CN207496927U - 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
- CN207496927U CN207496927U CN201721358662.1U CN201721358662U CN207496927U CN 207496927 U CN207496927 U CN 207496927U CN 201721358662 U CN201721358662 U CN 201721358662U CN 207496927 U CN207496927 U CN 207496927U
- Authority
- CN
- China
- Prior art keywords
- plate body
- fuselage
- buffer board
- fixedly connected
- plate
- 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 discloses a kind of fixed-wing unmanned planes for adapting to a variety of environment that take off, including fuselage, one end of the fuselage is equipped with shaft, propeller is interspersed in the shaft, the both sides of the fuselage are symmetrically fixedly connected with wing, the other end of the fuselage is equipped with tail vane, the both sides of the fuselage other end are also arranged with horizontal tail, the fuselage is equipped with mounting groove, buffer board is equipped in the mounting groove, the both ends of the buffer board are equipped with carriage, the side of the buffer board is fixedly connected with undercarriage, symmetrically there are two rotating bars for rotation connection on the buffer board.The utility model operation simple in structure is easy, by the first spring lever, second spring bar with the isostructural interaction of air bag so that unmanned plane can play the role of damping in landing, the damping device is simple in structure, it is of low cost, while energy consumption can be reduced, improve the scope of application.
Description
Technical field
The utility model is related to unmanned air vehicle technique field more particularly to a kind of fixed-wing for adapting to a variety of environment that take off nobody
Machine.
Background technology
The mode of taking off of fixed-wing unmanned plane includes catapult-assisted take-off and VTOL is taken off, and catapult-assisted take-off is needed in unmanned plane
Lower part setting ejection hook, relatively light, easy to operate, vertical take-off and landing drone can adapt to more complicated take off and drop
Environment is fallen, then in order to avoid flying the stability of unmanned plane during landing, damping device is designed on unmanned plane, but it is existing
The damping device of fixed-wing unmanned plane is expensive, complicated, and range of applicability is small.
Utility model content
The purpose of this utility model is in order to solve shortcoming in the prior art, such as：Existing fixed-wing unmanned plane
Damping device it is expensive, complicated, range of applicability is small.
To achieve these goals, the utility model employs following technical solution：
A kind of fixed-wing unmanned plane for adapting to a variety of environment that take off, including fuselage, one end of the fuselage is equipped with shaft, institute
It states and propeller is interspersed in shaft, the both sides of the fuselage are symmetrically fixedly connected with wing, and the other end of the fuselage is equipped with tail
Rudder, the both sides of the fuselage other end are also arranged with horizontal tail, and the fuselage is equipped with mounting groove, is equipped in the mounting groove slow
Punching, the both ends of the buffer board are equipped with carriage, and the side of the buffer board is fixedly connected with undercarriage, the buffering
It is symmetrically rotatablely connected there are two rotating bar on plate, the other end of each rotating bar to be connected with cylindrical bar, the buffer board
Side also symmetrically slidably connects sliding shoe, and the side of the sliding shoe is fixedly connected with second spring bar, the second spring
The other end of bar is fixedly connected with movable block, and one end of the movable block is slidably connected on the side wall of mounting groove, the movement
Limiting slot is equipped in block, the cylindrical bar is located in limiting slot, and the side of the movable block is symmetrically connected with two the first springs
Bar, the other end of first spring lever are connected on the side wall of mounting groove, and the opposite side of the movable block is equipped with loose slot, institute
It states and expansion plate is connected on cylindrical bar, the expansion plate and rotating bar are located in loose slot, and the side of the expansion plate is equipped with gas
Capsule, the side of the air bag are against the side of mounting groove.
Preferably, the carriage includes multiple kellies, and each kelly is connected in buffer board, each card
Pulley is rotatably connected on bar, the pulley is against on the inner wall of mounting groove.
Preferably, the undercarriage includes slide plate and supporting rod, and the supporting rod is fixedly connected on buffering in herringbone
The side of plate, the other end of the supporting rod are fixedly connected with slide plate.
Preferably, the slide plate includes the first plate body and the second plate body, and second plate body is fixedly connected on supporting rod,
Described arc-shaped one end for being fixedly connected on the second plate body of first plate body is additionally provided with idler wheel on second plate body.
