CN218394297U

CN218394297U - Novel spraying plating device of aircraft parts of environmental protection

Info

Publication number: CN218394297U
Application number: CN202222657664.8U
Authority: CN
Inventors: 祁怀伟; 王亮兵; 徐涛涛
Original assignee: Avic Surface Treatment Technology Tianjin Co ltd
Current assignee: Avic Surface Treatment Technology Tianjin Co ltd
Priority date: 2022-10-10
Filing date: 2022-10-10
Publication date: 2023-01-31
Anticipated expiration: 2032-10-10

Abstract

The utility model discloses a novel spraying plating of aircraft spare part of environmental protection device relates to aircraft spare part spraying plating technical field, including collecting the frame, the last fixed surface of collecting the frame is connected with the support frame, the fixed embedding of right flank of collecting the frame has motor one. The utility model discloses a collect the frame, one support frame, motor, the threaded rod is one, turning block is one, cooperation setting between fixed frame and the antislip strip, it can drive threaded rod one and rotate to rotate the turning block one, make two fixed frames be close to each other, can fix board type aircraft spare part, conveniently spray plating, motor work can drive fixed frame rotation, can rotate fixed board type aircraft spare part, make board type aircraft spare part turn-ups automatically, avoid artifical turn-ups, can conveniently spray plating to the another side of board type aircraft spare part, work efficiency when can improving board type aircraft spare part spray plating.

Description

Novel environment-friendly spraying device for aircraft parts

Technical Field

The utility model relates to an aircraft spare part spraying plating technical field specifically is a novel spraying plating of aircraft spare part of environmental protection device.

Background

When the airplane is produced and assembled, the parts of the airplane are very important to be processed, and when the parts of the spoiler, the flap and the like are processed, spraying is needed to be carried out on the parts of the spoiler, the flap and the like so as to improve the corrosion resistance, the heat resistance and the wear resistance of the parts of the airplane. Therefore, a novel environment-friendly spraying device for aircraft parts is provided to solve the problems.

SUMMERY OF THE UTILITY MODEL

Solves the technical problem

The utility model aims at providing a novel environment-friendly spraying device for aircraft parts in order to make up the defects of the prior art.

Technical scheme

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a novel spraying plating of aircraft spare part of environmental protection device, includes collects the frame, the last fixed surface of collecting the frame is connected with the support frame, the fixed right flank of collecting the frame is fixed to be inlayed and is had motor one, the left surface threaded connection of support frame has threaded rod one, turning block one is installed to the left end of threaded rod one, fixed frame, two are all installed to the right-hand member of threaded rod one and the output of motor one the antislip strip is all installed, two to the inner wall of fixed frame the upper surface of fixed frame all installs fixed subassembly, the spacing groove has been seted up to the upper surface of support frame, the inner wall sliding connection of spacing groove has the movable block, reciprocating motion subassembly is installed to the inner wall of spacing groove, the liquid pipe is installed to the bottom of movable block, the fixed intercommunication in bottom surface of crossing the liquid pipe has a set of head, the last surface mounting of support frame has spraying plating material bin, spraying plating material bin and the liquid pipe between be linked together through the hose.

Foretell, fixed subassembly include threaded connection in the threaded rod two of fixed frame upper surface, turning block two is installed on the top of threaded rod two.

The bottom end of the second threaded rod is rotatably connected with a fixed plate, and a group of rubber pads are mounted on the bottom surface of the fixed plate.

Foretell, the fixed surface of the upper surface of fixed frame inlays and has two guide cylinders, two the equal sliding connection of inner wall of guide cylinder has the guide bar, and the bottom of guide bar is connected with the fixed surface of fixed plate.

The reciprocating moving assembly comprises a second motor fixedly embedded in the outer surface of the support frame, a reciprocating lead screw is fixedly connected to the output end of the second motor, a threaded sleeve is connected to the outer surface of the reciprocating lead screw in a threaded mode, and the threaded sleeve is fixedly embedded in the moving block.

Foretell, the upper surface threaded connection of spraying plating material bin has the case lid, the front of spraying plating material bin is fixed to be inlayed and is had the transparent plate.

Has the advantages that:

compared with the prior art, the novel environment-friendly spraying device for the aircraft parts has the following beneficial effects:

1. the utility model discloses a collect the frame, one support frame, motor, the threaded rod is one, turning block is one, cooperation setting between fixed frame and the antislip strip, it can drive threaded rod one and rotate to rotate the turning block one, make two fixed frames be close to each other, can fix board type aircraft spare part, conveniently spray plating, motor work can drive fixed frame rotation, can rotate fixed board type aircraft spare part, make board type aircraft spare part turn-over automatically, avoid artifical turn-over, can conveniently spray plating to the another side of board type aircraft spare part, work efficiency when improving board type aircraft spare part.

2. The utility model discloses a spacing groove, the movable block, motor two, reciprocal lead screw, the thread bush, cross the liquid pipe, the spraying coating head, the cooperation setting between spraying coating material bin and the hose, the inside spraying coating material of spraying coating material bin inside enters into the inside of crossing the liquid pipe through the hose, the spraying coating material of crossing the liquid intraduct can be through spraying coating head blowout, can carry out the spraying coating to board type aircraft spare part, two works of motor can drive reciprocal lead screw and rotate, can make the movable block be reciprocating motion at the inner wall of spacing groove, the convenient spraying coating to board type aircraft spare part.

Additional advantages, objects, and features of the invention will be set forth in part in the description which follows and in part will become apparent to those having ordinary skill in the art upon examination of the following or may be learned from practice of the invention.

Drawings

Fig. 1 is a schematic perspective view of the front view of the present invention;

fig. 2 is a schematic perspective view of the rear view of the present invention;

fig. 3 is a schematic connection diagram of the fixing frame and the fixing assembly of the present invention;

fig. 4 is a schematic perspective view of the reciprocating assembly of the present invention.

In the figure: 1. a collection frame; 2. a support frame; 3. a first motor; 4. a first threaded rod; 5. rotating the first block; 6. a fixing frame; 7. anti-slip strips; 8. a fixing assembly; 801. a second threaded rod; 802. rotating the second block; 803. a fixing plate; 804. a rubber pad; 805. a guide cylinder; 806. a guide bar; 9. a limiting groove; 10. a moving block; 11. a reciprocating assembly; 111. a second motor; 112. a reciprocating screw rod; 113. a threaded bushing; 12. a liquid passing pipe; 13. a spray head; 14. a spray material storage tank; 15. a hose; 16. a box cover; 17. a transparent plate.

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.

As shown in fig. 1-4, the utility model provides a technical solution: the utility model provides a novel spraying plating of aircraft spare part of environmental protection device, is including collecting frame 1, collects the last fixed surface of frame 1 and is connected with support frame 2, and the right flank of collecting frame 1 is fixed to be inlayed and is had motor 3, and the collection frame 1 of setting can conveniently collect unnecessary spraying plating material when spraying plating, avoids spraying plating material to cause the pollution to the environment.

The left side threaded connection of support frame 2 has threaded rod one 4, and turning block one 5 is installed to the left end of threaded rod one 4, and round antiskid line has been seted up to the surface of turning block one 5, rotates turning block one 5 and can drive threaded rod one 4 and rotate, utilizes the screw-thread fit between threaded rod one 4 and the support frame 2, and threaded rod one 4 rotates and to make the one end of threaded rod one 4 remove.

Fixed frame 6 is all installed to the right-hand member of threaded rod 4 and the output of motor 3, and the right-hand member that is located left fixed frame 6 and threaded rod 4 rotates and is connected, and fixed frame 6 that is located the right side and the output fixed connection of motor 3, the work of motor 3 can drive fixed frame 6 and rotate.

Antislip strip 7 is all installed to the inner wall of two fixed frames 6, and the antislip strip 7 of setting can increase the frictional force of the 6 inner walls of fixed frame, can conveniently fix to plate class aircraft spare part.

