Automatic assembling device for aviation parts

Abstract

The utility model relates to the field of aviation part assembling, in particular to an automatic assembling device for aviation parts, which comprises a sliding rail, a first motor, a screw rod, a guide rod, a sliding block and the like, the left side of the front part of the sliding rail is connected with the first motor, the front part of the sliding rail is rotatably connected with the screw rod, and the screw rod is connected with an output shaft of the first motor; the guide rod is connected to the rear portion of the sliding rail, the sliding block is connected to the guide rod in a sliding mode, the sliding block is connected with the lead screw through threads, and the sliding block is connected with the sliding rail in a sliding mode. The clamp is limited through movement of the limiting ball, the position of the mechanical arm is adjusted through movement of the sliding block, then parts are assembled through movement of the clamp, and therefore the clamp can be assembled and disassembled, operation is easy, the clamp can be replaced conveniently to be suitable for assembly of the parts of different specifications, time is saved, and production efficiency is improved. And the position of the mechanical arm can be adjusted for use, the use range is expanded, and use is flexible and convenient.

Description

TECHNICAL FIELD

[0001] The utility model relates to aviation spare part assembly field especially, relates to a kind of for aviation spare part automatic assembly device. BACKGROUND

[0002] Aviation spare part refers to the various parts and components for manufacturing aircraft, helicopter, unmanned aerial vehicle and other aircraft, these components can be structural member, can also be non-structural member, cover the wide range from engine to instrument panel, from wing to landing gear, aviation spare part automatic assembly refers to using automation equipment and technology, such as robot, automated production line and special assembly tool, to complete the manufacturing and assembly process of aircraft and its components.

[0003] The existing aviation spare part assembly is usually by installing mechanical arm in specified position, then installing clamp on mechanical arm, and then moving clamp to hold and assemble spare part by operating mechanical arm, however, the current clamp installation process is more cumbersome, time-consuming, difficult to realize quick mounting and dismounting and replacement, poor flexibility, affect the efficiency of production, in addition, part of mechanical arm position is fixed and inconvenient to adjust, leading to limited use range, use is more inconvenient.

[0004] Therefore, a kind of aviation spare part automatic assembly device for being designed, which can mount and dismount clamp, is simple to operate, facilitate to replace clamp to adapt to different specifications of spare part assembly use, save time, improve the efficiency of production, and the position of mechanical arm can be adjusted, expand the range of use, use flexible and convenient. UTILITY MODEL CONTENT

[0005] In order to overcome the current clamp installation process is more cumbersome, time-consuming, difficult to realize quick mounting and dismounting and replacement, poor flexibility, affect the efficiency of production, in addition, part of mechanical arm position is fixed and inconvenient to adjust, leading to limited use range, use is more inconvenient, the utility model provides a kind of aviation spare part automatic assembly device for being designed, which can mount and dismount clamp, is simple to operate, facilitate to replace clamp to adapt to different specifications of spare part assembly use, save time, improve the efficiency of production, and the position of mechanical arm can be adjusted, expand the range of use, use flexible and convenient.

[0006] The utility model provides an automatic assembly device for aviation parts, including slide rail, first motor, screw rod, guide rod, sliding block, mechanical arm, installation component and storage component, the left side of slide rail front part is connected with first motor, the front part of slide rail rotatably connects with screw rod, the output shaft of first motor is connected with screw rod, the rear part of slide rail is connected with guide rod, the sliding block is slidably connected on the guide rod, the sliding block is connected with screw rod through the thread, the sliding block is slidably connected with slide rail, the upper side of sliding block is connected with mechanical arm, and the installation component for clamping aviation parts is equipped on mechanical arm, and the right side of slide rail is equipped with the storage component for storing the clamped parts.

[0007] Further, the sliding block is H-shaped.

[0008] Further, the mechanical arm has a plurality of joints.

[0009] Further, the installation component includes an electric push rod, a pressing block, a plurality of limiting balls, and a clamp. The electric push rod is connected to the inner side of the upper part of the mechanical arm. The pressing block is connected to the telescopic end of the electric push rod. The plurality of limiting balls are slidably connected to the upper part of the mechanical arm. The limiting balls are in contact with the pressing block. The clamp is connected to the mechanical arm. The limiting balls are in contact with the clamp.

[0010] Further, the storage component includes a placing box, a support frame, a second motor, a gear set, a placing plate, and a rack. The right side of the slide rail is connected with the placing box. The upper side of the upper part of the placing box is connected with the support frame. The lower part of the front side of the support frame is connected with the second motor. The support frame is provided with the gear set. The upper part of the placing box is slidably connected with the placing plate. The placing plate is also provided with a plurality of clamps. The lower side of the placing plate is connected with the rack.

