Clamp for polishing parts of civil aircraft

Abstract

The utility model discloses a kind of civil aircraft parts clamps for polishing, belong to civil aircraft parts processing field, and it includes support frame, the side fixed connection of support frame has clamping motor, the output shaft of clamping motor is fixedly connected with rotating screw column by shaft coupling, the outer wall of rotating screw column movably connects movable block, the side movable connection of movable block has limiting long column;By the support frame, clamping motor, rotating screw column, movable block, limiting long column, connecting small block, clamping plate, side hinge, protection frame, connecting bolt and lower hinge being set, the clamp for polishing of civil aircraft parts can be used more conveniently, it can be comprehensively protected when clamp is not used, reduce the damage of environment to clamp when not being used, improve the service life of clamp overall, reduce the frequency of subsequent maintenance of clamp, reduce the use cost of subsequent work.

Description

Technical Field

[0001] This utility model relates to the field of civil aircraft parts processing technology, specifically a jig for grinding civil aircraft parts. Background Technology

[0002] Civil aircraft components are the core elements that ensure the safe operation and performance of aircraft. They include key components such as engines, wings, landing gear, avionics systems, and hydraulic systems, as well as auxiliary components such as fasteners and seals. All of them must undergo strict material selection, precision manufacturing processes, and airworthiness certification to ensure that they have high strength, corrosion resistance, and fatigue resistance in extreme flight environments. Their quality and reliability directly determine the aircraft's flight safety, operational efficiency, and maintenance costs. In order to clamp and position these components during grinding, civil aircraft component grinding fixtures are required.

[0003] An investigation revealed that patent CN215700834U discloses a jig for grinding civil aircraft parts, comprising: a U-shaped support frame; a motor mounted on the side surface of the U-shaped support frame; a bidirectional screw fixedly connected to the output shaft of the motor through the side surface of the U-shaped support frame; two moving blocks screwed to the outer side of the bidirectional screw; connecting cylinders rotatably connected to both sides of the U-shaped support frame; rectangular connecting blocks slidably connected to the surfaces of the two adjacent connecting cylinders; round rods fixedly connected to the sides of the two adjacent rectangular connecting blocks; bearings sleeved on the outer sides of the two round rods; and connecting rods connecting the two bearings to the two moving blocks. This invention is easy to operate, provides good clamping effect, facilitates adjustment of clamping distance, and allows for flanging of parts and multi-directional grinding.

[0004] The aforementioned patent is not very convenient for users to use. When the fixture is not in use, it is not fully protected, which increases the damage to the fixture caused by the environment when it is not in use, reduces the overall service life of the fixture, increases the frequency of subsequent maintenance and repair, and increases the cost of subsequent work.

[0005] Therefore, this utility model provides a jig for grinding civil aircraft parts to solve the above problems. Utility Model Content

[0006] (a) Technical problems to be solved This utility model provides a jig for grinding civil aircraft parts, aiming to solve the problems mentioned in the background art.

[0007] (II) Technical Solution To achieve the above objectives, this utility model provides the following technical solution: a jig for grinding civil aircraft parts, including a support frame, a clamping motor fixedly connected to one side of the support frame, a rotating threaded column fixedly connected to the output shaft of the clamping motor via a coupling, a movable block movably connected to the outer wall of the rotating threaded column, a limiting column movably connected to one side of the movable block, and a connecting block fixedly connected to the top of the movable block.

[0008] A clamping plate is fixedly connected to the top of the connecting block, a side hinge is fixedly connected to one side of the support frame, a protective frame is fixedly connected to one side of the side hinge, a connecting bolt is movably connected inside the support frame, and a lower hinge is fixedly connected to the bottom of the support frame. This design makes the jig for grinding civil aircraft parts more convenient to use, provides comprehensive protection for the jig when it is not in use, reduces environmental damage to the jig when not in use, extends the overall service life of the jig, reduces the frequency of subsequent jig maintenance, and lowers the operating costs of subsequent work.

[0009] As a preferred technical solution of this application, an electric push rod is fixedly connected inside the support frame, and there are two support frames, with two electric push rods installed inside each support frame.

[0010] As a preferred technical solution of this application, the bottom end of the electric push rod is fixedly connected to a base, and the bottom area of ​​the base is larger than the bottom area of ​​the electric push rod.

[0011] As a preferred technical solution of this application, a locking bolt is movably connected to one side of the protective frame, a mounting plate is movably connected to the outer wall of the locking bolt, and a mounting handle is fixedly connected to one side of the mounting plate.

