CN215043659U

CN215043659U - Electric power inspection unmanned aerial vehicle with quick detach horn

Info

Publication number: CN215043659U
Application number: CN202120329533.XU
Authority: CN
Inventors: 栾少荣; 王杰
Original assignee: Individual
Current assignee: Individual
Priority date: 2021-02-05
Filing date: 2021-02-05
Publication date: 2021-12-07
Anticipated expiration: 2031-02-05

Abstract

The utility model discloses an electric power inspection unmanned aerial vehicle with quick detach horn, including unmanned aerial vehicle body, horn, fixed block, draw-in groove, cavity and fixed establishment, the equal swing joint in the left and right sides of unmanned aerial vehicle body has the horn, the unmanned aerial vehicle body left and right sides just is located the top and the equal fixedly connected with fixed block in bottom of horn, the draw-in groove has been seted up to one side that the fixed block is close to the horn, the cavity has been seted up to the inside position that corresponds the draw-in groove of horn, the inside of cavity is provided with fixed establishment, fixed establishment includes two bearing frames, and two bearing frame symmetries are installed at the top and the bottom of cavity inner wall, and two bearing frame equal swing joint in one side in opposite directions have the threaded rod. The utility model discloses an unmanned aerial vehicle body, horn, fixed block, draw-in groove, cavity and fixed establishment mutually support, have played the effect that can quick assembly disassembly horn, easy operation, and labour saving and time saving has improved work efficiency, and the practicality is strong, is worth promoting.

Description

Electric power inspection unmanned aerial vehicle with quick detach horn

Technical Field

The utility model relates to an unmanned air vehicle technical field specifically is an unmanned aerial vehicle is patrolled and examined to electric power with quick detach horn.

Background

With the development of laser radar technology, the implementation of inspection work by using a helicopter to carry a laser radar system gradually becomes a new means of power line inspection. But the horn of traditional unmanned aerial vehicle can't realize quick assembly disassembly, and this will delay a lot of time, especially when unmanned aerial vehicle gets off from the transport vechicle and prepares the installation, needs complicated installation, has wasted a large amount of time.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle is patrolled and examined to electric power with quick detach horn to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: an electric power inspection unmanned aerial vehicle with a quick-release horn comprises an unmanned aerial vehicle body, horns, fixing blocks, clamping grooves, a cavity and a fixing mechanism, wherein the horns are movably connected to the left side and the right side of the unmanned aerial vehicle body;

the fixing mechanism comprises two bearing seats, the two bearing seats are symmetrically arranged at the top and the bottom of the inner wall of the cavity, one opposite sides of the two bearing seats are movably connected with a threaded rod, the surface of the threaded rod is in threaded connection with a threaded block, one side of the threaded block, which is close to the unmanned aerial vehicle body, is fixedly connected with a connecting block, one side of the connecting block, which is far away from the threaded block, is fixedly connected with a fixture block, the position of the fixing plate, which is close to one side of the clamping groove and corresponds to the clamping groove, one side of the fixture block, which is far away from the fixing plate, penetrates through the clamping groove and extends into the clamping groove, the fixture block is movably connected with the machine arm, the two fixing plates are fixedly connected through a telescopic rod, one end of the threaded rod, which is far away from the bearing seats, is fixedly connected with a driven gear, one side of the driven gear, which is far away from the unmanned aerial vehicle body, is provided with a driving gear, the driving gear and the driven gear are meshed with each other, the two driving gears are mutually away from the middle point of one side and are fixedly connected with driving rotating shafts, one end, away from the driving gear, of each driving rotating shaft sequentially penetrates through the cavity and the machine arm and extends to the outer fixedly connected with handle of the machine arm, and the driving rotating shafts are movably connected with the machine arm.

Preferably, the horn is close to the mid point department fixedly connected with locating piece of unmanned aerial vehicle body one side, the constant head tank has been seted up to the unmanned aerial vehicle body left and right sides and the position that corresponds the locating piece, the joint between locating piece and the constant head tank.

