CN209480003U - A kind of unmanned plane flight collision avoidance device - Google Patents
A kind of unmanned plane flight collision avoidance device Download PDFInfo
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- CN209480003U CN209480003U CN201920163965.0U CN201920163965U CN209480003U CN 209480003 U CN209480003 U CN 209480003U CN 201920163965 U CN201920163965 U CN 201920163965U CN 209480003 U CN209480003 U CN 209480003U
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- wing
- unmanned plane
- mounting hole
- collision avoidance
- connecting rod
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Abstract
The utility model discloses a kind of unmanned plane flight collision avoidance devices; it is related to air vehicle technique field; lack effective Anticollision Measures to solve existing unmanned plane, the problem of during use usually unmanned plane being caused to hit with barrier, unmanned plane is caused to damage because of misoperation.Wing is provided on the outer wall of the body, and there are four wing settings, one end of the wing is provided with helical-blade, and one end of helical-blade and wing is sequentially connected, the lower surface of the wing is provided with support frame, one end of support frame as described above and the lower surface of wing are welded to connect, the upper and lower surfaces of the wing are respectively set there are two connecting rod, one end of the connecting rod is provided with connecting pin, the other end of the connecting rod is provided with anti-billiards, the connecting pin is internally provided with mounting hole, connecting hole is provided with below the mounting hole, and the inside of wing is arranged in connecting hole, the mounting hole and connecting hole are internally provided with bolt.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of unmanned plane flight collision avoidance device.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer, compared with manned aircraft, nobody
Machine is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane press 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 industrial application are that unmanned plane has really just needed；Mesh
It is preceding take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, newly
The application for hearing report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, has greatly expanded unmanned plane itself
Purposes, developed country also in actively extension industrial application and develop unmanned air vehicle technique.
Traditional unmanned plane lacks effective Anticollision Measures, usually can lead to nothing because of misoperation during use
It is man-machine to be hit with barrier, cause the damage of unmanned plane, we have proposed a kind of unmanned plane flight collision avoidance devices thus.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane flight collision avoidance devices, to solve in above-mentioned background technique
The traditional unmanned plane proposed lacks effective Anticollision Measures, usually can lead to nobody because of misoperation during use
The problem of machine is hit with barrier, and unmanned plane is caused to damage.
To achieve the above object, the utility model provides the following technical solutions: a kind of unmanned plane flight collision avoidance device, packet
Body is included, wing is provided on the outer wall of the body, and there are four wing settings, one end of the wing is provided with spiral
Leaf, and one end of helical-blade and wing is sequentially connected, the lower surface of the wing is provided with support frame, one end of support frame as described above
It is welded to connect with the lower surface of wing, the upper and lower surfaces of the wing are respectively set that there are two connecting rod, the connections
One end of bar is provided with connecting pin, and the other end of the connecting rod is provided with anti-billiards, and the connecting pin is internally provided with peace
Hole is filled, is provided with connecting hole below the mounting hole, and the inside of wing, the mounting hole and connecting hole is arranged in connecting hole
Be internally provided with bolt, lock nut is provided on the outer wall of the bolt, the lower surface of the lock nut is provided with flat
Gasket, the lower surface of the flat shim are provided with spring shim, and the lower surface of the spring shim is provided with casing, and casing is set
Set the inside in mounting hole and connecting hole.
Preferably, there are four the helical-blade settings, and the surrounding of four helical-blades is provided with protective case.
Preferably, the lower surface of support frame as described above is provided with pedestal, and the upper surface of the other end of support frame and pedestal is welded
It connects in succession.
Preferably, the connecting rod is provided with 16, and is respectively set on each wing there are four connecting rod.
Preferably, one end of the bolt is provided with protruding head, and the inside of connecting hole is arranged in protruding head.
Preferably, the vertical center line of the mounting hole is overlapped with the vertical center line of connecting hole.
Compared with prior art, the utility model has the beneficial effects that
The utility model plays the role of preventing unmanned plane and barrier impacts, anti-billiards setting by the anti-billiards being arranged
There are 16, and the distance between this 16 anti-billiards and body are both greater than at a distance from helical-blade and body, when unmanned plane exists
When in-flight striking barrier, the anticollision club in the connecting rod of body surrounding replaces body preferentially and barrier impacts, from
And achieve the purpose that complete the work of unmanned plane anticollision to unmanned plane body anticollision.
