CN106005370A - Quick dismantling device for unmanned aerial vehicle wing - Google Patents
Quick dismantling device for unmanned aerial vehicle wing Download PDFInfo
- Publication number
- CN106005370A CN106005370A CN201610626919.0A CN201610626919A CN106005370A CN 106005370 A CN106005370 A CN 106005370A CN 201610626919 A CN201610626919 A CN 201610626919A CN 106005370 A CN106005370 A CN 106005370A
- Authority
- CN
- China
- Prior art keywords
- wing
- fuselage
- button
- wings
- fixed
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention relates to a quick dismantling device, in particular to a quick dismantling device for unmanned aerial vehicle wings. The structure comprises wings and a fuselage, wing front casing pipes, wing back casing pipes and wing tubular girders are fixed on the wings, and the wing front casing pipes, wing back casing pipes and wing tubular girders are respectively inserted and embedded in corresponding sleeve holes on the fuselage, also the wings and the fuselage are also connected and fixed through a spring snap-fit mechanism. On the basis of meeting the demand of wing and fuselage connection strength, the quick dismantling device for unmanned aerial vehicle wings provided by the invention realizes the purpose of quick dismantling of wings.
Description
Technical field
The present invention 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.The machine of existing part unmanned plane
Body and airfoil member still use the mode of fixing connection, take big quantity space, and hold during packing, transporting and collect
Fragile, transport is got up very inconvenient.Some unmanned planes use insertion airfoil, i.e. wing is installed on fuselage pluggablely,
And be screwed, but the location comparison of screw is hidden, is not easy to dismounting.The unmanned plane wing also having and the connection side of fuselage
Formula adopt be screwed, these fixed form reliabilities of mode that rubber band is fixing the best, easy aged deterioration, dismount loaded down with trivial details, zero
Part is many, thereby results in working performance outside relatively low.
Summary of the invention
In order to solve problem of the prior art, the invention provides a kind of unmanned plane wing device for quickly disassembling, it is meeting wing and machine
On the basis of body bonding strength, it is achieved the purpose of fast assembling-disassembling wing.
The technical solution adopted in the present invention 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 sleeve and
Wing tubular girder, described wing anterior cannula, wing rear sleeve and wing tubular girder are inserted respectively and are embedded in the set hole that fuselage is corresponding
In, connect fixing between described wing and fuselage also by clamp button of the spring mechanism.
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, and described button bar is curved with the button on inner fixing member to be coordinated
Snapping, it is achieved the connection between inner fixing member and extenal fixation part.
The lift of wing, as the force transmission mechanism of wing Yu fuselage, is passed by wing anterior cannula, wing rear sleeve and wing tubular girder
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.In described clamp button of the spring is divided into
Fixture and extenal fixation part, inner fixing member is screwed in the buckle slot corresponding to fuselage, and extenal fixation part is screwed
In the buckle slot that wing is corresponding.
The technical scheme that the present invention provides has the benefit that
The present invention by wing anterior cannula, wing rear sleeve, wing tubular girder and clamp button of the spring with the use of, need not use
Screw, just achieves being reliably connected, further of wing and fuselage, it is achieved that the fast assembling-disassembling of wing and fuselage.
Accompanying drawing explanation
For the technical scheme being illustrated more clearly that in the embodiment of the present invention, in describing embodiment below, required use is attached
Figure is briefly described, it should be apparent that, the accompanying drawing in describing below is only some embodiments of the present invention, for this area
From the point of view of those of ordinary skill, on the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the overall structure schematic diagram of the unmanned plane wing device for quickly disassembling of the present invention；
Fig. 2 is the structural representation of the clamp button of the spring mechanism of the unmanned plane wing device for quickly disassembling of the present invention.
Detailed description of the invention
For making the object, technical solutions and advantages of the present invention clearer, below in conjunction with accompanying drawing embodiment of the present invention made into
One step ground describes in 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
Crossbeam 5 is inserted in the set hole being embedded in fuselage 2 correspondence respectively, also by clamp button of the spring mechanism 6 between described wing 1 and fuselage 2
Connect 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 is fixed on machine
Inner fixing member in body 2, described extenal fixation part includes base 61, and described base 61 front is connected by spring assembly 62 to be had
Button bar 63, described button bar 63 curved with the button on inner fixing member 64 coordinates snapping, it is achieved between inner fixing member and extenal fixation part
Connect.
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 Card
The button bars 63 that the button curved 64 of button inner fixing member clasps extenal fixation part, complete the fixing of wing and fuselage.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all the spirit and principles in the present invention it
In, any modification, equivalent substitution and improvement etc. made, should be included within the scope of the present invention.
