Airplane air inlet triangular port forming equipment with male die block sequential demolding mechanism

Abstract

The utility model belongs to the technical field of forming equipment, and particularly relates to airplane air inlet triangular port forming equipment with a male die block sequential demolding mechanism. The device comprises a device body, the interior of the device body is of a hollow structure, the two sides of the exterior of the device body are symmetrically distributed, and the device body structurally comprises an internal sheet-shaped core mold assembly and an external plate-shaped connecting block assembly; the outer plate-shaped connecting block assembly is fixedly installed outside the inner arc-shaped face forming face assembly, the inner surface of the outer plate-shaped connecting block assembly is tightly attached to the outer wall of the inner arc-shaped face forming face assembly, the inner arc-shaped face forming face assembly comprises an upper top face and a lower bottom face, and the upper top face and the lower bottom face are integrally formed. According to the utility model, each section is formed by mutually combining and assembling the sheet-shaped core molds, and the sheet-shaped core molds are small in single sheet size and light in weight, so that the working efficiency during assembly and disassembly can be effectively improved, and the demolding difficulty is reduced.

Description

Technical Field

[0001] This utility model belongs to the field of molding equipment technology, and relates to a molding equipment for the triangular port of an aircraft air intake with a sequential demolding mechanism for protruding modules. Background Technology

[0002] Aircraft air intakes supply the air needed for the aircraft's engines to operate, directly affecting engine efficiency. They play a crucial role in engine proper functioning and thrust, thus significantly impacting aircraft performance, especially fighter jets. Currently, commonly used aircraft air intakes primarily come in two structural forms: sheet metal composite structures and integral composite material structures. Because air passes through the inner surface of the air intake, extremely high requirements are placed on the smoothness and shape precision of the inner surfaces of the components.

[0003] Currently, the molding equipment used to produce this air intake mainly consists of two cores and several mounting and positioning blocks. The two cores are installed and fixed along the axial direction of the air intake, and positioning holes and screw fixing holes are designed on each side of the cores. The various components are mainly installed and fixed by connecting and fixing the cores. The two large core components themselves are fixed together by special bolts in the middle. The large size and weight of the two large core components ultimately increase the difficulty of internal demolding. Utility Model Content

[0004] The purpose of this invention is to address the above-mentioned problems by providing a triangular port forming equipment for an aircraft air intake with a sequential demolding mechanism for protruding modules.

[0005] To achieve the above objectives, the present invention adopts the following technical solution:

[0006] A triangular port forming device for an aircraft air intake with a sequential demolding mechanism for protruding modules includes a main body. The main body has a hollow internal structure, and its two external sides are symmetrically distributed. The main body includes an internal sheet-like core mold assembly and an external plate-like connecting block assembly. The external plate-like connecting block assembly is fixedly installed on the outside of the internal sheet-like core mold assembly, and its inner surface is tightly fitted to the outer wall of the internal sheet-like core mold assembly. The internal sheet-like core mold assembly includes an upper top surface and a lower bottom surface, which are integrally formed. The external plate-like connecting block assembly includes a side arc-shaped connecting block, a top connecting block, and a bottom connecting block.

[0007] In the above-mentioned aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism, the upper top surface includes a first upper arc surface, a second upper arc surface and a third upper arc surface. One side of the second upper arc surface is fixedly connected to the first upper arc surface, and the other side of the second upper arc surface is fixedly connected to the third upper arc surface.

[0008] In the above-mentioned aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism, the lower bottom surface includes a first lower bottom surface, a second lower bottom surface, and a side bottom surface. The first lower bottom surface and the second lower bottom surface are fixedly connected, and the side bottom surface is fixed to both sides of the second lower bottom surface.

[0009] In the above-mentioned aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism, the two sides of the first lower bottom surface are fixedly connected to the two sides of the first upper arc surface, and the two sides of the second lower bottom surface are fixedly connected to the two sides of the second upper arc surface and the third upper arc surface through the side bottom surface.

[0010] In the above-mentioned aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism, four sets of side arc-shaped connecting blocks are provided, and the side arc-shaped connecting blocks are fixedly installed in pairs on one side of the upper top surface and the lower bottom surface. One set of side arc-shaped connecting blocks is fixedly installed on one side of the first upper arc surface and the first lower bottom surface, and the top of the side arc-shaped connecting blocks is connected by a top connecting block. The other set of side arc-shaped connecting blocks is fixedly installed at the junction of the second upper arc surface and the third upper arc surface with the second lower bottom surface.

[0011] In the above-mentioned aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism, the bottom connecting block includes a horizontal connecting block and a vertical connecting block. There are two sets of horizontal connecting blocks and four sets of vertical connecting blocks. Both the horizontal connecting blocks and the vertical connecting blocks are fixed on the bottom surface.

[0012] In the above-mentioned aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism, the longitudinal connecting blocks are uniformly fixed between the two transverse connecting blocks.

[0013] In the above-mentioned aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism, the two sides of the transverse connecting block are fixedly provided with connecting edges, and the two ends of the longitudinal connecting block are fixedly overlapped on the connecting edges of the transverse connecting block.

[0014] In the above-mentioned aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism, one end of the bottom of the side arc-shaped connecting block is fixedly overlapped on the connecting edge of the transverse connecting block.

[0015] In the above-mentioned aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism, the cross-sections of the side arc-shaped connecting block, the top connecting block and the bottom connecting block are T-shaped structures.

[0016] Compared with existing technologies, the advantages of this utility model are:

[0017] 1. This utility model adopts a segmented cylindrical first upper arc surface, second upper arc surface and third upper arc surface, as well as a first lower bottom surface, second lower bottom surface and side bottom surface. Each segment is assembled by combining sheet-like core molds. The sheet-like core molds are small in size and light in weight, which can effectively improve the work efficiency during assembly and disassembly and reduce the difficulty of demolding.

[0018] 2. This utility model can significantly reduce the weight of the molding equipment, effectively avoiding problems such as deflection and deformation of the molding equipment caused by excessive weight in subsequent processes, thereby improving the precision of the molding equipment.

[0019] Other advantages, objectives and features of this invention will be partly apparent from the following description, and partly understood by those skilled in the art through study and practice of this invention. Attached Figure Description

[0020] Figure 1 This is a schematic diagram of the overall structure of this utility model.

[0021] Figure 2 This is a schematic diagram of the structure from another perspective of this utility model.

[0022] Figure 3 This is a top view of the structure of this utility model.

[0023] Figure 4 This is a schematic diagram of the structure of this utility model viewed from below.

[0024] Figure 5 This is a side view of the structure of this utility model.

[0025] Figure 6 This is a utility model Figure 3 Sectional view at point AA.

[0026] Figure 7 This is a schematic diagram of the internal sheet-like core mold assembly structure of this utility model.

[0027] Figure 8 This is a bottom view of the internal sheet-like core mold assembly of this utility model.

[0028] Figure 9 This is a utility model Figure 4 Enlarged diagram of point A in the middle.

[0029] In the diagram: 1. Main body of the equipment; 2. Internal sheet-like core mold assembly; 3. External plate-like connecting block assembly; 4. Top surface; 5. Side arc-shaped connecting block; 6. First upper arc surface; 7. Second upper arc surface; 8. Third upper arc surface; 9. First lower bottom surface; 10. Second lower bottom surface; 11. Side bottom surface; 12. Lower bottom surface; 13. Top connecting block; 14. Bottom connecting block; 15. Horizontal connecting block; 16. Vertical connecting block; 17. Connecting edge. Detailed Implementation

[0030] The present invention will be further described below with reference to the accompanying drawings.

[0031] like Figure 1-9 As shown, an aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism includes an equipment body 1. The interior of the equipment body 1 is a hollow structure, and the two sides of the exterior of the equipment body 1 are symmetrically distributed. The structure of the equipment body 1 includes an internal sheet-like core mold assembly 2 and an external plate-like connecting block assembly 3. The external plate-like connecting block assembly 3 is fixedly installed on the outside of the internal sheet-like core mold assembly 2, and the inner surface of the external plate-like connecting block assembly 3 is tightly fitted with the outer wall of the internal sheet-like core mold assembly 2. The internal sheet-like core mold assembly 2 includes an upper top surface 4 and a lower bottom surface 12, which are integrally formed together. The external plate-like connecting block assembly 3 includes a side arc-shaped connecting block 5, a top connecting block 13, and a bottom connecting block 14.

[0032] In this embodiment, the internal sheet-like core mold assembly 2 and the external plate-like connecting block assembly 3 can effectively improve the work efficiency during assembly and disassembly and reduce the difficulty of demolding.

[0033] Furthermore, the upper top surface 4 includes a first upper arc surface 6, a second upper arc surface 7, and a third upper arc surface 8. One side of the second upper arc surface 7 is fixedly connected to the first upper arc surface 6, and the other side of the second upper arc surface 7 is fixedly connected to the third upper arc surface 8.

