Aviation fairing composite part forming tool

Abstract

The utility model discloses an aviation fairing composite material piece forming tool which comprises a fixing base, the top of the fixing base is fixedly connected with a stamping table, the surface of the stamping table is provided with a die groove, the two sides of the fixing base are fixedly connected with supporting frames, the tops of the supporting frames are fixedly connected with a bearing plate, and the bearing plate is fixedly connected with the stamping table. The top of the bearing plate is fixedly connected with an air cylinder, and the bottom of the air cylinder is fixedly connected with an upper die plate. Through the electric push rod, the sliding plate is conveniently pushed to move, so that the sliding plate drives the sliding sleeve to move, the sliding sleeve moves to drive the pushing plate to move, the pushing plate pushes the pushing column to move, and the pushing column pushes the circular plate to move, so that the circular plate pushes parts placed on the surface of the mold groove to move; and the parts are effectively pushed out of the inner cavity of the mold groove, so that material taking is facilitated, the working efficiency of workers is improved, and the trouble of the workers is solved.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation, in particular to a molding tool for an aviation fairing composite part. Background Art

[0002] Aviation, a complex and strategic human activity, refers to the flight (navigation) activities of aircraft in the Earth's atmosphere (air space), as well as many related fields such as scientific research and education, industrial manufacturing, public transportation, professional operations, aviation sports, national defense and military, and government management. The fairing is used to protect satellites and other payloads to prevent satellites from being affected by harmful environments such as aerodynamics, aerodynamic heating, and acoustic vibration. It is an important part of the launch vehicle. Forming tooling is required in the process of processing fairing composites;

[0003] However, during the use of existing forming tooling, a stamping method is usually adopted. The parts are placed on a stamping table and the parts are stamped using stamping equipment. However, since the parts are placed in a stamping groove on the surface of the stamping table, and the inner wall of the stamping groove just coincides with the side of the part, when the stamping is completed, there is no gap on the side and no stress point. Therefore, in the process of taking the material, it brings trouble to the staff and wastes the time of the staff to take the material. For this reason, we propose a forming tool for aviation fairing composite parts. Utility Model Content

[0004] 1. Technical issues to be solved

[0005] In view of the deficiencies in the prior art, the purpose of the utility model is to provide an aviation fairing composite component forming tooling to facilitate material removal.

[0006] (II) Technical solution

[0007] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an aviation fairing composite part forming tool, comprising a fixed seat, the top of the fixed seat is fixedly connected to a stamping table, the surface of the stamping table is provided with a mold groove, both sides of the fixed seat are fixedly connected to a support frame, the top of the support frame is fixedly connected to a bearing plate, the top of the bearing plate is fixedly connected to a cylinder, the bottom of the cylinder is fixedly connected to an upper template, the bottom of the fixed seat is fixedly connected to a shell, the left side of the bottom of the inner cavity of the shell is fixedly connected to an electric push rod, the top of the electric push rod is fixedly connected to a sliding plate, the right side of the sliding plate is fixedly connected to a sliding sleeve, the inner cavity of the sliding sleeve is provided with a sliding rod, the right side of the sliding sleeve is fixedly connected to a push plate, the top of the push plate is fixedly connected to a push column, and the top of the push column passes through the inner cavity of the mold groove and is fixedly connected to a circular plate.

[0008] As a preferred solution, support columns are fixedly connected to the four sides of the bottom of the fixing seat, and an anti-slip pad is fixedly connected to the bottom of the support column.

[0009] Through the above technical solution, the anti-skid pad can effectively prevent the device from sliding during the operation, thereby improving the working stability of the device.

[0010] As a preferred solution, a first sliding groove is opened on one side of the inner cavity of the shell, and one side of the sliding plate is slidably connected to the inner cavity of the first sliding groove.

[0011] Through the above technical solution, the sliding stability of the sliding plate is improved through the first sliding groove.

[0012] As a preferred solution, mounting blocks are fixedly connected to both sides of the sliding sleeve, and mounting bolts are arranged on the surface of the mounting blocks.

[0013] Through the above technical solution, the push plate can be easily disassembled and assembled by using the mounting block and the mounting bolts.

[0014] As a preferred solution, threaded holes are provided at both ends of the left side of the push plate, and the surface of the mounting bolt is threadedly connected to the inner cavity of the threaded hole.

[0015] With the technical solution, bolts can be easily installed for connection through threaded holes.

[0016] As a preferred solution, a second slide groove is opened on the inner side of the support frame, and sliders are fixedly connected to both sides of the upper template, and the surfaces of the sliders are slidably connected to the inner cavity of the second slide groove.

[0017] Through the above technical solution, the second slide groove is used to limit the slider to prevent the upper template from shaking during the sliding process, thereby improving the sliding stability of the upper template, and indirectly improving the accuracy of stamping, solving the troubles of the staff.

