CN217074826U - Unmanned aerial vehicle clamping device - Google Patents

Unmanned aerial vehicle clamping device Download PDF

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Publication number
CN217074826U
CN217074826U CN202220776036.9U CN202220776036U CN217074826U CN 217074826 U CN217074826 U CN 217074826U CN 202220776036 U CN202220776036 U CN 202220776036U CN 217074826 U CN217074826 U CN 217074826U
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China
Prior art keywords
block group
unmanned aerial
clamping device
aerial vehicle
push block
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Active
Application number
CN202220776036.9U
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Chinese (zh)
Inventor
刘维刚
杨万里
高伟
孙国龙
赵文瑞
毛智力
李振远
熊峰
林雨达
张小刚
杨振
朱雅琼
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State Grid Xinjiang Electric Power Co Ltd Changji Power Supply Co
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State Grid Xinjiang Electric Power Co Ltd Changji Power Supply Co
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Priority to CN202220776036.9U priority Critical patent/CN217074826U/en
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Publication of CN217074826U publication Critical patent/CN217074826U/en
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Abstract

The utility model provides an unmanned aerial vehicle clamping device: the device comprises a left hand grip, a right hand grip, a main body, a push block group and a cylinder; the utility model discloses a quick battery clamping device, including main part, lateral guide, left side tongs, right side tongs, push block group, cylinder output shaft, push block group fixed connection, the utility model discloses simple structure, convenient operation, low in production cost through cylinder work, can make push block group promote the guide block, makes the movable block remove at lateral guide to control left side tongs and right side tongs, reach quick open and shut purpose, realized quick centre gripping unmanned aerial vehicle, the effect of quick replacement battery.

Description

Unmanned aerial vehicle clamping device
Technical Field
The utility model mainly relates to an unmanned aerial vehicle's technical field specifically is an unmanned aerial vehicle clamping device.
Background
Unmanned aircraft, abbreviated "drone" and abbreviated "UAV", is an unmanned aircraft that is operated by a radio remote control device and self-contained programmed control means, or autonomously by an onboard computer, either completely or intermittently, and is often more suited to tasks that are too "fool, dirty, or dangerous" than a manned aircraft.
At present unmanned aerial vehicle clamping structure, like patent application number: 201811521055.1, which includes a base having wheels hinged to the bottom thereof, a brake rod is arranged on the outer side of the wheel, hydraulic telescopic rods are symmetrically arranged on the upper end surface of the base, the hydraulic telescopic rod is connected with a hydraulic cylinder, the upper end of the hydraulic telescopic rod is fixed with a support body, the supporting body is provided with sliding guide rails at the vertical crossing symmetrical positions and the four corners, the side surface of each sliding guide rail is provided with a long positioning hole, the sliding guide rail is provided with an arc-shaped support rod and a linear support rod through a slide block, the linear support rod is arranged in the vertical direction of the arc-shaped support rod, the sliding block is fixed on the sliding guide rail through the long positioning hole by the positioning column, and the clamping device has the advantages of simple structure, adjustable height, suitability for unmanned aerial vehicles with different sizes, convenience in movement and strong practicability.
To above-mentioned technique, the inventor thinks that, its structure is complicated, complex operation, manufacturing cost is higher relatively, can not quick centre gripping unmanned aerial vehicle, and it is slow to change the battery, has the limitation
SUMMERY OF THE UTILITY MODEL
Complicated in order to improve the structure, complex operation, manufacturing cost is higher relatively, can not quick centre gripping unmanned aerial vehicle, changes the slow problem of battery, the utility model provides an unmanned aerial vehicle clamping device.
The utility model adopts the following technical proposal: the device comprises a left hand grip, a right hand grip, a main body, a push block group and a cylinder; the improved pneumatic tool comprises a main body, and is characterized in that a transverse guide rail is installed at the upper end of the main body, the transverse guide rail is movably connected with a plurality of movable blocks, the lower ends of a left hand grip and a right hand grip are respectively connected with different movable blocks, the left hand grip and the right hand grip are both connected with guide blocks, a push block group is matched with the guide blocks, the side ends of the push block group are movably connected with the side ends of the main body, and an air cylinder output shaft is fixedly connected with the push block group.
Adopt above-mentioned technical scheme, through cylinder work, can make ejector pad group promote the guide block, make the movable block remove at transverse guide to make left side tongs and right side tongs remove, reach the purpose of quick opening and shutting, realized quick centre gripping unmanned aerial vehicle, the effect of quick replacement battery.
Furthermore, the guide block is provided with a waist-shaped hole, pulleys are symmetrically arranged on the pushing block group, and the pulleys are movably connected with the waist-shaped hole.
By adopting the technical scheme, the pulleys on the two sides of the push block group respectively slide in the waist-shaped hole of the guide block of the left hand grab and the waist-shaped hole of the guide block of the right hand grab, so that the left hand grab and the right hand grab can be rapidly opened and closed.
Furthermore, a vertical guide rail is arranged at the side end of the main body, a sliding block is arranged at the side end of the push block group, and the sliding block is movably connected with the vertical guide rail.
By adopting the technical scheme, the vertical movement of the push block group is ensured through the movable connection of the slide block and the vertical guide rail, and the limiting effect is achieved.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses simple structure, convenient operation, low in production cost through cylinder work, can make ejector pad group promote the guide block, makes the movable block remove at transverse guide to make left side tongs and right side tongs remove about, reach the purpose of quick opening and shutting, realized quick centre gripping unmanned aerial vehicle, the effect of quick replacement battery.
2. The pulleys on the two sides of the push block group slide in the waist-shaped hole of the guide block of the left hand grip and the waist-shaped hole of the guide block of the right hand grip respectively, so that the left hand grip and the right hand grip can be opened and closed quickly.
3. Through slider and vertical guide rail swing joint, guaranteed ejector pad group vertical motion, reached spacing effect.
The present invention will be explained in detail with reference to the drawings and specific embodiments.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic view of the structure of the push block set of the present invention.
In the figure: 1. a left hand grip; 2. a right hand grip; 3. a main body; 31. a transverse guide rail; 32. a movable block; 33. a vertical guide rail; 4. pushing the block group; 41. a pulley; 42. a slider; 5. a cylinder; 6. a guide block; 61. a kidney-shaped hole.
Detailed Description
In order to facilitate understanding of the present invention, the present invention will be described more fully with reference to the accompanying drawings, in which several embodiments of the present invention are shown, but the present invention can be implemented in different forms, and is not limited to the embodiments described in the text, but rather, these embodiments are provided to make the disclosure of the present invention more thorough and comprehensive.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may be present, and when an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present, as the terms "vertical", "horizontal", "left", "right" and the like are used herein for descriptive purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs, and the use of the terms herein in the specification of the present invention are for the purpose of describing particular embodiments only and are not intended to limit the present invention, and the use of the term "and/or" herein includes any and all combinations of one or more of the associated listed items.
The first embodiment is as follows:
please refer to fig. 1-2, a clamping device for an unmanned aerial vehicle: the device comprises a left hand grip 1, a right hand grip 2, a main body 3, a push block group 4 and a cylinder 5; transverse guide 31 is installed to 3 upper ends of main part, transverse guide 31 swing joint has a plurality of movable blocks 32, left side tongs 1 with 2 lower extremes of right side tongs respectively with the difference the movable block 32 is connected, left side tongs 1 with right side tongs 2 all is connected with guide block 6, push away block group 4 with the cooperation of guide block 6, push away 4 sides of block group with 3 side swing joint of main part, 5 output shafts of cylinder with push away 4 fixed connection of block group.
Please refer to fig. 1-2 again, the guide block 6 is provided with a kidney-shaped hole 61, the push block group 4 is symmetrically provided with pulleys 41, the pulleys 41 are movably connected with the kidney-shaped hole 61, the side end of the main body 3 is provided with a vertical guide rail 33, the side end of the push block group 4 is provided with a slide block 42, and the slide block 42 is movably connected with the vertical guide rail 33.
The embodiment of the utility model provides a pair of unmanned aerial vehicle clamping device's implementation principle does:
when the battery is replaced, the unmanned aerial vehicle is clamped, the air cylinder 5 is started to push out, the air cylinder 5 pushes out to drive the push block group 4 to move upwards, the push block group 4 drives the sliding block 42 to move upwards on the vertical guide rail 33, the pulleys 41 on two sides of the push block group 4 move upwards in the kidney-shaped holes 61 of the two different guide blocks 6 respectively, the guide blocks 6 are pushed, the left hand grab 1 and the right hand grab 2 are close to each other, the movable blocks 32 at the lower end of the left hand grab 1 and the lower end of the right hand grab 2 move relatively on the transverse guide rail 31, the unmanned aerial vehicle is clamped, and the battery is replaced; after the replacement is completed, the starting cylinder 5 retracts, the air retraction drives the push block group 4 to move downwards, the push block group 4 drives the sliding block 42 to move downwards on the vertical guide rail 33, the pulleys 41 on the two sides of the push block group 4 move downwards in the waist-shaped holes 61 of the two different guide blocks 6 respectively, the guide blocks 6 are pulled, the left hand gripper 1 and the right hand gripper 2 are separated, the movable blocks 32 at the lower ends of the left hand gripper 1 and the right hand gripper 2 move oppositely on the transverse guide rail 31, and the unmanned aerial vehicle is loosened.
The present invention has been described above with reference to the accompanying drawings, and it is obvious that the present invention is not limited by the above-mentioned manner, if the method and the technical solution of the present invention are adopted, the present invention can be directly applied to other occasions without substantial improvement, and the present invention is within the protection scope of the present invention.

Claims (3)

1. The utility model provides an unmanned aerial vehicle clamping device which characterized in that: comprises a left-side gripper (1), a right-side gripper (2), a main body (3), a push block group (4) and a cylinder (5);
transverse guide (31) are installed to main part (3) upper end, transverse guide (31) swing joint has a plurality of movable block (32), left side tongs (1) with right side tongs (2) lower extreme respectively with different movable block (32) are connected, left side tongs (1) with right side tongs (2) all are connected with guide block (6), push away piece group (4) with guide block (6) cooperation, push away piece group (4) side with main part (3) side swing joint, cylinder (5) output shaft with push away piece group (4) fixed connection.
2. The clamping device of claim 1, wherein: the guide block (6) is provided with a waist-shaped hole (61), pulleys (41) are symmetrically installed on the push block group (4), and the pulleys (41) are movably connected with the waist-shaped hole (61).
3. The clamping device of claim 1, wherein: the main part (3) side is equipped with vertical guide rail (33), it is equipped with slider (42) to push away the piece group (4) side, slider (42) with vertical guide rail (33) swing joint.
CN202220776036.9U 2022-04-02 2022-04-02 Unmanned aerial vehicle clamping device Active CN217074826U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220776036.9U CN217074826U (en) 2022-04-02 2022-04-02 Unmanned aerial vehicle clamping device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220776036.9U CN217074826U (en) 2022-04-02 2022-04-02 Unmanned aerial vehicle clamping device

Publications (1)

Publication Number Publication Date
CN217074826U true CN217074826U (en) 2022-07-29

Family

ID=82554816

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202220776036.9U Active CN217074826U (en) 2022-04-02 2022-04-02 Unmanned aerial vehicle clamping device

Country Status (1)

Country Link
CN (1) CN217074826U (en)

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