Preferably, the expansion plate is divided into third plate body and the 4th plate body, and one end of the third plate body is mounted on cylinder
On bar, the 4th plate body is interspersed in third plate body.
Preferably, first plate body and the second plate body are integrally formed.
Compared with prior art, the beneficial effects of the utility model are：Operation simple in structure is easy, passes through the first spring
Bar, second spring bar are with the isostructural interaction of air bag so that unmanned plane can play the role of damping in landing, this subtracts
It is simple to shake apparatus structure, it is of low cost, while energy consumption can be reduced, improve the scope of application.
Description of the drawings
Fig. 1 be the utility model proposes a kind of a variety of environment that take off of adaptation fixed-wing unmanned plane Facad structure signal
Figure；
Fig. 2 is the partial enlargement structural representation of A in Fig. 1.
In figure：1 fuselage, 2 horizontal tails, 3 tail vanes, 4 buffer boards, 5 undercarriages, 6 air bags, 7 propellers, 8 shafts, 9 wings, 10 peaces
Tankage, 11 sliding shoes, 12 first spring levers, 13 cylindrical bars, 14 limiting slots, 15 movable blocks, 16 expansion plates, 17 rotating bars, 18
Two spring levers.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
It clearly and completely describes, it is clear that the described embodiments are only a part of the embodiments of the utility model rather than whole
Embodiment.
In the description of the present invention, it is to be appreciated that term " on ", " under ", "front", "rear", "left", "right",
The orientation or position relationship of the instructions such as " top ", " bottom ", " interior ", " outer " are based on orientation shown in the drawings or position relationship, are only
The utility model must have specific with the device or element for simplifying description rather than instruction or hint meaning for ease of description
Orientation, with specific azimuth configuration and operation, therefore it is not intended that limitation to the utility model.
With reference to Fig. 1-2, a kind of fixed-wing unmanned plane for adapting to a variety of environment that take off, including fuselage 1, one end of fuselage 1 is set
There is shaft 8, propeller 7 is interspersed in shaft 8, the both sides of fuselage 1 are symmetrically fixedly connected with wing 9, and the other end of fuselage 1 is equipped with
Tail vane 3, the both sides of 1 other end of fuselage are also arranged with horizontal tail 2, and fuselage 1 is equipped with mounting groove 10, buffering is equipped in mounting groove 10
Plate 4, the both ends of buffer board 4 are equipped with carriage, and carriage includes multiple kellies, and each kelly is connected in buffer board 4,
Pulley is rotatably connected on each kelly, pulley is against on the inner wall of mounting groove 10, is improved the slip fluency of buffer board 4, is kept away
Exempt from Caton phenomenon occur, the side of buffer board 4 is fixedly connected with undercarriage 5, and undercarriage 5 includes slide plate and supporting rod, supporting rod
The side of buffer board 4 is fixedly connected in herringbone, the other end of supporting rod is fixedly connected with slide plate, and supporting rod is in eight words
Shape can increase the firmness of undercarriage 5, and slide plate includes the first plate body and the second plate body, and the second plate body is fixedly connected on support
On bar, the arc-shaped one end for being fixedly connected on the second plate body of the first plate body is additionally provided with idler wheel on the second plate body, and the first plate body is in arc
Shape setting can improve the stability of unmanned plane landing, and the first plate body and the second plate body are integrally formed, and facilitate manufacture, buffer board
Symmetrically there are two rotating bar 17, the other end of each rotating bar 17 is connected with cylindrical bar 13 for rotation connection on 4, and the one of buffer board 4
Side also symmetrically slidably connects sliding shoe 11, and the side of sliding shoe 11 is fixedly connected with second spring bar 18, second spring bar 18
The other end be fixedly connected with movable block 15, one end of movable block 15 is slidably connected on the side wall of mounting groove 10, movable block 15
Interior to be equipped with limiting slot 14, cylindrical bar 13 is located in limiting slot 14, and the side of movable block 15 is symmetrically connected with two the first spring levers
12, the other end of the first spring lever 12 is connected on the side wall of mounting groove 10, and the opposite side of movable block 15 is equipped with loose slot, cylinder
It is connected with expansion plate 16 on bar 13, expansion plate 16 divides for third plate body and the 4th plate body, and one end of third plate body is mounted on cylinder
On bar 13, the 4th plate body is interspersed in third plate body, and expansion plate 16 and rotating bar 17 are located in loose slot, the side of expansion plate 16
Equipped with air bag 6, the side of air bag 6 is against the side of mounting groove 10.
