CN208053613U - A kind of flying wing type unmanned plane - Google Patents
A kind of flying wing type unmanned plane Download PDFInfo
- Publication number
- CN208053613U CN208053613U CN201820343788.XU CN201820343788U CN208053613U CN 208053613 U CN208053613 U CN 208053613U CN 201820343788 U CN201820343788 U CN 201820343788U CN 208053613 U CN208053613 U CN 208053613U
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- central body
- wing
- unmanned plane
- type unmanned
- wing type
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Abstract
The utility model discloses a kind of flying wing type unmanned planes, including central body, wing and propeller mounted on central body front end, the central body top is equipped with parachute compartment, lower part is equipped with load gondola, the wing can be folded towards central body, and be connected with central body locking when being fully deployed, and the central body lower surface is equipped with sliding block, the sliding block is slidably mounted on ejection orbit, to receive the power for catapult-assisted take-off.This unmanned plane uses flying wing type aerodynamic arrangement, load gondola can carry load flight, when machine itself needs transfer, be placed in babinet by folded wing, it occupies little space, facilitate storage and transport, and sliding block is equipped in central body lower surface, it can the catapult-assisted take-off directly in babinet, after popping up babinet, wing Automatic-expanding and locks again, very convenient, and parachute can be used to recycle.
Description
Technical field
The utility model is related to air vehicle technique field more particularly to a kind of flying wing type unmanned planes.
Background technology
When the wing of huge tailless aircraft is sufficiently large to receive personnel and cargo, fuselage and wing combine together, become
Flying wing.Flying wing is developed by tailless aircraft, without empennage and fuselage, the aircraft of only huge wing, and tool
Have the characteristics that lightweight construction and flight resistance are small, this structure can also be applied on unmanned plane.
Currently, unmanned plane is taking photo by plane, agricultural, express transportation, disaster relief, is observing wild animal, monitoring passes, catching an illness, surveying
It paints, news report, electric inspection process, the disaster relief, the fields such as movies-making have had been more and more widely used, the cost of unmanned plane
Very high, user and businessman are intended to unmanned plane and less accident occur, and since area is larger upon deployment for unmanned plane, occupy fortune
The larger space of load tool causes single freight volume few, increases logistics cost, and wing is easily damaged by collision friction, is made
User and businessman are intended to unmanned plane and less accident occur, and less accident occurs in order to protect, can usually be packaged unmanned plane
Encapsulation, it is to be transported to behind destination, then devan and be transferred on catapult-assisted take-off platform, such working efficiency is very low, time-consuming to take
Power.
Utility model content
In order to overcome the above-mentioned deficiencies of the prior art, the utility model provides a kind of flying wing type unmanned plane, uses winged
Yi Shi aerodynamic arrangements can carry load flight, and when transfer facilitates storage and transport, occupies little space, and catapult-assisted take-off is convenient.
Technical solution is used by the utility model solves its technical problem：
A kind of flying wing type unmanned plane, including central body, wing and the propeller mounted on central body front end, the central body
Top is equipped with parachute compartment, and lower part is equipped with load gondola, and the wing can be folded towards central body, and when being fully deployed in
Body locking connection, the central body lower surface is entreated to be equipped with sliding block, the sliding block is slidably mounted on ejection orbit, to receive
For the power of catapult-assisted take-off.
As an improvement of the above technical solution, the wing outer end is additionally provided with winglet.
As an improvement of the above technical solution, the winglet medial surface connects upper surface of the airfoil, institute by articulation piece
State winglet can around articulation piece fold/on wing.
As an improvement of the above technical solution, the upper surface of the airfoil connects central body upper surface by articulation piece, described
Wing can fold/be stretched on central body around articulation piece.
As an improvement of the above technical solution, the articulation piece is hinge.
As an improvement of the above technical solution, the winglet lateral surface is locked/is detached under wing by latch components
Surface.
