CN205854479U - Unmanned plane wing device for quickly disassembling - Google Patents
Unmanned plane wing device for quickly disassembling Download PDFInfo
- Publication number
- CN205854479U CN205854479U CN201620833677.8U CN201620833677U CN205854479U CN 205854479 U CN205854479 U CN 205854479U CN 201620833677 U CN201620833677 U CN 201620833677U CN 205854479 U CN205854479 U CN 205854479U
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- CN
- China
- Prior art keywords
- wing
- fuselage
- unmanned plane
- quickly disassembling
- rear sleeve
- 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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Abstract
This utility model relates to a kind of device for quickly disassembling, particularly to a kind of unmanned plane wing device for quickly disassembling.Its structure includes wing and fuselage, wing anterior cannula it is fixed with on wing, wing rear sleeve and wing tubular girder, described wing anterior cannula, wing rear sleeve is inserted respectively with wing tubular girder and is embedded in the set hole that fuselage is corresponding, connects fixing between described wing and fuselage also by clamp button of the spring mechanism.A kind of unmanned plane wing device for quickly disassembling of the present utility model, it is on the basis of meeting wing and fuselage bonding strength, it is achieved the purpose of fast assembling-disassembling wing.
Description
Technical field
This utility model relates to a kind of device for quickly disassembling, particularly to a kind of unmanned plane wing device for quickly disassembling.
Background technology
China's unmanned plane field quickly grows in recent years, and the unmanned plane yield of China occupies first place in the world.Existing part is unmanned
The fuselage of machine and airfoil member still use the mode of fixing connection, take big quantity space during packing, transporting and collect,
And being easily damaged, transport is got up very inconvenient.Some unmanned planes use insertion airfoil, i.e. wing is installed to pluggablely
On fuselage, and it is screwed, but the location comparison of screw is hidden, be not easy to dismounting.The unmanned plane wing also having and fuselage
Connected mode adopt be screwed, these fixed form reliabilities of mode that rubber band is fixing the best, easy aged deterioration, dismounting
Loaded down with trivial details, part is many, thereby results in working performance outside relatively low.
Utility model content
In order to solve problem of the prior art, this utility model provides a kind of unmanned plane wing device for quickly disassembling, and it is full
On the basis of foot wing and fuselage bonding strength, it is achieved the purpose of fast assembling-disassembling wing.
The technical scheme that this utility model is used is as follows:
A kind of unmanned plane wing device for quickly disassembling, including wing and fuselage, wing is fixed with wing anterior cannula, wing rear enclosure
Pipe and wing tubular girder, described wing anterior cannula, wing rear sleeve and wing tubular girder insert that to be embedded in fuselage corresponding respectively
Set hole in, connect fixing also by clamp button of the spring mechanism between described wing and fuselage.
Wing tubular girder is between described wing anterior cannula and wing rear sleeve.
Clamp button of the spring mechanism includes the extenal fixation part being fixed in wing and the inner fixing member being fixed in fuselage, described
Extenal fixation part includes base, and described base front is connected by spring assembly button bar, on described button bar and inner fixing member
Detain curved cooperation snapping, it is achieved the connection between inner fixing member and extenal fixation part.
Wing anterior cannula, wing rear sleeve and wing tubular girder are as the force transmission mechanism of wing Yu fuselage, by wing
Lift passes to fuselage.
The effect of clamp button of the spring mechanism is to prevent wing transverse movement, is not involved in the transmission of power between wing and fuselage.
The place that wing and fuselage connect has the buckle slot for fixing described clamp button of the spring mechanism.Described clamp button of the spring
Being divided into inner fixing member and extenal fixation part, inner fixing member is screwed in the buckle slot corresponding to fuselage, extenal fixation part spiral shell
Nail is fixed in the buckle slot that wing is corresponding.
The technical scheme that this utility model provides has the benefit that
This utility model by wing anterior cannula, wing rear sleeve, wing tubular girder and clamp button of the spring with the use of,
Screw need not be used, just achieve being reliably connected, further of wing and fuselage, it is achieved that wing is quickly torn open with fuselage
Dress.
Accompanying drawing explanation
In order to be illustrated more clearly that the technical scheme in this utility model embodiment, required in embodiment being described below
Accompanying drawing to be used is briefly described, it should be apparent that, the accompanying drawing in describing below is only realities more of the present utility model
Execute example, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to according to these accompanying drawings
Obtain other accompanying drawing.
Fig. 1 is the overall structure schematic diagram of unmanned plane wing device for quickly disassembling of the present utility model；
Fig. 2 is the structural representation of the clamp button of the spring mechanism of unmanned plane wing device for quickly disassembling of the present utility model.
