A wing assembly auxiliary device for commercial aircraft manufacturing

Abstract

The utility model relates to the technical field of commercial aircraft manufacturing, specifically to a wing assembly auxiliary device for commercial aircraft manufacturing, including a top plate, one side of the inner wall of the top plate is rotatably connected with a transport adjustment component, and the transport adjustment component includes a transmission rod, a motor, a fixed frame, a hydraulic rod, a connecting frame, a rotating rod and a roller. The utility model motor external power supply drives the transmission rod to rotate, and the transmission rod drives the fixed frame on one side to rotate. The top of the fixed frame is used to place the wing. After rotating to a specified angle, the hydraulic rod external power supply pushes the top connecting frame to move upward, and the rotating rod connected inside the connecting frame drives the roller to contact the bottom of the wing. At this time, the staff can push the wing to one side and align it with the position to be installed. The wing slides to one side on the roller surface, thereby achieving the effect of adjusting the wing installation angle, and the wing can be manually transported for installation, reducing the danger of crane transportation and installation.

Description

Technical Field

[0001] The utility model relates to the technical field of commercial aircraft manufacturing, in particular to a wing assembly auxiliary device for commercial aircraft manufacturing. Background Art

[0002] The airplane is one of the most important inventions in the early 20th century. Since its invention, the airplane has become an indispensable tool in modern times. It has profoundly changed and influenced people's lives and opened up the history of people conquering the blue sky. The existing commercial aircraft requires different assembly devices during manufacturing. However, the existing commercial aircraft manufacturing wing assembly auxiliary devices have the following disadvantages:

[0003] (1) The existing wing assembly auxiliary device for commercial aircraft manufacturing has a weak function of transporting wings. When in use, when installing the wing on a commercial aircraft, the wing needs to be pre-positioned to the position where it needs to be transported. The existing technology requires the use of a crane to place it on the installation frame, and the staff adjusts the installation position. The crane is unstable and will cause the wing to shake and collide with the aircraft, resulting in damage to the aircraft;

[0004] (2) The existing wing assembly auxiliary device for commercial aircraft manufacturing has a weak supporting function. When in use, the mounting frame is used to transport the wing to a designated location. However, during installation, the wing needs to move on the surface of the mounting frame. If the mounting frame cannot be fixed, the mounting frame will shake and move as a whole, resulting in unstable wing installation. Summary of the invention

[0005] The purpose of the utility model is to provide a wing assembly auxiliary device for commercial aircraft manufacturing to solve the problems raised in the above background technology. To achieve the above purpose, the utility model provides the following technical solutions: a wing assembly auxiliary device for commercial aircraft manufacturing, including a top plate, one side of the inner wall of the top plate is rotatably connected to a transport adjustment component, the transport adjustment component includes a transmission rod, a motor, a fixed frame, a hydraulic rod, a connecting frame, a rotating rod and a roller, one side of the transmission rod is rotatably connected to one side of the inner wall of the top plate, one side of the transmission rod is rotatably connected to a motor, one side of the transmission rod is fixedly connected to a fixed frame, the bottom wall of the fixed frame is fixedly connected to a hydraulic rod, the top of the hydraulic rod is fixedly connected to a connecting frame, the inner wall of the connecting frame is rotatably connected to a rotating rod, and the outer surface of the rotating rod is fixedly connected to a number of rollers;

[0006] The four corners of the bottom end of the top plate are fixedly connected to support columns, the bottom ends of the support columns are fixedly connected to the bottom plate, the middle part of the bottom end of the bottom plate is threadedly connected to a support and fixing assembly, the support and fixing assembly includes a circular plate, bolts, connecting columns, connecting plates, a hydraulic press and an anti-slip pad, a plurality of threaded holes are opened on the top of the circular plate, the inner walls of the threaded holes are threadedly connected to bolts, one side of the threaded outer surface is threadedly connected to the middle part of the bottom end of the bottom plate, the bottom end of the circular plate is fixedly connected to a connecting column, the bottom end of the connecting column is fixedly connected to a connecting plate, the top end of the connecting plate is fixedly connected to a plurality of hydraulic presses, and the bottom end of the hydraulic press is fixedly connected to an anti-slip pad.

