CN206502016U - A kind of all-wing aircraft unmanned plane of vertical lift - Google Patents
A kind of all-wing aircraft unmanned plane of vertical lift Download PDFInfo
- Publication number
- CN206502016U CN206502016U CN201720188153.2U CN201720188153U CN206502016U CN 206502016 U CN206502016 U CN 206502016U CN 201720188153 U CN201720188153 U CN 201720188153U CN 206502016 U CN206502016 U CN 206502016U
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- wing
- unmanned plane
- support
- vertical lift
- aircraft
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Abstract
The utility model belongs to apparatus field, and in particular to a kind of all-wing aircraft unmanned plane of vertical lift, 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, is used as the nose-gear of support aircraft.Unmanned plane of the present utility model is by the use of the wing tip and support of wing as undercarriage, and small volume is lightweight, and simple in construction, flight resistance is small, improves cruising time and the flight efficiency of vertical lift unmanned plane.
Description
Technical field
The utility model belongs to technical field of aircraft design, and in particular to a kind of all-wing aircraft unmanned plane of vertical lift.
Background technology
With developing rapidly for unmanned air vehicle technique field, VTOL all-wing aircraft unmanned plane also slowly rises, and traditional is vertical
Landing all-wing aircraft unmanned plane uses wheel undercarriage and independent vertical tail, for the aircraft that weight demands are strict, undercarriage
As extra heavy burden, flight resistance is added, the ejecting type unmanned plane without undercarriage does not possess vertical lift ability again.
The content of the invention
The problem of the utility model is for vertical lift all-wing aircraft unmanned plane undercarriage heaviness, and a kind of structure of research and design
Simply, the all-wing aircraft unmanned plane of the small vertical lift of flight resistance.
The utility model solves the technical scheme that its technical problem used：
A kind of all-wing aircraft unmanned plane of vertical lift, including fuselage and wing, it is characterised in that the wing tip of the wing is vertical
Downwardly directed ground, is used as the rear undercarriage of support aircraft；The lower front of the fuselage has support straight down, makees
To support the nose-gear of aircraft.
Further, the strut of fore-and-aft direction extension is fixed with the wing, the two ends of the strut set lifting
Propeller.
Further, there is the ejection for being used for making unmanned aerial vehicle ejecting take off to hook for the lower end of the support.
Further, the end of the wing tip is plane.
A kind of beneficial effect of the all-wing aircraft unmanned plane of vertical lift of the present utility model is：
1st, wing tip vertically downward and the support being arranged on below fore-body are regard as the undercarriage of unmanned plane, undercarriage
Small volume, it is lightweight, and do not increase flight resistance substantially, improve cruising time and the flight efficiency of unmanned plane.
2nd, set ejection to hook on support, unmanned plane is realized catapult-assisted take-off and can be vertically moved up or down, adapt to a variety of
Fly landing environment.
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 all-wing aircraft unmanned plane structure chart of vertical lift 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 embodiment of the all-wing aircraft unmanned plane of vertical lift of the present utility model as shown in Figure 1, including fuselage 2
With wing 1, wing 1 includes horizontally disposed wing-body 12 and is vertical downwardly directed to the wing tip 11 on ground, the wing tip 11 of left and right two
As the rear undercarriage of support aircraft, the lower front of fuselage 2 has support 3 straight down, is used as support aircraft
It is provided with nose-gear, support 3 and launches hook 4, the cohesive position of wing-body 12 and wing tip 11 is provided with a fore-and-aft direction and prolonged
The strut 5 stretched, 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 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 (4)
1. a kind of all-wing aircraft unmanned plane of vertical lift, including fuselage (2) and wing (1), it is characterised in that the wing (1)
Wing tip (11) is vertical downwardly directed to ground, is used as the rear undercarriage of support aircraft；The lower front of the fuselage (2) has perpendicular
Straight downward support (3), is used as the nose-gear of support aircraft.
2. the all-wing aircraft unmanned plane of vertical lift according to claim 1, it is characterised in that be fixed with the wing (1)
The strut (5) of one fore-and-aft direction extension, the two ends of the strut (5) set elevating screw (6).
3. the all-wing aircraft unmanned plane of vertical lift according to claim 1, it is characterised in that the lower end of the support, which has, to be used
Come the ejection hook for making unmanned aerial vehicle ejecting take off.
4. a kind of all-wing aircraft unmanned plane of vertical lift according to claim 1, it is characterised in that the end of the wing tip (11)
Portion is plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720188153.2U CN206502016U (en) | 2017-02-28 | 2017-02-28 | A kind of all-wing aircraft unmanned plane of vertical lift |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720188153.2U CN206502016U (en) | 2017-02-28 | 2017-02-28 | A kind of all-wing aircraft unmanned plane of vertical lift |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206502016U true CN206502016U (en) | 2017-09-19 |
Family
ID=59841608
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720188153.2U Active CN206502016U (en) | 2017-02-28 | 2017-02-28 | A kind of all-wing aircraft unmanned plane of vertical lift |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206502016U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113352823A (en) * | 2021-04-14 | 2021-09-07 | 南京理工大学 | Ejection fly-back device for land-air flight |
-
2017
- 2017-02-28 CN CN201720188153.2U patent/CN206502016U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113352823A (en) * | 2021-04-14 | 2021-09-07 | 南京理工大学 | Ejection fly-back device for land-air flight |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230105 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 |