CN207106845U - A kind of stealthy unmanned plane for extending cruising time - Google Patents
A kind of stealthy unmanned plane for extending cruising time Download PDFInfo
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- CN207106845U CN207106845U CN201721063507.7U CN201721063507U CN207106845U CN 207106845 U CN207106845 U CN 207106845U CN 201721063507 U CN201721063507 U CN 201721063507U CN 207106845 U CN207106845 U CN 207106845U
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- main wing
- electric expansion
- unmanned plane
- aileron
- fuselage
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Abstract
The utility model discloses a kind of stealthy unmanned plane for extending cruising time, it is related to unmanned plane field, and it is short to solve the current unmanned plane during flying time, is not suitable for long-distance flight；When running into air blast, because unmanned plane deadweight is small, therefore its state of flight is easily by airflow influence.The utility model includes fuselage, main wing, aileron, electric expansion plate and electric expansion bar, main wing is arranged on fuselage, aileron is arranged on main wing, electric expansion plate is arranged in main wing, the both ends of electric expansion bar are separately mounted on main wing and aileron, main wing, aileron and electric expansion plate are provided with solar panels, can be longer by the solar energy generation electric energy flight time of the present utility model, and stronger flight stability can be provided after electric expansion plate and aileron expansion.
Description
Technical field
It the utility model is related to unmanned plane field, and in particular to a kind of stealthy unmanned plane for extending cruising time.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates, or fully or intermittently independently operated by car-mounted computer.With someone
Drive an airplane and compare, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane presses application field,
Can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application, it is
Unmanned plane has really just needed；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation it is wild dynamic
The application in thing, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, greatly
Big has expanded the purposes of unmanned plane in itself, and developed country is also in actively extension sector application and development unmanned air vehicle technique.At present
The unmanned plane during flying time it is short, be not suitable for long-distance flight；When running into air blast, because unmanned plane deadweight is small, therefore it flies
Row state is easily by airflow influence.
Utility model content
The utility model purpose is to solve the current unmanned plane during flying time short, is not suitable for long-distance flight；When running into
During air blast, because unmanned plane deadweight is small, therefore its state of flight is easily by airflow influence.In view of the above-mentioned problems, this practicality is new
Type provides a kind of stealthy unmanned plane for extending cruising time, when it is applied can long-distance flight, and when running into air blast
It is not easy by airflow influence itself state of flight.
The purpose of this utility model is achieved through the following technical solutions：
A kind of stealthy unmanned plane for extending cruising time, including fuselage, electric expansion plate and electric expansion bar, the machine
Main wing is provided with it, and the main wing is provided with empennage across fuselage, the afterbody of the fuselage, and the electric expansion plate is fixed on main wing
On, the both ends of the main wing are symmetrically hinged a pair of ailerons, and the fixing end of the electric expansion bar is arranged on main wing, described electronic
The telescopic end of expansion link is arranged on aileron, and the upper surface of the main wing, aileron and electric expansion plate is equipped with solar panels.
Electric expansion plate can be packed up in take-off process and be changed into one block of plate and take in main wing by the utility model, and will
Aileron is folded up；In flight course, electric expansion plate is stretched out into main wing and expands into plurality of plates, and passes through electric expansion bar
Aileron is unfolded to coplanar with main wing, electric expansion plate is conllinear with the center of gravity of main wing and fuselage, the electric expansion plate now deployed
With aileron so that the utility model is bigger with air contact area, more preferable flight stability can be provided for the utility model, and
And the solar panels above main wing, aileron and electric expansion plate can provide solar energy for the utility model to be converted to electric energy, make
Obtain the flight time of the present utility model and flying distance is longer.
Further, the lower section of the fuselage is equipped with undercarriage, and the undercarriage includes roller, and undercarriage and roller are used for
So that the utility model can rise and fall on the ground.
Further, the lower section of the empennage is equipped with steering wheel, and steering wheel is loaded can save for steering on empennage
Undercarriage so that structure of the present utility model is more simple.
Further, multiple propellers are housed on the main wing, it is dynamic for awing providing flight for the utility model
Power.
Further, laser camouflage is scribbled in the fuselage, main wing, aileron, electric expansion plate, empennage and electric expansion bar
Material, radar invisible function can be realized in flight.
Further, the material of the fuselage, main wing, aileron, electric expansion plate, empennage and electric expansion bar is fine using carbon
Dimension, the material can also ensure that the utility model integrally has foot while ensureing that the overall weight of the utility model is light enough
Enough hardness.
By using the utility model, following beneficial effect can be produced：The utility model include fuselage, main wing, aileron,
Electric expansion plate and electric expansion bar, main wing are arranged on fuselage, and aileron is arranged on main wing, and electric expansion plate is arranged on main wing
In, the both ends of electric expansion bar are separately mounted on main wing and aileron, and main wing, aileron and electric expansion plate are provided with solar energy
Plate, can be longer by the solar energy generation electric energy flight time of the present utility model, energy after electric expansion plate and aileron expansion
Stronger flight stability is provided.
Brief description of the drawings
Accompanying drawing described herein is used for providing further understanding the utility model embodiment, forms the one of the application
Part, the restriction to the utility model embodiment is not formed.In the accompanying drawings：
Fig. 1 is part-structure cut-away view of the present utility model.
Mark and corresponding parts title in accompanying drawing：1- main wings, 2- empennages, 20- steering wheels, 3- fuselages, 4- is electronic to be stretched
Contracting plate, 6- electric expansion bars, 7- ailerons, 8- propellers, 9- undercarriages.