[0012] As a preferred technical solution of this application, one side of the movable block is movably connected to the outer wall of the limiting column, and the length of the limiting column is equal to the length of the rotating threaded column.

[0013] As a preferred technical solution of this application, the interior of the protective frame is movably connected to one side of the support frame via a side hinge, and the interior width of the protective frame is equal to the width of the support frame.

[0014] As a preferred technical solution of this application, the bottom of the support frame is fixedly connected to one side of the lower hinge, and the number of lower hinges is two.

[0015] (0) Beneficial effects This utility model provides a jig for grinding civil aircraft parts. By setting up a support frame, clamping motor, rotating threaded column, movable block, limiting column, connecting block, clamping plate, side hinge, protective frame, connecting bolt and lower hinge, the jig for grinding civil aircraft parts can be made more convenient to use. It can provide comprehensive protection for the jig when it is not in use, reduce the damage to the jig caused by the environment when it is not in use, extend the overall service life of the jig, reduce the number of subsequent maintenance and repairs, and reduce the operating costs of subsequent work. This utility model provides a jig for grinding civil aircraft parts. The electric push rod and base facilitate the height adjustment of the jig during use, improve the overall adaptability of the jig to the environment, facilitate its use by personnel at different heights, and promote the long-term use of the jig. Attached Figure Description

[0016] The accompanying drawings are provided to further illustrate the present invention and form part of the specification. They are used together with the embodiments of the present invention to explain the present invention, but do not constitute a limitation thereof. In the drawings:

[0017] Figure 1 This is a three-dimensional view of the overall structure of this utility model; Figure 2 This is a bottom view of the structure of this utility model; Figure 3 This is a top view of the structure of this utility model; Figure 4 This is a right view of the structure of this utility model; Figure 5 This is the utility model Figure 3 Enlarged view of the structure at point A in the middle; Figure 6 This is a rear view of the structure of this utility model.

[0018] In the picture: 1. Support frame; 2. Clamping motor; 3. Rotating threaded column; 4. Movable block; 5. Limiting column; 6. Connecting block; 7. Clamping plate; 8. Side hinge; 9. Protective frame; 10. Connecting bolt; 11. Electric push rod; 12. Base; 13. Locking bolt; 14. Mounting plate; 15. Mounting handle; 16. Lower hinge. Detailed Implementation

[0019] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0020] Please see Figure 1-6 The present invention provides a technical solution: a jig for grinding civil aircraft parts, including a support frame 1, a clamping motor 2 fixedly connected to one side of the support frame 1, a rotating threaded column 3 fixedly connected to the output shaft of the clamping motor 2 through a coupling, a movable block 4 movably connected to the outer wall of the rotating threaded column 3, a limiting column 5 movably connected to one side of the movable block 4, and a connecting block 6 fixedly connected to the top of the movable block 4.

[0021] A clamping plate 7 is fixedly connected to the top of the connecting block 6, a side hinge 8 is fixedly connected to one side of the support frame 1, a protective frame 9 is fixedly connected to one side of the side hinge 8, a connecting bolt 10 is movably connected inside the support frame 1, and a lower hinge 16 is fixedly connected to the bottom of the support frame 1. This makes the jig for grinding civil aircraft parts more convenient to use, provides comprehensive protection for the jig when it is not in use, reduces environmental damage to the jig when it is not in use, extends the overall service life of the jig, reduces the frequency of subsequent jig maintenance, and reduces the operating costs of subsequent work.

[0022] like Figure 1-5 As shown, based on Embodiment 1, this utility model provides a technical solution: an electric push rod 11 is fixedly connected inside the support frame 1, there are two support frames 1, and each support frame 1 is provided with two electric push rods 11 inside, which can adjust the overall working height of the fixture. The bottom end of the electric push rod 11 is fixedly connected to a base 12, and the bottom area of ​​the base 12 is larger than the bottom area of ​​the electric push rod 11, which improves the stability of the fixture during operation and is beneficial to the long-term use of the fixture.

[0023] A locking bolt 13 is movably connected to one side of the protective frame 9. A mounting plate 14 is movably connected to the outer wall of the locking bolt 13. A mounting handle 15 is fixedly connected to one side of the mounting plate 14, which facilitates locking the position of the two protective frames 9 when they are closed, and also facilitates moving the entire clamp when not in use.

