CN222079214U - Frock is used in assembly of aircraft system case - Google Patents

Frock is used in assembly of aircraft system case Download PDF

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Publication number
CN222079214U
CN222079214U CN202323589893.1U CN202323589893U CN222079214U CN 222079214 U CN222079214 U CN 222079214U CN 202323589893 U CN202323589893 U CN 202323589893U CN 222079214 U CN222079214 U CN 222079214U
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CN
China
Prior art keywords
fixedly connected
workbench
wall
valve core
cabinet body
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Active
Application number
CN202323589893.1U
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Chinese (zh)
Inventor
张增有
杨大清
许韬
吕转银
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Jiangsu Yuzhuang Technology Co ltd
Original Assignee
Yangzhou Yixing Machinery Co ltd
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Priority to CN202323589893.1U priority Critical patent/CN222079214U/en
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Publication of CN222079214U publication Critical patent/CN222079214U/en
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Abstract

The utility model discloses a tool for assembling a valve core of an aircraft system, which comprises a cabinet body, wherein one side of the outer wall of the cabinet body is rotationally connected with a cabinet door, the top surface of the cabinet body is fixedly connected with a workbench, the upper surface of the workbench is fixedly connected with a storage table, the upper surface of the workbench is fixedly connected with a clamping mechanism, and the upper surface of the workbench is fixedly connected with an adjusting mechanism. The utility model relates to the field of valve core assembly, and aims to solve the problem of unstable positioning of parts by arranging a clamping mechanism, driving a telescopic cylinder to operate by a motor and fixedly clamping a head and an auxiliary plate to fix a workpiece by one end of a telescopic rod, thereby reducing the working strength of dismounting the valve core. Through setting up porous fixed block and dead lever, the fixed porous fixed block of sliding plate upper surface has a plurality of holes of different specifications can place the dead lever of different specifications to the required size is established to the work piece cover of coping with different specifications.