Detailed description of the invention
Fig. 1 is the overall structure top view of the utility model；
Fig. 2 is the overall structure main view of the utility model；
Fig. 3 is the anticollision mechanism structural schematic diagram of the utility model；
Fig. 4 is the part A structure enlargement diagram of the utility model；
In figure: 1, body；2, wing；3, connecting rod；4, anti-billiards；5, protective case；6, helical-blade；7, pedestal；8, it supports
Frame；9, connecting pin；10, mounting hole；11, bolt；12, lock nut；13, flat shim；14, spring shim；15, connecting hole；16,
Casing；17, protruding head.
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.
Fig. 1-4 is please referred to, a kind of embodiment provided by the utility model: a kind of unmanned plane flight collision avoidance device, including
Body 1 is provided with wing 2 on the outer wall of body 1, and wing 2 plays the role of that unmanned plane is assisted to take off, and wing 2 is provided with four
A, one end of wing 2 is provided with helical-blade 6, and helical-blade 6 plays the role of that unmanned plane is driven to take off, and helical-blade 6 and wing 2
One end transmission connection, the lower surface of wing 2 is provided with support frame 8, and support frame 8 plays the role of supporting body 1, support frame 8
One end and the lower surface of wing 2 be welded to connect, the upper and lower surfaces of wing 2 are respectively set there are two connecting rod 3, connection
One end of bar 3 is provided with connecting pin 9, and the other end of connecting rod 3 is provided with anti-billiards 4, and connecting pin 9 is internally provided with mounting hole
10, mounting hole 10 plays the role of being easily installed, and the lower section of mounting hole 10 is provided with connecting hole 15, and connecting hole 15 is arranged in machine
The inside of the wing 2, mounting hole 10 and connecting hole 15 are internally provided with bolt 11, and bolt 11 plays the role of installing anticollision mechanism,
It is provided with lock nut 12 on the outer wall of bolt 11, the lower surface of lock nut 12 is provided with flat shim 13, under flat shim 13
Surface is provided with spring shim 14, and the lower surface of spring shim 14 is provided with casing 16, and casing 16 is arranged in 10 He of mounting hole
The inside of connecting hole 15, casing 16 play the role of accommodating protruding head 17.
Further, there are four the settings of helical-blade 6, and the surrounding of four helical-blades 6 is provided with protective case 5, and the four of setting
A helical-blade 6 plays the role of that unmanned plane is driven to take off, and the protective case 5 of the surrounding setting of helical-blade 6 plays protection helical-blade 6
Effect, the effect damaged so as to avoid helical-blade 6.
Further, the lower surface of support frame 8 is provided with pedestal 7, and the upper surface of the other end of support frame 8 and pedestal 7 is welded
It connects in succession, the pedestal 7 of the lower surface setting of support frame 8 plays the role of supporting unmanned plane, the other end and pedestal 7 of support frame 8
Upper surface be welded to connect connection between support frame 8 and pedestal 7 can be made more firm.
Further, connecting rod 3 is provided with 16, and is respectively set on each wing 2 there are four connecting rod 3, on wing 2
The connecting rod 3 of setting plays the role of installing anti-billiards 4 on wing 2, respectively arranged four connecting rods 3 on each wing 2
Play the role of that four anti-billiards 4 are installed on each wing 2.
Further, one end of bolt 11 is provided with protruding head 17, and the inside of connecting hole 15 is arranged in protruding head 17, bolt 11
The protruding head 17 of one end setting plays the role of being contracted to 16 inside of casing, so that casing 16 expands, so that the root of bolt 11
Portion is stuck in the inside of connecting hole 15, so that the connection between connecting pin 9 and wing 2 is more firm.
Further, the vertical center line of mounting hole 10 is overlapped with the vertical center line of connecting hole 15, mounting hole 10 and connection
Hole 15, which plays the role of being inserted into convenient for bolt 11, to be connected, the vertical center line of mounting hole 10 and the vertical center line weight of connecting hole 15
Close the installment work that can effectively facilitate anticollision mechanism.
