CN209159982U - A kind of fixed-wing unmanned plane of flight stability - Google Patents
A kind of fixed-wing unmanned plane of flight stability Download PDFInfo
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- CN209159982U CN209159982U CN201822069168.4U CN201822069168U CN209159982U CN 209159982 U CN209159982 U CN 209159982U CN 201822069168 U CN201822069168 U CN 201822069168U CN 209159982 U CN209159982 U CN 209159982U
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Abstract
The utility model relates to air vehicle technique fields, and disclose a kind of flight stability fixed-wing nobody, including cabin, wing is fixedly installed at left and right sides of the cabin and close to the one end at top, two wing inner roof walls and leading edge slat machine is fixedly installed between inner left wall and right side inner wall.The fixed-wing unmanned plane of the flight stability, pass through two wing inner roof walls and is fixedly installed with leading edge slat between inner left wall and right side inner wall, the design of trailing edge flap is fixedly installed with by two wing inner bottom walls and between inner left wall and right side inner wall, aircraft be can achieve while takeoff phase opens leading edge slat and trailing edge flap provides lift and keep stable purpose, wing aileron is fixedly installed with by two wings, the design of fixed fin is fixedly installed with by vertical tail, unmanned plane can be further reached for, the purpose of stability is provided, to realize the effect of flight stability.
Description
Technical field
The utility model relates to air vehicle technique field, the fixed-wing unmanned plane of specially a kind of flight stability.
Background technique
Unmanned plane is to utilize the not manned aircraft of radio robot and the presetting apparatus provided for oneself manipulation, Huo Zheyou
Car-mounted computer fully or intermittently automatically operates, unmanned plane at present take photo by plane, agricultural, plant protection, miniature self-timer, express delivery fortune
Defeated, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making and system
The application in romance etc. field is made, the purposes of unmanned plane itself has greatly been expanded, developed country also answers in actively extension industry
With with develop unmanned air vehicle technique.
Fixed-wing unmanned plane in currently available technology, wing structure is too simple, wants in flight course to air-flow
It asks higher, is not easy to fly in the case where air-flow is relatively unstable, and be unable to cope with a bit complicated air-flow environment, influence
The normal flight of unmanned plane, state of flight is unstable and oil consumption is higher, so propose a kind of fixed-wing unmanned plane of flight stability
To solve the problems, such as above-mentioned propose.
Utility model content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the utility model provides a kind of fixed-wing unmanned plane of flight stability, has winged
The advantages that row is stablized, economic fuel-efficient, solves the problems, such as that state of flight is unstable and oil consumption is higher.
(2) technical solution
To realize that above-mentioned flight stability, economic fuel-efficient purpose, the utility model provide the following technical solutions: a kind of flight
Stable fixed-wing unmanned plane, including cabin are fixedly installed with head, the fixed peace in the bottom of the cabin at the top of the cabin
Equipped with tail, wing, two wing inner roof walls are fixedly installed at left and right sides of the cabin and close to the one end at top
And leading edge slat is fixedly installed between inner left wall and right side inner wall, two wing inner bottom walls and be located at left side
It is fixedly installed with trailing edge flap between inner wall and right side inner wall, the cabin inner roof wall and is fixed close to one end of inner left wall
Camera is installed, the inner left wall of the head is fixedly installed with preceding camera, the cabin inner bottom wall and close left side
One end of inner wall is fixedly installed with lower camera, two wing inner roof walls and be located at two trailing edge flaps mutually from one end it is equal
Be fixedly installed with wing aileron, two wings mutually from one end be fixedly installed with preceding winglet, on the left of the tail
Be fixedly installed with lateral empennage with right side, two lateral empennages mutually from one end be fixedly installed with rear winglet,
Two lateral empennage inner bottom walls and empennage aileron, the machine are fixedly installed between inner left wall and right side inner wall
The outer surface of tail is fixedly installed with vertical tail, inner wall and the fixation between inner roof wall and inner bottom wall on the right side of the vertical tail
Fixed fin is installed, the bottom of the cabin is fixedly installed with the undercarriage place position that quantity is two, rises described in two
It falls frame place position inner roof wall and is fixedly installed with undercarriage close to one end of inner left wall, the top movable of the undercarriage connects
It is connected to lifting wheel, the right side inner wall of the tail is fixedly installed with rear camera.