Description

Frock is used in assembly of aircraft system case
Technical Field
The utility model relates to the field of valve core assembly, in particular to a tooling for assembling a valve core of an aircraft system.
Background
During the assembly or repair of an aircraft, the valve core of a plurality of parts needs to be assembled or disassembled, the valve core is arranged in a shell of the related parts, the valve core can be disassembled and assembled only from the orifice end of the shell, and the tool for disassembling and assembling the valve core is a key for determining the normal disassembly and assembly of the valve core of the aircraft system.
Although having a number of technical advantages. However, the disadvantage is that the traditional tool for assembling the valve core of the aircraft basically relies on manual holding when in use, and the problem of unstable positioning of parts exists, so that the working strength of disassembling the valve core is high.
Disclosure of utility model
Aiming at the defects of the prior art, the technical scheme adopted by the utility model for solving the technical problems is that the tooling for assembling the valve core of the aircraft system comprises a cabinet body, wherein one side of the outer wall of the cabinet body is rotationally connected with a cabinet door, the top surface of the cabinet body is fixedly connected with a workbench, the upper surface of the workbench is fixedly connected with a storage table, the upper surface of the workbench is fixedly connected with a clamping mechanism, and the upper surface of the workbench is fixedly connected with an adjusting mechanism.
As a preferred implementation mode, the fixture comprises a clamping table, the bottom surface of clamping table is fixedly connected with the upper surface of workstation, the upper surface fixedly connected with brace table of clamping table, the upper surface fixedly connected with motor of brace table, the one end of motor is rotated and is connected with flexible jar, the inner wall sliding connection of flexible jar has the telescopic link, the one end fixedly connected with gripping head of telescopic link, the upper surface fixedly connected with accessory plate of clamping table.
As a preferred implementation mode, the inner wall of one side of the cabinet body close to the cabinet door is fixedly connected with a built-in cabinet, the top surface of the cabinet body is fixedly connected with a fixed frame, and the outer wall of the fixed frame is fixedly connected with the outer wall of the workbench.
As a preferred implementation mode, the upper surface fixedly connected with base of workstation, the upper surface fixedly connected with first gag lever post of workstation, the one end fixedly connected with limiting plate of first gag lever post, the bottom surface of limiting plate and the top surface sliding connection of base.
As a preferred implementation mode, the top surface sliding connection of limiting plate has the sliding plate, the outer wall fixedly connected with second gag lever post of sliding plate one side, the outer wall of second gag lever post and the bottom surface fixed connection of putting the thing platform, the upper surface fixedly connected with porous fixed block of sliding plate, the inner wall sliding connection of porous fixed block has the dead lever.
As a preferred implementation mode, the adjusting mechanism comprises a fixed plate, the bottom surface of the fixed plate is fixedly connected with the upper surface of the workbench, a screw is connected with the inner wall of the fixed plate in a threaded manner, an adjusting hole is formed in one end of the screw, an adjusting head is fixedly connected with the other end of the screw, and one side, close to the limiting plate, of the adjusting head is in contact with the outer wall of the limiting plate.
The beneficial effects of the utility model are as follows:
1. According to the utility model, the clamping mechanism is arranged, the motor drives the telescopic cylinder to operate, and the workpiece is fixed by the clamping head and the auxiliary plate fixedly at one end of the telescopic rod, so that the problem of unstable positioning of parts is solved, and the working strength of dismounting the valve core is reduced.
2. According to the utility model, the porous fixing blocks and the fixing rods are arranged, and the porous fixing blocks fixed on the upper surface of the sliding plate are provided with a plurality of holes with different specifications, so that the fixing rods with different specifications can be placed, and the required size of the workpiece sleeve with different specifications can be dealt with.
Drawings
FIG. 1 is a front view of the present utility model;
FIG. 2 is a partial cross-sectional view of the present utility model;
FIG. 3 is a schematic view of the structure of the utility model at A;
FIG. 4 is a partial cross-sectional view of the present utility model;
FIG. 5 is a schematic view of the structure of the present utility model at B.
The device comprises a cabinet body 1, a built-in cabinet 11, a fixed frame 12, a cabinet door 2, a cabinet door 3, a workbench 31, a base 32, a first limiting rod 33, a limiting plate 34, a second limiting rod 35, a sliding plate 36, a porous fixing block 37, a fixing rod 4, a placing table 5, a clamping mechanism 51, a clamping table 52, a supporting table 53, a motor 54, a telescopic cylinder 55, a telescopic rod 56, a clamping head 57, an auxiliary plate 6, an adjusting mechanism 61, a fixing plate 62, a screw rod 621, an adjusting hole 63 and an adjusting head.