[0024] One side of the movable block 4 is movably connected to the outer wall of the limiting column 5, and the length of the limiting column 5 is equal to the length of the rotating threaded column 3, which allows the movable block 4 to move in a stable straight line. The interior of the protective frame 9 is movably connected to one side of the support frame 1 through the side hinge 8, and the interior width of the protective frame 9 is equal to the width of the support frame 1, which allows the protective frame 9 to cover and protect the top of the support frame 1 and its connecting parts. The bottom of the support frame 1 is fixedly connected to one side of the lower hinge 16, and there are two lower hinges 16, which facilitates the stacking of the two support frames 1.

[0025] like Figure 1-5 As shown, when a user needs to use a jig for grinding civil aircraft parts, the electric push rod 11 extends, causing the base 12 to contact the ground. This allows the support frame 1 to reach an appropriate working height. The part to be clamped is placed at the connection center of the two support frames 1. The clamping motor 2 operates, and the output shaft of the clamping motor 2 rotates, causing the rotating threaded column 3 to rotate. The rotation of the rotating threaded column 3 causes the movable block 4 to move, thereby allowing the movable block 4 to drive the connecting small block 6 to move on the clamping plate 7. This allows the two clamping plates 7 to clamp the part, thus completing the subsequent grinding. When the electric push rod 11 is not used, it retracts, causing the base 12 to retract into the support frame 1. The protective frame 9 is rotated by the side hinge 8, allowing the protective frame 9 to cover the sides and top of the support frame 1. The connecting bolt 10 is rotated and removed. Then, the two protective frames 9 are stacked on top of each other by the lower hinge 16. The mounting plate 14 is locked to the two protective frames 9 by the locking bolt 13. Now, the entire jig can be moved to the appropriate position by the mounting handle 15.

[0026] In the description of this utility model, it should be understood that the terms "upper", "lower", "front", "rear", "left", "right", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, and are only for the convenience of describing this utility model, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this utility model.

[0027] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of this utility model, and are not intended to limit it. Although this utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that modifications can still be made to the technical solutions described in the foregoing embodiments, or equivalent substitutions can be made to some of the technical features. Such modifications or substitutions do not cause the essence of the corresponding technical solutions to deviate from the spirit and scope of the technical solutions of the embodiments of this utility model.

Claims

1. A jig for grinding civil aircraft parts, comprising a support frame (1), characterized in that: A clamping motor (2) is fixedly connected to one side of the support frame (1). The output shaft of the clamping motor (2) is fixedly connected to a rotating threaded column (3) via a coupling. A movable block (4) is movably connected to the outer wall of the rotating threaded column (3). A limit column (5) is movably connected to one side of the movable block (4). A connecting block (6) is fixedly connected to the top of the movable block (4). A clamp (7) is fixedly connected to the top of the connecting block (6), a side hinge (8) is fixedly connected to one side of the support frame (1), a protective frame (9) is fixedly connected to one side of the side hinge (8), a connecting bolt (10) is movably connected inside the support frame (1), and a lower hinge (16) is fixedly connected to the bottom of the support frame (1).

2. The jig for grinding civil aircraft parts according to claim 1, characterized in that: An electric push rod (11) is fixedly connected inside the support frame (1). There are two support frames (1), and each support frame (1) is provided with two electric push rods (11).

3. A jig for grinding civil aircraft parts according to claim 2, characterized in that: The bottom end of the electric push rod (11) is fixedly connected to a base (12), and the bottom area of ​​the base (12) is larger than the bottom area of ​​the electric push rod (11).

4. A jig for grinding civil aircraft parts according to claim 1, characterized in that: A locking bolt (13) is movably connected to one side of the protective frame (9), and a mounting plate (14) is movably connected to the outer wall of the locking bolt (13). A mounting handle (15) is fixedly connected to one side of the mounting plate (14).

5. A jig for grinding civil aircraft parts according to claim 1, characterized in that: One side of the movable block (4) is movably connected to the outer wall of the limiting column (5), and the length of the limiting column (5) is equal to the length of the rotating threaded column (3).

6. A jig for grinding civil aircraft parts according to claim 1, characterized in that: The interior of the protective frame (9) is movably connected to one side of the support frame (1) via a side hinge (8), and the interior width of the protective frame (9) is equal to the width of the support frame (1).

7. A jig for grinding civil aircraft parts according to claim 1, characterized in that: The bottom of the support frame (1) is fixedly connected to one side of the lower hinge (16), and there are two lower hinges (16).

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