Preferably, the outer surface of the cabin is fixedly installed with solar panels, at the axle center of cabin and at the axle center of head
It is maintained on same horizontal line.
Preferably, the shape size of the upper camera, preceding camera, lower camera and rear camera is consistent and
For wide-angle camera.
Preferably, the shape size of two wings is consistent, and same water is maintained at the axle center of two wings
On line, the shape of two wings is in a rectangular trapezoid.
Preferably, the preceding winglet is that isogonism is trapezoidal with rear winglet, after the area of preceding winglet is greater than
The area of winglet.
Preferably, the quantity of the undercarriage is three, is provided in the undercarriage place position of cabin inner left wall
One undercarriage, there are two undercarriages for setting in the undercarriage place position of inner wall on the right side of cabin.
(3) beneficial effect
Compared with prior art, the utility model provides a kind of fixed-wing unmanned plane of flight stability, and having following has
Beneficial effect:
1, the fixed-wing unmanned plane of the flight stability passes through two wing inner roof walls and is located at inner left wall and right side inner wall
Between be fixedly installed with leading edge slat, it is fixed through two wing inner bottom walls and between inner left wall and right side inner wall
The design of trailing edge flap is installed, aircraft is can achieve in takeoff phase opening leading edge slat and trailing edge flap and the same of lift is provided
When and keep stable purpose, be fixedly installed with wing aileron by two wings, be fixedly installed with by vertical tail vertical
The design of straight stabilization can further be reached for unmanned plane and provide the purpose of stability, to realize flight stability
Effect.
2, the fixed-wing unmanned plane of the flight stability, by two wings mutually from one end be fixedly installed with before wingtip it is small
The wing, by two lateral empennages mutually from one end be fixedly installed with the design of rear winglet, in the process of unmanned plane during flying
In, effective increase wing aspect ratio, while the vortex generated with wing is confronted with each other counteractings, can achieve reduction induced drag
Purpose is fixedly installed with the design of solar panels by the outer surface of cabin, can achieve energy-efficient purpose, thus realize through
It helps fuel-efficient effect.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the utility model the structure left view；
Fig. 3 is the portion A partial enlarged view in the utility model Fig. 2.
In figure: 1 cabin, 2 heads, 3 tails, 4 wings, 5 leading edge slats, 6 trailing edge flaps, camera on 7,8 preceding cameras,
Winglet, 13 empennage ailerons, 14 vertical tails, 15 are vertically pacified behind winglet, 11 lateral empennages, 12 before 9 wing ailerons, 10
Determine face, 16 undercarriage place positions, 17 undercarriages, 18 lifting wheels, 19 lower cameras, 20 rear cameras.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3, a kind of fixed-wing unmanned plane of flight stability, including cabin 1 are please referred to, the top of cabin 1 is fixedly mounted
Have a head 2, the outer surface of cabin 1 is fixedly installed with solar panels, at the axle center of cabin 1 be maintained at same at the axle center of head 2
On one horizontal line, the bottom of cabin 1 is fixedly installed with tail 3, the fixed peace in one end of 1 left and right sides of cabin and close top
Equipped with wing 4, the shape size of two wings 4 is consistent, and is maintained on same waterline at the axle center of two wings 4, two
The shape of a wing 4 is in a rectangular trapezoid, two 4 inner roof walls of wing and is fixedly mounted between inner left wall and right side inner wall