The utility model is described in further detail below with reference to the drawings and the detailed description. The embodiments of the utility model have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the utility model in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. The embodiments were chosen and described in order to best explain the principles of the utility model and the practical application, and to enable others of ordinary skill in the art to understand the utility model for various embodiments with various modifications as are suited to the particular use contemplated.
Examples
Referring to fig. 1-5, the utility model provides a tool for assembling a valve core of an aircraft system, which comprises a cabinet body 1, wherein one side of the outer wall of the cabinet body 1 is rotatably connected with a cabinet door 2, the top surface of the cabinet body 1 is fixedly connected with a workbench 3, the upper surface of the workbench 3 is fixedly connected with a storage table 4, the upper surface of the workbench 3 is fixedly connected with a clamping mechanism 5, and the upper surface of the workbench 3 is fixedly connected with an adjusting mechanism 6.
The fixture 5 includes the centre gripping platform 51, the bottom surface and the upper surface fixed connection of workstation 3 of centre gripping platform 51, the upper surface fixed connection of centre gripping platform 51 has supporting bench 52, the upper surface fixed connection of supporting bench 52 has motor 53, the one end rotation of motor 53 is connected with flexible jar 54, the inner wall sliding connection of flexible jar 54 has telescopic link 55, the one end fixedly connected with gripping head 56 of telescopic link 55, the upper surface fixed connection of centre gripping platform 51 has accessory plate 57.
The inner wall of the side of the cabinet body 1, which is close to the cabinet door 2, is fixedly connected with a built-in cabinet 11, the top surface of the cabinet body 1 is fixedly connected with a fixed frame 12, and the outer wall of the fixed frame 12 is fixedly connected with the outer wall of the workbench 3.
The upper surface fixedly connected with base 31 of workstation 3, the upper surface fixedly connected with first gag lever post 32 of workstation 3, the one end fixedly connected with limiting plate 33 of first gag lever post 32, the bottom surface of limiting plate 33 and the top surface sliding connection of base 31.
The top surface sliding connection of limiting plate 33 has sliding plate 35, and the outer wall fixedly connected with second gag lever post 34 of sliding plate 35 one side, the outer wall of second gag lever post 34 and the bottom surface fixed connection of putting thing platform 4, the upper surface fixedly connected with porous fixed block 36 of sliding plate 35, the inner wall sliding connection of porous fixed block 36 has dead lever 37.
The adjusting mechanism 6 comprises a fixed plate 61, the bottom surface of the fixed plate 61 is fixedly connected with the upper surface of the workbench 3, a screw 62 is connected with the inner wall of the fixed plate 61 in a threaded manner, an adjusting hole 621 is formed in one end of the screw 62, an adjusting head 63 is fixedly connected with the other end of the screw 62, and one side, close to the limiting plate 33, of the adjusting head 63 is in contact with the outer wall of the limiting plate 33.
When the device is used, the device main body is supported by the cabinet body 1, the cabinet body 1 is opened through the cabinet door 2, the built-in cabinet 11 fixedly connected in the device main body can play a purpose of conveniently storing workpieces, the transparent acrylic plate convenient to detach is fixed on the fixed frame 12 and used for protecting a working area on the isolation workbench 3, the base 31 is fixed on the workbench 3, one end of the upper surface rod of the workbench 3 is fixed on the limiting plate 33, the screw rod 62 on the fixed plate 61 is rotated through the adjusting hole 621 in the adjusting mechanism 6, the adjusting head 63 fixed on the screw rod 62 can push or pull the limiting plate 33 under the action of threaded connection, the first limiting rod 32 and the second limiting rod 34 are piston rods, the top surface of the limiting plate 33 is slidably connected with the sliding plate 35, the outer wall on one side of the sliding plate 35 is fixed with the second limiting rod 34, the second limiting rod 34 is fixed on the bottom surface of the object placing table 4, the porous fixed block 36 on the sliding plate 35 is provided with a plurality of holes 37 with different specifications, so that the fixing rods 37 with different specifications can be placed on the auxiliary motor 5, the auxiliary motor can be moved on the clamping cylinder 57 or the auxiliary motor 5 to be moved on the clamping cylinder 57 through the large part of the auxiliary motor 5, namely, the auxiliary motor 57 is far from the clamping cylinder 57, and the auxiliary motor 57 is driven to be placed on the clamping table 53, and is far away from the clamping cylinder 57, or is far from the clamping table 57, and is far from the clamping motor, or is far from the clamping motor, and is far from the workpiece is far from the clamping motor.
It will be apparent that the described embodiments are only some, but not all, embodiments of the utility model. All other embodiments, which can be made by those skilled in the art and which are included in the embodiments of the present utility model without the inventive step, are intended to be within the scope of the present utility model. Structures, devices and methods of operation not specifically described and illustrated herein are implemented by conventional means in the art unless specifically indicated and limited by the context.

