CN214238263U

CN214238263U - Clamping structure and mechanical arm with same

Info

Publication number: CN214238263U
Application number: CN202023249988.5U
Authority: CN
Inventors: 张光旭
Original assignee: Guangdong Hongyuan Intelligent Technology Co ltd
Current assignee: Guangdong Hongyuan Intelligent Technology Co ltd
Priority date: 2020-12-29
Filing date: 2020-12-29
Publication date: 2021-09-21
Anticipated expiration: 2030-12-29

Abstract

The utility model particularly discloses a press from both sides tight structure, including clamping device, clamping device includes: the supporting assembly comprises a supporting longitudinal frame and a supporting transverse frame, and the supporting longitudinal frame is vertically connected to the side end of the supporting transverse frame; the adjusting assembly is fixed on the supporting transverse frame and used for twisting the position of a power supply baffle rod of the unmanned aerial vehicle; the clamping component is located the side of the vertical frame of support and scalable round trip movement, and it is used for pressing from both sides the power of getting unmanned aerial vehicle. The utility model discloses a press from both sides tight structure simple operation in a flexible way, reduce the manual work and dismantle the battery, work efficiency is higher.

Description

Clamping structure and mechanical arm with same

Technical Field

The utility model relates to an unmanned air vehicle technique field, concretely relates to press from both sides tight structure and have its arm.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.

However, unmanned aerial vehicle needs artifical in person operation to dismantle its power battery after using a certain time, and operating procedure is comparatively complicated, and efficiency is low excessively.

SUMMERY OF THE UTILITY MODEL

The to-be-solved technical problem of the utility model is to overcome prior art not enough, provide a press from both sides tight structure. The clamping structure is convenient and flexible, manual disassembly of the battery is reduced, and the working efficiency is higher.

The utility model discloses the above-mentioned problem that will solve is through following technical scheme in order to realize:

a clamping arrangement comprising a clamping device, the clamping device comprising: the supporting assembly comprises a supporting longitudinal frame and a supporting transverse frame, and the supporting longitudinal frame is vertically connected to the side end of the supporting transverse frame; the adjusting assembly is fixed on the supporting transverse frame and used for twisting the position of a power supply baffle rod of the unmanned aerial vehicle; the clamping component is located the side of the vertical frame of support and scalable round trip movement, and it is used for pressing from both sides the power of getting unmanned aerial vehicle.

Preferably, two of the support longitudinal frames are selected and are distributed and fixed at the side ends of the support transverse frame side by side, and a placement cavity is formed between the support longitudinal frames.

Preferably, two clamping parts are selected and respectively arranged on the two supporting longitudinal frames.

Preferably, the clamping component is movably connected inside the first mounting cavity at the side end of the supporting longitudinal frame through a first telescopic driving component, so that the clamping component can be driven to move back and forth in the same direction.

Preferably, the clamping component can be a straight-line-shaped plate, and a clamping cavity is formed between the straight-line-shaped plate and the supporting transverse frame.

Preferably, the clamping member includes a rotating member and a second driving member fixed to a back of the supporting transversal frame and drivingly connected to the rotating member through the supporting transversal frame.

Preferably, the rotating component is a rotating column, a clamping groove is formed in the middle of the rotating column, and the inner wall of the clamping groove can be tightly attached to the outer wall of the power supply blocking rod.

Preferably, the front side end of the longitudinal support is fixed with a power start-stop control rod for starting or closing a power switch of the unmanned aerial vehicle.

Preferably, a mechanical arm comprises any one of the clamping structures, and further comprises a robot body, wherein the robot body is connected to the side end of the supporting transverse frame.

Has the advantages that: adopt structure after, when pressing from both sides tight structure and being close to unmanned aerial vehicle's power, the rotation of drive adjustment subassembly makes the installation direction of power spacer bar take place rotatoryly, and then makes the unmanned aerial vehicle power expose relatively before pressing from both sides tight structure, drives clamping part and pins the unmanned aerial vehicle power and goes out its pull immediately, alright realize that the simple operation is nimble, work efficiency is high, reduces the artifical function of dismantling the battery.

Drawings

Fig. 1 is a schematic view of a main structure of a clamping structure according to the present invention.

Fig. 2 is a clamping structure and unmanned aerial vehicle cooperation schematic diagram.

FIGS. 1-2: 1-a clamping device; 11-power start stop control lever; 12-a support assembly; 121-supporting a longitudinal frame; 1211 — a first mounting cavity; 122-supporting transverse frames; 13-an adjustment assembly; 131-a rotating member; 132-a second drive component; 14-placing a cavity; 15-a clamping member; 2-the unmanned aerial vehicle body; 21-power supply

Detailed Description

The present invention will be described in further detail with reference to the following drawings and specific examples, which are not intended to limit the present invention in any manner.

The directional designations of "front", "rear", "left" and "right" described in this specification are determined according to the schematic drawings used in this specification.

