CN208963299U - A kind of unmanned plane wing fast assembling disassembling structure - Google Patents
A kind of unmanned plane wing fast assembling disassembling structure Download PDFInfo
- Publication number
- CN208963299U CN208963299U CN201821739338.9U CN201821739338U CN208963299U CN 208963299 U CN208963299 U CN 208963299U CN 201821739338 U CN201821739338 U CN 201821739338U CN 208963299 U CN208963299 U CN 208963299U
- Authority
- CN
- China
- Prior art keywords
- wing
- interconnecting piece
- limit
- unmanned plane
- bolt
- 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.)
- Active
Links
Abstract
The utility model discloses a kind of unmanned plane wing fast assembling disassembling structures, including transmission shaft, propeller, body, wing, body interconnecting piece, threaded hole, bolt, empennage, wing connection, T shape key, through-hole, T-slot, elastic cushion and limited block, the transmission shaft is located at the head of body, and the both ends of transmission shaft are separately connected the propeller of engine body exterior and the motor of internal body, empennage is fixed in the tail portion of body, organism interconnecting piece is fixedly mounted in the two sides of the body, several threaded holes are provided on body interconnecting piece, wing is installed in body interconnecting piece by threaded hole and bolt.The utility model can quickly dismount wing, facilitate the carrying of long span fixed-wing unmanned plane.
Description
Technical field
The utility model relates to Flight Vehicle Structure fields, more particularly, to a kind of unmanned plane wing fast assembling disassembling structure.
Background technique
Unmanned plane is using the not manned aircraft of radio robot and the presetting apparatus provided for oneself manipulation, usually
The equipment such as automatic pilot, presetting apparatus are installed.Ground staff can track it by equipment such as radars, is fixed
Position, remote control, telemetering and Digital Transmission, therefore it is widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..It is small
Type unmanned plane is for general unmanned plane, other than having the advantages that unmanned plane, also because its size is smaller, using spirit
The advantages such as living are more widely used.
Unmanned plane is generally divided into three classes: single rotor, more rotors, fixed-wing unmanned plane.Wherein, fixed-wing unmanned plane has boat
The advantages of duration, speed are fast, flight efficiency height etc., is widely used.In order to increase fixed-wing unmanned plane load carrying behaviour, it is lengthened
Spanwise length is common method, although increasing the lifting capacity of unmanned plane in this way, also increases fixed-wing unmanned plane
Carrying difficulty, for fixed-wing unmanned plane heavy-duty flight increase threshold.For the ease of carry long span fixed-wing nobody
It is most important to design a kind of fast assembling disassembling structure for machine.
Utility model content
The utility model is to overcome above situation insufficient, it is desirable to provide a kind of technical solution that can solve the above problem.
A kind of unmanned plane wing fast assembling disassembling structure, including transmission shaft, propeller, body, wing, body interconnecting piece, spiral shell
Bolt, empennage, limiting slot, position line, limit tenon, limited block, installation sheet and limit mortise, the transmission shaft are located at the head of body
Portion, and the both ends of transmission shaft are separately connected the propeller of engine body exterior and the motor of internal body, fix in the tail portion of body
There is empennage, organism interconnecting piece is fixedly mounted in the two sides of the body, and several threaded holes are provided on body interconnecting piece, are passed through
Threaded hole and bolt install wing in body interconnecting piece.
As a further solution of the present invention: the wing includes limiting slot, position line and limit tenon, the limit
Position slot position is decorated with position line in the junction of airfoil root and wing-body in the root of wing, and at the edge of airfoil root
Place is equipped with limit tenon.
As a further solution of the present invention: the body interconnecting piece include limited block, installation sheet and limit mortise,
It is provided with card slot in the side of body interconnecting piece, limited block is installed in card slot, which is mounted on bolt by installation sheet
On, and the limit mortise matched with limit tenon is provided on the inside of card slot.
As a further solution of the present invention: it is cased with elastic washer in the threaded post of the bolt, the elastic washer
Between the head and body interconnecting piece of bolt.
As a further solution of the present invention: the empennage is welded on the tail portion of body.
Compared with prior art, the utility model has the beneficial effects that
The utility model can quickly dismount wing, facilitate the carrying of long span fixed-wing unmanned plane.
The additional aspect and advantage of the utility model will be set forth in part in the description, partially will be from following description
In become obvious, or recognized by the practice of the utility model.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, before not making the creative labor property
It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is the utility model structure diagram.
Fig. 2 is the structural schematic diagram of wing connection in the utility model.
Fig. 3 is the structural schematic diagram of body interconnecting piece in the utility model.
In figure: transmission shaft 1, body 3, wing 4, body interconnecting piece 5, bolt 6, empennage 7, limiting slot 41, is determined propeller 2
Bit line 42, limit tenon 43, limited block 51, installation sheet 52 and limit mortise 53.