There is a leading edge slat 5, two 4 inner bottom walls of wing and be fixedly installed with trailing edge flap 6 between inner left wall and right side inner wall,
One end of 1 inner roof wall of cabin and close inner left wall is fixedly installed with camera 7, upper camera 7, preceding camera 8, lower camera shooting
First 19 and the shape size of rear camera 20 be consistent and be wide-angle camera, before the inner left wall of head is fixedly installed with
Camera 8,1 inner bottom wall of cabin and is fixedly installed with lower camera 19 close to one end of inner left wall, two 4 inner roof walls of wing and
Positioned at two 6 phases of trailing edge flap from one end be fixedly installed with wing aileron 9, two 4 phases of wing from the fixed peace in one end
Equipped with preceding winglet 10, preceding winglet 10 is that isogonism is trapezoidal with rear winglet 12, and the area of preceding winglet 10 is big
In the area of rear winglet 12,3 left and right side of tail is fixedly installed with lateral empennage 11, two lateral 11 phases of empennage from
One end be fixedly installed with rear winglet 12, two lateral 11 inner bottom walls of empennage and be located at inner left wall and right side inner wall it
Between be fixedly installed with empennage aileron 13, the outer surface of tail 3 is fixedly installed with vertical tail 14,14 right side inner wall of vertical tail
And fixed fin 15 is fixedly installed between inner roof wall and inner bottom wall, it is two that the bottom of cabin 1, which is fixedly installed with quantity,
One end of a undercarriage place position 16, two 16 inner roof walls of undercarriage place position and close inner left wall has been fixedly installed with
Frame 17 is fallen, the quantity of undercarriage 17 is three, is provided with one in the undercarriage place position 16 of 1 inner left wall of cabin and rises and falls
Frame 17, there are two undercarriage 17, the top movables of undercarriage 17 for setting in the undercarriage place position 16 of 1 right side inner wall of cabin
It is connected with lifting wheel 18, the right side inner wall of tail 3 is fixedly installed with rear camera 20.
In conclusion the fixed-wing unmanned plane of the flight stability, pass through two 4 inner roof walls of wing and be located at inner left wall and
It is fixedly installed with leading edge slat 5 between the inner wall of right side, pass through two 4 inner bottom walls of wing and is located at inner left wall and right side inner wall
Between be fixedly installed with the design of trailing edge flap 6, can achieve aircraft in takeoff phase and open leading edge slat 5 and trailing edge flap
While 6 offer lift and stable purpose is kept, wing aileron 9 is fixedly installed with by two wings 4, passes through vertical end
The wing 14 is fixedly installed with the design of fixed fin 15, can further be reached for unmanned plane and provide the purpose of stability, from
And realize the effect of flight stability.
Also, by two 4 phases of wing from one end be fixedly installed with before winglet 10, pass through two lateral empennages
11 phases from one end be fixedly installed with the design of rear winglet 12, during unmanned plane during flying, effective increase wing
Aspect ratio, while the vortex generated with wing is confronted with each other counteractings, be can achieve the purpose of reduction induced drag, is passed through cabin 1
Outer surface be fixedly installed with the designs of solar panels, can achieve energy-efficient purpose, to realize economic fuel-efficient purpose.
It should be noted that the terms "include", "comprise" or its any other variant are intended to the packet of nonexcludability
Contain, so that the process, method, article or equipment for including a series of elements not only includes those elements, but also including
Other elements that are not explicitly listed, or further include for elements inherent to such a process, method, article, or device.