Preferably, the fixed block is movably connected with the machine arm.

Preferably, the surface of the connecting block is movably connected with the inner wall of the cavity.

Preferably, the surface of the fixing plate is movably connected with the inner wall of the cavity.

Compared with the prior art, the beneficial effects of the utility model are as follows:

the utility model discloses an unmanned aerial vehicle body, horn, fixed block, draw-in groove, cavity and fixed establishment mutually support, have played the effect that can quick assembly disassembly horn, easy operation, and labour saving and time saving has improved work efficiency, and the practicality is strong, is worth promoting.

Drawings

FIG. 1 is a structural section view in elevation of the present invention;

fig. 2 is an enlarged schematic view of a in fig. 1 according to the present invention.

In the figure: 1 unmanned aerial vehicle body, 2 horn, 3 fixed block, 4 draw-in grooves, 5 cavities, 6 fixed establishment, 601 bearing frame, 602 threaded rod, 603 screw block, 604 connecting block, 605 fixed plate, 606 fixture block, 607 telescopic link, 608 driven gear, 609 driving gear, 610 initiative pivot, 611 handle, 7 locating pieces, 8 constant head tank.

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.

Please refer to fig. 1-2, an electric power inspection unmanned aerial vehicle with quick detach horn, including unmanned aerial vehicle body 1, horn 2, fixed block 3, draw-in groove 4, cavity 5 and fixed establishment 6, the equal swing joint in left and right sides of unmanned aerial vehicle body 1 has horn 2, the top and the equal fixedly connected with fixed block 3 in bottom that unmanned aerial vehicle body 1 left and right sides just is located horn 2, swing joint between fixed block 3 and the horn 2, draw-in groove 4 has been seted up to one side that fixed block 3 is close to horn 2, cavity 5 has been seted up to the inside position that corresponds draw-in groove 4 of horn 2, the inside of cavity 5 is provided with fixed establishment 6, locating slot 8 has been seted up to the 1 left and right sides of unmanned aerial vehicle body and the position that corresponds locating piece 7, the joint between locating piece 7 and the locating slot 8.

The fixing mechanism 6 comprises two bearing seats 601, the two bearing seats 601 are symmetrically installed at the top and the bottom of the inner wall of the cavity 5, opposite sides of the two bearing seats 601 are movably connected with a threaded rod 602, the surface of the threaded rod 602 is in threaded connection with a threaded block 603, one side of the threaded block 603 close to the unmanned aerial vehicle body 1 is fixedly connected with a connecting block 604, the surface of the connecting block 604 is movably connected with the inner wall of the cavity 5, one side of the connecting block 604 far away from the threaded block 603 is fixedly connected with a fixing plate 605, the surface of the fixing plate 605 is movably connected with the inner wall of the cavity 5, one side of the fixing plate 605 close to the clamping groove 4 and corresponding to the clamping groove 4 is fixedly connected with a clamping block 606, one side of the clamping block 606 far away from the fixing plate 605 penetrates through the clamping groove 4 and extends into the clamping groove 4, the clamping block 606 is movably connected with the machine arm 2, and the two fixing plates 605 are fixedly connected through a telescopic rod 607, one end fixedly connected with driven gear 608 that bearing frame 601 was kept away from to threaded rod 602, one side that unmanned aerial vehicle body 1 was kept away from to driven gear 608 is provided with the driving gear 609, intermeshing between driving gear 609 and the driven gear 608, two driving gears 609 the equal fixedly connected with initiative pivot 610 of midpoint department of keeping away from one side each other, the one end that driving gear 609 was kept away from to initiative pivot 610 runs through cavity 5 and horn 2 in proper order and extends to the outside fixedly connected with handle 611 of horn 2, swing joint between initiative pivot 610 and the horn 2.