Working principle: in use, the mounting hole 10 inside connecting pin 9 is aligned with the connecting hole 15 on unmanned plane wing 2,
Bolt 11, casing 16 are fitted into mounting hole 10 and connecting hole 15 again, tighten bolt 11, bolt 11 drives tail portion after tightening
Protruding head 17 is shunk, and there are several openings in the tail portion of casing 16, and after bolt 11 is tightened, the tail portion of protruding head 17 is just brought to opening
16 the inside of casing, rushes casing 16 greatly, achievees the purpose that expansion, and then bolt 11 is fixed on the inside of connecting hole 15, reach
The purpose taken root is respectively mounted four on each wing 2 in the same way so that connecting pin 9 is fixedly connected with wing 2
Anticollision mechanism, so that each connecting rod 3 is symmetrical about the central point of body 1, when unmanned plane awing strikes obstacle
When object, the anti-billiards 4 in the connecting rod 3 of 1 surrounding of body can replace body 1 preferentially and barrier impacts, to reach to body 1
The purpose of anticollision completes the work of unmanned plane anticollision.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and
And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in
All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting
Related claim.
Claims (6)
1. a kind of unmanned plane flight collision avoidance device, including body (1), it is characterised in that: be arranged on the outer wall of the body (1)
Have wing (2), and wing (2) setting there are four, one end of the wing (2) is provided with helical-blade (6), and helical-blade (6) with
One end of wing (2) is sequentially connected, and the lower surface of the wing (2) is provided with support frame (8), one end of support frame as described above (8)
It being welded to connect with the lower surface of wing (2), the upper and lower surfaces of the wing (2) are respectively set there are two connecting rod (3),
One end of the connecting rod (3) is provided with connecting pin (9), and the other end of the connecting rod (3) is provided with anti-billiards (4), described
Connecting pin (9) is internally provided with mounting hole (10), is provided with connecting hole (15) below the mounting hole (10), and connecting hole
(15) setting is in the inside of wing (2), and the mounting hole (10) and connecting hole (15) are internally provided with bolt (11), the spiral shell
It is provided on the outer wall of bolt (11) lock nut (12), the lower surface of the lock nut (12) is provided with flat shim (13), institute
The lower surface for stating flat shim (13) is provided with spring shim (14), and the lower surface of the spring shim (14) is provided with casing
(16), and casing (16) is arranged in the inside of mounting hole (10) and connecting hole (15).
2. a kind of unmanned plane flight collision avoidance device according to claim 1, it is characterised in that: the helical-blade (6) sets
There are four setting, and the surrounding of four helical-blades (6) is provided with protective case (5).
3. a kind of unmanned plane flight collision avoidance device according to claim 1, it is characterised in that: support frame as described above (8)
Lower surface is provided with pedestal (7), and the upper surface of the other end of support frame (8) and pedestal (7) is welded to connect.
4. a kind of unmanned plane flight collision avoidance device according to claim 1, it is characterised in that: the connecting rod (3) sets
16 are equipped with, and is respectively set on each wing (2) there are four connecting rod (3).
5. a kind of unmanned plane flight collision avoidance device according to claim 1, it is characterised in that: the one of the bolt (11)
End is provided with protruding head (17), and protruding head (17) setting is in the inside of connecting hole (15).
6. a kind of unmanned plane flight collision avoidance device according to claim 1, it is characterised in that: the mounting hole (10)
Vertical center line is overlapped with the vertical center line of connecting hole (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920163965.0U CN209480003U (en) | 2019-01-30 | 2019-01-30 | A kind of unmanned plane flight collision avoidance device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920163965.0U CN209480003U (en) | 2019-01-30 | 2019-01-30 | A kind of unmanned plane flight collision avoidance device |
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| Publication Number | Publication Date |
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| CN209480003U true CN209480003U (en) | 2019-10-11 |
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| CN201920163965.0U Active CN209480003U (en) | 2019-01-30 | 2019-01-30 | A kind of unmanned plane flight collision avoidance device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112781550A (en) * | 2020-12-30 | 2021-05-11 | 镇江市勘察测绘研究院 | Unmanned aerial vehicle-based terrain mapping method for mine pit landform |
-
2019
- 2019-01-30 CN CN201920163965.0U patent/CN209480003U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112781550A (en) * | 2020-12-30 | 2021-05-11 | 镇江市勘察测绘研究院 | Unmanned aerial vehicle-based terrain mapping method for mine pit landform |
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