CN220548356U - Processing frock of carbon fiber unmanned aerial vehicle casing spare - Google Patents

Abstract

The utility model discloses a processing tool for a carbon fiber unmanned aerial vehicle shell part, which relates to the field of unmanned aerial vehicle processing and comprises a workbench, a supporting device, a horn positioning assembly and a driving device, wherein the supporting device is arranged at the center of the workbench and is used for supporting and lifting and adjusting the center of the unmanned aerial vehicle shell, a plurality of sliding grooves are formed in the workbench at equal intervals along the periphery of the supporting device, the horn positioning assembly is arranged in each sliding groove, the supporting device, the horn positioning assembly and the driving device are arranged, when different unmanned aerial vehicle shells are positioned and fixed, the unmanned aerial vehicle shell part can be lifted firstly, then the horn positioning assembly and the driving device are utilized to enable a top block to be inserted into a horn of the unmanned aerial vehicle shell, so that the unmanned aerial vehicle shell can be positioned and fixed, multiple profiling blocks are not required to be arranged according to the shape of the unmanned aerial vehicle, the positioning tool is high in adaptability, in addition, only two power elements of an electric cylinder and an electric push rod are required to be controlled in the positioning process, and the positioning process is convenient and quick.

Description

Processing frock of carbon fiber unmanned aerial vehicle casing spare

Technical Field

The utility model relates to the field of unmanned aerial vehicle machining, in particular to a machining tool for a carbon fiber unmanned aerial vehicle shell.

Background

The carbon fiber unmanned aerial vehicle shell part is formed by paving carbon fiber prepreg inside a die, sheathing the die into a vacuum bag, and sending the vacuum bag into an autoclave for forming, wherein after the manufacturing, redundant carbon fibers at a die assembly part are manually cut and polished, most unmanned aerial vehicle shells consist of a central shell and a plurality of machine arms, and the machine arms are also connected with extension arms for installing power elements;

this kind of unmanned aerial vehicle casing need utilize specific profile modeling piece and cooperation location frock to fix central casing after the shaping, just can cut it and polish, and a plurality of location frock need be prepared to the unmanned aerial vehicle central casing of current different shapes and size, and adaptability is not high, and the location process is comparatively troublesome, and current partial location frock in addition is after the location is accomplished, and its location clamp department leads to the fact sheltering from easily, leads to the unnecessary material of this place inconvenient cutting.

Disclosure of Invention

The utility model aims to provide a processing tool for a carbon fiber unmanned aerial vehicle shell piece, which aims to solve the problems in the background art.

The utility model provides a processing frock of carbon fiber unmanned aerial vehicle casing spare, includes workstation, strutting arrangement, horn locating component and drive arrangement, strutting arrangement locates the center of workstation for support and lift adjustment to unmanned aerial vehicle casing's center, be equipped with a plurality of spouts along strutting arrangement's circumference equidistance on the workstation, be equipped with horn locating component in the spout, the horn locating component includes baffle, slider and support column, the top fixedly connected with slider of baffle, slider sliding connection is in the spout, the top of slider is equipped with the support column, the top fixedly connected with kicking block of support column, the bottom of baffle rotates and is connected with the traveller, drive arrangement includes the actuating strip, the actuating strip is equipped with a plurality of along strutting arrangement's circumference equidistance, and its quantity is half of spout quantity, be equipped with the spacing groove on the actuating strip, two adjacent traveller sliding connection are in same spacing inslot, a plurality of the actuating strip drives the traveller and is close to and keep away from the workstation center when being close to and keep away from in step, makes the kicking block insert in the horn, realizes the fixed to unmanned aerial vehicle casing.

Preferably, the number of the sliding grooves is four, and the number of the driving strips is two.

Preferably, the supporting device comprises an electric cylinder, wherein the electric cylinder is arranged below the workbench and is fixedly connected with the workbench, and an output shaft of the electric cylinder penetrates through the center of the workbench and is fixedly connected with a bottom plate.

Preferably, the driving device further comprises a rack, a gear and an electric push rod, wherein the rack is fixedly connected to the driving rod, the gear is rotationally connected with the workbench, the rack is meshed with the gear, and when the gear rotates, the rack is mutually close to or mutually far away from the workbench, the rack is in sliding connection with a limiting block arranged on the workbench, the electric push rod is fixedly connected with the workbench, and an output shaft of the electric push rod is fixedly connected with one of the driving rods.

Preferably, the driving bar is fixedly connected with two sliding bars, and the sliding bars are in sliding connection with the workbench.

Preferably, the top block is conical and is made of rubber.

The utility model has the advantages that: through setting up strutting arrangement, horn locating component and drive arrangement, when fixing in the location to the unmanned aerial vehicle casing of difference, can go up and down unmanned aerial vehicle casing spare earlier, reuse horn locating component and drive arrangement make the kicking block can insert in the horn of unmanned aerial vehicle casing, can realize fixing in the location of unmanned aerial vehicle casing, need not to be equipped with multiple profile modeling locating piece according to unmanned aerial vehicle's shape, and adaptability is higher, and only needs two power original paper of control electric cylinder and electric putter in the location process, location process convenient and fast.

Drawings

Fig. 1 is a schematic structural diagram of the device after positioning a unmanned aerial vehicle shell;

FIG. 2 is a schematic view of the structure of the bottom of the workbench;

fig. 3 is a schematic view of the structure of the working table after being cut away.

In the figure: 1. a work table; 11. a chute; 2. a support device; 21. an electric cylinder; 22. a bottom plate;

3. a horn positioning assembly; 31. a baffle; 32. a slide block; 33. a support column; 34. a top block; 35. a spool;

4. a driving device; 41. a drive bar; 411. a limit groove; 42. a rack; 43. a gear; 44. an electric push rod; 45. a slide bar; 46. a limiting block; 5. unmanned aerial vehicle casing.

Detailed Description

The utility model is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand.

As shown in fig. 1 to 3, a processing frock of carbon fiber unmanned aerial vehicle casing spare, including workstation 1, strutting arrangement 2, horn locating component 3 and drive arrangement 4, strutting arrangement 2 locates the center of workstation 1 for support and lift adjustment to unmanned aerial vehicle casing 5's center, circumference equidistance along strutting arrangement 2 is equipped with a plurality of spouts 11 on the workstation 1, be equipped with horn locating component 3 in spout 11, horn locating component 3 includes baffle 31, slider 32 and support column 33, the top fixedly connected with slider 32 of baffle 31, slider 32 sliding connection is in spout 11, the top of slider 32 is equipped with support column 33, the top fixedly connected with kicking block 34 of support column 33, the bottom rotation of baffle 31 is connected with slide column 35, drive arrangement 4 includes driving strip 41, driving strip 41 is equipped with a plurality of along the circumference equidistance of strutting arrangement 2, and its quantity is half of spout 11 quantity, be equipped with spacing groove 411 on the driving strip 41, two adjacent slide column 35 sliding connection are in same place in the same slide groove and drive in two and are close to the same place in the slider 35 and drive column 35 and keep away from the realization of the synchronous machine casing 5 and insert in the same place in the workstation and keep away from the fixed station 5.

In this embodiment, the number of the sliding grooves 11 is four, and the number of the driving bars 41 is two.

In this embodiment, the supporting device 2 includes an electric cylinder 21, the electric cylinder 21 is disposed below the workbench 1 and is fixedly connected with the workbench 1, and an output shaft of the electric cylinder 21 passes through the center of the workbench 1 and is fixedly connected with a bottom plate 22.

In this embodiment, the driving device 4 further includes a rack 42, a gear 43 and an electric push rod 44, where the rack 42 is fixedly connected to the driving strip 41, the gear 43 is rotationally connected to the workbench 1, the rack 42 is meshed with the gear 43, and when the gear 42 rotates, the racks 42 are close to each other or far away from each other, and when the number of the unmanned aerial vehicle arms is greater than four, the number of the sliding grooves 11, the driving strip 41 and the racks 42 can be increased, and the racks are staggered from top to bottom to avoid interference, the rack 42 is slidably connected to a limiting block 46 provided on the workbench 1, the electric push rod 44 is fixedly connected to the workbench 1, and an output shaft of the electric push rod is fixedly connected to one of the driving strips 41.

In this embodiment, two sliding rods 45 are fixedly connected to the driving bar 41, and the sliding rods 45 are slidably connected to the workbench 1. The slide bar 45 is used to limit the drive bar 41.

In this embodiment, the top block 34 is conical and made of rubber. Avoiding damage to the horn.

The working process and the principle thereof are as follows:

the device is applied to the existing positioning of a plurality of multi-rotor unmanned aerial vehicle, the existing horn of the multi-rotor unmanned aerial vehicle is in a hollow state, and the extension arm can be inserted into the existing horn in a certain fixing mode to form a complete unmanned aerial vehicle.

