CN213008720U

CN213008720U - Processing equipment of unmanned aerial vehicle position adjusting device

Info

Publication number: CN213008720U
Application number: CN202022129378.5U
Authority: CN
Inventors: 刘仁华; 付森峰; 刘智国
Original assignee: Huizhou Zhonghe Aviation Technology Co ltd
Current assignee: Huizhou Zhonghe Aviation Technology Co ltd
Priority date: 2020-09-25
Filing date: 2020-09-25
Publication date: 2021-04-20
Anticipated expiration: 2030-09-25

Abstract

The utility model discloses a processing device of an unmanned aerial vehicle azimuth adjusting device, which comprises a machine body, a screw device, an azimuth adjusting device, a first holding tank, a first magnet, a first limit groove, a first push block, a first slide groove and a first wiring jack, wherein the screw device comprises a first shell, a support plate, a first motor, a first screw body, a spring plate, a limit block, a wiring plug, a second limit groove, a second push block, a second slide groove, a second magnet, a second holding tank, a third magnet and a second wiring jack, compared with the existing unmanned aerial vehicle, the designed screw device is modularized and combined, which is convenient for maintenance, and can also carry heavier objects by adding the screw device, the azimuth adjusting device designed by the utility model can assist the azimuth adjustment of the unmanned aerial vehicle, the flexible and rapid direction adjustment of the unmanned aerial vehicle can be realized.

Description

Processing equipment of unmanned aerial vehicle position adjusting device

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle position adjusting device's processing equipment.

Background

Unmanned aerial vehicle is an unmanned aerial vehicle who uses radio remote control or is by self program control as the owner, compare with manned aircraft, it has small, the cost is low, high durability and convenient use, require lowly to the operational environment, advantages such as battlefield viability is stronger, nevertheless the screw that current unmanned aerial vehicle used is fixed on the fuselage, can't increase and decrease the screw quantity according to the article weight of carrying of reality, also can not convenient change is overhauld, the position adjustment mode that current unmanned aerial vehicle adopted is the rotational speed through control screw motor and turns to the realization, but the unable quick realization unmanned aerial vehicle position adjustment of this kind of mode.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle position adjusting device's processing equipment to solve the problem that proposes in the above-mentioned background art.

In order to solve the technical problem, the utility model provides a following technical scheme: a processing device of an unmanned aerial vehicle direction adjusting device comprises a machine body, a propeller device, a direction adjusting device, a first accommodating groove, a first magnet, a first limit groove, a first push block, a first slide groove and a first wiring jack, wherein the propeller devices are distributed on the outer walls of two sides of the machine body and comprise a first machine shell, a support plate, a first motor, a first propeller body, an elastic sheet, a limit block, a wiring plug, a second limit groove, a second push block, a second slide groove, a second magnet, a second accommodating groove, a third magnet and a second wiring jack, the outer walls of two sides of the machine body are distributed with the first machine shell, the inner wall of one side of the first machine shell is fixedly connected with the support plate, the outer wall of the top end of the support plate is fixedly connected with the first motor, the outer wall of one side of the output end of the first motor is fixedly connected with the first propeller body, a second limiting groove is symmetrically formed in the outer wall of one side of the first casing, a second push block is connected to the inner wall of one side of the second limiting groove in a sliding mode, a second sliding block is fixedly connected to the outer wall of the top end of the second push block, second sliding grooves are symmetrically formed in the outer wall of the top end of the first casing, the second sliding block is connected to the inner wall of one side of each second sliding groove in a sliding mode, a second accommodating groove is symmetrically formed in the outer wall of one side of the first casing, a third magnet is fixedly connected to the inner wall of one side of each second accommodating groove, second wiring jacks are symmetrically formed in the outer walls of two sides of the first casing, and direction adjusting devices are symmetrically arranged on the outer walls of two sides of the machine body;

the direction adjusting device comprises a second motor, a screw rod, a bearing, a gear, a first rotating shaft, a through hole, a fixed block, a third motor, a second propeller body, a second rotating shaft and a second machine shell, a second motor is fixedly connected on the inner wall of one side of the machine body, a screw rod is fixedly connected on the outer wall of one side of the output end of the second motor, a bearing is fixedly connected on the inner wall of one side of the machine body, and the screw rod is rotationally connected on the inner wall of one side of the bearing, the outer wall of one side of the screw rod is engaged and connected with a gear, a first rotating shaft is fixedly connected on the inner wall of one side of the gear, through holes are symmetrically arranged on the outer walls of the two sides of the machine body, the first rotating shaft is rotatably connected to the inner wall of one side of the through hole, the outer wall of one side of the first rotating shaft is fixedly connected with a fixed block, fixedly connected with third motor on one side outer wall of fixed block, fixedly connected with second screw body on one side outer wall of third motor output.

