CN214351834U

CN214351834U - Clamping device for unmanned aerial vehicle part machining

Info

Publication number: CN214351834U
Application number: CN202022202995.3U
Authority: CN
Inventors: 梁丽娜; 孙勋; 孙克伦
Original assignee: Donghai County Tengxiang Aviation Technology Co ltd
Current assignee: Donghai County Tengxiang Aviation Technology Co ltd
Priority date: 2020-09-30
Filing date: 2020-09-30
Publication date: 2021-10-08
Anticipated expiration: 2030-09-30

Abstract

The utility model discloses an unmanned aerial vehicle is clamping device for parts machining, including workstation, fixed plate, second stopper and second fixed block, the inside of workstation all is provided with first stopper, and the inboard of first stopper is provided with first gim peg, and the outside of first gim peg is provided with first fixed block simultaneously, the fixed plate all sets up in the top of workstation, and the top of fixed plate is provided with first loop bar, the outside of first loop bar is provided with the second loop bar, and the place ahead of second loop bar is provided with the second gim peg, and one side of second gim peg is provided with the second stopper simultaneously. In this unmanned aerial vehicle is clamping device for parts machining, through setting up second loop bar and first loop bar, first loop bar has played fixed effect to the second loop bar, and the second loop bar has played the effect that reciprocates to the grip block, and convenient to use person adjusts not co-altitude according to not equidimension part to need not to dismantle the part, and the operation and simple.

Description

Clamping device for unmanned aerial vehicle part machining

Technical Field

The utility model relates to an unmanned aerial vehicle processing correlation technique field specifically is an unmanned aerial vehicle is clamping device for parts machining.

Background

The unmanned aerial vehicle is an unmanned aerial vehicle for short, and is also called as UAV (unmanned aerial vehicle) in English, the unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, a part needs to be clamped by a clamping device in the manufacturing process of the unmanned aerial vehicle, and therefore the clamping device for unmanned aerial vehicle part machining is needed.

But unmanned aerial vehicle clamping device for parts machining who uses at present, it is not convenient for change not equidimension grip block according to different processing part sizes, is not convenient for go up and down with the grip block, is not convenient for rotatory with the grip block.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle is clamping device for parts machining to solve the unmanned aerial vehicle clamping device for parts machining of the present use that proposes in the above-mentioned background art, it is not convenient for change not equidimension grip block according to different processing part sizes, is not convenient for go up and down the grip block, is not convenient for with the rotatory problem of grip block.

In order to achieve the above object, the utility model provides a following technical scheme: a clamping device for unmanned aerial vehicle part processing comprises a workbench, a fixing plate, a second limiting block and a second fixing block, wherein a first limiting block is arranged inside the workbench, a first fixing bolt is arranged on the inner side of the first limiting block, a first fixing block is arranged on the outer side of the first fixing bolt, the fixing plate is arranged above the workbench, a first loop bar is arranged above the fixing plate, a second loop bar is arranged on the outer side of the first loop bar, a second fixing bolt is arranged in front of the second loop bar, a second limiting block is arranged on one side of the second fixing bolt, the second fixing block is arranged on one side of the second loop bar, third fixing bolts are arranged at two ends of the second fixing block, a third limiting block is arranged on the outer side of one end of each third fixing bolt, a rotating shaft is arranged in front of each third limiting block, a first connecting block is arranged on one side of each rotating shaft, and the both ends of first connecting block all are provided with the second connecting block, the inboard of second connecting block is provided with the fourth gim peg, and the one end of fourth gim peg is provided with the grip block, and one side of grip block is provided with the non slipping spur simultaneously.

Preferably, the fixed plate forms a telescopic structure through the first limiting block and the first fixing bolt, and the fixed plate is symmetrically arranged along the central axis of the workbench.

Preferably, the second loop bar and the fixing plate form a lifting structure through the first loop bar, and the second loop bar is movably connected with the first loop bar.

Preferably, the second fixing bolt is in threaded connection with the second sleeve rod, and the outer side of the second fixing bolt and the inner side of the second sleeve rod are both in threaded arrangement.

Preferably, the third fixing bolts form a lifting structure with the rotating shaft through the second fixing blocks, and the third fixing bolts are symmetrically arranged with respect to the central axis of the rotating shaft.

Preferably, the fourth fixing bolt is in threaded connection with the clamping block, and one side of the clamping block is in open-hole design.

Preferably, the length of the inner side of the antiskid block is larger than that of the outer side of the clamping block, and the inner side of the antiskid block is tightly attached to the outer side of the clamping block.

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

1. this unmanned aerial vehicle is clamping device for parts machining through setting up second loop bar and first loop bar, and first loop bar has played fixed effect to the second loop bar, and the second loop bar has played the effect that reciprocates to the grip block, and convenient to use person adjusts not co-altitude according to not equidimension part to need not to dismantle the part, and the operation and simple.

2. This clamping device for unmanned aerial vehicle parts machining through setting up third gim peg, second fixed block and pivot, and the third gim peg has played the effect that reciprocates to the second fixed block, and the second fixed block has played fixed effect to the pivot, and the pivot is convenient for rotatory the grip block, and convenient to use person makes the part rotatory according to processing different part positions, and convenient to use person uses.

3. This clamping device for unmanned aerial vehicle parts machining through setting up fourth gim peg and grip block, and the fourth gim peg has played fixed effect to the grip block, and the grip block has played fixed effect to the part to convenient to use person is according to the grip block of the bigger equidimension of different part sizes, and easy operation is convenient, very big increase the practicality of device.

Drawings

Fig. 1 is a schematic view of the front cross-sectional structure of the present invention;

FIG. 2 is a schematic view of the front view of the present invention;

FIG. 3 is a schematic view of a side view cross-sectional structure of the first and second rods of the present invention;

fig. 4 is an enlarged schematic view of a portion a of fig. 1 according to the present invention.

In the figure: 1. a work table; 2. a first stopper; 3. a first securing latch; 4. a first fixed block; 5. a fixing plate; 6. a first loop bar; 7. a second loop bar; 8. a second securing latch; 9. a second limiting block; 10. a second fixed block; 11. a third securing latch; 12. a third limiting block; 13. a rotating shaft; 14. a first connection block; 15. a second connecting block; 16. a fourth securing latch; 17. a clamping block; 18. and (4) anti-skid blocks.

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.

Referring to fig. 1-4, the present invention provides a technical solution: a clamping device for unmanned aerial vehicle part processing comprises a workbench 1, a fixing plate 5, a second limiting block 9 and a second fixing block 10, wherein the workbench 1 is internally provided with the first limiting block 2, the inner side of the first limiting block 2 is provided with a first fixing bolt 3, the outer side of the first fixing bolt 3 is provided with the first fixing block 4, the fixing plate 5 is arranged above the workbench 1, the upper part of the fixing plate 5 is provided with a first sleeve rod 6, the outer side of the first sleeve rod 6 is provided with a second sleeve rod 7, the front part of the second sleeve rod 7 is provided with a second fixing bolt 8, one side of the second fixing bolt 8 is provided with the second limiting block 9, the second fixing block 10 is arranged at one side of the second sleeve rod 7, the two ends of the second fixing block 10 are provided with third fixing bolts 11, the outer side of one end of the third fixing bolt 11 is provided with a third limiting block 12, and the front part of the third limiting block 12 is provided with a rotating shaft 13, one side of the rotating shaft 13 is provided with a first connecting block 14, both ends of the first connecting block 14 are provided with second connecting blocks 15, the inner side of each second connecting block 15 is provided with a fourth fixing bolt 16, one end of each fourth fixing bolt 16 is provided with a clamping block 17, and one side of each clamping block 17 is provided with an anti-skid block 18.

Further, fixed plate 5 constitutes extending structure through first stopper 2 and first gim peg 3, and fixed plate 5 sets up with 1 axis symmetry of workstation, through setting up fixed plate 5, first stopper 2 and first gim peg 3, fixed plate 5 has played fixed effect to first loop bar 6, first stopper 2 has played fixed effect to fixed plate 5, first gim peg 3 has played the effect of removal to first stopper 2, and easy operation, convenient to use person uses.

Further, second loop bar 7 constitutes elevation structure through first loop bar 6 and fixed plate 5, and second loop bar 7 and first loop bar 6 swing joint, through setting up second loop bar 7 and first loop bar 6, first loop bar 6 has played fixed effect to second loop bar 7, and second loop bar 7 has played the effect that reciprocates to clamping block 17 to the operation is and simple.

Further, second gim peg 8 and second loop bar 7 threaded connection, and the 8 outsides of second gim peg and the inboard setting of second loop bar 7 are the screw thread form, and through setting up second gim peg 8 and second loop bar 7, second gim peg 8 has played fixed effect to second loop bar 7, and threaded setting installation dismantlement is simple and convenient, and convenient to use person uses.

Further, third gim peg 11 constitutes elevation structure through second fixed block 10 and pivot 13, and third gim peg 11 sets up with pivot 13 axis symmetry, and through setting up third gim peg 11, second fixed block 10 and pivot 13, third gim peg 11 has played the effect that reciprocates to second fixed block 10, second fixed block 10 has played fixed effect to pivot 13, pivot 13 is convenient for rotate grip block 17, convenient to use person uses.

Further, fourth gim peg 16 and grip block 17 threaded connection, and grip block 17 one side is the design of trompil formula, and through setting up fourth gim peg 16 and grip block 17, fourth gim peg 16 has played fixed effect to grip block 17, and grip block 17 has played fixed effect to the part to convenient to use person is according to the more not equidimension grip block 17 of different part sizes, and easy operation is convenient.