Detailed description of the invention
For making the purpose of this utility model, technical scheme and advantage clearer, new to this practicality below in conjunction with accompanying drawing
Type embodiment is described in further detail.
Embodiment one
As shown in Figure 1, a kind of unmanned plane wing device for quickly disassembling, including wing 1 and fuselage 2, wing 1 is fixed with wing
Anterior cannula 3, wing rear sleeve 4 and wing tubular girder 5, described wing anterior cannula 3, wing rear sleeve 4 and wing tubulose are big
Beam 5 is inserted in the set hole being embedded in fuselage 2 correspondence respectively, connects also by clamp button of the spring mechanism 6 between described wing 1 and fuselage 2
Fixing.
In the present embodiment, wing tubular girder 5 is between described wing anterior cannula 3 and wing rear sleeve 4.
As shown in Figure 2, the clamp button of the spring mechanism 6 of the present embodiment includes the extenal fixation part being fixed in wing 1 and fixes
Inner fixing member in fuselage 2, described extenal fixation part includes base 61, and described base 61 front is connected by spring assembly 62
Button bar 63, described button bar 63 curved with the button on inner fixing member 64 is had to coordinate snapping, it is achieved between inner fixing member and extenal fixation part
Connection.
Wing anterior cannula 3, wing rear sleeve 4 and wing tubular girder 5 insert in the set hole of fuselage 2 correspondence, then use spring
The button bars 63 that the button curved 64 of buckle inner fixing member clasps extenal fixation part, complete the fixing of wing and fuselage.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this utility model, all in this practicality
Within novel spirit and principle, any modification, equivalent substitution and improvement etc. made, should be included in guarantor of the present utility model
Within the scope of protecting.
Claims (3)
1. a unmanned plane wing device for quickly disassembling, including wing and fuselage, it is characterised in that be fixed with wing on described wing
Anterior cannula, wing rear sleeve and wing tubular girder, described wing anterior cannula, wing rear sleeve and wing tubular girder are respectively
Insert and be embedded in the set hole that fuselage is corresponding, connect also by clamp button of the spring mechanism fixing between described wing and fuselage.
Unmanned plane wing device for quickly disassembling the most according to claim 1, it is characterised in that described wing tubular girder is positioned at
Between described wing anterior cannula and wing rear sleeve.
Unmanned plane wing device for quickly disassembling the most according to claim 1, it is characterised in that described clamp button of the spring mechanism includes
The extenal fixation part being fixed in wing and the inner fixing member being fixed in fuselage, described extenal fixation part includes base, the described end
Seat front is connected by spring assembly button bar, and described button bar is curved with the button on inner fixing member coordinates snapping, it is achieved interior fixing
Connection between part and extenal fixation part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620833677.8U CN205854479U (en) | 2016-08-03 | 2016-08-03 | Unmanned plane wing device for quickly disassembling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620833677.8U CN205854479U (en) | 2016-08-03 | 2016-08-03 | Unmanned plane wing device for quickly disassembling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205854479U true CN205854479U (en) | 2017-01-04 |
Family
ID=57654827
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620833677.8U Expired - Fee Related CN205854479U (en) | 2016-08-03 | 2016-08-03 | Unmanned plane wing device for quickly disassembling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205854479U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850121A (en) * | 2017-11-28 | 2019-06-07 | 天津天航智远科技有限公司 | A kind of small drone wing and fuselage fast assembling disassembling structure |
| RU2784091C1 (en) * | 2022-07-11 | 2022-11-23 | Общество с ограниченной ответственностью "Научно Инженерная Компания" | Light aircraft wing folding mechanism and wing folding method |
-
2016
- 2016-08-03 CN CN201620833677.8U patent/CN205854479U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850121A (en) * | 2017-11-28 | 2019-06-07 | 天津天航智远科技有限公司 | A kind of small drone wing and fuselage fast assembling disassembling structure |
| RU2785388C1 (en) * | 2022-03-21 | 2022-12-07 | Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации | Foldable wing console for high-speed aircraft |
| RU2784091C1 (en) * | 2022-07-11 | 2022-11-23 | Общество с ограниченной ответственностью "Научно Инженерная Компания" | Light aircraft wing folding mechanism and wing folding method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PP01 | Preservation of patent right |
Effective date of registration: 20181212 Granted publication date: 20170104 |
|
| PP01 | Preservation of patent right | ||
| PD01 | Discharge of preservation of patent |
Date of cancellation: 20201212 Granted publication date: 20170104 |
|
| PD01 | Discharge of preservation of patent | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170104 Termination date: 20180803 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |