CN210220822U

CN210220822U - Unmanned aerial vehicle counter-braking equipment

Info

Publication number: CN210220822U
Application number: CN201920932505.XU
Authority: CN
Inventors: Lechun Chen; 陈乐春
Original assignee: Digital Eagle Technology Yancheng Co Ltd
Current assignee: Digital Eagle Technology Yancheng Co Ltd
Priority date: 2019-06-20
Filing date: 2019-06-20
Publication date: 2020-03-31
Anticipated expiration: 2029-06-20

Abstract

The utility model discloses an unmanned aerial vehicle reverse system equipment, its structure includes the fixing base, be provided with the slide rail on the fixing base, the inside of slide rail is provided with the pulley, the top of pulley is provided with the dead lever, the top of dead lever is provided with the adjustment disk, be provided with fixing bolt and mount pad on the adjustment disk, fixing bolt swing joint be in the right side of adjustment disk, the mount pad fixed connection be in the upper surface of adjustment disk, be provided with the track groove on the mount pad, the inside in track groove is provided with slider and threaded rod, slider swing joint be in the inside in track groove, the threaded rod swing joint be in the left and right sides of mount pad, the upper end of slider is provided with the bracing piece. The utility model discloses speed when having accelerated the installation of unmanned aerial vehicle reverse system equipment has avoided the long-time back of using of unmanned aerial vehicle reverse system equipment to place the board and has appeared not hard up phenomenon, has improved the stability in the unmanned aerial vehicle reverse system equipment use.

Description

Unmanned aerial vehicle counter-braking equipment

Technical Field

The utility model relates to a reverse system equipment technical field specifically is an unmanned aerial vehicle reverse system equipment.

Background

According to patent 201721690256.5, an unmanned aerial vehicle reverse braking device comprises a tripod, wherein a horizontal fixing plate is arranged at the top of the tripod, a mounting seat is arranged at the top of the fixing plate, track grooves are formed in two sides of the top of the mounting seat, sliding blocks are arranged in the track grooves, a horizontal buffer spring is arranged between one side of each of the two sliding blocks and the track grooves, the tops of the two sliding blocks extend to the outside of the track grooves and are connected with horizontal placing plates, a vertically upward limiting plate is arranged on one side, away from each other, of each of the two placing plates, a vertical sliding cavity is arranged in each of the two limiting plates, mounting blocks are arranged in each of the two sliding cavities, a horizontal rotating positioning shaft is rotatably arranged in each of the two mounting blocks, and a vertically upward driving rod is rotatably connected to the tops of the mounting blocks, the top of actuating lever extends to the outside of limiting plate and is provided with the control block, two rotate to install the reverse rifle of unmanned aerial vehicle between the location axle, the both sides side of the reverse rifle of unmanned aerial vehicle all is provided with the locating piece, two all be provided with evenly distributed's locating hole on the locating piece, locating hole and rotation location axle looks adaptation.

At present, the existing unmanned aerial vehicle counter-braking equipment has some defects, such as; the speed when current unmanned aerial vehicle counter-braking equipment is installed is slower, place the board after unmanned aerial vehicle counter-braking equipment uses for a long time and appear not hard up phenomenon easily, the stability in the unmanned aerial vehicle counter-braking equipment use has been reduced, and current unmanned aerial vehicle counter-braking equipment can not let unmanned aerial vehicle counter-braking equipment carry out angle modulation in the use in addition, has reduced the application range of unmanned aerial vehicle counter-braking equipment, has weakened the flexibility in the unmanned aerial vehicle counter-braking equipment use. For this reason, new technical solutions need to be designed to solve the problem.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the problem that the plate is easy to loose after the unmanned aerial vehicle anti-system equipment among the prior art is used for a long time, the stability in the use of the unmanned aerial vehicle anti-system equipment is reduced, and the existing unmanned aerial vehicle anti-system equipment can not let the unmanned aerial vehicle anti-system equipment carry out angle modulation in the use, the application range of the unmanned aerial vehicle anti-system equipment is reduced, the flexibility in the use of the unmanned aerial vehicle anti-system equipment is weakened, and the unmanned aerial vehicle anti-system equipment that proposes.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle reverse braking device comprises a fixed seat, wherein a slide rail is arranged on the fixed seat, a pulley is arranged inside the slide rail, a fixed rod is arranged above the pulley, an adjusting disc is arranged above the fixed rod, a fixed bolt and a mounting seat are arranged on the adjusting disc, the fixed bolt is movably connected to the right side of the adjusting disc, the mounting seat is fixedly connected to the upper surface of the adjusting disc, a track groove is arranged on the mounting seat, a sliding block and a threaded rod are arranged inside the track groove, the sliding block is movably connected inside the track groove, the threaded rod is movably connected to the left side and the right side of the mounting seat, a support rod is arranged at the upper end of the sliding block, a jogged groove and a placing plate are arranged on the support rod, the jogged groove is positioned in the middle of the support rod, and the placing plate is fixedly connected, the upper surface of placing the board is provided with the limiting plate.

Preferably, the slide rail is circular and located inside the fixing seat, and the pulley is embedded inside the slide rail.

Preferably, the lower end of the fixed rod is connected with the pulley through a rivet and is embedded in the slide rail, the upper end of the fixed rod is connected with the bottom of the adjusting disc through threads, and the adjusting disc is connected with the upper surface of the fixed seat through a fixed bolt.

Preferably, the slider is fitted in the track groove, and the placement plate is connected to the slider through a support rod.

Preferably, the left end of the threaded rod is embedded in the embedding groove and movably connected with the inside of the supporting rod, and the right end of the threaded rod is connected with the mounting seat through threads.

Compared with the prior art, the utility model provides an unmanned aerial vehicle counter-braking equipment possesses following beneficial effect:

1. the utility model discloses a slider, the combination of threaded rod and gomphosis groove, twist out the threaded rod from the inside in track groove earlier, so that let the slider pass through the bracing piece and drive and place the board and remove in the top of mount pad, let the interval between the limiting plate adjust to the biggest, then put into the unmanned aerial vehicle reverse system equipment and place on the board, rotate the threaded rod again and let the slider remove in the inside in track groove, the one end of threaded rod can rotate in the inside of gomphosis groove, so that reach the limiting plate with the tight effect of unmanned aerial vehicle reverse system equipment clamp, effectual speed when accelerating the installation of unmanned aerial vehicle reverse system equipment, place the board after having avoided unmanned aerial vehicle reverse system equipment to use for a long time and appear not hard up phenomenon, the stability in the unmanned aerial vehicle reverse system equipment use has been improved.

2. The utility model discloses a slide rail, the pulley, the dead lever, adjustment disk and fixing bolt's combination, when needing angle regulation in the unmanned aerial vehicle reverse system equipment use, it is not hard up with fixing bolt earlier, rotate unmanned aerial vehicle reverse system equipment after that, at this moment the mount pad can drive the adjustment disk and rotate together, in adjustment disk pivoted, the dead lever can drive the pulley and rotate in the inside of slide rail, the effectual unmanned aerial vehicle reverse system equipment that has realized carries out angle modulation in the use, the application range of unmanned aerial vehicle reverse system equipment has been increased, the flexibility in the unmanned aerial vehicle reverse system equipment use has been improved.

Drawings

Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:

fig. 1 is a front view of a reverse braking device of an unmanned aerial vehicle according to the present invention;

fig. 2 is the utility model relates to a mount pad cross-sectional view of unmanned aerial vehicle reverse system equipment.

In the figure: the fixing seat comprises a fixing seat 1, a sliding rail 2, a pulley 3, a fixing rod 4, an adjusting disc 5, a fixing bolt 6, a mounting seat 7, a rail groove 8, a sliding block 9, a threaded rod 10, a supporting rod 11, an embedding groove 12, a placing plate 13 and a limiting plate 14.

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.

In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "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 simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

Referring to fig. 1-2, the present invention provides a technical solution: an unmanned aerial vehicle reverse braking device comprises a fixed seat 1, a slide rail 2 is arranged on the fixed seat 1, a pulley 3 is arranged inside the slide rail 2, a fixed rod 4 is arranged above the pulley 3, an adjusting disc 5 is arranged above the fixed rod 4, a fixed bolt 6 and a mounting seat 7 are arranged on the adjusting disc 5, the fixed bolt 6 is movably connected to the right side of the adjusting disc 5, the mounting seat 7 is fixedly connected to the upper surface of the adjusting disc 5, a track groove 8 is arranged on the mounting seat 7, a sliding block 9 and a threaded rod 10 are arranged inside the track groove 8, the sliding block 9 is movably connected inside the track groove 8, the threaded rod 10 is movably connected to the left side and the right side of the mounting seat 7, a support rod 11 is arranged at the upper end of the sliding block 9, an embedded groove 12 and a placing plate 13 are arranged on the support rod 11, the embedded groove 12 is positioned, the upper surface of the placing plate 13 is provided with a stopper plate 14.

