Tool clamp for high-precision aviation parts

Abstract

The utility model relates to the field of aeronautical parts, and discloses a high-precision aeronautical part tool clamp which comprises a bottom plate, four sets of rectangular blocks are fixedly installed on the top of the bottom plate, fixing blocks are fixedly installed on the two sides of the bottom of the bottom plate, and a protection box is arranged at the bottom of the bottom plate. The top of the protection box and the bottom of the fixing block are fixedly installed, and limiting assemblies used for limiting aviation parts are arranged on the two sides of the top of the bottom plate correspondingly. Through mutual cooperation of the rotating rod, the clamping block, the fixing sleeve, the electric push rod, the connecting sleeve and the rotating block, when an aviation part is placed on the bottom plate, the electric push rod can be started at the moment, the telescopic end of the electric push rod drives the connecting sleeve to move towards the inner side, and the connecting sleeve moves to drive the rotating block, the rotating rod and the clamping block to rotate; and therefore, the aviation parts can be limited, and then the aviation parts can be subjected to punching and other procedures.

Description

Technical Field

[0001] This utility model relates to the field of aerospace parts, and in particular to a tooling fixture for high-precision aerospace parts. Background Technology

[0002] Aviation components are the basic building blocks of aircraft (including airplanes, helicopters, drones, and other types of aircraft). From the fuselage frame of an aircraft to the tiny parts of the engine, from the structural components of the wings to the elements of the avionics system, these components each perform their own function and work together to ensure that the aircraft can operate safely and efficiently. They are the cornerstone of the aviation industry, and their performance and quality directly determine the overall performance and safety of the aircraft.

[0003] Aerospace component manufacturing is a core component of the aviation industry, and its manufacturing precision and quality directly determine the performance and safety of aircraft. Tooling and fixtures, as indispensable auxiliary equipment in the aerospace component processing, undertake the critical tasks of positioning and clamping components, ensuring that machining tools can precisely cut, drill, grind, and perform other operations on the components according to predetermined paths. From turbine blades in aircraft engines to key connecting parts in the fuselage structure, tooling and fixtures, like the skillful hands of a craftsman, precisely shape raw materials in the manufacturing of various aerospace components, laying the foundation for building high-performance aircraft.

[0004] When machining parts in aerospace equipment, tooling fixtures are required for positioning to prevent movement during machining and increase machining accuracy. However, existing tooling fixtures for aerospace parts cannot position parts of different sizes, and some parts need to be lifted for construction, which affects the applicability of tooling fixtures. Therefore, a high-precision tooling fixture for aerospace parts is proposed to solve the above problems. Utility Model Content

[0005] To overcome the above shortcomings, this utility model provides a high-precision aerospace component tooling fixture, which aims to improve the problem that existing aerospace component tooling fixtures cannot position components of different sizes, and that some components need to be lifted for construction, thus affecting the low applicability of the tooling fixtures.

[0006] To achieve the above objectives, the present invention adopts the following technical solution:

[0007] A high-precision aerospace component tooling fixture includes a base plate, four sets of rectangular blocks fixedly installed on the top of the base plate, fixing blocks fixedly installed on both sides of the bottom of the base plate, a protective box provided at the bottom of the base plate, the top of the protective box and the bottom of the fixing blocks fixedly installed, limiting components for limiting the aerospace components are provided on both sides of the top of the base plate, and an ejection component for ejecting the aerospace components is provided at the bottom of the base plate.

[0008] As a further description of the above technical solution:

[0009] The limiting assembly includes two sets of rotating rods. The front and rear ends of the rotating rods extend to the outside of the rectangular block and are fixedly mounted with clamping blocks. The rotating rods and the rectangular block are rotatably mounted. Fixed sleeves are fixedly mounted on both sides of the bottom of the base plate. An electric push rod is fixedly mounted inside the fixed sleeve. A connecting sleeve is fixedly mounted on the telescopic end of the electric push rod. A rotating block is fixedly mounted on the surface of the rotating rod. The bottom of the rotating block extends to the bottom of the base plate. The inside of the connecting sleeve is movably mounted to the rotating block via a shaft pin.

[0010] As a further description of the above technical solution:

[0011] Connecting plates are provided on both sides of the top of the base plate. The outer side of the connecting plate and the inner side of the clamping block are fixedly installed. Several sets of clamping claws are fixedly installed on the inner side of the connecting plate.

[0012] As a further description of the above technical solution:

[0013] The ejection assembly includes two sets of telescopic cylinders. The bottom of the telescopic cylinders and the bottom of the inner wall of the protective box are fixedly installed. The telescopic end of the telescopic cylinder extends through to the top of the base plate and is slidably installed with the base plate. A push plate is fixedly installed on the telescopic end of the telescopic cylinder.

[0014] As a further description of the above technical solution:

[0015] Mounting blocks are fixedly installed on both the front and rear sides of the protective box, and mounting slots are provided on the top of the mounting blocks.

[0016] As a further description of the above technical solution:

[0017] The bottom of the protective box is provided with a threaded groove, and a rotating ring is installed inside the threaded groove.

[0018] As a further description of the above technical solution:

[0019] The top of the push plate is provided with a protective plate, the bottom of the protective plate is in contact with the top of the push plate, and the four corners of the bottom of the push plate are detachably installed by bolts and the protective plate.

[0020] This utility model has the following beneficial effects:

[0021] 1. In this utility model, through the cooperation of the rotating rod, clamping block, fixed sleeve, electric push rod, connecting sleeve and rotating block, when the aviation parts are placed on the bottom plate, the electric push rod can be activated. The extension end of the electric push rod drives the connecting sleeve to move inward. The movement of the connecting sleeve drives the rotating block, rotating rod and clamping block to rotate, thereby limiting the aviation parts. Subsequently, the aviation parts can be drilled and other processes can be performed.

[0022] 2. In this utility model, through the cooperation of the telescopic cylinder and the push plate, after the aerospace parts are processed, the telescopic cylinder can be activated. The telescopic end of the telescopic cylinder drives the push plate to move to the top. The push plate moving to the top can push out the processed aerospace parts, thereby making it easy to remove the aerospace parts. Attached Figure Description

[0023] Figure 1 This is a schematic diagram of the top structure of the base plate of this utility model;

[0024] Figure 2 This is a cross-sectional view of the protective box of this utility model;

[0025] Figure 3 This utility model Figure 2 Enlarged structural diagram at point A in the middle;

[0026] Figure 4 This utility model Figure 2 Enlarged structural diagram at point B in the middle.

[0027] Legend:

[0028] 1. Base plate; 2. Rectangular block; 3. Fixing block; 4. Protective box; 5. Limiting assembly; 51. Rotating rod; 52. Clamping block; 53. Fixing sleeve; 54. Electric push rod; 55. Connecting sleeve; 56. Rotating block; 57. Connecting plate; 58. Gripper; 6. Ejection assembly; 61. Telescopic cylinder; 62. Push plate; 63. Protective plate; 7. Mounting block; 8. Mounting groove; 9. Threaded groove; 10. Rotating ring. Detailed Implementation

[0029] 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.

[0030] Reference Figure 1-4This utility model provides an embodiment of a high-precision aerospace component tooling fixture, including a base plate 1. Four sets of rectangular blocks 2 are fixedly installed on the top of the base plate 1, and fixing blocks 3 are fixedly installed on both sides of the bottom of the base plate 1. A protective box 4 is provided at the bottom of the base plate 1, with the top of the protective box 4 and the bottom of the fixing blocks 3 fixedly installed. Limiting components 5 for limiting the aerospace components are provided on both sides of the top of the base plate 1, and an ejection component 6 for ejecting the aerospace components is provided at the bottom of the base plate 1. First, the aerospace components to be processed can be placed on the base plate 1, and then the aerospace components can be limited by the limiting components 5. At this time, the aerospace components can be drilled, ground, and other processes. When the aerospace components are processed, the aerospace components can be ejected by the ejection component 6 so that the workers can take the aerospace components away.

[0031] Reference Figure 1-4 The limiting assembly 5 includes two sets of rotating rods 51. The front and rear ends of each rotating rod 51 extend to the outside of the rectangular block 2 and are fixedly mounted with clamping blocks 52. The rotating rods 51 and the rectangular block 2 are rotatably mounted. Fixed sleeves 53 are fixedly mounted on both sides of the bottom of the base plate 1. An electric push rod 54 is fixedly mounted inside the fixed sleeve 53. A connecting sleeve 55 is fixedly mounted at the telescopic end of the electric push rod 54. A rotating block 56 is fixedly mounted on the surface of the rotating rod 51. The bottom of the rotating block 56 extends to the bottom of the base plate 1. The connecting sleeve 55 is movably mounted to the rotating block 56 via a shaft pin. Through the mutual cooperation of the rotating rods 51, clamping blocks 52, fixed sleeves 53, electric push rods 54, connecting sleeves 55, and rotating blocks 56, when the aircraft zero... When the component is placed on the base plate 1, the electric push rod 54 can be activated. The telescopic end of the electric push rod 54 drives the connecting sleeve 55 to move inward. The movement of the connecting sleeve 55 drives the rotating block 56, the rotating rod 51, and the clamping block 52 to rotate, thereby limiting the aerospace component. Subsequently, processes such as drilling can be performed on the aerospace component. Connecting plates 57 are provided on both sides of the top of the base plate 1. The outer side of the connecting plate 57 and the inner side of the clamping block 52 are fixedly installed. Several sets of clamps 58 are fixedly installed on the inner side of the connecting plate 57. Through the cooperation of the connecting plate 57 and the clamps 58, when the clamping block 52 rotates inward, the connecting plate 57 and the clamps 58 rotate inward, thereby stably limiting the aerospace component.

[0032] Reference Figure 1-4The ejection assembly 6 includes two sets of telescopic cylinders 61. The bottom of the telescopic cylinders 61 is fixedly installed on the bottom of the inner wall of the protective box 4. The telescopic end of the telescopic cylinder 61 extends through to the top of the base plate 1 and is slidably installed with the base plate 1. A push plate 62 is fixedly installed on the telescopic end of the telescopic cylinder 61. Through the cooperation of the telescopic cylinder 61 and the push plate 62, after the aerospace parts are processed, the telescopic cylinder 61 can be activated. The telescopic end of the telescopic cylinder 61 drives the push plate 62 to move upward. The push plate 62 moves upward and ejects the processed aerospace parts, thus facilitating their removal. A protective plate 63 is provided on the top of the push plate 62. The bottom of the protective plate 63 contacts the top of the push plate 62. The four corners of the bottom of the push plate 62 are detachably installed with the protective plate 63 by bolts. The protective plate 63 allows for... The protective box 4 is designed to protect aircraft parts from scratches caused by the push plate 62 when lifting them. Mounting blocks 7 are fixedly installed on both the front and rear sides of the protective box 4. Mounting slots 8 are formed on the top of the mounting blocks 7. Through the cooperation of the mounting blocks 7 and the mounting slots 8, the protective box 4 can be placed on a table. Bolts can then pass through the mounting slots 8 and be fixed to the table, allowing the entire box to be carried anywhere for operation. A threaded groove 9 is formed at the bottom of the protective box 4. A rotating ring 10 is installed inside the threaded groove 9. Through the cooperation of the threaded groove 9 and the rotating ring 10, when aircraft parts need to be lifted for processing, the rotating ring 10 can be rotated to enter the threaded groove 9. Then, a crane can lift the rotating ring 10, allowing the aircraft parts to be processed.