In the utility model, when user uses the device, when landing, buffer board 4 is filled unmanned plane by sliding
It puts and is moved in mounting groove 10, first time damping, the angle of latter two right rotating bar 17 are then realized by second spring bar 18
Expand so that move movable block 15 to both sides so that the first spring lever 12 compresses, and realizes second of damping, finally using stretching
16 extruding gasbag 6 of contracting plate realizes third time damping.
The preferable specific embodiment of the above, only the utility model, but the scope of protection of the utility model is not
This is confined to, in the technical scope that any one skilled in the art discloses in the utility model, according to this practicality
Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
Claims (6)
1. a kind of fixed-wing unmanned plane for adapting to a variety of environment that take off, including fuselage (1), which is characterized in that the fuselage (1)
One end is equipped with shaft (8), is interspersed with propeller (7) on the shaft (8), the both sides of the fuselage (1) are symmetrically fixedly connected with
Wing (9), the other end of the fuselage (1) are equipped with tail vane (3), and the both sides of fuselage (1) other end are also arranged with horizontal tail
(2), the fuselage (1) is equipped with mounting groove (10), and buffer board (4) is equipped in the mounting groove (10), the buffer board (4)
Both ends are equipped with carriage, and the side of the buffer board (4) is fixedly connected with undercarriage (5), symmetrical on the buffer board (4)
Rotating bar (17) that there are two rotation connections, the other end of each rotating bar (17) to be connected with cylindrical bar (13), the buffering
The side of plate (4) also symmetrically slidably connects sliding shoe (11), and the side of the sliding shoe (11) is fixedly connected with second spring
Bar (18), the other end of the second spring bar (18) are fixedly connected with movable block (15), and one end of the movable block (15) is slided
It is dynamic to be connected on the side wall of mounting groove (10), limiting slot (14) is equipped in the movable block (15), the cylindrical bar (13) is located at
In limiting slot (14), the side of the movable block (15) is symmetrically connected with two the first spring levers (12), first spring lever
(12) the other end is connected on the side wall of mounting groove (10), and the opposite side of the movable block (15) is equipped with loose slot, the circle
Expansion plate (16) is connected on mast (13), the expansion plate (16) and rotating bar (17) are in loose slot, the expansion plate
(16) side is equipped with air bag (6), and the side of the air bag (6) is against the side of mounting groove (10).
A kind of 2. fixed-wing unmanned plane for adapting to a variety of environment that take off according to claim 1, which is characterized in that the cunning
Dynamic device includes multiple kellies, and each kelly is connected in buffer board (4), and cunning is rotatably connected on each kelly
Wheel, the pulley are against on the inner wall of mounting groove (10).
3. a kind of fixed-wing unmanned plane for adapting to a variety of environment that take off according to claim 1, which is characterized in that described
It falls frame (5) and includes slide plate and supporting rod, the supporting rod is fixedly connected on the side of buffer board (4), the branch in herringbone
The other end of strut is fixedly connected with slide plate.
A kind of 4. fixed-wing unmanned plane for adapting to a variety of environment that take off according to claim 3, which is characterized in that the cunning
Plate includes the first plate body and the second plate body, and second plate body is fixedly connected on supporting rod, and first plate body is arc-shaped solid
Surely one end of the second plate body is connected to, idler wheel is additionally provided on second plate body.
5. a kind of fixed-wing unmanned plane for adapting to a variety of environment that take off according to claim 1, which is characterized in that described to stretch
Contracting plate (16) is divided into third plate body and the 4th plate body, and one end of the third plate body is mounted on cylindrical bar (13), and the described 4th
Plate body is interspersed in third plate body.
6. a kind of fixed-wing unmanned plane for adapting to a variety of environment that take off according to claim 4, which is characterized in that described the
One plate body and the second plate body are integrally formed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721358662.1U CN207496927U (en) | 2017-10-20 | 2017-10-20 | 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 |
|---|---|---|---|
| CN201721358662.1U CN207496927U (en) | 2017-10-20 | 2017-10-20 | A kind of fixed-wing unmanned plane for adapting to a variety of environment that take off |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207496927U true CN207496927U (en) | 2018-06-15 |
Family
ID=62501007
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721358662.1U Active CN207496927U (en) | 2017-10-20 | 2017-10-20 | A kind of fixed-wing unmanned plane for adapting to a variety of environment that take off |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207496927U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108910021A (en) * | 2018-07-25 | 2018-11-30 | 苏州频聿精密机械有限公司 | A kind of undercarriage mounting connection structure |
| CN114013231A (en) * | 2021-11-25 | 2022-02-08 | 广东汇天航空航天科技有限公司 | Propeller fixing device and flight equipment |
-
2017
- 2017-10-20 CN CN201721358662.1U patent/CN207496927U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108910021A (en) * | 2018-07-25 | 2018-11-30 | 苏州频聿精密机械有限公司 | A kind of undercarriage mounting connection structure |
| CN108910021B (en) * | 2018-07-25 | 2021-11-30 | 苏州市东挺河智能科技发展有限公司 | Undercarriage erection joint structure |
| CN114013231A (en) * | 2021-11-25 | 2022-02-08 | 广东汇天航空航天科技有限公司 | Propeller fixing device and flight equipment |
| CN114013231B (en) * | 2021-11-25 | 2023-04-18 | 广东汇天航空航天科技有限公司 | Screw fixing device and flight equipment |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204802082U (en) | Land, water and air no. 3 four coaxial rotor crafts of dwelling | |
| CN205469772U (en) | It is preceding to little volume unmanned aerial vehicle of folded form | |
| CN207496927U (en) | A kind of fixed-wing unmanned plane for adapting to a variety of environment that take off | |
| CN108674636A (en) | A kind of twin-engined quadrotor drones and its leg means | |
| CN206243479U (en) | Flapping wing aircraft | |
| CN204688409U (en) | The unmanned vehicle that a kind of many rotors and fixed-wing combine | |
| CN105841915B (en) | A kind of full machine flutter wind tunnel model supports system for simulating the longitudinal degress of feedom | |
| CN105059537B (en) | UAV (unmanned aerial vehicle) | |
| CN205396534U (en) | Rotor unmanned aerial vehicle verts | |
| CN106494618B (en) | Plumage formula flapping-wing aircraft | |
| CN202569558U (en) | Remote controlled single-rotor helicopter model structure | |
| CN204998755U (en) | Rotor unmanned aerial vehicle balance adjustment device | |
| CN100591400C (en) | Steering mechanism for model helicopter | |
| CN207737514U (en) | A kind of main wing splicing assembly jig | |
| CN208102315U (en) | A kind of amphibious aircraft undercarriage mechanical control device | |
| CN202666408U (en) | Six-arm model aerial propeller | |
| CN206569258U (en) | A kind of unmanned plane undercarriage | |
| CN109911189A (en) | A kind of horizontal double rotor unmanned plane based on 3D printing | |
| CN205366062U (en) | Change axial device of rotor craft | |
| CN207374651U (en) | A kind of VTOL fixed-wing unmanned plane | |
| CN203816222U (en) | Model airplane spiral frame | |
| CN206278258U (en) | A kind of control system of the rollover of aircraft, driftage and yaw stability | |
| CN207191192U (en) | A kind of automobile tail fin with multiple functions | |
| RU128182U1 (en) | SECURITY PLAN (OPTIONS) | |
| CN206502016U (en) | A kind of all-wing aircraft unmanned plane of vertical lift |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200617 Address after: Room 205-2, building 1616, Chuangxin Road, Songbei District, Harbin City, Heilongjiang Province Patentee after: Harbin epers Intelligent Equipment Technology Co., Ltd Address before: 528400 the 3 floor B area of A plant, 10 Cui Wei Road, Chui Heng District, Zhongshan, Guangdong. Patentee before: ZHONGSHAN XINGTU AVIATION AND SPACEFLIGHT TECHNOLOGY Co.,Ltd. |