As shown in fig. 1-2, a clamping structure comprises a clamping device 1, wherein the clamping device 1 comprises a supporting assembly 12, an adjusting assembly 13 and a clamping component 15, the supporting assembly 12 comprises a supporting longitudinal frame 121 and a supporting transverse frame 122, and the supporting longitudinal frame 121 is vertically connected to the side end of the supporting transverse frame 122; the clamping component 15 is fixed on the supporting transverse frame 122, and is used for twisting the position of a power supply blocking rod of the unmanned aerial vehicle 2; the clamping parts 15 are located at the side ends of the supporting longitudinal frame 121 and can move back and forth in a telescopic mode, and the clamping parts 15 are used for clamping the power supply 21 of the unmanned aerial vehicle 2.

When pressing from both sides tight structure and being close to unmanned aerial vehicle's power, the rotation of drive adjustment subassembly makes the installation direction of power spacer bar take place rotatoryly, and then makes the unmanned aerial vehicle power expose relatively before pressing from both sides tight structure, drives clamping part and pins the unmanned aerial vehicle power and goes out its pull immediately, alright obtain the simple operation flexibility, work efficiency is high, reduces the artifical tight structure of clamp of dismantling the battery.

Specifically, support vertical frame 121 chooses for use two and be and distribute side by side and fix the side of supporting horizontal frame 122, and support and form between vertical frame 121 and place cavity 14, through controlling two vertical frame combinations can make the stability of placeeing after the unmanned aerial vehicle power presss from both sides tightly improved, guarantee the smoothness nature of work.

Specifically, the two clamping members 15 are selected and respectively located on the two longitudinal supporting frames 121, and the clamping stability of the power supply can be further improved by the mutual matching of the clamping members on the left side and the clamping members on the right side.

Specifically, the clamping component 15 is movably connected inside the first installation cavity at the side end of the longitudinal support frame 121 through a first telescopic driving component, so that the clamping component 15 can be driven to move back and forth in the same direction; the clamping component can be suitable for clamping more power supplies with different specifications through the operation of the first telescopic driving component, and the use functions of the clamping component are widened.

The clamping component 15 can be a linear plate, a clamping cavity is formed between the linear plate and the supporting transverse frame 122, the clamping cavity can be formed more quickly to clamp the power supply through the matching between the linear plate and the supporting transverse frame, and the power supply cannot be cut or damaged; of course, the clamping member 15 may also be a hook or other hook, and is not limited herein.

Specifically, the adjusting assembly 13 includes a rotating component 131 and a second driving component 132, the second driving component 132 is fixed to the back of the supporting transverse frame 122 and penetrates through the supporting transverse frame 122 to be in transmission connection with the rotating component 131, the rotating component 131 is rotated by 90 degrees by the driving of the second driving component 132, and then the position of the power supply blocking rod is adjusted by 90 degrees, which is a prerequisite for the smoothness of the subsequent clamping process.

The second driving member 132 is a rotary cylinder, but other rotary driving members may be used as the power.

Specifically, the rotating component 131 selects a rotating column, a clamping groove is formed in the middle of the rotating column, and the inner wall of the clamping groove can be tightly attached to the outer wall of the power supply blocking rod.

Specifically, the preceding side of supporting vertical frame 121 is fixed with power start-stop control lever 11, power start-stop control lever 11 is used for starting or closing unmanned aerial vehicle's switch, can start or close the unmanned aerial vehicle power more fast through power start-stop control lever.

A mechanical arm comprises the clamping structure and a robot body, wherein the robot body is connected to the side end of the supporting transverse frame 122, and a six-axis robot is selected and used for the robot body.

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. A clamping arrangement, comprising a clamping device, the clamping device comprising:

the supporting assembly comprises a supporting longitudinal frame and a supporting transverse frame, and the supporting longitudinal frame is vertically connected to the side end of the supporting transverse frame;

the adjusting assembly is fixed on the supporting transverse frame and used for twisting the position of a power supply baffle rod of the unmanned aerial vehicle;

the clamping component is located the side of the vertical frame of support and scalable round trip movement, and it is used for pressing from both sides the power of getting unmanned aerial vehicle.

2. A clamping structure as claimed in claim 1, wherein said supporting longitudinal frames are selected from two and fixed to the lateral ends of said supporting transversal frames in a side-by-side arrangement, and a housing cavity is formed between said supporting longitudinal frames.

3. A clamping arrangement according to claim 1, wherein two of said clamping members are provided on each of said two longitudinal support members.

4. The clamping structure as claimed in claim 1, wherein said clamping member is movably connected to the inside of the first mounting cavity at the side end of said supporting longitudinal frame by a first telescopic driving member, so that the clamping member can be driven back and forth in the same direction.

5. A clamping arrangement according to claim 1, wherein said clamping member is formed from a sheet material in the form of a channel, said channel forming a clamping cavity with said transverse support frame.

6. A clamping arrangement according to claim 1, wherein the clamping means comprises a rotary member and a second drive member secured to the back of the support cross frame and drivingly connected to the rotary member through the support cross frame.

7. The clamping structure as claimed in claim 6, wherein the rotating member is a rotating column, and a clamping groove is formed in the middle of the rotating column, and the inner wall of the clamping groove can be tightly attached to the outer wall of the power supply blocking rod.

8. The clamping structure as claimed in claim 1, wherein a power start and stop lever is fixed to the front side end of the supporting longitudinal frame for starting or stopping a power switch of the drone.

9. A robot arm comprising the clamp structure of any one of claims 1 to 8, and further comprising a robot body attached to a side end of the support cross frame.