Further, inboard length of non slipping spur 18 and the outside length of grip block 17, and the non slipping spur 18 inboard big closely laminate with the grip block 17 outside, through setting up non slipping spur 18, non slipping spur 18 has increased the frictional force of grip block 17, and convenient to use person steps up the unmanned aerial vehicle part, avoids the unmanned aerial vehicle part to drop in the course of working, very big increase the practicality of device.

The working principle is as follows: for the clamping device for the unmanned aerial vehicle part processing, firstly, when the unmanned aerial vehicle part needs to be processed, the first fixing bolt 3 is rotated anticlockwise by hand, at the moment, the fixing plate 5 moves outwards, the clamping block 17 moves outwards, the unmanned aerial vehicle part is placed in the middle of the clamping block 17 by hand, the first fixing bolt 3 is rotated clockwise by hand, at the moment, the fixing plate 5 moves inwards, the clamping block 17 moves inwards, the first fixing bolt 3 is screwed up by clockwise rotation, at the moment, the unmanned aerial vehicle part is fixed by the clamping block 17, secondly, when different parts need to be processed, the fourth fixing bolt 16 is rotated anticlockwise by hand, the clamping block 17 is disassembled, the clamping block 17 with the corresponding part size is replaced, the fourth fixing bolt 16 is rotated and fixed clockwise, then when the clamping block 17 needs to be lifted, the second fixing bolt 8 is rotated anticlockwise by hand, remove second loop bar 7 to suitable height, grip block 17 moves to suitable height along with second loop bar 7 this moment, again with the hand with the clockwise rotation of second gim peg 8 fixed, at last when needs are rotatory with grip block 17, with the hand with third gim peg 11 anticlockwise rotation, again with the hand rotatory grip block 17, when grip block 17 is rotatory to suitable angle, with the hand with third gim peg 11 clockwise rotation fixed, accomplish whole unmanned aerial vehicle is clamping device's for parts machining use process so.

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 clamping device for parts machining, includes workstation (1), fixed plate (5), second stopper (9) and second fixed block (10), its characterized in that: the inner part of the workbench (1) is provided with a first limiting block (2), the inner side of the first limiting block (2) is provided with a first fixing bolt (3), the outer side of the first fixing bolt (3) is provided with a first fixing block (4), the fixing plate (5) is arranged above the workbench (1), a first sleeve rod (6) is arranged above the fixing plate (5), the outer side of the first sleeve rod (6) is provided with a second sleeve rod (7), the front of the second sleeve rod (7) is provided with a second fixing bolt (8), one side of the second fixing bolt (8) is provided with a second limiting block (9), the second fixing block (10) is arranged on one side of the second sleeve rod (7), the two ends of the second fixing block (10) are provided with third fixing bolts (11), the outer side of one end of each third fixing bolt (11) is provided with a third limiting block (12), and the place ahead of third stopper (12) is provided with pivot (13), one side of pivot (13) is provided with first connecting block (14), and the both ends of first connecting block (14) all are provided with second connecting block (15), the inboard of second connecting block (15) is provided with fourth gim peg (16), and the one end of fourth gim peg (16) is provided with grip block (17), and one side of grip block (17) is provided with non slipping spur (18) simultaneously.

2. The clamping device of claim 1, wherein the clamping device comprises: the fixed plate (5) and the first fixing bolt (3) form a telescopic structure through the first limiting block (2), and the fixed plate (5) is symmetrically arranged on the axis of the workbench (1).

3. The clamping device of claim 1, wherein the clamping device comprises: the second loop bar (7) and the fixing plate (5) form a lifting structure through the first loop bar (6), and the second loop bar (7) is movably connected with the first loop bar (6).

4. The clamping device of claim 1, wherein the clamping device comprises: the second fixing bolt (8) is in threaded connection with the second loop bar (7), and the outer side of the second fixing bolt (8) and the inner side of the second loop bar (7) are both in threaded arrangement.

5. The clamping device of claim 1, wherein the clamping device comprises: the third fixing bolts (11) and the rotating shaft (13) form a lifting structure through the second fixing blocks (10), and the third fixing bolts (11) are symmetrically arranged with the axis of the rotating shaft (13).

6. The clamping device of claim 1, wherein the clamping device comprises: the fourth fixing bolt (16) is in threaded connection with the clamping block (17), and one side of the clamping block (17) is in open-hole design.

7. The clamping device of claim 1, wherein the clamping device comprises: the length of the inner side of the anti-skid block (18) is larger than that of the outer side of the clamping block (17), and the inner side of the anti-skid block (18) is tightly attached to the outer side of the clamping block (17).