[0018] As a preferred solution, both ends of the sliding rod are fixedly connected to both ends of the inner cavity of the shell, and the inner cavity of the sliding sleeve is slidably connected to the surface of the sliding rod.

[0019] Through the above technical solution, the stability of the slide bar in use is improved by setting the connection relationship between the slide bar and the housing.

[0020] (III) Beneficial effects

[0021] Compared with the prior art, the utility model provides an aviation fairing composite component forming tooling, which has the following beneficial effects.

[0022] 1. The utility model uses an electric push rod to facilitate the movement of the sliding plate, so that the sliding plate drives the sliding sleeve to move, and the movement of the sliding sleeve drives the pushing plate to move, and the pushing plate drives the pushing column to move, and the pushing column drives the circular plate to move, so that the circular plate pushes the parts placed on the surface of the mold groove to move, and effectively pushes the parts out of the inner cavity of the mold groove, which is convenient for work and material removal, thereby improving the work efficiency of the staff and solving the troubles of the staff. Through the cylinder, it is convenient to push the upper template to move, so that the upper template can stamp the parts placed in the inner cavity of the mold groove, which is convenient for the staff to use later.

[0023] 2. The utility model uses the second slide groove to limit the slider, preventing the upper template from shaking during the sliding process, thereby improving the sliding stability of the upper template, and also indirectly improving the accuracy of stamping, solving the troubles of the staff. The anti-slip pad can effectively prevent the equipment from sliding during the process, thereby improving the working stability of the equipment. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 It is a schematic diagram of the structure of the utility model;

[0025] Figure 2 This is a cross-sectional view of the shell structure of the utility model;

[0026] Figure 3 This is the left side diagram of the push plate structure of the utility model.

[0027] In the figure: 1. fixed seat; 2. stamping table; 3. mold groove; 4. round plate; 5. support frame; 6. upper mold plate; 7. slider; 8. load-bearing plate; 9. cylinder; 10. shell; 11. support column; 12. electric push rod; 13. sliding plate; 14. sliding sleeve; 15. first slide groove; 16. sliding rod; 17. pushing column; 18. pushing plate; 19. mounting bolts; 20. mounting block. DETAILED DESCRIPTION

[0028] 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.

[0029] See also Figure 1-3The utility model discloses a tool for forming composite parts of an aviation fairing, comprising a fixed seat 1, a stamping table 2 is fixedly connected to the top of the fixed seat 1, a mold groove 3 is opened on the surface of the stamping table 2, support frames 5 are fixedly connected to both sides of the fixed seat 1, a bearing plate 8 is fixedly connected to the top of the support frame 5, a cylinder 9 is fixedly connected to the top of the bearing plate 8, an upper template 6 is fixedly connected to the bottom of the cylinder 9, a shell 10 is fixedly connected to the bottom of the fixed seat 1, an electric push rod 12 is fixedly connected to the left side of the bottom of the inner cavity of the shell 10, a sliding plate 13 is fixedly connected to the top of the electric push rod 12, a sliding sleeve 14 is fixedly connected to the right side of the sliding plate 13, a sliding rod 16 is provided in the inner cavity of the sliding sleeve 14, a push plate 18 is fixedly connected to the right side of the sliding sleeve 14, a push column 17 is fixedly connected to the top of the push plate 18, and a circular plate 4 is fixedly connected to the top of the push column 17 which passes through the inner cavity of the mold groove 3.

[0030] Through the above technical scheme, the electric push rod 12 is used to facilitate the sliding plate 13 to move, so that the sliding plate 13 drives the sliding sleeve 14 to move, and the movement of the sliding sleeve 14 drives the pushing plate 18 to move, and the pushing plate 18 drives the pushing column 17 to move, and the pushing column 17 drives the circular plate 4 to move, so that the circular plate 4 pushes the parts placed on the surface of the mold groove 3 to move, and effectively pushes the parts out of the inner cavity of the mold groove 3, which is convenient for work to take materials, thereby improving the work efficiency of the staff and solving the troubles of the staff. Through the cylinder 9, it is easy to push the upper template 6 to move, so that the upper template 6 punches the parts placed in the inner cavity of the mold groove 3, which is convenient for the staff to use later.