[0007] Preferably, a slot is provided at the top of the bottom plate, and a partition is fixedly connected to the inner wall of the slot.

[0008] Preferably, connecting grooves are provided at four corners of the bottom end of the base plate, and pulleys are fixedly connected to the inner walls of the connecting grooves.

[0009] Preferably, a fixing seat is fixedly connected to one side of the top of the fixing frame, and a clamping plate is rotatably connected to one side of the fixing seat.

[0010] Preferably, a placement groove is provided on the other side of the top of the fixing frame, and the inner wall of the placement groove is clamped to one side of the bottom end of the clamping plate.

[0011] Preferably, a mounting groove is provided at the top of the clamping plate, and a handle is fixedly connected to the inner wall of the mounting groove.

[0012] Compared with the prior art, the beneficial effects of the utility model are:

[0013] 1. A wing assembly auxiliary device for commercial aircraft manufacturing is provided with a transmission rod, a motor, a fixed frame, a hydraulic rod, a connecting frame, a rotating rod and a roller. When in use, the motor external power supply drives the transmission rod to rotate, and the transmission rod drives the fixed frame on one side to rotate. The top of the fixed frame is used to place the wing. After rotating to a specified angle, the hydraulic rod external power supply pushes the connecting frame at the top to move upward, and the rotating rod connected inside the connecting frame drives the roller to contact the bottom of the wing. At this time, the staff can push the wing to one side and align it with the position where it needs to be installed. The wing slides to one side on the surface of the roller, thereby achieving the effect of adjusting the wing installation angle, and the wing can be manually transported for installation, reducing the danger of crane transportation and installation. 2. This wing assembly auxiliary device for commercial aircraft manufacturing is provided with a circular plate, bolts, connecting columns, connecting plates, a hydraulic press and anti-skid pads. When in use, the circular plate is fixed to the bottom end of the device by rotating the bolts, the circular plate fixes the connecting columns, the connecting columns fix the connecting plates, the connecting columns are used to raise the distance between the circular plate and the connecting plates to facilitate the installation of bolts by workers, and then the anti-skid pad can be pushed toward the bottom through the external power supply of the hydraulic press, the anti-skid pad expands the support area on the surface, and can prevent the device from sliding, firmly fixing and supporting the device, thereby achieving the effect of adjustable support for the device to prevent shaking. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 It is a schematic diagram of the overall appearance of the utility model;

[0015] Figure 2 This is a schematic diagram of the disassembly of the transport adjustment component of the utility model;

[0016] Figure 3 This is a schematic diagram of the disassembly of the support and fixing components of the utility model;

[0017] Figure 4 It is an enlarged schematic diagram of the fixing seat, the clamping plate and the handle of the utility model.

[0018] In the figure: 1. top plate; 2. transmission rod; 3. motor; 4. fixed frame; 5. hydraulic rod; 6. connecting frame; 7. rotating rod; 8. roller; 9. support column; 10. bottom plate; 11. circular plate; 12. bolt; 13. connecting column; 14. connecting plate; 15. hydraulic press; 16. anti-slip pad; 17. partition; 18. pulley; 19. fixed seat; 20. splint; 21. handle; 22. slot. DETAILED DESCRIPTION

[0019] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0020] See also Figure 1-Figure 4 As shown, a technical solution provided by the utility model:

[0021] A wing assembly auxiliary device for commercial aircraft manufacturing includes a top plate 1, one side of the inner wall of the top plate 1 is rotatably connected to a transport adjustment component, the transport adjustment component includes a transmission rod 2, a motor 3, a fixed frame 4, a hydraulic rod 5, a connecting frame 6, a rotating rod 7 and a roller 8, one side of the transmission rod 2 is rotatably connected to one side of the inner wall of the top plate 1, one side of the transmission rod 2 is rotatably connected to the motor 3, one side of the transmission rod 2 is fixedly connected to the fixing frame 4, the inner bottom wall of the fixing frame 4 is fixedly connected to the hydraulic rod 5, the top of the hydraulic rod 5 is fixedly connected to the connecting frame 6, the inner wall of the connecting frame 6 is rotatably connected to the rotating rod 7, and the outer surface of the rotating rod 7 is fixedly connected to a plurality of rollers 8; the four corners of the bottom end of the top plate 1 are fixedly connected to A support column 9, the bottom end of the support column 9 is fixedly connected to a bottom plate 10, the middle part of the bottom end of the bottom plate 10 is threadedly connected to a support and fixing assembly, the support and fixing assembly includes a circular plate 11, a bolt 12, a connecting column 13, a connecting plate 14, a hydraulic press 15 and an anti-skid pad 16, a plurality of threaded holes are opened at the top of the circular plate 11, the inner wall of the threaded hole is threadedly connected to the bolt 12, one side of the threaded outer surface is threadedly connected to the middle part of the bottom end of the bottom plate 10, the bottom end of the circular plate 11 is fixedly connected to a connecting column 13, the bottom end of the connecting column 13 is fixedly connected to a connecting plate 14, the top end of the connecting plate 14 is fixedly connected to a plurality of hydraulic presses 15, and the bottom end of the hydraulic press 15 is fixedly connected to an anti-skid pad 16;

[0022] In this embodiment, preferably, a slot 22 is provided at the top of the bottom plate 10, and a partition 17 is fixedly connected to the inner wall of the slot 22;

[0023] In this embodiment, preferably, connecting grooves are provided at the four corners of the bottom end of the bottom plate 10, and pulleys 18 are fixedly connected to the inner walls of the connecting grooves;

[0024] In this embodiment, preferably, a fixing seat 19 is fixedly connected to one side of the top of the fixing frame 4, and a clamping plate 20 is rotatably connected to one side of the fixing seat 19;

[0025] In this embodiment, preferably, a placement groove is opened on the other side of the top of the fixing frame 4, and the inner wall of the placement groove is clamped to one side of the bottom end of the clamping plate 20;

[0026] In this embodiment, preferably, a mounting groove is provided at the top of the clamping plate 20, and a handle 21 is fixedly connected to the inner wall of the mounting groove.

[0027] When a wing assembly auxiliary device for commercial aircraft manufacturing of the present embodiment is used, the slot 22 and the partition 17 are installed. The interior of the slot 22 is used to place installation tools, which is convenient for workers to take tools to install the wing. The partition 17 is used to separate different tools to prevent mixing and difficulty in distinguishing, thereby achieving the function of a limiting tool. Through the installation of the pulley 18, when the device is driven to move by the trailer, the pulley 18 can drive the device to move on the ground, thereby achieving the function of moving the device. The clamping plate 20 is fixed by the fixing seat 19, and the hand-held handle 21 can pull the clamping plate 20 to one side to unfold it. When the wing is placed on the surface of the top plate 1, the clamping plate 20 is driven to flip to the other side to fix the wing, thereby achieving the function of fixing and clamping the wing. The motor 3 is connected to an external power supply to drive the transmission rod 2 to rotate, and the transmission rod 2 drives the fixed frame 4 on one side to rotate. The top of the fixed frame 4 is used to place the wing. After rotating to a specified angle, The external power supply of the hydraulic rod 5 pushes the connecting frame 6 at the top to move upward, and the rotating rod 7 connected inside the connecting frame 6 drives the roller 8 to contact the bottom of the wing. The staff can push the wing to one side at this time to align it with the position where it needs to be installed. The wing slides to one side on the surface of the roller 8, thereby achieving the effect of adjusting the wing installation angle, and the wing can be manually transported for installation, reducing the danger of crane transportation and installation, and the circular plate 11 is fixed to the bottom of the device by rotating the bolt 12. The circular plate 11 fixes the connecting column 13, and the connecting column 13 fixes the connecting plate 14. The connecting column 13 is used to raise the distance between the circular plate 11 and the connecting plate 14 to facilitate the staff to install the bolt 12, and then the anti-skid pad 16 can be pushed to the bottom through the external power supply of the hydraulic press 15. The anti-skid pad 16 expands the support area on the surface and can prevent the device from sliding, firmly fixing and supporting the device, thereby achieving the effect of adjustable support to prevent shaking of the device.