Further, the symmetry is fixed with the second magnetite on the both sides outer wall of first casing, first holding tank has been seted up in the distribution on the both sides outer wall of fuselage, the first magnetite of fixedly connected with on the inner wall of one side of first holding tank, and the second magnetite adsorbs to be connected on the outer wall of one side of first magnetite.

Further, the shell fragment is symmetrically fixed on the outer wall of one side of the first casing, the stopper is fixedly connected to the outer wall of one side of the shell fragment, the outer walls of the two sides of the machine body are provided with first limiting grooves in a distributed manner, the stopper is clamped and connected to the inner wall of one side of the first limiting groove, the inner wall of one side of the first limiting groove is provided with a first push block in a sliding manner, the outer wall of the top end of the first push block is provided with a first sliding block in a fixed manner, the outer wall of the top end of the machine body is provided with a first sliding groove in a distributed manner, and the first sliding block is connected to the inner wall of one.

Furthermore, wiring plugs are symmetrically fixed on the outer walls of the two sides of the first casing, first wiring jacks are distributed on the outer walls of the two sides of the machine body, and the wiring plugs are inserted into the first wiring jacks.

Further, fixedly connected with second pivot on one side outer wall of fixed block, the symmetry is fixed with the second casing on the both sides outer wall of fuselage, and the second pivot rotates to be connected on one side inner wall of second casing.

Further, the second motor is of a stepping motor type.

Compared with the prior art, the utility model discloses the beneficial effect who reaches is: the utility model discloses a compare in current unmanned aerial vehicle, the screw device of design is the modularization combination formula, and not only the easy access can also carry heavier article through addding the screw device, the utility model discloses a position adjustment device can assist unmanned aerial vehicle's position adjustment, can realize that unmanned aerial vehicle is nimble, rapid carry out the position adjustment.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:

fig. 1 is a schematic top sectional structure of the present invention;

FIG. 2 is an enlarged view of the structure of the area A in FIG. 1;

fig. 3 is a top view and sectional structure diagram of the first housing of the present invention;

in the figure: 1. a body; 2. a propeller device; 3. an azimuth adjusting device; 4. a first accommodating groove; 5. a first magnet; 6. a first limit groove; 7. a first push block; 8. a first slider; 9. a first chute; 10. a first wiring receptacle; 21. a first housing; 22. a support plate; 23. a first motor; 24. a first propeller body; 25. a spring plate; 26. a limiting block; 27. a wiring plug; 28. a second limit groove; 29. a second push block; 210. a second slider; 211. a second chute; 212. a second magnet; 213. a second accommodating groove; 214. a third magnet; 215. a second wiring receptacle; 31. a second motor; 32. a screw rod; 33. a bearing; 34. a gear; 35. a first rotating shaft; 36. a through hole; 37. a fixed block; 38. a third motor; 39. a second propeller body; 310. a second rotating shaft; 311. a second housing.

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 efforts belong to the protection scope of the present invention.

Referring to fig. 1-3, the present invention provides a technical solution: a processing device of an unmanned aerial vehicle orientation adjusting device comprises a machine body 1, a propeller device 2, an orientation adjusting device 3, a first accommodating groove 4, a first magnet 5, a first limit groove 6, a first push block 7, a first slide block 8, a first slide groove 9 and a first wiring jack 10, wherein the propeller device 2 is distributed on the outer walls of two sides of the machine body 1, the propeller device 2 comprises a first machine shell 21, a support plate 22, a first motor 23, a first propeller body 24, an elastic sheet 25, a limit block 26, a wiring plug 27, a second limit groove 28, a second push block 29, a second slide block 210, a second slide groove 211, a second magnet 212, a second accommodating groove 213, a third magnet 214 and a second wiring jack 215, the first machine shell 21 is distributed on the outer walls of two sides of the machine body 1, the support plate 22 is fixedly connected to the inner wall of one side of the first machine shell 21, the first motor 23 is fixedly connected to the outer wall of the top end of the support plate 22, a first propeller body 24 is fixedly connected to the outer wall of one side of the output end of the first motor 23, a second limit groove 28 is symmetrically formed on the outer wall of one side of the first housing 21, a second push block 29 is slidably connected to the inner wall of one side of the second limit groove 28, a second slider 210 is fixedly connected to the outer wall of the top end of the second push block 29, a second chute 211 is symmetrically formed on the outer wall of the top end of the first housing 21, the second slider 210 is slidably connected to the inner wall of one side of the second chute 211, a second accommodating groove 213 is symmetrically formed on the outer wall of one side of the first housing 21, a third magnet 214 is fixedly connected to the inner wall of one side of the second accommodating groove 213, second wiring jacks 215 are symmetrically formed on the outer walls of two sides of the first housing 21, and orientation adjusting devices 3 are symmetrically arranged on the outer walls of two;