[0033] Working principle: First, the protective box 4 is fixed by passing bolts through the mounting slot 8. Then, the aerospace parts to be processed are placed on the bottom plate 1. Then, the electric push rod 54 can be activated. The telescopic end of the electric push rod 54 drives the connecting sleeve 55 to move inward. The movement of the connecting sleeve 55 drives the rotating block 56, the rotating rod 51 and the clamping block 52 to rotate. The inward rotation of the clamping block 52 will drive the connecting plate 57 and the gripper 58 to rotate inward, thereby limiting the aerospace parts. Then, the aerospace parts can be drilled and other processes can be performed.

[0034] After the aerospace parts are processed, the telescopic cylinder 61 can be activated. The telescopic end of the telescopic cylinder 61 drives the push plate 62 to move to the top. The push plate 62 moving to the top can push out the processed aerospace parts, so that the aerospace parts can be easily removed.

[0035] When it is necessary to lift some aerospace parts for processing, the rotating ring 10 can be rotated and will enter the threaded groove 9. Then the rotating ring 10 can be rotated to enter the threaded groove 9, and then the crane can lift the rotating ring 10, so that some aerospace parts that need to be lifted can be processed. Finally, the aerospace parts can be processed.

[0036] Finally, it should be noted that the above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. A high-precision aerospace component tooling fixture, comprising a base plate (1), characterized in that: Four sets of rectangular blocks (2) are fixedly installed on the top of the base plate (1). Fixing blocks (3) are fixedly installed on both sides of the bottom of the base plate (1). A protective box (4) is provided at the bottom of the base plate (1). The top of the protective box (4) and the bottom of the fixing blocks (3) are fixedly installed. Limiting components (5) for limiting the aviation parts are provided on both sides of the top of the base plate (1). An ejection component (6) for ejecting the aviation parts is provided at the bottom of the base plate (1).

2. The high-precision aerospace component tooling fixture according to claim 1, characterized in that: The limiting component (5) includes two sets of rotating rods (51). The front end and rear end of the rotating rods (51) extend to the outside of the rectangular block (2) and are fixedly installed with clamping blocks (52). The rotating rods (51) and the rectangular block (2) are rotatably installed. Fixed sleeves (53) are fixedly installed on both sides of the bottom of the base plate (1). An electric push rod (54) is fixedly installed inside the fixed sleeve (53). A connecting sleeve (55) is fixedly installed at the telescopic end of the electric push rod (54). A rotating block (56) is fixedly installed on the surface of the rotating rods (51). The bottom of the rotating block (56) extends to the bottom of the base plate (1). The inside of the connecting sleeve (55) is movably installed with the rotating block (56) through a shaft pin.

3. The high-precision aerospace component tooling fixture according to claim 2, characterized in that: The bottom plate (1) has connecting plates (57) on both sides of its top. The outer side of the connecting plate (57) and the inner side of the clamping block (52) are fixedly installed. Several sets of clamping claws (58) are fixedly installed on the inner side of the connecting plate (57).

4. The tooling fixture for high-precision aerospace parts according to claim 1, characterized in that: The ejection assembly (6) includes two sets of telescopic cylinders (61). The bottom of the telescopic cylinder (61) and the bottom of the inner wall of the protective box (4) are fixedly installed. The telescopic end of the telescopic cylinder (61) extends through to the top of the base plate (1) and is slidably installed with the base plate (1). A push plate (62) is fixedly installed on the telescopic end of the telescopic cylinder (61).

5. A high-precision aerospace component tooling fixture according to claim 1, characterized in that: The protective box (4) has mounting blocks (7) fixedly installed on both the front and rear sides, and the top of the mounting block (7) has a mounting groove (8).

6. A high-precision aerospace component tooling fixture according to claim 1, characterized in that: The bottom of the protective box (4) is provided with a threaded groove (9), and a rotating ring (10) is installed inside the threaded groove (9).

7. A high-precision aerospace component tooling fixture according to claim 4, characterized in that: The top of the push plate (62) is provided with a protective plate (63), the bottom of the protective plate (63) is in contact with the top of the push plate (62), and the four corners of the bottom of the push plate (62) are detachably installed by bolts and the protective plate (63).

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