[0011] Further, the gear set includes a pinion and a gear. The lower part of the support frame is rotatably connected with the pinion. The output shaft of the second motor is connected with the pinion. The upper part of the support frame is connected with the gear. The pinion and the gear are meshed with each other. The rack and the gear are meshed with each other.

[0012] Beneficial effects: 1. The utility model discloses a clamp limiting position through the movement of the limiting ball, adjusts the position of the mechanical arm through the movement of the sliding block, and then assembles the parts through the movement of the clamp, so that the clamp can be assembled and disassembled, the clamp can be replaced to adapt to the assembly of parts of different specifications, time is saved, production efficiency is improved, the position of the mechanical arm can be adjusted, the range of use is expanded, and the use is flexible and convenient.

[0013] 2. The utility model discloses a second motor reverse operation makes the pinion reverse rotation, and the pinion and the gear are meshed with each other and move, and the gear and the rack are meshed with each other and move, so that the placing plate moves reversely, and then drives the clamp on the placing plate to move reversely and is stored, so that the clamp of different specifications can be stored, the time of looking for is reduced, the speed of replacement is improved, the clamp is protected, and the service life of the clamp is prolonged. Attached Figure Description

[0014] Figure 1 This is a three-dimensional structural diagram of the present invention.

[0015] Figure 2 This is a three-dimensional cross-sectional view of the slide rail and lead screw components of this utility model.

[0016] Figure 3 This is a three-dimensional cross-sectional view of the first type of installation component of this utility model.

[0017] Figure 4 This is a cross-sectional view of the second three-dimensional structure of the mounting component of this utility model.

[0018] Figure 5 This is a three-dimensional structural diagram of the storage component of this utility model.

[0019] The names and numbers of the components in the diagram are as follows: 1-slide rail, 2-first motor, 3-lead screw, 4-guide rod, 5-sliding block, 6-robotic arm, 7-electric push rod, 8-pressing block, 9-limiting ball, 10-clamp, 11-placement box, 12-support frame, 13-second motor, 14-gear set, 15-placement plate, 16-rack. Detailed Implementation

[0020] The present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments, but this does not limit the scope of protection and application of the present invention.

[0021] An automated assembly device for aerospace components, such as Figures 1-5As shown, including slide rail 1, the first motor 2, screw rod 3, guide rod 4, sliding block 5, mechanical arm 6, electric push rod 7, extrusion block 8, limit ball 9, clamp 10, placement box 11, support frame 12, second motor 13, gear set 14, placement plate 15 and rack 16, the first motor 2 is connected to the left side of the front of the slide rail 1, the slide rail 1 is rotatably connected to the front of the screw rod 3, the screw rod 3 is connected with the output shaft of the first motor 2, the slide rail 1 is connected with the guide rod 4 at the rear, the guide rod 4 is slidably connected with the sliding block 5, the sliding block 5 is connected with the screw rod 3 through the thread, the sliding block 5 is slidably connected with the slide rail 1, the sliding block 5 is H-shaped, the sliding block 5 is connected with the mechanical arm 6 on the upper side, the mechanical arm 6 has four joints, the mechanical arm 6 is connected with the electric push rod 7 on the inner side of the upper part, the extrusion block 8 is connected on the telescopic end of the electric push rod 7, the mechanical arm 6 is slidably connected with six limit balls 9 on the upper part, the limit balls 9 are in contact with the extrusion block 8, the clamp 10 is clamped on the mechanical arm 6, the limit balls 9 are in contact with the clamp 10, the slide rail 1 is connected with the placement box 11 on the right side, the support frame 12 is connected on the upper side of the upper part in the placement box 11, the second motor 13 is connected on the front side of the lower part of the support frame 12, the gear set 14 is arranged on the support frame 12, the gear set 14 includes a pinion and a gear, the pinion is rotatably connected on the lower part of the support frame 12, the pinion is connected with the output shaft of the second motor 13, the gear is connected on the upper part of the support frame 12, the gear is meshed with the pinion, the placement plate 15 is slidably connected on the upper part of the placement box 11, six clamps 10 are also placed on the placement plate 15, the rack 16 is connected on the lower side of the placement plate 15, the rack 16 is meshed with the gear.