As an improvement of the above technical solution, central body following table is locked/be detached to the wing lower surface by latch components
Face.
As an improvement of the above technical solution, the latch components include hook and lock, are equipped with successively on the lock
Press section, torsional spring and hook part, the press section and torsional spring can be respectively acting on hook part so that hook part is detached from and fastens hook.
As an improvement of the above technical solution, the central body rear end is equipped with card slot, for being locked in ejection before ejection
On platform.
As an improvement of the above technical solution, the rear airfoil end is additionally provided with aileron.
The beneficial effects of the utility model have：
This unmanned plane uses flying wing type aerodynamic arrangement, load gondola that can carry load flight, need to shift in machine itself
When, it is placed in babinet, is occupied little space by folded wing, facilitate storage and transport, and be equipped in central body lower surface
Sliding block, can the catapult-assisted take-off directly in babinet, after popping up babinet, wing Automatic-expanding and locks again, very convenient, and can
It is recycled using parachute.
Description of the drawings
Below in conjunction with the accompanying drawings and specific embodiment the utility model is described in further detail, wherein：
Fig. 1 is the structural schematic diagram of the utility model embodiment；
Fig. 2 is another structural schematic diagram of the utility model embodiment；
Fig. 3 is the partial structural diagram of the utility model embodiment；
Fig. 4 is the structural schematic diagram after the utility model embodiment folds.
Specific implementation mode
Referring to Fig. 1, a kind of flying wing type unmanned plane of the utility model, including central body 1, wing 2 and be mounted on central body 1
The propeller 3 of front end, propeller 3 are capable of providing flying power, and 1 top of the central body is equipped with parachute compartment 4, after the completion of flight
It is recycled using parachute, 2 rear end of the wing is additionally provided with aileron 12, manipulates the lifting action of unmanned plane, 2 outer end of the wing is also
Equipped with winglet 8.
With further reference to Fig. 2,1 lower part of central body is equipped with load gondola 5, and load gondola 5 can carry load flight, in described
1 lower surface of body is entreated to be equipped with sliding block 6, the sliding block 6 is slidably mounted on ejection orbit 71, to receive for catapult-assisted take-off
Power, in the present embodiment, sliding block 6 is deposited in a babinet 7, and ejection orbit 71 is laid on the bottom of babinet 7, and box back is also set
There are ejection platform 72,1 rear end of the central body to be equipped with card slot 11, card slot 11 is used to be locked in ejection platform 72 before ejection,
When needing ejection, ejection platform, which first discharges, is detached from card slot 11 so that this unmanned plane can be along ejection rail under the action of thrust
71 catapult-assisted take-off of road.
With further reference to Fig. 4, the wing 2 can be folded towards central body 1, and be locked with central body 1 when being fully deployed
Connection, specifically, 2 upper surface of the wing connect 1 upper surface of central body by articulation piece 10, and the wing 2 can be around articulation piece
10 fold/are stretched on central body 1.Similarly, 8 medial surface of the winglet connects 2 upper surface of wing by articulation piece 10,
The winglet 8 can around articulation piece 10 fold/on wing 2, in the present embodiment, the articulation piece 10 be hinge, when
Before ejection, winglet 8 and wing 2 are folded on central body 1, reduces area occupied, is conveniently stored in babinet 7, is convenient for
Delivery vehicle transports, and can the catapult-assisted take-off directly in babinet.
With further reference to Fig. 3,2 lower surface of the wing passes through 9 lockings of latch components/1 lower surface of disengaging central body；It is described
8 lateral surface of winglet is by 9 lockings of latch components/2 lower surface of disengaging wing, and specifically, the latch components 9 include hook
91 are equipped with press section 921, torsional spring 922 and hook part 923, the press section 921 and torsional spring successively with lock 92, described latch on 92
922 can be respectively acting on hook part 923 so that hook part 923 be detached from and fasten hook 91, when this unmanned plane by high speed release babinet 7 it
Afterwards, wing 2 automatically deploys to state concordant with central body 1 and is locked by latch components 9, and then winglet 8 stretches automatically
With 2 plumbness of wing and locked by latch components 9, achieve the purpose that take off.
The above, the only better embodiment of the utility model, but the utility model is not limited to above-mentioned reality
Example is applied, as long as it reaches the technique effect of the utility model with any same or similar means, should all belong to the utility model
Protection domain.
Claims (10)
1. a kind of flying wing type unmanned plane, it is characterised in that：Including central body, wing and propeller mounted on central body front end,
The central body top is equipped with parachute compartment, and lower part is equipped with load gondola, and the wing can be folded towards central body, and complete
It is connected with central body locking when expansion, the central body lower surface is equipped with sliding block, and the sliding block is slidably mounted in ejection rail
On road, to receive the power for catapult-assisted take-off.
2. a kind of flying wing type unmanned plane according to claim 1, it is characterised in that：It is small that the wing outer end is additionally provided with wing tip
The wing.
3. a kind of flying wing type unmanned plane according to claim 2, it is characterised in that：The winglet medial surface passes through hinge
Fitting connect upper surface of the airfoil, the winglet can around articulation piece fold/on wing.
4. a kind of flying wing type unmanned plane according to claim 1, it is characterised in that：The upper surface of the airfoil passes through articulation piece
Central body upper surface is connected, the wing can fold/be stretched on central body around articulation piece.
5. a kind of flying wing type unmanned plane according to claim 3 or 4, it is characterised in that：The articulation piece is hinge.
6. a kind of flying wing type unmanned plane according to claim 2, it is characterised in that：The winglet lateral surface passes through lock
Buckle assembly locks/it is detached from wing lower surface.
7. a kind of flying wing type unmanned plane according to claim 1, it is characterised in that：The wing lower surface passes through lock group
Central body lower surface is locked/be detached to part.
8. a kind of flying wing type unmanned plane described according to claim 6 or 7, it is characterised in that：The latch components include hook
And lock, be equipped with press section, torsional spring and hook part on the lock successively, the press section and torsional spring can be respectively acting on hook part with
Hook part is set to be detached from and fasten hook.
9. a kind of flying wing type unmanned plane according to claim 1, it is characterised in that：The central body rear end is equipped with card slot,
For being locked in ejection platform before ejection.
10. a kind of flying wing type unmanned plane according to claim 1, it is characterised in that：The rear airfoil end is additionally provided with aileron.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820343788.XU CN208053613U (en) | 2018-03-13 | 2018-03-13 | A kind of flying wing type unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820343788.XU CN208053613U (en) | 2018-03-13 | 2018-03-13 | A kind of flying wing type unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208053613U true CN208053613U (en) | 2018-11-06 |
Family
ID=63988966
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820343788.XU Active CN208053613U (en) | 2018-03-13 | 2018-03-13 | A kind of flying wing type unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208053613U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108394548A (en) * | 2018-03-13 | 2018-08-14 | 珠海天晴航空航天科技有限公司 | A kind of flying wing type unmanned plane |
-
2018
- 2018-03-13 CN CN201820343788.XU patent/CN208053613U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108394548A (en) * | 2018-03-13 | 2018-08-14 | 珠海天晴航空航天科技有限公司 | A kind of flying wing type unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP02 | Change in the address of a patent holder |
Address after: Room 102, floor 1, 3 workshop, No. 6898, Zhuhai Avenue, Hongqi Town, Jinwan District, Zhuhai City, Guangdong Province Patentee after: ZHUHAI TIANQING AEROSPACE TECHNOLOGY Co.,Ltd. Address before: 519000 Guangdong Province, Zhuhai city planning exhibition hall on the third floor of the aviation city Jinwan District 312-30 room Patentee before: ZHUHAI TIANQING AEROSPACE TECHNOLOGY Co.,Ltd. |
|
| CP02 | Change in the address of a patent holder |