CN212766804U - Unmanned aerial vehicle emitter - Google Patents
Unmanned aerial vehicle emitter Download PDFInfo
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- CN212766804U CN212766804U CN202021761793.6U CN202021761793U CN212766804U CN 212766804 U CN212766804 U CN 212766804U CN 202021761793 U CN202021761793 U CN 202021761793U CN 212766804 U CN212766804 U CN 212766804U
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- unmanned aerial
- aerial vehicle
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Abstract
The utility model discloses an unmanned aerial vehicle emitter, including the device platform, the fixed surface of device platform is connected with the handle, the fixed surface of device platform is connected with and supports the seat of honour, the inner wall sliding connection who supports the seat of honour has the piston rod, it has the spring to support the seat of honour to have cup jointed, the fixed surface of piston rod is connected with the fixed plate, the bottom surface fixedly connected with hydraulic stem of fixed plate, the output fixedly connected with of hydraulic stem supports the seat down, the hydraulic stem is provided with the removal wheel keeping away from the one end that supports the seat of honour. The utility model discloses a motor drives the threaded rod and rotates, makes the removal piece remove to take place the angle of platform through the connecting rod adjustment, make launch unmanned aerial vehicle's angle more nimble, the quantity that takes place the bench transmission hole has four, can launch four unmanned aerial vehicle once, accomplishes unmanned aerial vehicle's sky overall arrangement fast, and the handle is convenient, and the delivery of whole device removes and takes turns to make things convenient for the device to remove.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle launches technical field, especially relates to an unmanned aerial vehicle emitter.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.
A device for unmanned aerial vehicle transmission on the existing market, most devices once only can launch an unmanned aerial vehicle, and the angle of unmanned aerial vehicle transmission can not change, and is not flexible enough.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle emitter who proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme: an unmanned aerial vehicle launching device comprises a device platform, wherein a handle is fixedly connected to the surface of the device platform, a supporting upper seat is fixedly connected to the lower surface of the device platform, a piston rod is slidably connected to the inner wall of the supporting upper seat, a spring is sleeved on the supporting upper seat, a fixing plate is fixedly connected to the surface of the piston rod, a hydraulic rod is fixedly connected to the bottom surface of the fixing plate, the output end of the hydraulic rod is fixedly connected with a supporting lower seat, a moving wheel is arranged at one end, away from the supporting upper seat, of the hydraulic rod, a first connecting plate is fixedly connected to one side of the device platform, one end of the first connecting plate is rotatably connected with a second connecting plate through a rotating shaft, a launching platform is fixedly connected to one end of the second connecting plate, a connecting rod is rotatably connected to the surface of the launching platform through a rotating shaft, a supporting groove is formed in the upper surface of the device platform, the other side of the inner wall of the supporting groove is fixedly connected with a motor, the surface of the threaded rod is in threaded connection with a moving block, and a transmitting hole is formed in the transmitting platform.
Preferably, the output end of the motor is fixedly connected with the threaded rod, and the surface of the moving block is rotatably connected with the connecting rod through the rotating shaft.
Preferably, the surface of the upper support seat is fixedly connected with a reinforcing rib, and the surface of the piston rod is connected with the lower support seat in a sliding manner.
Preferably, the number of the handles is two, and the positions of the two handles are symmetrically distributed on the surface of the device table.
Preferably, the number of the connecting rods, the supporting grooves, the threaded rods, the motors and the moving blocks is two, and the positions of the two connecting rods, the supporting grooves, the threaded rods, the motors and the moving blocks are symmetrically distributed on the upper surface of the device platform.
Preferably, the number of the emission holes is four, and the four emission holes are uniformly distributed in the emission platform.
The utility model discloses following beneficial effect has:
1. compared with the prior art, this unmanned aerial vehicle emitter drives the threaded rod through the motor and rotates, makes the movable block remove to take place the angle of platform through the connecting rod adjustment, make the angle of launching unmanned aerial vehicle more nimble, the quantity that takes place bench launch hole has four, can launch four unmanned aerial vehicles once, accomplishes unmanned aerial vehicle's sky overall arrangement fast, and the handle is convenient, and the consignment of whole device removes and takes turns to the device and removes.
2. Compared with the prior art, this unmanned aerial vehicle emitter should open the hydraulic stem before through launching unmanned aerial vehicle, and the hydraulic stem promotes to support down the seat and moves down and prop up the device, prevents that the device from appearing removing when the transmission, supports seat and piston rod and takes place to slide, and further compression spring cushions, makes the device have better stability when launching unmanned aerial vehicle and mobile device, reduces the harm that the device received.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention.
Fig. 2 is a schematic diagram of the internal structure of the present invention.
Fig. 3 is a side view of the launching pad structure of the present invention.
Illustration of the drawings:
1. a device table; 2. a handle; 3. supporting the upper seat; 4. a piston rod; 5. a spring; 6. a fixing plate; 7. a hydraulic lever; 8. supporting the lower seat; 9. a moving wheel; 10. a first connecting plate; 11. a second connecting plate; 12. a launch pad; 13. a connecting rod; 14. supporting the groove; 15. a threaded rod; 16. an electric motor; 17. a moving block; 18. an emission aperture.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-3, the utility model provides a pair of unmanned aerial vehicle emitter: the device comprises a device platform 1, a handle 2 is fixedly connected to the surface of the device platform 1, a supporting upper seat 3 is fixedly connected to the lower surface of the device platform 1, a piston rod 4 is slidably connected to the inner wall of the supporting upper seat 3, the supporting upper seat 3 is sleeved with a spring 5, a fixing plate 6 is fixedly connected to the surface of the piston rod 4, a hydraulic rod 7 is fixedly connected to the bottom surface of the fixing plate 6, a supporting lower seat 8 is fixedly connected to the output end of the hydraulic rod 7, the supporting upper seat 3 and the piston rod 4 slide to further compress the spring 5 for buffering and reduce the vibration of the device, a moving wheel 9 is arranged at one end of the hydraulic rod 7 far away from the supporting upper seat 3, a first connecting plate 10 is fixedly connected to one side of the device platform 1, one end of the first connecting plate 10 is rotatably connected with a second connecting plate 11 through a rotating shaft, one end of the second connecting plate 11 is fixedly, the upper surface of the device platform 1 is provided with a supporting groove 14, one side of the inner wall of the supporting groove 14 is rotatably connected with a threaded rod 15 through a rotating shaft, the other side of the inner wall of the supporting groove 14 is fixedly connected with a motor 16, the motor 16 drives the threaded rod 15 to rotate, a moving block 17 moves, the angle of the launching platform 12 is adjusted through a connecting rod 13, the surface of the threaded rod 15 is in threaded connection with the moving block 17, and a launching hole 18 is formed in the launching platform 12.
The output and the threaded rod 15 fixed connection of motor 16, the surface of movable block 17 rotates with connecting rod 13 through the pivot to be connected, support the fixed surface of seat of honour 3 and be connected with the strengthening rib, the surface of piston rod 4 with support down 8 sliding connection, the quantity of handle 2 has two, the position symmetric distribution of two handles 2 is on the surface of device platform 1, connecting rod 13, prop up groove 14, threaded rod 15, the quantity of motor 16 and movable block 17 has two, two connecting rods 13, prop up groove 14, threaded rod 15, the position symmetric distribution of motor 16 and movable block 17 is on the upper surface of device platform 1, the quantity of emission hole 18 has four, four emission hole 18 evenly distributed are in launching pad 12, the utility model discloses a pneumatic emission mode, because the pneumatic emission unmanned aerial vehicle technique is prior art, do not describe at the time.
The working principle is as follows: handle 2 is convenient, the delivery of the integrated device, it makes things convenient for the device to remove wheel 9, hydraulic stem 7 should be opened before launching unmanned aerial vehicle, hydraulic stem 7 promotes to support 8 downstream and props up the device, the preventing device removes when the transmission, take place to slide through supporting upper seat 3 and piston rod 4, further compression spring 5, cushion, make the device have better stability when launching unmanned aerial vehicle and mobile device, reduce the harm that the device received, open motor 16, motor 16 drives threaded rod 15 and rotates, make movable block 17 remove, thereby adjust the angle of launching pad 12 through connecting rod 13, make the angle of launching unmanned aerial vehicle more nimble, the quantity that takes place bench launching hole 18 has four, can launch four unmanned aerial vehicles once, accomplish unmanned aerial vehicle's sky overall arrangement fast.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle emitter, includes device platform (1), its characterized in that: the surface of the device platform (1) is fixedly connected with a handle (2), the lower surface of the device platform (1) is fixedly connected with an upper supporting seat (3), the inner wall of the upper supporting seat (3) is connected with a piston rod (4) in a sliding manner, the upper supporting seat (3) is sleeved with a spring (5), the surface of the piston rod (4) is fixedly connected with a fixed plate (6), the bottom surface of the fixed plate (6) is fixedly connected with a hydraulic rod (7), the output end of the hydraulic rod (7) is fixedly connected with a lower supporting seat (8), one end of the hydraulic rod (7) far away from the upper supporting seat (3) is provided with a movable wheel (9), one side of the device platform (1) is fixedly connected with a first connecting plate (10), one end of the first connecting plate (10) is rotatably connected with a second connecting plate (11) through a rotating shaft, one end of the second connecting plate (11) is fixedly connected, the surface of the launching platform (12) is rotatably connected with a connecting rod (13) through a rotating shaft, a supporting groove (14) is formed in the upper surface of the device platform (1), one side of the inner wall of the supporting groove (14) is rotatably connected with a threaded rod (15) through the rotating shaft, the other side of the inner wall of the supporting groove (14) is fixedly connected with a motor (16), a movable block (17) is connected to the surface of the threaded rod (15) in a threaded mode, and a launching hole (18) is formed in the launching platform (12).
2. An unmanned aerial vehicle emitter device according to claim 1, wherein: the output end of the motor (16) is fixedly connected with the threaded rod (15), and the surface of the moving block (17) is rotatably connected with the connecting rod (13) through a rotating shaft.
3. An unmanned aerial vehicle emitter device according to claim 1, wherein: the surface of the upper support seat (3) is fixedly connected with a reinforcing rib, and the surface of the piston rod (4) is connected with the lower support seat (8) in a sliding manner.
4. An unmanned aerial vehicle emitter device according to claim 1, wherein: the number of the handles (2) is two, and the positions of the two handles (2) are symmetrically distributed on the surface of the device table (1).
5. An unmanned aerial vehicle emitter device according to claim 1, wherein: the device comprises a device platform (1) and is characterized in that the number of the connecting rods (13), the supporting grooves (14), the threaded rods (15), the motors (16) and the moving blocks (17) is two, and the positions of the two connecting rods (13), the supporting grooves (14), the threaded rods (15), the motors (16) and the moving blocks (17) are symmetrically distributed on the upper surface of the device platform (1).
6. An unmanned aerial vehicle emitter device according to claim 1, wherein: the number of the emission holes (18) is four, and the four emission holes (18) are uniformly distributed in the emission platform (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021761793.6U CN212766804U (en) | 2020-08-21 | 2020-08-21 | Unmanned aerial vehicle emitter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021761793.6U CN212766804U (en) | 2020-08-21 | 2020-08-21 | Unmanned aerial vehicle emitter |
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| Publication Number | Publication Date |
|---|---|
| CN212766804U true CN212766804U (en) | 2021-03-23 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202021761793.6U Active CN212766804U (en) | 2020-08-21 | 2020-08-21 | Unmanned aerial vehicle emitter |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114110350A (en) * | 2021-12-02 | 2022-03-01 | 浙江天铂云科光电股份有限公司 | Intelligent recognition device based on temperature vision |
| CN118306596A (en) * | 2024-06-07 | 2024-07-09 | 中北大学 | Underwater anchoring type transmitting device for unmanned aerial vehicle |
-
2020
- 2020-08-21 CN CN202021761793.6U patent/CN212766804U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114110350A (en) * | 2021-12-02 | 2022-03-01 | 浙江天铂云科光电股份有限公司 | Intelligent recognition device based on temperature vision |
| CN118306596A (en) * | 2024-06-07 | 2024-07-09 | 中北大学 | Underwater anchoring type transmitting device for unmanned aerial vehicle |
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