When the unmanned aerial vehicle shell 5 needs to be positioned, the unmanned aerial vehicle is firstly placed on the bottom plate 22, a foundation support is carried out on the unmanned aerial vehicle, then the electric push rod 44 is started, the driving bar 41 on the output shaft of the electric push rod 44 is close to the gear 43, and the rest driving bars 41 are synchronously close to the gear 43 under the transmission action of the gear 43 and the rack 42.

When the driving bar 41 moves to the center, the sliding column 35 can be driven to move to the center under the action of the limiting slot 411 and move along the sliding slot 11 under the limiting action of the sliding slot 11, so that the plurality of top blocks 34 synchronously move to the center until the top blocks 34 approach the arm, and the electric push rod 44 is suspended.

Subsequently, the position of the unmanned aerial vehicle arm is adjusted, the height of the bottom plate 22 is adjusted by utilizing the electric cylinder 21, so that the axis of the top block 34 is aligned with the axis of the arm, finally, the electric push rod 44 is started again, so that the top block 34 is inserted into the unmanned aerial vehicle arm, the position of the unmanned aerial vehicle can be subjected to self-adaptive fine adjustment by adopting the conical structure of the top block 4, and finally, the positioning and fixing of the unmanned aerial vehicle are realized.

The carbon fiber unmanned aerial vehicle housing 5 can be finished and polished through a plurality of cutting and polishing devices.

It will be appreciated by those skilled in the art that the present utility model can be embodied in other specific forms without departing from the spirit or essential characteristics thereof. Accordingly, the above disclosed embodiments are illustrative in all respects, and not exclusive. All changes that come within the scope of the utility model or equivalents thereto are intended to be embraced therein.

Claims (6)

1. The utility model provides a processing frock of carbon fiber unmanned aerial vehicle casing spare, its characterized in that includes workstation (1), strutting arrangement (2), horn locating component (3) and drive arrangement (4), the center of workstation (1) is located to strutting arrangement (2) for support and lift adjustment to the center of unmanned aerial vehicle casing (5), circumference equidistance along strutting arrangement (2) is equipped with a plurality of spouts (11) on workstation (1), be equipped with horn locating component (3) in spout (11), horn locating component (3) include baffle (31), slider (32) and support column (33), the top fixedly connected with slider (32) of baffle (31), slider (32) sliding connection is in spout (11), the top of slider (32) is equipped with support column (33), the top fixedly connected with kicking block (34) of support column (33), the bottom rotation of baffle (31) is connected with sliding column (35), drive arrangement (4) are including drive strip (41), drive strip (2) are equipped with a plurality of equally spaced apart from one another in a plurality of limit grooves (41) along circumference of support strip (41), two adjacent sliding columns (35) are in sliding connection in the same limiting groove (411), and a plurality of driving strips (41) drive the sliding columns (35) to be close to and far away from the center of the workbench (1) when being close to and far away from synchronously, so that the top block (34) is inserted into the unmanned aerial vehicle arm, and the unmanned aerial vehicle shell (5) is fixed.

2. The machining tool for the carbon fiber unmanned aerial vehicle shell member according to claim 1, wherein the number of the sliding grooves (11) is four, and the number of the driving strips (41) is two.

3. The processing tool for the carbon fiber unmanned aerial vehicle shell member according to claim 1, wherein the supporting device (2) comprises an electric cylinder (21), the electric cylinder (21) is arranged below the workbench (1) and is fixedly connected with the workbench (1), and an output shaft of the electric cylinder (21) penetrates through the center of the workbench (1) and is fixedly connected with a bottom plate (22).

4. The machining tool for the carbon fiber unmanned aerial vehicle shell part according to claim 1, wherein the driving device (4) further comprises a rack (42), a gear (43) and an electric push rod (44), the driving strips (41) are fixedly connected with the rack (42), the gear (43) is rotationally connected with the workbench (1), the rack (42) is meshed with the gear (43), the racks (42) are mutually close to or mutually far away from each other when the gear (43) rotates, the rack (42) is in sliding connection with a limiting block (46) arranged on the workbench (1), the electric push rod (44) is fixedly connected with the workbench (1), and an output shaft of the electric push rod is fixedly connected with one of the driving strips (41).

5. The processing tool for the carbon fiber unmanned aerial vehicle shell member according to claim 1, wherein two sliding rods (45) are fixedly connected to the driving strip (41), and the sliding rods (45) are in sliding connection with the workbench (1).

6. The tooling for machining the shell of the carbon fiber unmanned aerial vehicle according to claim 1, wherein the top block (34) is conical and is made of rubber.