[0031] Specifically, the bottom of the fixed seat 1 is fixedly connected with support columns 11 all around, and the bottom of the support column 11 is fixedly connected with an anti-slip pad. A first slide groove 15 is provided on one side of the inner cavity of the shell 10, and one side of the sliding plate 13 is slidably connected to the inner cavity of the first slide groove 15. Both sides of the sliding sleeve 14 are fixedly connected with mounting blocks 20, and the surface of the mounting block 20 is provided with mounting bolts 19. Both ends of the left side of the push plate 18 are provided with threaded holes, and the surface of the mounting bolts 19 is threadedly connected to the inner cavity of the threaded holes. A second slide groove is provided on the inner side of the support frame 5, and both sides of the upper template 6 are fixedly connected. A slider 7 is connected, and the surface of the slider 7 is slidably connected to the inner cavity of the second slide groove. Both ends of the slide rod 16 are fixedly connected to the two ends of the inner cavity of the shell 10. The inner cavity of the sliding sleeve 14 is slidably connected to the surface of the slide rod 16. The second slide groove is used to limit the slider 7 to prevent the upper template 6 from shaking during the sliding process, thereby improving the sliding stability of the upper template 6, and indirectly improving the accuracy of stamping, solving the troubles of the staff. Through the anti-slip pad, the equipment can be effectively prevented from sliding during the process, thereby improving the working stability of the equipment.

[0032] The working principle of the utility model is as follows: first, the user places the parts on the surface of the mold groove 3, and then the user starts the cylinder 9 through the external controller, and the cylinder 9 pushes the upper template 6 to move, so that the upper template 6 moves to punch the parts placed on the surface of the mold groove 3, which is convenient for the staff to use later. When the mold is stamped, the user starts the electric push rod 12 through the external controller, and the electric push rod 12 is convenient to push the sliding plate 13 to move, so that the sliding plate 13 drives the sliding sleeve 14 to move, and the movement of the sliding sleeve 14 drives the push plate 18 to move, and the push plate 18 drives the push column 17 to move, and the push column 17 drives the circular plate 4 to move, so that the circular plate 4 pushes the parts placed on the surface of the mold groove 3 to move, effectively pushing the parts out of the inner cavity of the mold groove 3, facilitating the work of taking materials, thereby improving the work efficiency of the staff and solving the troubles of the staff.

[0033] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the utility model, rather than to limit the protection scope of the utility model. Although the utility model has been described in detail with reference to the preferred embodiments, ordinary technicians in this field should understand that the technical solution of the utility model can be modified or replaced by equivalents without departing from the essence and scope of the technical solution of the utility model.

Claims

1. An aviation fairing composite component forming tool, comprising a fixing seat (1), characterized in that: The top of the fixed seat (1) is fixedly connected to a punching table (2), a mold groove (3) is provided on the surface of the punching table (2), both sides of the fixed seat (1) are fixedly connected to support frames (5), the top of the support frame (5) is fixedly connected to a bearing plate (8), the top of the bearing plate (8) is fixedly connected to a cylinder (9), the bottom of the cylinder (9) is fixedly connected to an upper mold plate (6), the bottom of the fixed seat (1) is fixedly connected to a shell (10), and the bottom of the inner cavity of the shell (10) is fixedly connected to the upper mold plate (6). An electric push rod (12) is fixedly connected to the left side, a sliding plate (13) is fixedly connected to the top of the electric push rod (12), a sliding sleeve (14) is fixedly connected to the right side of the sliding plate (13), a sliding rod (16) is provided in the inner cavity of the sliding sleeve (14), a push plate (18) is fixedly connected to the right side of the sliding sleeve (14), a push column (17) is fixedly connected to the top of the push plate (18), and a circular plate (4) is fixedly connected to the top of the push column (17) which passes through the inner cavity of the mold groove (3).

2. The aircraft fairing composite component forming tool according to claim 1, characterized in that: The bottom of the fixing seat (1) is fixedly connected to support columns (11) on all sides thereof, and the bottom of the support columns (11) is fixedly connected to an anti-slip pad.

3. The aircraft fairing composite component forming tool according to claim 1, characterized in that: A first sliding groove (15) is provided on one side of the inner cavity of the shell (10), and one side of the sliding plate (13) is slidably connected to the inner cavity of the first sliding groove (15).

4. The aircraft fairing composite component forming tool according to claim 1, characterized in that: Both sides of the sliding sleeve (14) are fixedly connected with mounting blocks (20), and the surface of the mounting blocks (20) is provided with mounting bolts (19).

5. The aircraft fairing composite component forming tool according to claim 1, characterized in that: Both ends of the left side of the push plate (18) are provided with threaded holes, and the surface of the mounting bolt (19) is threadedly connected to the inner cavity of the threaded hole.

6. The aircraft fairing composite component forming tool according to claim 1, characterized in that: A second slide groove is provided on the inner side of the support frame (5), and sliders (7) are fixedly connected to both sides of the upper template (6), and the surface of the slider (7) is slidably connected to the inner cavity of the second slide groove.

7. The aircraft fairing composite component forming tool according to claim 1, characterized in that: Both ends of the sliding rod (16) are fixedly connected to the two ends of the inner cavity of the shell (10), and the inner cavity of the sliding sleeve (14) is slidably connected to the surface of the sliding rod (16).

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