In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that including the element
Process, method, article or equipment in there is also other identical elements.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of fixed-wing unmanned plane of flight stability, including cabin (1), it is characterised in that: the top of the cabin (1) is fixed
It is equipped with head (2), the bottom of the cabin (1) is fixedly installed with tail (3), at left and right sides of the cabin (1) and close to top
The one end in portion is fixedly installed with wing (4), two wing (4) inner roof walls and between inner left wall and right side inner wall
It is fixedly installed with leading edge slat (5), two wing (4) inner bottom walls and solid between inner left wall and right side inner wall
Dingan County is equipped with trailing edge flap (6), and one end of cabin (1) inner roof wall and close inner left wall is fixedly installed with camera
(7), the inner left wall of the head is fixedly installed with preceding camera (8), cabin (1) inner bottom wall and close to inner left wall
One end is fixedly installed with lower camera (19), two wing (4) inner roof walls and be located at two trailing edge flaps (6) mutually from one
End be fixedly installed with wing aileron (9), two wings (4) mutually from one end be fixedly installed with preceding winglet
(10), tail (3) left and right side is fixedly installed with lateral empennage (11), two lateral empennages (11) mutually from
One end is fixedly installed with rear winglet (12), two lateral empennage (11) inner bottom walls and is located at inner left wall and right side
It is fixedly installed between inner wall empennage aileron (13), the outer surface of the tail (3) is fixedly installed with vertical tail (14), institute
It states inner wall on the right side of vertical tail (14) and is fixedly installed with fixed fin (15), the machine between inner roof wall and inner bottom wall
The bottom in cabin (1) is fixedly installed with the undercarriage place position (16) that quantity is two, and two undercarriage place positions (16) are interior
One end of roof and close inner left wall is fixedly installed with undercarriage (17), and the top movable of the undercarriage (17) is connected with
The right side inner wall of lifting wheel (18), the tail (3) is fixedly installed with rear camera (20).
2. a kind of fixed-wing unmanned plane of flight stability according to claim 1, it is characterised in that: the cabin (1)
Outer surface is fixedly installed with solar panels, is maintained at same horizontal line at the axle center of head (2) at the axle center of cabin (1)
On.
3. a kind of fixed-wing unmanned plane of flight stability according to claim 1, it is characterised in that: the upper camera
(7), the shape size of preceding camera (8), lower camera (19) and rear camera (20) is consistent and is wide-angle camera.
4. a kind of fixed-wing unmanned plane of flight stability according to claim 1, it is characterised in that: two wings
(4) shape size is consistent, and is maintained on same waterline at the axle center of two wings (4), the shape of two wings (4)
It is in a rectangular trapezoid.
5. a kind of fixed-wing unmanned plane of flight stability according to claim 1, it is characterised in that: the preceding winglet
It (10) is that isogonism is trapezoidal with rear winglet (12), the area of preceding winglet (10) is greater than the face of rear winglet (12)
Product.
6. a kind of fixed-wing unmanned plane of flight stability according to claim 1, it is characterised in that: the undercarriage (17)
Quantity be three, close to cabin (1) inner left wall undercarriage place position (16) in is provided with a undercarriage (17), it is close
There are two undercarriage (17) for setting in the undercarriage place position (16) of inner wall on the right side of cabin (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822069168.4U CN209159982U (en) | 2018-12-11 | 2018-12-11 | A kind of fixed-wing unmanned plane of flight stability |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822069168.4U CN209159982U (en) | 2018-12-11 | 2018-12-11 | A kind of fixed-wing unmanned plane of flight stability |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209159982U true CN209159982U (en) | 2019-07-26 |
Family
ID=67343033
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822069168.4U Expired - Fee Related CN209159982U (en) | 2018-12-11 | 2018-12-11 | A kind of fixed-wing unmanned plane of flight stability |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209159982U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113232832A (en) * | 2021-03-29 | 2021-08-10 | 南京航空航天大学 | Amphibious aircraft |
-
2018
- 2018-12-11 CN CN201822069168.4U patent/CN209159982U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113232832A (en) * | 2021-03-29 | 2021-08-10 | 南京航空航天大学 | Amphibious aircraft |
| CN113232832B (en) * | 2021-03-29 | 2023-08-22 | 南京航空航天大学 | Amphibious aircraft |
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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: 20191212 Address after: 050000 102, floor 1, No. 856, Zhongshan West Road, Qiaoxi District, Shijiazhuang City, Hebei Province Patentee after: Hebei mengke Intelligent Technology Co.,Ltd. Address before: 264200 Second Floor, Building 3, South Zone, Zhongke Innovation Industrial Park, Fengchao Street, Weihai Economic and Technological Development Zone, Shandong Province Patentee before: Shandong Changxiang Intelligent Technology Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190726 Termination date: 20211211 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |