CN206502025U - A kind of fixed-wing unmanned plane for adapting to a variety of environment that take off - Google Patents
A kind of fixed-wing unmanned plane for adapting to a variety of environment that take off Download PDFInfo
- Publication number
- CN206502025U CN206502025U CN201720188460.0U CN201720188460U CN206502025U CN 206502025 U CN206502025 U CN 206502025U CN 201720188460 U CN201720188460 U CN 201720188460U CN 206502025 U CN206502025 U CN 206502025U
- Authority
- CN
- China
- Prior art keywords
- wing
- unmanned plane
- take
- fixed
- environment
- 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
Landscapes
- Toys (AREA)
Abstract
The utility model belongs to apparatus field, and in particular to a kind of fixed-wing unmanned plane of a variety of environment that take off of adaptation, including fuselage and wing, it is characterised in that the wing tip of the wing is vertical downwardly directed to ground, is used as the rear undercarriage of support aircraft；The lower front of the fuselage has support straight down, as the nose-gear of support aircraft, and ejection is provided with the support and is hooked, and the strut of fore-and-aft direction extension is fixed with the wing, and the two ends of the strut set elevating screw.Unmanned plane of the present utility model can catapult-assisted take-off, and can be vertically moved up or down, can adapt to a variety of environment that take off.
Description
Technical field
The utility model belongs to technical field of aircraft design, and in particular to a kind of fixed-wing of a variety of environment that take off of adaptation
Unmanned plane.
Background technology
The mode of taking off of fixed-wing unmanned plane is taken off including catapult-assisted take-off and VTOL, and catapult-assisted take-off is needed in unmanned plane
Bottom set ejection to hook, it is relatively light, it is simple to operate, but ejection device is complicated heavy, it is dangerous high, will to place
Ask high.VUAV can adapt to more complicated takeoff and landing environment, but generally have heavy wheeled rise and fall
Frame, adds the extra load weight of aircraft, and adds flight resistance, and fuel consumption is big, and flight efficiency is low.
The content of the invention
The utility model is the defect for catapult-assisted take-off unmanned plane and vertical lift unmanned plane, and research and design one kind is simultaneous
Has the fixed-wing unmanned plane of a variety of environment that take off of the adaptation of catapult-assisted take-off and VTOL.
The utility model solves the technical scheme that its technical problem used：
A kind of fixed-wing unmanned plane for adapting to a variety of environment that take off, including fuselage and wing, it is characterised in that the wing
Wing tip be vertical downwardly directed to ground, be used as support aircraft rear undercarriage；The lower front of the fuselage have it is vertical to
Under support, ejection is provided with as the nose-gear of support aircraft, on the support and is hooked, before being fixed with one on the wing
Rear is to the strut of extension, and the two ends of the strut set elevating screw.
Further, the wing tip of the wing including horizontal wing-body and vertically downward, the strut is arranged on machine
The joining place of the wing and wing tip.
Further, the strut is integrally formed with wing.
Further, the end of the wing tip is plane.
Further, it is characterised in that the ejection hooks the lower end for being arranged on the support.
A kind of beneficial effect of fixed-wing unmanned plane for adapting to a variety of environment that take off of the present utility model is：
1st, catapult-assisted take-off can be realized, vertical lift can be realized again, unmanned plane is suitable for a variety of landing environment that take off.
2nd, the wing tip of wing directly does undercarriage, significantly reduces the weight of vertical lift unmanned plane, reduces flight resistance
Power, improves cruising time and the flight efficiency of unmanned plane.
3rd, strut and wing are integrally formed, and simplify manufacturing process, make that the surface of unmanned plane is more smooth, and streamline is rounder and more smooth,
The stability of unmanned plane appearance is improved, flight resistance is reduced.
Brief description of the drawings
The utility model is described in further detail with reference to the accompanying drawings and detailed description.
Fig. 1 is a kind of fixed-wing unmanned plane structure chart for adapting to a variety of environment that take off of the present utility model.
Wherein：1st, wing, 11, wing tip, 12, wing-body, 2, fuselage, 3, support, 4, ejection hook, 5, strut, 6, lifting
Propeller, 7, tail undercarriage.
Embodiment
The utility model is described in further detail presently in connection with accompanying drawing.These accompanying drawings are simplified schematic diagram,
Only illustrate basic structure of the present utility model in a schematic way, therefore it only shows the composition relevant with the utility model.
A kind of specific implementation for the fixed-wing unmanned plane for adapting to a variety of environment that take off of the present utility model as shown in Figure 1
Example, including fuselage 2 and wing 1, wing 1 include horizontally disposed wing-body 12 and are vertical downwardly directed to the wing tip 11 on ground,
The wing tip 11 of left and right two is as the rear undercarriage for supporting aircraft, and the lower front of fuselage 2 has support 3 straight down, as
Support and ejection hook 4 is provided with the nose-gear of aircraft, support 3, the cohesive position of wing-body 12 and wing tip 11 is provided with
The strut 5 of one fore-and-aft direction extension, the two ends of strut 5 set elevating screw 6.
The rubber band of catapult-launching gear is hung over into ejection to hook on 4, the ejection for launching i.e. achievable unmanned plane using rubber band rises
Fly.If because the influence of flying field is, it is necessary to take off vertically, by starting four lifting spiral shells installed in the rear and front end of strut 5
Rotation oar 6 makes unmanned plane take off vertically, and four elevating screws 6 are closed after taking off, then pass through the tail undercarriage 7 of airplane tail group
Power is provided forward, makes unmanned plane high-speed flight.
In order that the shell of unmanned plane has more preferable curve and a sealing, strut 5, wing 1 and fuselage 2 can integrally into
Type, so both simplifies processing technology, turn avoid welding or the mode such as bolt connection is fixed and gap and connection easily occurs not
Smooth defect.
In order that nose-gear and rear undercarriage it is stable by unmanned plane support on the ground, the wing tip 11 contacted with ground
End be plane, the end of the support 3 contact with ground is also plane.
The rubber band of catapult-launching gear is hung for convenience, and ejection hooks 4 lower ends for being arranged on support 3.
It should be appreciated that specific embodiment described above is only used for explaining the utility model, it is not used to limit this reality
With new.The obvious changes or variations extended out by spirit of the present utility model is still in protection of the present utility model
Among scope.
Claims (5)
1. a kind of fixed-wing unmanned plane for adapting to a variety of environment that take off, including fuselage (2) and wing (1), it is characterised in that described
The wing tip (11) of wing (1) is vertical downwardly directed to ground, is used as the rear undercarriage of support aircraft；The front portion of the fuselage (2)
Lower section has support (3) straight down, as the nose-gear of support aircraft, and ejection is provided with the support (3) and is hooked
(4) strut (5) of fore-and-aft direction extension, is fixed with the wing (1), the two ends of the strut (5) set elevating screws
Oar (6).
2. the fixed-wing unmanned plane according to claim 1 for adapting to a variety of environment that take off, it is characterised in that the wing
(1) wing tip (11) including horizontal wing-body (12) and vertically downward, the strut (5) is arranged on wing (1) and wing tip
(11) joining place.
3. the fixed-wing unmanned plane according to claim 2 for adapting to a variety of environment that take off, it is characterised in that the strut
(5) it is integrally formed with wing (1).
4. a kind of fixed-wing unmanned plane for adapting to a variety of environment that take off according to claim 1, it is characterised in that the wing
The end of sharp (11) is plane.