Specific embodiment
Below by the technical scheme in the utility model embodiment is clearly and completely described, it is clear that described
Embodiment is only the utility model a part of the embodiment, instead of all the embodiments.Based on the implementation in the utility model
Example, every other embodiment obtained by those of ordinary skill in the art without making creative efforts belong to
The range of the utility model protection.
Please refer to Fig. 1~3, in the utility model embodiment, a kind of unmanned plane wing fast assembling disassembling structure, including transmission shaft
1, propeller 2, body 3, wing 4, body interconnecting piece 5, bolt 6, empennage 7, limiting slot 41, position line 42, limit tenon 43, limit
Position block 51, installation sheet 52 and limit mortise 53, the transmission shaft 1 is located at the head of body 3, and the both ends of transmission shaft 1 connect respectively
The motor inside propeller 2 and body 3 to pick outside body 3, is fixed with empennage 7 in the tail portion of body 3, the body 3
Organism interconnecting piece 5 is fixedly mounted in two sides, and several threaded holes are provided on body interconnecting piece 5, is existed by threaded hole and bolt 6
Wing 4 is installed in body interconnecting piece 5.
The wing 4 includes that limiting slot 41, position line 42 and limit tenon 43, the limiting slot 41 are located at the root of wing 4
It is decorated with position line 42 in the junction of 4 root of wing and 4 main body of wing, and is equipped with limit tenon in the edge of 4 root of wing in portion
First 43.
The body interconnecting piece 5 includes limited block 51, installation sheet 52 and limit mortise 53, in the side of body interconnecting piece 5
It is provided with card slot, limited block 51 is installed in card slot, which is mounted on bolt 6 by installation sheet 52, and in card slot
Inside on be provided with and the limit mortise 53 that matches of limit tenon 43.
It is cased with elastic washer in the threaded post of the bolt 6, which is located at head and the body interconnecting piece of bolt 6
Between 5.
The empennage 8 is welded on the tail portion of body 3.
The working principle of the utility model is:
It is matched by the limit tenon 43 on the limit mortise 53 and wing 4 on body interconnecting piece 5 and is mounted on wing 4
On body 3, the depth that wing 4 is inserted into body interconnecting piece 5 is adjusted by observation position line 42.When wing 4 is inserted into body connection
In portion 5 when suitable position, then bolt 6 is screwed down on body interconnecting piece 5, so that bolt 6 drives limit by installation sheet 52
Position block 51 moves down, and final limited block 51 is caught in limiting slot 41.Pass through limit mortise 53 and limit tenon 43 and limit
Wing 4 is fixed on body 3 by the collective effect of block 51 and limiting slot 41.
When needing to remove wing 4, bolt 6 is turned upwards on body interconnecting piece 5, so that limited block 51 rises, work as limit
After position block 51 is detached from limiting slot 41, wing 4 is extracted outward, makes to limit tenon 43 and limit mortise 53 to be detached from.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and
And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in
All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting
Related claim.
Claims (5)
1. a kind of unmanned plane wing fast assembling disassembling structure, including transmission shaft, propeller, body, wing, body interconnecting piece, bolt,
Empennage, limiting slot, position line, limit tenon, limited block, installation sheet and limit mortise, which is characterized in that the transmission shaft is located at
The head of body, and the both ends of transmission shaft are separately connected the propeller of engine body exterior and the motor of internal body, in body
Tail portion is fixed with empennage, and organism interconnecting piece is fixedly mounted in the two sides of the body, and several spiral shells are provided on body interconnecting piece
Pit installs wing in body interconnecting piece by threaded hole and bolt.
2. unmanned plane wing fast assembling disassembling structure according to claim 1, which is characterized in that the wing includes limit
Slot, position line and limit tenon, the limiting slot are located at the root of wing, are decorated in the junction of airfoil root and wing-body
Position line, and limit tenon is equipped in the edge of airfoil root.
3. unmanned plane wing fast assembling disassembling structure according to claim 1, which is characterized in that the body interconnecting piece includes
Limited block, installation sheet and limit mortise, are provided with card slot in the side of body interconnecting piece, limited block are equipped in card slot, the limit
Position block is mounted on bolt by installation sheet, and the limit mortise matched with limit tenon is provided on the inside of card slot.
4. unmanned plane wing fast assembling disassembling structure according to claim 1, which is characterized in that in the threaded post of the bolt
It is cased with elastic washer, which is located between the head and body interconnecting piece of bolt.