the azimuth adjusting device 3 comprises a second motor 31, a screw rod 32, a bearing 33, a gear 34, a first rotating shaft 35, a through hole 36, a fixed block 37, a third motor 38, a second propeller body 39, a second rotating shaft 310 and a second casing 311, wherein the second motor 31 is fixedly connected to the inner wall of one side of the machine body 1, the screw rod 32 is fixedly connected to the outer wall of one side of the output end of the second motor 31, the bearing 33 is fixedly connected to the inner wall of one side of the machine body 1, the screw rod 32 is rotatably connected to the inner wall of one side of the bearing 33, the gear 34 is engaged and connected to the outer wall of one side of the screw rod 32, the first rotating shaft 35 is fixedly connected to the inner wall of one side of the gear 34, the through holes 36 are symmetrically arranged on the outer walls of two sides of the machine body 1, the first rotating shaft 35 is rotatably connected to the inner wall of one side of the through hole 36, the, a second propeller body 39 is fixedly connected to the outer wall of one side of the output end of the third motor 38; the second magnets 212 are symmetrically fixed on the outer walls of two sides of the first machine shell 21, the first accommodating grooves 4 are distributed on the outer walls of two sides of the machine body 1, the inner wall of one side of each first accommodating groove 4 is fixedly connected with a first magnet 5, and the second magnets 212 are connected to the outer wall of one side of each first magnet 5 in an adsorption manner, so that the first machine shell 21 and the machine body 1 are tightly attached; an elastic sheet 25 is symmetrically fixed on the outer wall of one side of the first machine shell 21, a limiting block 26 is fixedly connected on the outer wall of one side of the elastic sheet 25, first limiting grooves 6 are distributed on the outer walls of two sides of the machine body 1, the limiting blocks 26 are connected to the inner wall of one side of the first limiting grooves 6 in a clamping manner and used for fixing the first machine shell 21, a first push block 7 is connected to the inner wall of one side of the first limiting grooves 6 in a sliding manner, a first slide block 8 is fixedly connected to the outer wall of the top end of the first push block 7, a first slide groove 9 is distributed on the outer wall of the top end of the machine body 1, the first slide block 8 is connected to the inner wall of one side of the first slide groove 9 in a sliding manner and used for pushing the limiting block 26; the outer walls of two sides of the first casing 21 are symmetrically fixed with wiring plugs 27, the outer walls of two sides of the machine body 1 are distributed with first wiring jacks 10, and the wiring plugs 27 are inserted into the first wiring jacks 10 for providing electric quantity; a second rotating shaft 310 is fixedly connected to the outer wall of one side of the fixed block 37, second housings 311 are symmetrically fixed to the outer walls of the two sides of the machine body 1, the second housings 311 are used for protecting the second propeller body 39, and the second rotating shaft 310 is rotatably connected to the inner wall of one side of the second housing 311; the second motor 31 is a stepping motor, which facilitates control of the deflection angle of the azimuth adjusting device 3;

when the propeller device 2 of the unmanned aerial vehicle is assembled, firstly, the wiring plug 27 on the first shell 21 is inserted into the first wiring jack 10 on the body 1, the elastic piece 25 and the limiting block 26 are inserted into the first limiting groove 6, and the second magnet 212 is inserted into the first accommodating groove 4 and mutually adsorbed with the first magnet 5; when the propeller device 2 is additionally installed, the wiring plug 27 on the first shell 21 of other propeller devices 2 can be inserted into the second wiring jack 215, the elastic piece 25 and the limiting block 26 are inserted into the second limiting groove 28, the second magnet 212 is inserted into the second accommodating groove 213 and mutually adsorbed with the third magnet 214, and when the propeller device is disassembled, the second sliding block 210 is only required to slide along the second sliding groove 211 to drive the second push block 29 to push the limiting block 26 so as to separate the limiting block 26 from the second limiting groove 28, so that the disassembly can be completed; use the utility model discloses when flying, start first motor 23 in the backup pad 22, drive first screw body 24 and rotate, make unmanned aerial vehicle lift off, start second motor 31 and drive lead screw 32 at bearing 33 internal rotation, drive gear 34, make first pivot 35 at the 36 internal rotations of through-hole, make 37 skew angles of fixed block, second pivot 310 is at 311 internal rotations of second casing this moment, stop through controlling opening of third motor 38, control second screw body 39's rotational speed, can the position of auxiliary adjustment unmanned aerial vehicle.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