The upper surfaces of the two fixing frames 6 are respectively provided with a fixing assembly 8, each fixing assembly 8 comprises a second threaded rod 801 in threaded connection with the upper surface of the corresponding fixing frame 6, the top end of the second threaded rod 801 is provided with a second rotating block 802, the bottom end of the second threaded rod 801 is rotatably connected with a fixing plate 803, and the bottom surface of the fixing plate 803 is provided with a group of rubber pads 804 which are arranged at equal intervals.

The second rotating block 802 can drive the second threaded rod 801 to rotate, the second threaded rod 801 rotates to enable the fixing plate 803 to move downwards by means of threaded fit between the second threaded rod 801 and the fixing frame 6, the parts of the plate-type airplane can be fixed, the parts of the plate-type airplane are prevented from moving during spraying, and friction force on the bottom surface of the fixing plate 803 can be increased by the aid of the arranged rubber pad 804.

Two symmetrical guide cylinders 805 are fixedly embedded on the upper surface of the fixed frame 6, guide rods 806 are slidably connected to the inner walls of the two guide cylinders 805, and the bottom ends of the guide rods 806 are fixedly connected with the upper surface of the fixed plate 803.

When the second threaded rod 801 drives the fixing plate 803 to move, the guide rod 806 can slide on the inner wall of the guide cylinder 805, the fixing plate 803 can be guided and limited, and the stability of the fixing plate 803 in moving can be ensured.

The limiting groove 9 has been seted up to the upper surface of support frame 2, and the inner wall sliding connection of limiting groove 9 has movable block 10, and the limiting groove 9 of setting can lead and spacing to movable block 10, can make movable block 10 slide at the inner wall of limiting groove 9.

Reciprocating motion subassembly 11 is installed to the inner wall of spacing groove 9, and reciprocating motion subassembly 11 is including the fixed second 111 of inlaying in the motor of support frame 2 surface, and the output fixedly connected with of the second 111 of motor has reciprocating lead screw 112, and reciprocating lead screw 112's surface threaded connection has threaded sleeve 113, and threaded sleeve 113 is fixed to be inlayed in the inside of movable block 10.

The second motor 111 can drive the reciprocating screw rod 112 to rotate when working, and the reciprocating screw rod 112 can make the moving block 10 do reciprocating motion on the inner wall of the limiting groove 9 by utilizing the threaded fit between the reciprocating screw rod 112 and the threaded sleeve 113.

A liquid passing pipe 12 is installed at the bottom end of the moving block 10, a group of spraying heads 13 which are arranged at equal intervals are fixedly communicated with the bottom surface of the liquid passing pipe 12, a spraying material storage tank 14 is installed on the upper surface of the support frame 2, and the spraying material storage tank 14 is communicated with the liquid passing pipe 12 through a hose 15.

The thermal spraying material storage box 14 is internally provided with a heat source device for heating the thermal spraying material, the thermal spraying material in the thermal spraying material storage box 14 can enter the interior of the liquid passing pipe 12 through the hose 15 by the self power of the heat source in the thermal spraying material storage box 14, the thermal spraying material in the liquid passing pipe 12 can be sprayed out through the thermal spraying head 13, and the thermal spraying of the plate-type airplane parts can be carried out.

Spraying plating material storage box 14's upper surface threaded connection has case lid 16, opens case lid 16, can conveniently add spraying plating material to spraying plating material storage box 14's inside, and spraying plating material storage box 14's front is fixed to be inlayed and is had transparent plate 17, and the volume of the inside spraying plating material of spraying plating material storage box 14 can conveniently be observed to the transparent plate 17 of setting.