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, described base
Front by spring assembly connect have button bar, described button bar is curved with the button on inner fixing member coordinates snapping, it is achieved inner fixing member with
Connection between extenal fixation part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610626919.0A CN106005370A (en) | 2016-08-03 | 2016-08-03 | Quick dismantling device for unmanned aerial vehicle wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610626919.0A CN106005370A (en) | 2016-08-03 | 2016-08-03 | Quick dismantling device for unmanned aerial vehicle wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106005370A true CN106005370A (en) | 2016-10-12 |
Family
ID=57135283
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610626919.0A Pending CN106005370A (en) | 2016-08-03 | 2016-08-03 | Quick dismantling device for unmanned aerial vehicle wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106005370A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107697265A (en) * | 2017-09-11 | 2018-02-16 | 珠海天晴航空航天科技有限公司 | A kind of fuselage wing attachment structure and locking device |
| CN109094767A (en) * | 2018-09-07 | 2018-12-28 | 佛山皖和新能源科技有限公司 | A kind of fixed-wing unmanned plane quick-replaceable wing |
| CN112520011A (en) * | 2020-12-14 | 2021-03-19 | 中宇航通(北京)航空集团有限公司 | Quick-release quick-lock structure and method and unmanned aerial vehicle |
| CN112977797A (en) * | 2021-02-23 | 2021-06-18 | 四川大学 | High-strength light detachable fixed-wing scouting and hitting unmanned aerial vehicle |
| EP4043337A4 (en) * | 2019-09-05 | 2023-01-18 | Autel Robotics Co., Ltd. | Wing-dismounting assembly and aircraft |
-
2016
- 2016-08-03 CN CN201610626919.0A patent/CN106005370A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107697265A (en) * | 2017-09-11 | 2018-02-16 | 珠海天晴航空航天科技有限公司 | A kind of fuselage wing attachment structure and locking device |
| CN109094767A (en) * | 2018-09-07 | 2018-12-28 | 佛山皖和新能源科技有限公司 | A kind of fixed-wing unmanned plane quick-replaceable wing |
| EP4043337A4 (en) * | 2019-09-05 | 2023-01-18 | Autel Robotics Co., Ltd. | Wing-dismounting assembly and aircraft |
| CN112520011A (en) * | 2020-12-14 | 2021-03-19 | 中宇航通(北京)航空集团有限公司 | Quick-release quick-lock structure and method and unmanned aerial vehicle |
| CN112977797A (en) * | 2021-02-23 | 2021-06-18 | 四川大学 | High-strength light detachable fixed-wing scouting and hitting unmanned aerial vehicle |
| CN112977797B (en) * | 2021-02-23 | 2022-02-01 | 四川大学 | High-strength light detachable fixed-wing scouting and hitting unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106005370A (en) | Quick dismantling device for unmanned aerial vehicle wing | |
| CN202707723U (en) | Butt joint structure of connecting rods | |
| CN106477031A (en) | A kind of SUAV landing buffer system | |
| CN205707294U (en) | Folding piece in a kind of horn on Multi-axis aircraft | |
| CN205186520U (en) | Multi -rotor unmanned aerial vehicle detachable support arm | |
| CN205854479U (en) | Unmanned plane wing device for quickly disassembling | |
| CN107757323B (en) | Locking structure | |
| CN109263866A (en) | A kind of unmanned plane drop in water surface floating frame | |
| CN206299660U (en) | A kind of middle-size and small-size unmanned airship hanging quick-release coupling | |
| CN204368408U (en) | For being fixedly connected with the mounting structure of model plane fuselage and wing | |
| CN107140221A (en) | A kind of anti-friction tail apparatus of aircraft and the aircraft with it | |
| CN208775000U (en) | A kind of folding unmanned plane horn and unmanned plane | |
| CN106218855A (en) | Unmanned plane horizontal tail device for quickly disassembling | |
| CN203540064U (en) | Non-gluing wing deck of airplane model | |
| CN203552683U (en) | Miniature portable metronome equipped with support, hang rope and back clip | |
| CN207388774U (en) | Connecting-piece structure in a kind of new energy vehicle suspension | |
| CN205891214U (en) | Wing grafting structure | |
| CN203612217U (en) | Universal hinging device for cable supporting | |
| CN205010476U (en) | Unmanned aerial vehicle's wing is disassembled soon | |
| CN207975358U (en) | A kind of new structural flexible collar | |
| CN105691599A (en) | Undercarriage disassembly and assembly structure of aircraft | |
| CN205854464U (en) | Unmanned plane horizontal tail device for quickly disassembling | |
| CN205707387U (en) | A kind of unmanned plane pair GPS supports | |
| CN205770112U (en) | A kind of power cantilever double location quick lock in fold mechanism | |
| CN204225980U (en) | A kind of automobile exhaust pipe supporting frame |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161012 |
|
| WD01 | Invention patent application deemed withdrawn after publication |