During the use, when the horn 2 needs to be dismantled, only need anticlockwise rotation handle 611, thereby it is rotatory to drive initiative pivot 610 and driving gear 609, thereby it is rotatory to drive driven gear 608 and threaded rod 602 in proper order by driving gear 609, thereby it drives connecting block 604 to make threaded block 603, fixed plate 605 and fixture block 606 move to the one side that is close to driven gear 608, compress telescopic link 607 simultaneously, until fixture block 606 breaks away from draw-in groove 4 completely can, then take horn 2 out from two fixed blocks 3, the same reason, when the horn 2 needs to be installed, insert positioning block 7 of horn 2 in the constant head tank 8, then clockwise rotation handle 611, thereby can make fixture block 606 insert and carry on spacingly in the draw-in groove 4, thereby can accomplish fixedly.

The utility model discloses the electrical components who appears in all are connected with external master controller electricity to the master controller can be for the computer etc. to play the conventional known equipment of control, the utility model discloses in circuit and control that relate to be prior art, do not carry out too much repetitious description here.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an unmanned aerial vehicle is patrolled and examined to electric power with quick detach horn, includes unmanned aerial vehicle body (1), horn (2), fixed block (3), draw-in groove (4), cavity (5) and fixed establishment (6), its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein the left side and the right side of the unmanned aerial vehicle body (1) are movably connected with machine arms (2), fixed blocks (3) are fixedly connected to the left side and the right side of the unmanned aerial vehicle body (1) and positioned at the top and the bottom of each machine arm (2), one sides, close to the machine arms (2), of the fixed blocks (3) are provided with clamping grooves (4), cavities (5) are formed in the machine arms (2) in positions corresponding to the clamping grooves (4), and fixing mechanisms (6) are arranged in the cavities (5);

the fixing mechanism (6) comprises two bearing seats (601), the two bearing seats (601) are symmetrically arranged at the top and the bottom of the inner wall of the cavity (5), one opposite sides of the two bearing seats (601) are movably connected with a threaded rod (602), the surface of the threaded rod (602) is in threaded connection with a threaded block (603), one side, close to the unmanned aerial vehicle body (1), of the threaded block (603) is fixedly connected with a connecting block (604), one side, far away from the threaded block (603), of the connecting block (604) is fixedly connected with a fixing plate (605), one side, close to one side of the clamping groove (4), of the fixing plate (605) is fixedly connected with a clamping block (606) corresponding to the clamping groove (4), one side, far away from the fixing plate (605), of the clamping block (606) penetrates through the clamping groove (4) and extends into the clamping groove (4), the clamping block (606) is movably connected with the clamping groove (4), and the clamping block (606) is movably connected with the machine arm (2), through telescopic link (607) fixed connection between two fixed plates (605), one end fixedly connected with driven gear (608) of bearing frame (601) are kept away from in threaded rod (602), one side that unmanned aerial vehicle body (1) was kept away from in driven gear (608) is provided with driving gear (609), intermeshing between driving gear (609) and driven gear (608), two driving gear (609) are kept away from the equal fixedly connected with initiative pivot (610) of midpoint department of one side each other, the outside fixedly connected with handle (611) that cavity (5) and horn (2) just extended to horn (2) are run through in proper order to the one end that driving gear (609) were kept away from in initiative pivot (610), swing joint between initiative pivot (610) and horn (2).

2. The power inspection unmanned aerial vehicle with quick detach horn of claim 1 characterized in that: the utility model discloses an unmanned aerial vehicle, including horn (2) and locating piece (7), the central point department fixedly connected with locating piece (7) that is close to unmanned aerial vehicle body (1) one side, locating slot (8) have been seted up to the position that unmanned aerial vehicle body (1) left and right sides just corresponds locating piece (7), the joint between locating piece (7) and locating slot (8).

3. The power inspection unmanned aerial vehicle with quick detach horn of claim 1 characterized in that: the fixed block (3) is movably connected with the machine arm (2).

4. The power inspection unmanned aerial vehicle with quick detach horn of claim 1 characterized in that: the surface of the connecting block (604) is movably connected with the inner wall of the cavity (5).

5. The power inspection unmanned aerial vehicle with quick detach horn of claim 1 characterized in that: the surface of the fixing plate (605) is movably connected with the inner wall of the cavity (5).