[0022] When the automatic assembly of aviation parts is needed, the device can be used, so that the slide rail 1 and the placing box 11 are in contact with the ground, then the clamp 10 is taken up, so that the clamp 10 is clamped with the mechanical arm 6, the mechanical arm 6 has four joints, then the electric push rod 7 is started, the extrusion block 8 is driven to move by the electric push rod 7, and then the limit ball 9 is driven to move and contact with the clamp 10 for limiting, and then the clamp 10 is installed, then the first motor 2 is started, the screw rod 3 is driven to rotate by the first motor 2, and under the action of the screw, the sliding block 5 moves along the slide rail 1 and the guide rod 4, the sliding block 5 is H-shaped, after moving to the appropriate position, the first motor 2 is turned off, the mechanical arm 6 is started again, the clamp 10 is driven to move by the mechanical arm 6 to clamp and assemble the parts, when different specifications of parts need to be assembled, the mechanical arm 6 is turned off, the electric push rod 7 is reversely operated, the extrusion block 8 is reversely moved and reset, then the clamp 10 is taken off, the limit ball 9 is reversely moved and reset, then the second motor 13 is started, the pinion is driven to rotate by the second motor 13, the pinion and the gear wheel are meshed with each other to move, so that the gear wheel rotates, the gear wheel and the rack 16 are meshed with each other to move, so that the placing plate 15 moves along the placing box 11, and then drives the clamp 10 on the placing plate 15 to move out, then the clamp 10 of appropriate specification is taken out, then the clamp 10 used before is placed on the placing plate 15, then the second motor 13 is reversely operated, the pinion is reversely rotated, the pinion and the gear wheel are meshed with each other to move, so that the gear wheel is reversely rotated, the gear wheel and the rack 16 are meshed with each other to move, so that the placing plate 15 is reversely moved, and then drives the clamp 10 on the placing plate 15 to reversely move and store, and then the second motor 13 is turned off, so that the clamp 10 of different specifications can be stored, the time for searching is reduced, the replacement speed is improved, the clamp 10 is protected, the service life of the clamp 10 is prolonged, then the clamp 10 is in contact with the mechanical arm 6, then the above operation is repeated to install and use the clamp 10, and then the assembly of parts is continued, so that the clamp 10 can be assembled and disassembled, the operation is simple, the clamp 10 is convenient to replace, different specifications of parts can be assembled and used, time is saved, the production efficiency is improved, the position of the mechanical arm 6 can be adjusted, the use range is expanded, the use is flexible and convenient, after use, the mechanical arm 6 can be turned off.

[0023] The above merely describes a specific implementation of the present application, but the protection scope of the present application is not limited thereto, any skilled person in the art can easily think of changes or replacements within the technical range disclosed by the present application, which should be covered within the protection scope of the present application. Therefore, the protection scope of the present application should be subject to the protection scope of the claims.

Claims

1. An automated assembly device for aircraft parts, characterized in that, The system includes a slide rail (1), a first motor (2), a lead screw (3), a guide rod (4), a sliding block (5), a robotic arm (6), an installation component, and a storage component. The first motor (2) is connected to the left front of the slide rail (1). The lead screw (3) is rotatably connected to the front of the slide rail (1). The lead screw (3) is connected to the output shaft of the first motor (2). The guide rod (4) is connected to the rear of the slide rail (1). The sliding block (5) is slidably connected to the guide rod (4). The sliding block (5) is connected to the lead screw (3) by a thread. The sliding block (5) is slidably connected to the slide rail (1). The robotic arm (6) is connected to the upper side of the sliding block (5). The robotic arm (6) is equipped with an installation component for clamping aerospace parts. The right side of the slide rail (1) is equipped with a storage component for storing the clamped parts.

2. The automatic assembly device for aerospace parts according to claim 1, characterized in that, The sliding block (5) is H-shaped.

3. The automatic assembly device for aerospace parts according to claim 2, characterized in that, The robotic arm (6) consists of multiple joints.

4. An automated assembly device for aerospace components according to claim 3, characterized in that, The mounting assembly includes an electric push rod (7), a pressing block (8), a limiting ball (9), and a clamp (10). The electric push rod (7) is connected to the inner side of the upper part of the robotic arm (6). The pressing block (8) is connected to the telescopic end of the electric push rod (7). Multiple limiting balls (9) are slidably connected to the upper part of the robotic arm (6). All limiting balls (9) are in contact with the pressing block (8). The clamp (10) is clamped on the robotic arm (6). All limiting balls (9) are in contact with the clamp (10).

5. An automated assembly device for aerospace components according to claim 4, characterized in that, The storage components include a storage box (11), a support frame (12), a second motor (13), a gear set (14), a storage plate (15), and a rack (16). The storage box (11) is connected to the right side of the slide rail (1). The support frame (12) is connected to the upper part of the storage box (11). The second motor (13) is connected to the lower front part of the support frame (12). The gear set (14) is provided on the support frame (12). The storage plate (15) is slidably connected to the upper part of the storage box (11). Multiple clamps (10) are also placed on the storage plate (15). The rack (16) is connected to the lower side of the storage plate (15).

6. An automated assembly device for aerospace components according to claim 5, characterized in that, The gear set (14) includes a small gear and a large gear. The small gear is rotatably connected to the lower part of the support frame (12). The small gear is connected to the output shaft of the second motor (13). The large gear is connected to the upper part of the support frame (12). The large gear and the small gear mesh with each other. The rack (16) meshes with the large gear.

Images