Aviation composite material plate forming tool

Abstract

An aviation composite plate forming tool belongs to the technical field of aviation composite forming and is characterized by comprising an electric control case and a working platform connected to the middle of the upper surface of the electric control case, and a bending groove is formed in the middle of the upper surface of the working platform. A plurality of movable rolling shafts are vertically and evenly distributed and inserted in the rear portion of the upper surface of the working platform, a plurality of rail sliding grooves are transversely and evenly distributed in the front edge of the upper surface of the working platform, and a positioning device is inserted in the middle of the interior of each rail sliding groove. And a plurality of locking devices are transversely and uniformly distributed and connected to the middle of the rear surface of the working platform, so that the time for adjusting and positioning by workers is saved, the workers can quickly adjust the depth of the bending groove at any time, and the preparation time for adjusting the equipment by the workers is shortened.

Description

Technical field:

[0001] The utility model belongs to the technical field of forming equipment for sliding hole composite materials, and in particular relates to a forming tool for aviation composite material plates. Background technology:

[0002] In long-term work practice, there is only one existing plate bending positioning structure. When a plate is bent multiple times, workers need to position it multiple times, which takes a lot of time for workers to prepare. In addition, workers need to manually adjust the groove depth for different angles of bending. Utility model content:

[0003] The purpose of the utility model is that the staff can adjust different positions at one time, saving the staff's time for adjusting the positioning, and the staff can quickly adjust the depth of the bending groove at any time, reducing the staff's preparation time for adjusting the equipment, and facilitating the staff's operation and use. The technical solution is as follows:

[0004] A tool for forming aviation composite material plates, characterized in that it includes an electric control box 1 and a working platform 2 connected to the middle of the upper surface of the electric control box 1, a bending groove 3 is provided in the middle of the upper surface of the working platform 2, a plurality of movable rollers 4 are evenly distributed vertically at the rear of the upper surface of the working platform 2, a plurality of track slides 5 are evenly distributed horizontally at the front edge of the upper surface of the working platform 2, a positioning device 6 is inserted in the middle of each track slide 5, a plurality of locking devices 7 are evenly distributed horizontally in the middle of the rear surface of the working platform 2, the bending groove 3 includes a groove 3-1, a lower plate 3-2, a cylinder 3-3 and an inclined surface 3-4, a plurality of lower plates 3-2 are evenly distributed horizontally in the middle of the lower surface of the groove 3-1, a cylinder 3-3 is connected to the middle of the lower surface of the lower plate 3-2, inclined surfaces 3-4 are symmetrically provided at the edges of the front and rear surfaces of the groove 3-1, the position and size of the groove 3-1 correspond to the position and size of the pressure head, and the lower plate 3-2 The positioning device 6 is made of metal material, and includes a slide column 6-1, a scale 6-2, a cardboard 6-3 and a rubber pad 6-4. The rear edge of the side surface of the slide column 6-1 is provided with a scale 6-2, the front edge of the upper side surface of the slide column 6-1 is connected with a cardboard 6-3, and the middle of the rear surface of the cardboard 6-3 is connected with a rubber pad 6-4. The slide column 6-1 is inserted into the rear surface of the working platform 2, and the slide column 6-1 penetrates the working platform 2 and is inserted into the track slot 5. The cardboard 6-3 is inserted into the track slot 5. Inside the rail slide groove 5, the locking device 7 includes an outer ring 7-1, anti-slip grooves 7-2, a clamping tube 7-3 and slots 7-4. The side surface of the outer ring 7-1 is provided with a plurality of anti-slip grooves 7-2 around it, a clamping tube 7-3 is inserted at the center of the rear surface of the outer ring 7-1, and a plurality of slots 7-4 are evenly distributed around the rear edge of the side surface of the clamping tube 7-3. The sliding column 6-1 is inserted through the clamping tube 7-3, and the outer ring 7-1 and the clamping tube 7-3 are connected to each other by threads.

[0005] The beneficial effects of the utility model are as follows: the staff can adjust different positions at one time, saving the staff's time for adjusting the positions, and the staff can quickly adjust the depth of the bending groove at any time, reducing the staff's preparation time for adjusting the equipment, and facilitating the staff's operation and use. Description of the drawings:

[0006] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0007] Figure 2 It is a schematic diagram of the structure of the bending and pressing groove 3 of the utility model;

[0008] Figure 3 It is a schematic diagram of the structure of the positioning device 6 of the utility model;

[0009] Figure 4 It is a schematic diagram of the structure of the locking device 7 of the utility model;

[0010] In the figure: electronic control box 1, working platform 2, bending groove 3, movable roller 4, track slide 5, positioning device 6, locking device 7, groove 3-1, lower plate 3-2, cylinder 3-3, inclined surface 3-4, slide column 6-1, scale 6-2, clamping plate 6-3, rubber pad 6-4, outer ring 7-1, anti-slip pattern 7-2, clamping tube 7-3, slot 7-4. Specific implementation method:

[0011] Reference Figure 1 The aerospace composite material plate forming tool is characterized in that it includes an electric control box 1 and a working platform 2 connected to the middle of the upper surface of the electric control box 1, a bending groove 3 is provided in the middle of the upper surface of the working platform 2, a plurality of movable rollers 4 are evenly distributed vertically at the rear of the upper surface of the working platform 2, a plurality of track grooves 5 are evenly distributed horizontally at the front edge of the upper surface of the working platform 2, a positioning device 6 is inserted in the middle of each track groove 5, a plurality of locking devices 7 are evenly distributed horizontally in the middle of the rear surface of the working platform 2, the bending groove 3 includes a groove 3-1, a lower plate 3-2, a cylinder 3-3 and an inclined surface 3-4, a plurality of lower plates 3-2 are evenly distributed horizontally in the middle of the lower surface of the groove 3-1, a cylinder 3-3 is connected to the middle of the lower surface of the lower plate 3-2, inclined surfaces 3-4 are symmetrically provided at the edges of the front and rear surfaces of the groove 3-1, the position and size of the groove 3-1 correspond to the position and size of the pressure head, and the lower plate 3- 2 is made of metal material, the positioning device 6 includes a slide column 6-1, a scale 6-2, a card plate 6-3 and a rubber pad 6-4, the rear edge of the side surface of the slide column 6-1 is provided with a scale 6-2, the upper front edge of the side surface of the slide column 6-1 is connected with a card plate 6-3, the middle of the rear surface of the card plate 6-3 is connected with a rubber pad 6-4, the slide column 6-1 is inserted into the rear surface of the working platform 2, and the slide column 6-1 penetrates the working platform 2 and is inserted into the track slot 5, the card plate 6-3 is inserted into the track slot 5, and the card plate 6-3 is inserted into the track slot 5. Installed inside the rail slide groove 5, the locking device 7 includes an outer ring 7-1, anti-slip grooves 7-2, a clamping tube 7-3 and slots 7-4. The side surface of the outer ring 7-1 is provided with a plurality of anti-slip grooves 7-2 around it, a clamping tube 7-3 is inserted at the center of the rear surface of the outer ring 7-1, and a plurality of slots 7-4 are evenly distributed around the rear edge of the side surface of the clamping tube 7-3. The sliding column 6-1 is inserted through the clamping tube 7-3, and the outer ring 7-1 and the clamping tube 7-3 are connected to each other by threads.

[0012] When adjusting the positioning, the staff first slides the slide column 6-1 on the sliding positioning device 6 in the work table 2, and at the same time the card plate 6-3 slides in the track slide groove 5. The staff observes the scale 6-2 to adjust the position of the card plate 6-3. After the adjustment, the staff turns the outer ring 7-1 on the locking device 7 to tighten the groove 7-4 on the clamping tube 7-3 to clamp the slide column 6-1. When adjusting the angle, the staff starts the cylinder 3-3 on the bending groove 3 to move the lower plate 3-2 up and down to adjust the depth of the groove 3-1. When moving the plate, the movable roller 4 can reduce the friction between the plate and the work platform 2. Finally, the staff starts the electronic control box 1 to perform plate bending.

[0013] Of course, the above description is not a limitation of the present invention, and the present invention is not limited to the above examples. Changes, modifications, additions or substitutions made by technicians in this technical field within the essential scope of the present invention should also fall within the protection scope of the present invention.

Claims

1. An aviation composite material sheet forming tool, characterized by: The invention comprises an electric control box (1) and a working platform (2) connected to the middle of the upper surface of the electric control box (1), wherein a bending groove (3) is provided in the middle of the upper surface of the working platform (2), a plurality of movable rollers (4) are evenly distributed vertically at the rear of the upper surface of the working platform (2), a plurality of track grooves (5) are evenly distributed horizontally at the front edge of the upper surface of the working platform (2), a positioning device (6) is inserted in the middle of each track groove (5), and a plurality of locking devices (7) are evenly distributed horizontally at the middle of the rear surface of the working platform (2).

2. The aviation composite material sheet forming tool according to claim 1, characterized in that: The bending and pressing groove (3) comprises a groove (3-1), a lower plate (3-2), a cylinder (3-3) and an inclined surface (3-4); a plurality of lower plates (3-2) are evenly distributed and inserted in a horizontal row in the middle of the lower surface of the groove (3-1); a cylinder (3-3) is connected to the middle of the lower surface of the lower plate (3-2); inclined surfaces (3-4) are symmetrically arranged at the upper edges of the front and rear surfaces of the groove (3-1); the position and size of the groove (3-1) correspond to the position and size of the pressure head; and the lower plate (3-2) is made of metal.

3. The aviation composite material sheet forming tool according to claim 1, characterized in that: The positioning device (6) comprises a slide post (6-1), a scale (6-2), a card plate (6-3) and a rubber pad (6-4); the rear edge of the side surface of the slide post (6-1) is provided with a scale (6-2); the front edge above the side surface of the slide post (6-1) is connected to a card plate (6-3); the middle of the rear surface of the card plate (6-3) is connected to a rubber pad (6-4); the slide post (6-1) is inserted into the rear surface of the working platform (2); the slide post (6-1) penetrates the working platform (2) and is inserted into the track slide groove (5); the card plate (6-3) is inserted into the track slide groove (5).

4. The aviation composite material sheet forming tool according to claim 3, characterized in that: The locking device (7) comprises an outer ring (7-1), anti-skid patterns (7-2), a clamping tube (7-3) and slots (7-4); a plurality of anti-skid patterns (7-2) are arranged around the side surface of the outer ring (7-1); a clamping tube (7-3) is inserted at the center of the rear surface of the outer ring (7-1); a plurality of slots (7-4) are evenly distributed around the rear edge of the side surface of the clamping tube (7-3); the sliding column (6-1) is inserted into the clamping tube (7-3); and the outer ring (7-1) and the clamping tube (7-3) are connected to each other by threads.

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