The working principle is as follows: the device is when using, at first place the board type aircraft spare part of treating processing between two fixed frames 6, it can drive threaded rod 4 to rotate turning block 5, thereby can make two fixed frames 6 be close to each other, can fix board type aircraft spare part, rotate turning block two 802 subsequently, turning block two 802 can drive threaded rod two 801 and rotate, thereby can make fixed plate 803 move under the direction of guide cylinder 805 and guide bar 806, can carry out the fixing once more to board type aircraft spare part, can guarantee the fixed effect to board type aircraft spare part, then through the inside heat source self power of spraying coating material bin 14, can make the inside spraying coating material of spraying coating material bin 14 pass through the inside of hose 15 entering liquid pipe 12, the inside spraying coating material of liquid pipe 12 can spout through spraying head 13, can carry out spraying coating to board type aircraft spare part, motor two 111 works and can drive reciprocating screw rod 112 and rotate, can make movable block 10 do reciprocating motion at the inner wall of spacing groove 9, conveniently carry out spraying coating to board type aircraft spare part, after the completion of board type aircraft spare part spraying, 3 after the one side of starting up, 3 can drive the board type aircraft spare part and can make the motor rotate the fixed frame 6 and carry out the automatic spraying to the another side of turning of board type aircraft spare part, thereby make the plane of the board type aircraft spare part rotate.

It should be noted that, in the present specification, the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, which are only for convenience of description of the present invention and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise expressly specified or limited, the terms "fixedly disposed," "mounted," "connected," and "connected" are to be construed broadly, e.g., "mounted" may be fixedly connected, or may be detachably connected, or may be integrally connected; "connected" may be mechanically or electrically connected; "connected" may be directly connected or indirectly connected through an intermediate medium, or may be a connection between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various 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. A novel environment-friendly spraying device for aircraft parts comprises a collecting frame (1), and is characterized in that: collect last fixed surface of frame (1) and be connected with support frame (2), the fixed surface of the right side of collecting frame (1) inlays and has motor (3), the left surface threaded connection of support frame (2) has threaded rod (4), turning block (5) are installed to the left end of threaded rod (4), fixed frame (6) are all installed to the right-hand member of threaded rod (4) and the output of motor (3), two antislip strip (7) are all installed to the inner wall of fixed frame (6), two fixed subassembly (8) are all installed to the upper surface of fixed frame (6), spacing groove (9) have been seted up to the upper surface of support frame (2), the inner wall sliding connection of spacing groove (9) has movable block (10), reciprocating motion subassembly (11) are installed to the inner wall of spacing groove (9), cross liquid pipe (12) is installed to the bottom of movable block (10), the fixed intercommunication in bottom surface of crossing liquid pipe (12) has a set of spraying head (13), the last surface mounting of support frame (2) has spraying material bin (14), spraying material bin (14) and cross between hose (12) and be linked together.

2. A novel and environmentally friendly aircraft component deposition apparatus as claimed in claim 1, further comprising: fixed subassembly (8) including threaded connection in threaded rod two (801) of fixed frame (6) upper surface, turning block two (802) are installed on the top of threaded rod two (801).

3. A novel and environmentally friendly aircraft component deposition apparatus as claimed in claim 2, further comprising: the bottom end of the second threaded rod (801) is rotatably connected with a fixing plate (803), and a group of rubber pads (804) are installed on the bottom surface of the fixing plate (803).

4. A novel and environmentally friendly aircraft component deposition apparatus as claimed in claim 3, further comprising: the upper surface of fixed frame (6) is fixed to inlay and is had two guide cylinders (805), two the equal sliding connection of inner wall of guide cylinder (805) has guide bar (806), and the upper surface fixed connection of the bottom of guide bar (806) and fixed plate (803).

5. A novel and environmentally friendly aircraft component deposition apparatus as claimed in claim 1, further comprising: the reciprocating movement assembly (11) comprises a second motor (111) fixedly embedded in the outer surface of the support frame (2), the output end of the second motor (111) is fixedly connected with a reciprocating screw rod (112), the outer surface of the reciprocating screw rod (112) is in threaded connection with a threaded sleeve (113), and the threaded sleeve (113) is fixedly embedded in the moving block (10).

6. A novel and environmentally friendly aircraft component deposition apparatus as claimed in claim 1, further comprising: the upper surface threaded connection of spraying material storage box (14) has case lid (16), the front of spraying material storage box (14) is fixed inlays and is had transparent plate (17).