Claims (6)

1. The tool for assembling the valve core of the aircraft system comprises a cabinet body (1) and is characterized in that one side of the outer wall of the cabinet body (1) is rotationally connected with a cabinet door (2), the top surface of the cabinet body (1) is fixedly connected with a workbench (3), the upper surface of the workbench (3) is fixedly connected with a storage table (4), the upper surface of the workbench (3) is fixedly connected with a clamping mechanism (5), and the upper surface of the workbench (3) is fixedly connected with an adjusting mechanism (6).
2. The tool for assembling the valve core of the aircraft system according to claim 1, wherein the clamping mechanism (5) comprises a clamping table (51), the bottom surface of the clamping table (51) is fixedly connected with the upper surface of the workbench (3), a supporting table (52) is fixedly connected with the upper surface of the clamping table (51), a motor (53) is fixedly connected with the upper surface of the supporting table (52), one end of the motor (53) is rotatably connected with a telescopic cylinder (54), the inner wall of the telescopic cylinder (54) is slidably connected with a telescopic rod (55), one end of the telescopic rod (55) is fixedly connected with a clamping head (56), and an auxiliary plate (57) is fixedly connected with the upper surface of the clamping table (51).
3. The tool for assembling the valve core of the aircraft system according to claim 1, wherein the inner wall of one side, close to the cabinet door (2), of the cabinet body (1) is fixedly connected with a built-in cabinet (11), the top surface of the cabinet body (1) is fixedly connected with a fixed frame (12), and the outer wall of the fixed frame (12) is fixedly connected with the outer wall of the workbench (3).
4. The tool for assembling the valve core of the aircraft system according to claim 1, wherein the base (31) is fixedly connected to the upper surface of the workbench (3), the first limiting rod (32) is fixedly connected to the upper surface of the workbench (3), the limiting plate (33) is fixedly connected to one end of the first limiting rod (32), and the bottom surface of the limiting plate (33) is slidably connected with the top surface of the base (31).
5. The tool for assembling the valve core of the aircraft system according to claim 4, wherein the top surface of the limiting plate (33) is slidably connected with a sliding plate (35), the outer wall of one side of the sliding plate (35) is fixedly connected with a second limiting rod (34), the outer wall of the second limiting rod (34) is fixedly connected with the bottom surface of the object placing table (4), the upper surface of the sliding plate (35) is fixedly connected with a porous fixing block (36), and the inner wall of the porous fixing block (36) is slidably connected with a fixing rod (37).
6. The tool for assembling the valve core of the aircraft system according to claim 4, wherein the adjusting mechanism (6) comprises a fixed plate (61), the bottom surface of the fixed plate (61) is fixedly connected with the upper surface of the workbench (3), a screw (62) is connected with the inner wall of the fixed plate (61) in a threaded manner, an adjusting hole (621) is formed in one end of the screw (62), an adjusting head (63) is fixedly connected with the other end of the screw (62), and one side, close to the limiting plate (33), of the adjusting head (63) is in contact with the outer wall of the limiting plate (33).
CN202323589893.1U 2023-12-27 2023-12-27 Frock is used in assembly of aircraft system case Active CN222079214U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202323589893.1U CN222079214U (en) 2023-12-27 2023-12-27 Frock is used in assembly of aircraft system case

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202323589893.1U CN222079214U (en) 2023-12-27 2023-12-27 Frock is used in assembly of aircraft system case

Publications (1)

Publication Number Publication Date
CN222079214U true CN222079214U (en) 2024-11-29

Family

ID=93596045

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202323589893.1U Active CN222079214U (en) 2023-12-27 2023-12-27 Frock is used in assembly of aircraft system case

Country Status (1)

Country Link
CN (1) CN222079214U (en)

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GR01 Patent grant
GR01 Patent grant
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TR01 Transfer of patent right

Effective date of registration: 20241225

Address after: No. 39 Yuyuan Road, Shiqiao Town, Yangzhou Economic and Technological Development Zone, Jiangsu Province 225000

Patentee after: Jiangsu Yuzhuang Technology Co.,Ltd.

Country or region after: China

Address before: 225606 No. 23, Chaoyang Road, Cheluo Town, Gaoyou City, Yangzhou City, Jiangsu Province

Patentee before: YANGZHOU YIXING MACHINERY Co.,Ltd.

Country or region before: China