanical detection of closing and opening
CN103527008B (en) * 2012-07-06 2016-03-30 哈尔滨飞机工业集团有限责任公司 Drawing and pressing type quick-detachable lock
CN103527008A (en) * 2012-07-06 2014-01-22 哈尔滨飞机工业集团有限责任公司 Pulling and pressing type quick-release lock
CN103132826A (en) * 2013-02-07 2013-06-05 玉环县天润航空机械制造厂 Locking mechanism of cockpit door
CN103132826B (en) * 2013-02-07 2015-03-11 玉环天润航空机械制造有限公司 Locking mechanism of cockpit door
CN104328948B (en) * 2013-07-22 2019-03-29 Eads飞机设计有限公司 For monitoring the monitoring system of two-piece type radome fairing locking unit
CN104328948A (en) * 2013-07-22 2015-02-04 Eads飞机设计有限公司 System for monitoring state of two-part-cowl lock unit
US10377493B2 (en) 2013-08-30 2019-08-13 Rockwell Collins, Inc. Mobile galley cart with heating, cooling and braking functionality
CN105492319A (en) * 2013-08-30 2016-04-13 B/E航空公司 Mobile Kitchen Cart
US10137987B2 (en) 2013-08-30 2018-11-27 B/E Aerospace, Inc. Mobile galley cart with heating, cooling and braking functionality
CN105625839A (en) * 2014-10-31 2016-06-01 中国航空工业集团公司西安飞机设计研究所 Mechanism locking device
CN105625839B (en) * 2014-10-31 2017-10-31 中国航空工业集团公司西安飞机设计研究所 A kind of mechanism locking device
CN104863421A (en) * 2015-05-27 2015-08-26 北京航空航天大学 Quick connecting, locking and unlocking mechanism
CN104863421B (en) * 2015-05-27 2017-03-01 北京航空航天大学 A kind of quick connection lock is determined and unlocking mechanism
CN105133972A (en) * 2015-09-24 2015-12-09 江西洪都航空工业集团有限责任公司 Hook-type lock safety mechanism for aviation cockpit
CN106527088A (en) * 2016-09-06 2017-03-22 江西亿铂电子科技有限公司 Photosensitive element box
CN106527088B (en) * 2016-09-06 2023-09-08 江西亿铂电子科技有限公司 A photosensitive element box
CN109958347A (en) * 2019-04-04 2019-07-02 上海宇航系统工程研究所 A kind of retaining mechanism for tensing and pushing open
CN109958347B (en) * 2019-04-04 2020-07-14 上海宇航系统工程研究所 Locking mechanism capable of being pulled and pushed
CN110700689A (en) * 2019-09-29 2020-01-17 中航通飞研究院有限公司 Cabin door latch mechanism
CN110700689B (en) * 2019-09-29 2022-06-10 中航通飞华南飞机工业有限公司 Cabin door latch mechanism
CN111114782A (en) * 2019-12-29 2020-05-08 宏光空降装备有限公司 Mooring and automatic release lock mounted on side wall
CN111114782B (en) * 2019-12-29 2022-03-22 宏光空降装备有限公司 A tethered, self-release lock mounted on a sidewall
CN113229192A (en) * 2021-05-13 2021-08-10 厦门大学 Frame-type multilayer cultivation box and frame-type multilayer abalone cultivation box
CN115573631A (en) * 2022-10-09 2023-01-06 中国航空工业集团公司西安飞机设计研究所 Aircraft cabin door lock mechanism safety locking mechanism
CN115584897A (en) * 2022-10-09 2023-01-10 中国航空工业集团公司西安飞机设计研究所 A drop-type aircraft cabin door lock mechanism
CN115584897B (en) * 2022-10-09 2024-08-13 中国航空工业集团公司西安飞机设计研究所 Falling type aircraft cabin door lock mechanism
WO2024178776A1 (en) * 2023-02-28 2024-09-06 玉环天润航空机械制造有限公司 Locking mechanism for landing gear door of unmanned aerial vehicle, and door system

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: HANZHONG AIRCRAFT BUBBRANCH, XI'AN AIRCRAFT INTERN

Free format text: FORMER OWNER: SHAANXI AIRCRAFT INDUSTRY (GROUP) CORPORATION LTD.

Effective date: 20121030

C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20121030

Address after: 723213 box 34, Shaanxi, Hanzhoung

Patentee after: Xi'an aircraft, international aviation manufacturing, Limited by Share Ltd, Hanzhoung aircraft branch

Address before: 723213 mailbox, Hanzhoung, Shaanxi, 34

Patentee before: Shaanxi aircraft industry (Group) Co., Ltd.

CX01 Expiry of patent term

Granted publication date: 20081022

CX01 Expiry of patent term