Embodiment
For the purpose of this utility model, technical scheme and advantage is more clearly understood, with reference to embodiment and accompanying drawing,
The utility model is described in further detail, and exemplary embodiment of the present utility model and its explanation are only used for explaining this
Utility model, it is not intended as to restriction of the present utility model.
As shown in figure 1, a kind of stealthy unmanned plane for extending cruising time, including fuselage 3, electric expansion plate 4 and electronic
Expansion link 6, fuselage 3 are provided with main wing 1, and main wing 1 is equipped with multiple propellers 8 on fuselage 3, main wing 1, and the afterbody of fuselage 3 is set
There is empennage 2, the lower section of empennage 2 is equipped with steering wheel 20, and electric expansion plate 4 is fixed on main wing 1, and the both ends of main wing 1 are symmetrically hinged
A pair of ailerons 7, the fixing end of electric expansion bar 6 are arranged on main wing 1, and the telescopic end of electric expansion bar 6 is arranged on aileron 7,
The upper surface of main wing 1, aileron 7 and electric expansion plate 4 is equipped with solar panels.The lower section of fuselage 3 is equipped with undercarriage 9, and undercarriage 9 wraps
Include roller.Doping induced by laser is scribbled in fuselage 3, main wing 1, aileron 7, electric expansion plate 4, empennage 2 and electric expansion bar 6.Machine
Body 3, main wing 1, aileron 7, electric expansion plate 4, the material of empennage 2 and electric expansion bar 6 use carbon fiber.
Preferably, main wing 1 and electric expansion plate 4 are in the same plane, and empennage 2 and main wing 1 are orthogonal.In order to save
Cost, undercarriage 9 need not make contractile undercarriage.During flight is glided, aileron 7 and main wing 1 are in obtuse angle；Taking off
During, aileron 7 and main wing 1 are at an acute angle.
Above-described embodiment, the purpose of this utility model, technical scheme and beneficial effect are entered
One step describes in detail, should be understood that and the foregoing is only specific embodiment of the present utility model, is not used to limit
Determine the scope of protection of the utility model, it is all within the spirit and principles of the utility model, any modification for being made, equally replace
Change, improve, should be included within the scope of protection of the utility model.
Claims (6)
1. a kind of stealthy unmanned plane for extending cruising time, it is characterised in that including fuselage (3), electric expansion plate (4) and electricity
Dynamic expansion link (6), the fuselage (3) are provided with main wing (1), and the main wing (1) is across fuselage (3), the afterbody of the fuselage (3)
Provided with empennage (2), the electric expansion plate (4) is fixed on main wing (1), and the both ends of the main wing (1) are symmetrically hinged a pair of pairs
The wing (7), the fixing end of the electric expansion bar (6) are arranged on main wing (1), the telescopic end installation of the electric expansion bar (6)
On aileron (7), the upper surface of the main wing (1), aileron (7) and electric expansion plate (4) is equipped with solar panels.
A kind of 2. stealthy unmanned plane for extending cruising time according to claim 1, it is characterised in that：The fuselage
(3) lower section is equipped with undercarriage (9), and the undercarriage (9) includes roller.
A kind of 3. stealthy unmanned plane for extending cruising time according to claim 1, it is characterised in that：The empennage
(2) lower section is equipped with steering wheel (20).
A kind of 4. stealthy unmanned plane for extending cruising time according to claim 1, it is characterised in that：The main wing
(1) multiple propellers (8) are housed on.
A kind of 5. stealthy unmanned plane for extending cruising time according to claim 1, it is characterised in that：The fuselage
(3), doping induced by laser is scribbled in main wing (1), aileron (7), electric expansion plate (4), empennage (2) and electric expansion bar (6).
A kind of 6. stealthy unmanned plane for extending cruising time according to claim 1, it is characterised in that：The fuselage
(3), the material of main wing (1), aileron (7), electric expansion plate (4), empennage (2) and electric expansion bar (6) uses carbon fiber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721063507.7U CN207106845U (en) | 2017-08-24 | 2017-08-24 | A kind of stealthy unmanned plane for extending cruising time |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721063507.7U CN207106845U (en) | 2017-08-24 | 2017-08-24 | A kind of stealthy unmanned plane for extending cruising time |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207106845U true CN207106845U (en) | 2018-03-16 |
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ID=61570716
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721063507.7U Active CN207106845U (en) | 2017-08-24 | 2017-08-24 | A kind of stealthy unmanned plane for extending cruising time |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207106845U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107685849A (en) * | 2017-08-24 | 2018-02-13 | 泸州深远世宁无人机科技有限公司 | Solar energy unmanned plane with stealthy function |
| CN111661346A (en) * | 2020-07-04 | 2020-09-15 | 河北柒壹壹玖工业自动化技术有限公司 | Unmanned aerial vehicle device based on flexible solar energy thin film battery |
-
2017
- 2017-08-24 CN CN201721063507.7U patent/CN207106845U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107685849A (en) * | 2017-08-24 | 2018-02-13 | 泸州深远世宁无人机科技有限公司 | Solar energy unmanned plane with stealthy function |
| CN111661346A (en) * | 2020-07-04 | 2020-09-15 | 河北柒壹壹玖工业自动化技术有限公司 | Unmanned aerial vehicle device based on flexible solar energy thin film battery |
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