CN211196669U

CN211196669U - Aerial survey unmanned aerial vehicle bracket

Info

Publication number: CN211196669U
Application number: CN201922400733.5U
Authority: CN
Inventors: 付妍
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-12-27
Filing date: 2019-12-27
Publication date: 2020-08-07
Anticipated expiration: 2029-12-27

Abstract

The utility model discloses an aerial survey unmanned aerial vehicle bracket relates to unmanned aerial vehicle bracket technical field. The novel electric cooker comprises a base, the inside of base is provided with the cavity, and the inside of cavity is provided with motor and battery, and the battery is located one side of motor, the upper end outer wall fixed mounting of motor has the disc, and the lateral wall of disc has seted up a plurality of circular slot, a plurality of the inside of circular slot all rotates and is connected with the ball, the upper end outer wall fixed mounting of base has the ring, and the ring is located the outside of disc, the ring channel has been seted up to the inside wall of ring, a plurality of ball and ring channel sliding connection, the upper end outer wall fixed mounting of disc has two fixed blocks, two the upper end outer wall of fixed block all sets up flutedly. The utility model discloses in, be convenient for play buffering and absorbing effect when aerial survey unmanned aerial vehicle descends on placing the board, stability when also can the person of facilitating the use increase aerial survey unmanned aerial vehicle show.

Description

Aerial survey unmanned aerial vehicle bracket

Technical Field

The utility model relates to an unmanned aerial vehicle bracket technical field especially relates to an aerial survey unmanned aerial vehicle bracket.

Background

Aerial survey unmanned aerial vehicle is the powerful supplement of traditional aerial photogrammetry means, have flexible, high-efficient quick, meticulous accuracy, the operating cost is low, application scope is wide, characteristics such as production cycle is short, have obvious advantage in the aspect of the high resolution image of small region and flight difficulty area acquires fast, along with the development of unmanned aerial vehicle and digital camera technique, digital aerial photography technique based on the unmanned aerial vehicle platform has demonstrate its unique advantage, but current aerial survey unmanned aerial vehicle bracket is not convenient for play buffering and absorbing effect when aerial survey unmanned aerial vehicle descends on placing the board, stability when also the person of also being convenient for increases aerial survey unmanned aerial vehicle show.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle bracket of aerial survey that proposes.

In order to achieve the above purpose, the utility model adopts the following technical scheme: an aerial survey unmanned aerial vehicle bracket comprises a base, wherein a cavity is arranged in the base, a motor and a storage battery are arranged in the cavity, the storage battery is positioned on one side of the motor, a disc is fixedly arranged on the outer wall of the upper end of the motor, a plurality of circular grooves are formed in the outer wall of the disc, balls are rotatably connected in the circular grooves, a circular ring is fixedly arranged on the outer wall of the upper end of the base and positioned outside the disc, a circular groove is formed in the inner side wall of the circular ring, the balls are slidably connected with the circular groove, two fixing blocks are fixedly arranged on the outer wall of the upper end of the disc, grooves are formed in the outer walls of the upper ends of the two fixing blocks, moving blocks are movably arranged in the two grooves, a placing disc is fixedly arranged on the outer wall of the upper ends of the two moving blocks, and, the outer wall of horizontal pole has cup jointed two lantern rings, and two lantern rings and place and all articulate between the dish and have the connecting rod, two all be provided with the second spring of cup jointing on the horizontal pole between lantern ring and the fixed block.

As a further description of the above technical solution:

a first spring is arranged between the groove and the moving block.

As a further description of the above technical solution:

the vertical sections of the groove and the moving block are T-shaped.

As a further description of the above technical solution:

and a baffle ring is fixedly arranged on the outer wall of the upper end of the placing disc.

As a further description of the above technical solution:

the specifications of a plurality of circular grooves are the same and are distributed in an annular array.

As a further description of the above technical solution:

and the motor is electrically connected with the storage battery.

Advantageous effects

The utility model provides an aerial survey unmanned aerial vehicle bracket. The method has the following beneficial effects:

(1): this aerial survey unmanned aerial vehicle bracket pushes the first spring in the recess through placing two movable blocks under the dish, drives the lantern ring extrusion second spring with placing the articulated connecting rod of dish to can play buffering and absorbing effect when aerial survey unmanned aerial vehicle descends and placing the board.

(2): this aerial survey unmanned aerial vehicle bracket is through opening the switch of motor through the user, and the motor drives the disc and rotates, and a plurality of ball rotates in the inside of circular slot, and a plurality of ball slides in the inside of ring channel to can reduce disc pivoted frictional force, also can increase disc pivoted stability, convenient to use person is to the omnidirectional show of aerial survey unmanned aerial vehicle, thereby stability when can the person of facilitating the use increase the show of aerial survey unmanned aerial vehicle.

Drawings

Fig. 1 is a schematic view of an overall structure of an aerial survey unmanned aerial vehicle bracket according to the present invention;

fig. 2 is a combined view of the moving block and the fixed block of the present invention;

fig. 3 is an enlarged view of fig. 2 at a according to the present invention;

fig. 4 is a combined view of the disc and the circular groove of the present invention.

Illustration of the drawings:

1. a base; 2. a circular ring; 3. a disc; 4. a motor; 5. an annular groove; 6. a circular groove; 7. a ball bearing; 8. a fixed block; 9. a moving block; 10. a first spring; 11. a cross bar; 12. a collar; 13. a second spring; 14. a connecting rod; 15. placing a tray; 16. and (4) a baffle ring.

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.