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 may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle position adjusting device's processing equipment, includes fuselage (1), screw device (2), position adjusting device (3), first holding tank (4), first magnetite (5), first spacing groove (6), first ejector pad (7), first slider (8), first spout (9) and first wiring jack (10), its characterized in that: the propeller device (2) is distributed on the outer walls of two sides of the machine body (1), the propeller device (2) comprises a first machine shell (21), a supporting plate (22), a first motor (23), a first propeller body (24), an elastic sheet (25), a limiting block (26), a wiring plug (27), a second limiting groove (28), a second pushing block (29), a second sliding block (210), a second sliding groove (211), a second magnet (212), a second accommodating groove (213), a third magnet (214) and a second wiring jack (215), the first machine shell (21) is distributed on the outer walls of two sides of the machine body (1), the supporting plate (22) is fixedly connected on the inner wall of one side of the first machine shell (21), the first motor (23) is fixedly connected on the outer wall of the top end of the supporting plate (22), the first propeller body (24) is fixedly connected on the outer wall of one side of the output end of the first motor (23), a second limit groove (28) is symmetrically arranged on the outer wall of one side of the first shell (21), a second push block (29) is connected on the inner wall of one side of the second limit groove (28) in a sliding way, a second sliding block (210) is fixedly connected on the outer wall of the top end of the second push block (29), a second sliding chute (211) is symmetrically arranged on the outer wall of the top end of the first shell (21), and the second sliding block (210) is connected on the inner wall of one side of the second sliding chute (211) in a sliding way, a second accommodating groove (213) is symmetrically arranged on the outer wall of one side of the first shell (21), a third magnet (214) is fixedly connected on the inner wall of one side of the second accommodating groove (213), the outer walls of two sides of the first machine shell (21) are symmetrically provided with second wiring jacks (215), the outer walls of the two sides of the machine body (1) are symmetrically provided with azimuth adjusting devices (3);

the azimuth adjusting device (3) comprises a second motor (31), a screw rod (32), a bearing (33), a gear (34), a first rotating shaft (35), a through hole (36), a fixing block (37), a third motor (38), a second propeller body (39), a second rotating shaft (310) and a second casing (311), wherein the second motor (31) is fixedly connected to the inner wall of one side of the machine body (1), the screw rod (32) is fixedly connected to the outer wall of one side of the output end of the second motor (31), the bearing (33) is fixedly connected to the inner wall of one side of the machine body (1), the screw rod (32) is rotatably connected to the inner wall of one side of the bearing (33), the gear (34) is engaged and connected to the outer wall of one side of the screw rod (32), the first rotating shaft (35) is fixedly connected to the inner wall of one side of the gear (34), the through holes (36) are symmetrically formed in the outer walls, and first pivot (35) rotate to be connected on one side inner wall of through-hole (36), fixedly connected with fixed block (37) on one side outer wall of first pivot (35), fixedly connected with third motor (38) on one side outer wall of fixed block (37), fixedly connected with second screw body (39) on one side outer wall of third motor (38) output.

2. The processing equipment of an unmanned aerial vehicle position adjustment device of claim 1, characterized in that: the symmetry is fixed with second magnetite (212) on the both sides outer wall of first casing (21), first holding tank (4) have been seted up in the distribution on the both sides outer wall of fuselage (1), first magnetite of fixedly connected with (5) on one side inner wall of first holding tank (4), and second magnetite (212) adsorb to be connected on one side outer wall of first magnetite (5).

3. The processing equipment of an unmanned aerial vehicle position adjustment device of claim 1, characterized in that: the novel mechanical hand is characterized in that elastic pieces (25) are symmetrically fixed on the outer wall of one side of the first casing (21), limit blocks (26) are fixedly connected to the outer wall of one side of each elastic piece (25), first limit grooves (6) are distributed on the outer walls of the two sides of the machine body (1), the limit blocks (26) are clamped and connected to the inner wall of one side of each first limit groove (6), first push blocks (7) are connected to the inner wall of one side of each first limit groove (6) in a sliding mode, first sliding grooves (9) are distributed and formed in the outer wall of the top end of each first push block (7), and the first sliding blocks (8) are connected to the inner wall of one side of each first sliding groove (9) in a sliding mode.

4. The processing equipment of an unmanned aerial vehicle position adjustment device of claim 1, characterized in that: the portable multifunctional portable telephone is characterized in that wiring plugs (27) are symmetrically fixed on the outer walls of two sides of the first casing (21), first wiring jacks (10) are distributed on the outer walls of two sides of the machine body (1), and the wiring plugs (27) are inserted into the first wiring jacks (10).

5. The processing equipment of an unmanned aerial vehicle position adjustment device of claim 1, characterized in that: fixedly connected with second pivot (310) on the outer wall of one side of fixed block (37), the symmetry is fixed with second casing (311) on the both sides outer wall of fuselage (1), and second pivot (310) rotate to be connected on one side inner wall of second casing (311).

6. The processing equipment of an unmanned aerial vehicle position adjustment device of claim 1, characterized in that: the second motor (31) is of the type of a stepper motor.