5. unmanned plane wing fast assembling disassembling structure according to claim 1, which is characterized in that the empennage is welded on body
Tail portion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821739338.9U CN208963299U (en) | 2018-10-26 | 2018-10-26 | A kind of unmanned plane wing fast assembling disassembling structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821739338.9U CN208963299U (en) | 2018-10-26 | 2018-10-26 | A kind of unmanned plane wing fast assembling disassembling structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208963299U true CN208963299U (en) | 2019-06-11 |
Family
ID=66761392
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821739338.9U Active CN208963299U (en) | 2018-10-26 | 2018-10-26 | A kind of unmanned plane wing fast assembling disassembling structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208963299U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111366043A (en) * | 2020-03-23 | 2020-07-03 | 上海机电工程研究所 | Missile wing connecting structure suitable for releasing thermal stress |
| WO2021043336A3 (en) * | 2019-09-05 | 2021-04-22 | 深圳市道通智能航空技术股份有限公司 | Wing detachment assembly and aircraft |
| CN113247235A (en) * | 2021-06-10 | 2021-08-13 | 佛山智壹科技有限公司 | Unmanned plane |
| CN113401329A (en) * | 2020-03-16 | 2021-09-17 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle wing quick assembly disassembly mechanism and have its unmanned aerial vehicle |
| CN114291257A (en) * | 2022-01-24 | 2022-04-08 | 歌尔科技有限公司 | Unmanned aerial vehicle |
-
2018
- 2018-10-26 CN CN201821739338.9U patent/CN208963299U/en active Active
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021043336A3 (en) * | 2019-09-05 | 2021-04-22 | 深圳市道通智能航空技术股份有限公司 | Wing detachment assembly and aircraft |
| EP4023548A4 (en) * | 2019-09-05 | 2023-01-25 | Autel Robotics Co., Ltd. | Wing detachment assembly and aircraft |
| CN113401329A (en) * | 2020-03-16 | 2021-09-17 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle wing quick assembly disassembly mechanism and have its unmanned aerial vehicle |
| CN113401329B (en) * | 2020-03-16 | 2023-03-14 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle wing quick assembly disassembly mechanism and have its unmanned aerial vehicle |
| CN111366043A (en) * | 2020-03-23 | 2020-07-03 | 上海机电工程研究所 | Missile wing connecting structure suitable for releasing thermal stress |
| CN113247235A (en) * | 2021-06-10 | 2021-08-13 | 佛山智壹科技有限公司 | Unmanned plane |
| CN114291257A (en) * | 2022-01-24 | 2022-04-08 | 歌尔科技有限公司 | Unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208963299U (en) | A kind of unmanned plane wing fast assembling disassembling structure | |
| CN207917151U (en) | Oily electricity mixing VTOL fixed-wing unmanned plane | |
| US4067518A (en) | Drag reducer for lift surface of aircraft | |
| CN204507257U (en) | A kind of fuel power multi-rotor aerocraft | |
| CN208053611U (en) | Efficient electric gliding unmanned plane | |
| CN205221105U (en) | Solar energy VTOL fixed wing uavs | |
| CN203544372U (en) | Fixed-wing aircraft additionally provided with cross-flow fan | |
| CN204310050U (en) | Many bodies can divide unmanned plane | |
| CN110816806A (en) | Cluster type bionic solar unmanned aerial vehicle | |
| CN204473119U (en) | Lightweight unmanned plane | |
| CN204368408U (en) | For being fixedly connected with the mounting structure of model plane fuselage and wing | |
| CN204433031U (en) | Portable fast assembling-disassembling unmanned plane | |
| CN202449217U (en) | Recycling mechanism for controlling unmanned aerial vehicle through deep stall | |
| CN206704550U (en) | To the depopulated helicopter fuselage interior structure of arrangement after a kind of turboaxle motor | |
| CN109815528A (en) | A method of the aircraft parameters optimization based on large-scale composite wing gas | |
| CN209553482U (en) | Total lift body solar energy unmanned vehicle | |
| CN206766336U (en) | A kind of aircraft that can prevent from being caught by birds | |
| CN209479973U (en) | A kind of cross flow fan lift-rising autogyro | |
| CN208963301U (en) | A kind of unmanned plane folding wing | |
| CN208419754U (en) | High speed per hour unmanned plane target drone | |
| CN203698646U (en) | Flying wing imitating rapidly ascending unmanned plane | |
| CN204473125U (en) | The unmanned plane of flight stability | |
| CN205388979U (en) | Battery structure for unmanned aerial vehicle | |
| CN206243438U (en) | Integration inclines horn | |
| CN209535457U (en) | A kind of unmanned plane rotor |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 045000 Nan'ao Village Exit, Guanshan Town, Pingding County, Yangquan City, Shanxi Province Patentee after: Shanxi Henghe Baiwang Intelligent Technology Co.,Ltd. Address before: Guan Shan Zhen Nan Ao Cun, Pingding County, Yangquan City, Shanxi Province 045200 Patentee before: SHANXI HENGHE TRADING CO.,LTD. |
|
| CP03 | Change of name, title or address |