Referring to fig. 1-4, an aerial survey unmanned aerial vehicle bracket comprises a base 1, wherein a cavity is arranged inside the base 1, a motor 4 and a storage battery are arranged inside the cavity, the storage battery is positioned at one side of the motor 4, a disc 3 is fixedly arranged on the outer wall of the upper end of the motor 4, a plurality of circular grooves 6 are arranged on the outer wall of the disc 3, balls 7 are rotatably connected inside the circular grooves 6, a circular ring 2 is fixedly arranged on the outer wall of the upper end of the base 1, the circular ring 2 is positioned outside the disc 3, a circular groove 5 is arranged on the inner wall of the circular ring 2, the balls 7 are slidably connected with the circular groove 5, two fixed blocks 8 are fixedly arranged on the outer wall of the upper end of the disc 3, grooves are arranged on the outer walls of the upper ends of the two fixed blocks 8, moving blocks 9 are movably arranged inside the two grooves, and a placing disc 15 is fixedly, two fixed block 8 is preceding fixed mounting has horizontal pole 11, two lantern rings 12 have been cup jointed to the outer wall of horizontal pole 11, and two lantern rings 12 and place and all articulate between the dish 15 and have connecting rod 14, two all be provided with the second spring 13 of cup jointing on horizontal pole 11 between lantern ring 12 and the fixed block 8.

Can play buffering and absorbing effect when aerial survey unmanned aerial vehicle descends on placing the board, can increase 3 pivoted stability of disc, the person of being convenient for use is to the omnidirectional show of aerial survey unmanned aerial vehicle.

Referring to fig. 2, a first spring 10 is provided between the groove and the moving block 9.

Can play buffering and absorbing effect when aerial survey unmanned aerial vehicle lands on placing the platform.

Referring to fig. 2, the vertical cross-sections of the grooves and the moving block 9 are both T-shaped.

The groove can prevent the moving block 9 from moving out of the groove, and the moving block 9 is limited.

Referring to fig. 1-2, a stop ring 16 is fixedly mounted on the outer wall of the upper end of the placing plate 15.

The retaining ring 16 prevents the aerial survey drone from moving out of the placing tray 15.

Referring to fig. 2-3, a plurality of the circular grooves 6 have the same specification and are distributed in an annular array.

The distribution of the balls 7 can be made more uniform, thereby increasing the stability of the disc 3 when it rotates.

Referring to fig. 2, the motor 4 is electrically connected to the battery.

The accumulator can provide electrical energy for the motor 4.

The working principle is as follows: when the aerial survey unmanned aerial vehicle lands on the placing disc 15, the retaining ring 16 can prevent the aerial survey unmanned aerial vehicle from moving out of the placing disc 15, when the aerial survey unmanned aerial vehicle lands on the placing disc 15, the two moving blocks 9 under the placing disc 15 extrude the first springs 10 in the grooves, the connecting rod 14 hinged with the placing disc 15 drives the lantern ring 12 to extrude the second springs 13, so that the cushioning and shock-absorbing effects can be achieved when the aerial survey unmanned aerial vehicle lands on the placing plate, the motor 4 is opened by a user, the motor 4 drives the disc 3 to rotate, the plurality of balls 7 rotate in the circular groove 6, the plurality of balls 7 slide in the circular groove 5, so that the friction force generated by the rotation of the disc 3 can be reduced, the stability of the rotation of the disc 3 can be increased, the user can conveniently display the aerial survey unmanned aerial vehicle in all directions, and the stability of the user when the aerial survey unmanned aerial vehicle is displayed can, the motor 4 is a low-speed motor 4, the model of the motor 4 is 5IK60GU-CF, and the model of the storage battery is CW 12-4.

In the description herein, references to the description of "one embodiment," "an example," "a specific example," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. The aerial survey unmanned aerial vehicle bracket comprises a base (1) and is characterized in that a cavity is arranged inside the base (1), a motor (4) and a storage battery are arranged inside the cavity, the storage battery is positioned on one side of the motor (4), a disc (3) is fixedly mounted on the outer wall of the upper end of the motor (4), a plurality of circular grooves (6) are formed in the outer side wall of the disc (3), a plurality of balls (7) are rotatably connected inside the circular grooves (6), a ring (2) is fixedly mounted on the outer wall of the upper end of the base (1), the ring (2) is positioned outside the disc (3), a ring groove (5) is formed in the inner side wall of the ring (2), the plurality of balls (7) are slidably connected with the ring groove (5), two fixing blocks (8) are fixedly mounted on the outer wall of the upper end of the disc (3), and grooves are formed in the outer walls of the upper ends of the two fixing blocks (, the inside equal movable mounting of two recesses has movable block (9), and the upper end outer wall fixed mounting of two movable blocks (9) places dish (15), two fixed block (8) fixed mounting has horizontal pole (11) before, the outer wall of horizontal pole (11) has cup jointed two lantern rings (12), and all articulates between two lantern rings (12) and place dish (15) has connecting rod (14), two all be provided with second spring (13) of cup jointing on horizontal pole (11) between lantern ring (12) and fixed block (8).

2. An aerial survey drone carrier as claimed in claim 1, characterised in that a first spring (10) is provided between the groove and the moving mass (9).

3. An aerial survey drone carrier as claimed in claim 1, characterised in that the vertical cross-sections of the grooves and of the mobile blocks (9) are both T-shaped.

4. An aerial survey unmanned aerial vehicle carrier as claimed in claim 1, characterized in that, the outer wall of the upper end of placing disc (15) is fixedly mounted with a baffle ring (16).

5. An aerial survey drone carrier according to claim 1, characterised in that several of the circular slots (6) are of the same size and are distributed in an annular array.

6. An aerial survey drone carrier as claimed in claim 1, characterised in that there is an electrical connection between the motor (4) and the accumulator.