Slide rail 2 is the ring shape to be located the inside of fixing base 1, pulley 3 gomphosis is in the inside of slide rail 2.

The lower extreme of dead lever 4 is connected with pulley 3 through the rivet to the gomphosis is in the inside of slide rail 2, and the upper end of dead lever 4 is connected with the bottom of adjusting disk 5 through the screw thread, and adjusting disk 5 is connected with the upper surface of fixing base 1 through fixing bolt 6.

The slider 9 is fitted in the track groove 8, and the mounting plate 13 is connected to the slider 9 via the support rod 11.

The left end of the threaded rod 10 is embedded in the embedding groove 12 and movably connected with the inside of the support rod 11, and the right end of the threaded rod 10 is connected with the mounting seat 7 through threads.

In the utility model, when the unmanned aerial vehicle reverse braking device is used, firstly, the threaded rod 10 is twisted out from the inside of the track groove 8, so that the slide block 9 drives the placing plate 13 to move above the mounting seat 7 through the support rod 11, the space between the limiting plates 14 is adjusted to the maximum, then the unmanned aerial vehicle reverse braking device is placed on the placing plate 13, then the threaded rod 10 is rotated to allow the slide block 9 to move in the track groove 8, so as to achieve the effect that the limiting plates 14 clamp the unmanned aerial vehicle reverse braking device, the speed of the unmanned aerial vehicle reverse braking device during installation is effectively accelerated, the phenomenon that the placing plate 13 is loosened after the unmanned aerial vehicle reverse braking device is used for a long time is avoided, the stability of the unmanned aerial vehicle reverse braking device during use is improved, when the angle of the unmanned aerial vehicle reverse braking device needs to be adjusted during use, the fixing bolt 6 is loosened firstly, rotate unmanned aerial vehicle anti-system equipment again after that, at this moment mount pad 7 can drive adjusting disk 5 and rotate together, when adjusting disk 5 rotated, dead lever 4 can drive pulley 3 and rotate in the inside of slide rail 2, and the effectual unmanned aerial vehicle anti-system equipment that has realized carries out angle modulation in the use, has increased the application range of unmanned aerial vehicle anti-system equipment, has improved the flexibility of unmanned aerial vehicle anti-system equipment in the use.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above, it will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, but that the invention may be embodied in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims

1. The utility model provides an unmanned aerial vehicle counter-braking equipment, includes fixing base (1), its characterized in that: the fixing seat is characterized in that a sliding rail (2) is arranged on the fixing seat (1), a pulley (3) is arranged inside the sliding rail (2), a fixing rod (4) is arranged above the pulley (3), an adjusting disc (5) is arranged above the fixing rod (4), a fixing bolt (6) and a mounting seat (7) are arranged on the adjusting disc (5), the fixing bolt (6) is movably connected to the right side of the adjusting disc (5), the mounting seat (7) is fixedly connected to the upper surface of the adjusting disc (5), a track groove (8) is arranged on the mounting seat (7), a sliding block (9) and a threaded rod (10) are arranged inside the track groove (8), the sliding block (9) is movably connected inside the track groove (8), the threaded rod (10) is movably connected to the left side and the right side of the mounting seat (7), a supporting rod (11) is arranged at the upper end of the sliding block (9), the supporting rod (11) is provided with a tabling groove (12) and a placing plate (13), the tabling groove (12) is located in the middle of the supporting rod (11), the placing plate (13) is fixedly connected to the upper end of the supporting rod (11), and a limiting plate (14) is arranged on the upper surface of the placing plate (13).

2. An unmanned aerial vehicle counteraction apparatus according to claim 1, wherein: the sliding rail (2) is annular and is positioned in the fixed seat (1), and the pulley (3) is embedded in the sliding rail (2).

3. An unmanned aerial vehicle counteraction apparatus according to claim 1, wherein: the lower end of the fixed rod (4) is connected with the pulley (3) through a rivet and is embedded in the sliding rail (2), the upper end of the fixed rod (4) is connected with the bottom of the adjusting disc (5) through threads, and the adjusting disc (5) is connected with the upper surface of the fixed seat (1) through a fixed bolt (6).

4. An unmanned aerial vehicle counteraction apparatus according to claim 1, wherein: the sliding block (9) is embedded in the track groove (8), and the placing plate (13) is connected with the sliding block (9) through a support rod (11).

5. An unmanned aerial vehicle counteraction apparatus according to claim 1, wherein: the left end of the threaded rod (10) is embedded in the embedding groove (12) and movably connected with the inside of the supporting rod (11), and the right end of the threaded rod (10) is connected with the mounting seat (7) through threads.