CN204041666U - A kind of quick-detachable lock with sealing function - Google Patents

A kind of quick-detachable lock with sealing function Download PDF

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Publication number
CN204041666U
CN204041666U CN201420518524.5U CN201420518524U CN204041666U CN 204041666 U CN204041666 U CN 204041666U CN 201420518524 U CN201420518524 U CN 201420518524U CN 204041666 U CN204041666 U CN 204041666U
Authority
CN
China
Prior art keywords
lock body
quick
detachable
sealing function
lock
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 - Fee Related
Application number
CN201420518524.5U
Other languages
Chinese (zh)
Inventor
谢明洁
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 Hangtai Precision Manufacturing Co Ltd
Original Assignee
Guizhou Hangtai Precision Manufacturing 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 Hangtai Precision Manufacturing Co Ltd filed Critical Guizhou Hangtai Precision Manufacturing Co Ltd
Priority to CN201420518524.5U priority Critical patent/CN204041666U/en
Application granted granted Critical
Publication of CN204041666U publication Critical patent/CN204041666U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

Have a quick-detachable lock for sealing function, comprise upper lock body, stopper ring, lid panel, framework, down lock body, described upper lock body is located at lid panel surrounding by stopper ring, and down lock body is riveted on the framework of aircraft; Described down lock body is provided with seal closure.The utility model compared with the prior art, the basis of common quick-detachable lock increases seal closure, adds the sealing function of quick-detachable lock, effectively can completely cut off in cabin, expand the Applicable scope of quick-detachable lock out of my cabin; Structure is simple, by force functional, and easy to implement, effect is safe and reliable; Various machinery industry can be popularized and applied to, have good economic benefit and social benefit.

Description

A kind of quick-detachable lock with sealing function
Technical field
The utility model relates to a kind of quick-detachable lock with sealing function, belongs to organism component technical field.
Background technique
Quick-detachable lock is mainly used in the fixing of stressed less, the lid of repeatedly opening of aircraft and cabin inner electronic equipment, mainly plays the effect of quick-release and locking stop.The upper lock body of existing quick-detachable lock is arranged on lid panel surrounding by stopper ring, and down lock body is riveted on the framework of aircraft, and during installation, the position of upper lock body is corresponding with down lock body.When filling the lid of aircraft, the upper lock body of lid surrounding being aimed at the core bore of down lock body on aircraft, realizing unlatching and the locking of lid by rotating upper lock body.
Owing to there is gap between the upper lock body of common quick-detachable lock and down lock body, the thing such as rainwater, dust can not be stoped to enter in cabin, therefore can only to limit in cabin and without the lid of seal request.
Model utility content
The purpose of this utility model is to overcome deficiency of the prior art, thus provides a kind of quick-detachable lock with sealing function.
Have a quick-detachable lock for sealing function, comprise upper lock body, stopper ring, lid panel, framework, down lock body, described upper lock body is located at lid panel surrounding by stopper ring, and down lock body is riveted on the framework of aircraft; Described down lock body is provided with seal closure.
The beneficial effect of employing technique scheme is:
1. the utility model compared with the prior art, and the basis of common quick-detachable lock increases seal closure, adds the sealing function of quick-detachable lock, effectively can completely cut off in cabin, expand the Applicable scope of quick-detachable lock out of my cabin.
2. the utility model structure is simple, by force functional, and easy to implement, effect is safe and reliable.
3. the utility model can be popularized and applied to various machinery industry, has good economic benefit and social benefit.
Accompanying drawing explanation
Fig. 1 is quick-detachable lock lock body structure schematic diagram in prior art.
In figure: 1-upper lock body, 2-stopper ring, 3-lid panel, 4-framework, 5-down lock body.
Fig. 2 is the quick-detachable lock structural representation that the utility model has sealing function.
In figure: 1-upper lock body, 2-stopper ring, 3-lid panel, 4-framework, 5-down lock body, 6-seal closure.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described in further detail:
Have a quick-detachable lock for sealing function, as shown in Figure 2, comprise upper lock body 1, stopper ring 2, lid panel 3, framework 4, down lock body 5, described upper lock body 1 is located at lid panel 3 surrounding by stopper ring 2, and down lock body 5 is riveted on the framework 4 of aircraft; Described down lock body 5 is provided with seal closure 6, is adopted by seal closure 6 the mode full weld of welding on down lock body 5, makes lock body form sealing, is entered in cabin to prevent the thing such as rainwater, dust by upper lock body through down lock body.

Claims (1)

1. one kind has the quick-detachable lock of sealing function, comprise upper lock body (1), stopper ring (2), lid panel (3), framework (4), down lock body (5), described upper lock body (1) is located at lid panel (3) surrounding by stopper ring (2), and down lock body (5) is riveted on the framework (4) of aircraft; It is characterized in that: described down lock body (5) is provided with seal closure (6).
CN201420518524.5U 2014-09-11 2014-09-11 A kind of quick-detachable lock with sealing function Expired - Fee Related CN204041666U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420518524.5U CN204041666U (en) 2014-09-11 2014-09-11 A kind of quick-detachable lock with sealing function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420518524.5U CN204041666U (en) 2014-09-11 2014-09-11 A kind of quick-detachable lock with sealing function

Publications (1)

Publication Number Publication Date
CN204041666U true CN204041666U (en) 2014-12-24

Family

ID=52242335

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420518524.5U Expired - Fee Related CN204041666U (en) 2014-09-11 2014-09-11 A kind of quick-detachable lock with sealing function

Country Status (1)

Country Link
CN (1) CN204041666U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105089393A (en) * 2015-08-07 2015-11-25 中国航天空气动力技术研究院 Non-bearing quick-release lock of small unmanned aerial vehicle
CN108945385A (en) * 2018-07-06 2018-12-07 江西洪都航空工业集团有限责任公司 A kind of economic simple quick-release lid

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105089393A (en) * 2015-08-07 2015-11-25 中国航天空气动力技术研究院 Non-bearing quick-release lock of small unmanned aerial vehicle
CN105089393B (en) * 2015-08-07 2017-03-22 中国航天空气动力技术研究院 Non-bearing quick-release lock of small unmanned aerial vehicle
CN108945385A (en) * 2018-07-06 2018-12-07 江西洪都航空工业集团有限责任公司 A kind of economic simple quick-release lid

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20141224

Termination date: 20200911

CF01 Termination of patent right due to non-payment of annual fee