5. a kind of fixed-wing unmanned plane for adapting to a variety of environment that take off according to claim 1, it is characterised in that the bullet
Penetrate the lower end that hook (4) is arranged on the support (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720188460.0U CN206502025U (en) | 2017-02-28 | 2017-02-28 | A kind of fixed-wing unmanned plane for adapting to a variety of environment that take off |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720188460.0U CN206502025U (en) | 2017-02-28 | 2017-02-28 | A kind of fixed-wing unmanned plane for adapting to a variety of environment that take off |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206502025U true CN206502025U (en) | 2017-09-19 |
Family
ID=59841508
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720188460.0U Active CN206502025U (en) | 2017-02-28 | 2017-02-28 | A kind of fixed-wing unmanned plane for adapting to a variety of environment that take off |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206502025U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045576A (en) * | 2018-01-15 | 2018-05-18 | 缪顺文 | Deformable bionical rotor flapping wing fixed-wing one aircraft |
| CN108583876A (en) * | 2018-04-24 | 2018-09-28 | 北京航空航天大学 | A kind of mechanism of aerial wing tip docking/separation |
-
2017
- 2017-02-28 CN CN201720188460.0U patent/CN206502025U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108045576A (en) * | 2018-01-15 | 2018-05-18 | 缪顺文 | Deformable bionical rotor flapping wing fixed-wing one aircraft |
| CN108583876A (en) * | 2018-04-24 | 2018-09-28 | 北京航空航天大学 | A kind of mechanism of aerial wing tip docking/separation |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201923320U (en) | Twin-engine vertical take-off and landing fixed-wing unmanned aerial vehicle | |
| CN204452934U (en) | The double mode aircraft of rotor, fixed-wing | |
| CN103935509B (en) | One vert quadrotor coordinate hoisting transportation device | |
| CN203005747U (en) | Tilt rotor aircraft | |
| CN107571994B (en) | Aircraft | |
| CN207943165U (en) | A kind of unmanned vehicle and its ascending, descending frame | |
| CN204197290U (en) | A kind of novel tiltrotor aircraft | |
| CN208377055U (en) | A kind of Fixed Wing AirVehicle | |
| CN108791874A (en) | A kind of tilting duct power unmanned vehicle | |
| CN109178301A (en) | A kind of fixed-wing rotor mixing unmanned plane | |
| CN206984353U (en) | A kind of VTOL fixed-wing unmanned plane | |
| CN103786881A (en) | Tilting rotor wing helicopter | |
| CN203638093U (en) | Tiltable four-rotor aircraft | |
| CN206502025U (en) | A kind of fixed-wing unmanned plane for adapting to a variety of environment that take off | |
| CN112340013A (en) | Fixed wing aircraft with tiltable duct | |
| CN112896499A (en) | Vertical take-off and landing aircraft with combined layout of tilting duct and fixed propeller | |
| CN109533319A (en) | A kind of tilting rotor unmanned vehicle structural system with the overlap joint wing | |
| CN209176908U (en) | A kind of rotor fixed-wing unmanned plane of composite drive | |
| CN105523182A (en) | Vertaplane with front tilting rotor wing and rear tilting rotor wing | |
| CN203842313U (en) | Novel remote control model with combination of vertical take-off and landing and level fight characteristic of fixed wing | |
| CN211253017U (en) | Unmanned aerial vehicle with tandem wings capable of vertically taking off and landing | |
| CN203428026U (en) | Small duct-type aircraft | |
| CN211281472U (en) | Duct tail sitting posture VTOL unmanned aerial vehicle | |
| CN206358351U (en) | A kind of wing and the double two axle aircraft verted of engine | |
| CN209209028U (en) | One kind is verted three rotor VTOL all-wing aircraft of type |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230103 Address after: Room 2211, 22nd Floor, Block D, Zhizhen Building, No. 7 Zhichun Road, Haidian District, Beijing 100088 Patentee after: TIANXUN INNOVATION (BEIJING) TECHNOLOGY CO.,LTD. Address before: Building A1, Zhongke entrepreneurship center, Changzhou science and Education City, No.18, middle Changwu Road, Changzhou City, Jiangsu Province, 213000 Patentee before: VOLITATION (CHANGZHOU) INTELLIGENT TECHNOLOGY CO.,LTD. |
|
| TR01 | Transfer of patent right |