[0028] The above shows and describes the basic principle, main features and advantages of the utility model. Those skilled in the art should understand that the utility model is not limited by the above embodiments. The above embodiments and descriptions are only preferred examples of the utility model and are not used to limit the utility model. Without departing from the spirit and scope of the utility model, the utility model may have various changes and improvements, which fall within the scope of the utility model to be protected. The scope of protection of the utility model is defined by the attached claims and their equivalents.

Claims

1. A wing assembly auxiliary device for commercial aircraft manufacturing, characterized in that: include A top plate (1), wherein one side of the inner wall of the top plate (1) is rotatably connected to a transport adjustment component, wherein the transport adjustment component comprises a transmission rod (2), a motor (3), a fixed frame (4), a hydraulic rod (5), a connecting frame (6), a rotating rod (7) and a roller (8), wherein one side of the transmission rod (2) is rotatably connected to one side of the inner wall of the top plate (1), one side of the transmission rod (2) is rotatably connected to the motor (3), one side of the transmission rod (2) is fixedly connected to the fixing frame (4), the inner bottom wall of the fixing frame (4) is fixedly connected to a hydraulic rod (5), the top end of the hydraulic rod (5) is fixedly connected to the connecting frame (6), the inner wall of the connecting frame (6) is rotatably connected to a rotating rod (7), and the outer surface of the rotating rod (7) is fixedly connected to a plurality of rollers (8); The top plate (1) is fixedly connected to support columns (9) at the four corners of the bottom end, the support columns (9) are fixedly connected to the bottom plate (10), the bottom of the bottom plate (10) is threadedly connected to a support fixing assembly, the support fixing assembly comprising a circular plate (11), bolts (12), a connecting column (13), a connecting plate (14), a hydraulic press (15) and an anti-skid pad (16), the top of the circular plate (11) is provided with a plurality of threaded holes, the inner walls of the threaded holes are threadedly connected to bolts (12), one side of the threaded outer surface is threadedly connected to the middle of the bottom end of the bottom plate (10), the bottom of the circular plate (11) is fixedly connected to a connecting column (13), the bottom of the connecting column (13) is fixedly connected to a connecting plate (14), the top of the connecting plate (14) is fixedly connected to a plurality of hydraulic presses (15), and the bottom of the hydraulic press (15) is fixedly connected to an anti-skid pad (16).

2. A wing assembly auxiliary device for commercial aircraft manufacturing according to claim 1, characterized in that: A slot (22) is provided at the top of the bottom plate (10), and a partition plate (17) is fixedly connected to the inner wall of the slot (22).

3. The wing assembly auxiliary device for commercial aircraft manufacturing according to claim 1, characterized in that: The bottom corners of the bottom plate (10) are provided with connection grooves, and the inner wall of the connection groove is fixedly connected to a pulley (18).

4. The wing assembly auxiliary device for commercial aircraft manufacturing according to claim 1, characterized in that: A fixing seat (19) is fixedly connected to one side of the top end of the fixing frame (4), and a clamping plate (20) is rotatably connected to one side of the fixing seat (19).

5. The wing assembly auxiliary device for commercial aircraft manufacturing according to claim 1, characterized in that: A placement groove is provided on the other side of the top end of the fixing frame (4), and the inner wall of the placement groove is clamped to one side of the bottom end of the clamping plate (20).

6. The wing assembly auxiliary device for commercial aircraft manufacturing according to claim 4, characterized in that: A mounting groove is formed at the top of the clamping plate (20), and a handle (21) is fixedly connected to the inner wall of the mounting groove.

Images