[0034] Specifically, the lower bottom surface 12 includes a first lower bottom surface 9, a second lower bottom surface 10, and a side bottom surface 11. The first lower bottom surface 9 and the second lower bottom surface 10 are fixedly connected, and the side bottom surface 11 is fixed to both sides of the second lower bottom surface 10.

[0035] In this embodiment, the internal sheet-like core mold assembly 2 and the external plate-like connecting block assembly 3 are combined and assembled with each other. The sheet-like core mold is small in size and light in weight, which can effectively improve the work efficiency during assembly and disassembly.

[0036] Furthermore, the two sides of the first lower bottom surface 9 are fixedly connected to the two sides of the first upper arc surface 6, and the two sides of the second lower bottom surface 10 are fixedly connected to the two sides of the second upper arc surface 7 and the third upper arc surface 8 through the side bottom surface 11.

[0037] In this embodiment, the upper top surface 4 and the lower bottom surface 12 can be assembled together.

[0038] Furthermore, four sets of the side arc-shaped connecting blocks 5 are provided, and the side arc-shaped connecting blocks 5 are fixedly installed in pairs on one side of the upper top surface 4 and the lower bottom surface 12. One set of side arc-shaped connecting blocks 5 is fixedly installed on one side of the first upper arc surface 6 and the first lower bottom surface 9, and the top of the side arc-shaped connecting blocks 5 is connected by the top connecting block 13. The other set of side arc-shaped connecting blocks 5 is fixedly installed at the junction of the second upper arc surface 7 and the third upper arc surface 8 with the second lower bottom surface 10.

[0039] In this embodiment, the side arc-shaped connecting block 5 is used to connect the upper top surface 4 and the lower bottom surface 12, thereby improving the strength of the connection between the upper top surface 4 and the lower bottom surface 12.

[0040] Furthermore, the bottom connecting block 14 includes a horizontal connecting block 15 and a vertical connecting block 16. There are two sets of horizontal connecting blocks 15 and four sets of vertical connecting blocks 16. Both the horizontal connecting blocks 15 and the vertical connecting blocks 16 are fixed to the bottom surface.

[0041] In this embodiment, the connection strength between the bottom surfaces 12 can be improved by using the horizontal connecting block 15 and the vertical connecting block 16.

[0042] Furthermore, the longitudinal connecting blocks 16 are uniformly fixed between the two transverse connecting blocks 15.

[0043] In this embodiment, the longitudinal connecting block 16 is used to connect the transverse connecting block 15, which can improve the strength between the longitudinal connecting block 16 and the transverse connecting block 15.

[0044] Furthermore, the two sides of the transverse connecting block 15 are fixedly provided with connecting edges 17, and both ends of the longitudinal connecting block 16 are fixedly overlapped on the connecting edges 17 of the transverse connecting block 15.

[0045] In this embodiment, the fixing effect of the transverse connecting block 15 can be improved by the above method.

[0046] Furthermore, one end of the bottom of the side arc-shaped connecting block 5 is fixedly attached to the connecting edge 17 of the transverse connecting block 15.

[0047] In this embodiment, the stability of the connection between the side arc-shaped connecting block 5 and the transverse connecting block 15 can be improved.

[0048] Furthermore, the cross-sections of the side arc-shaped connecting block 5, the top connecting block 13, and the bottom connecting block 14 are T-shaped structures.

[0049] In this embodiment, the side arc-shaped connecting block 5, the top connecting block 13, and the bottom connecting block 14 can improve strength through a T-shaped structure.

[0050] The working principle of this utility model is as follows:

[0051] In use, this invention first assembles the internal sheet-like core mold assembly 2 by connecting it with the external plate-like connecting block assembly 3. The composite material is then laid up on the surface of the aircraft air intake triangular end molding equipment. After vacuuming, heating and pressurizing are applied to allow the composite material to adhere to the surface of the molding equipment. The equipment is then heated and cured, and finally cooled before being removed to obtain the complete aircraft air intake triangular end product. The invention employs segmented cylindrical first upper arc surface 6, second upper arc surface 7, and third upper arc surface 8, as well as a first lower bottom surface 9, second lower bottom surface 10, and side bottom surface 11. Each segment is assembled from sheet-like core molds. The small size and light weight of each sheet-like core mold effectively improves the efficiency of assembly and disassembly, and reduces the difficulty of demolding.

[0052] The specific embodiments described herein are merely illustrative examples illustrating the spirit of this utility model. Those skilled in the art to which this utility model pertains may make various modifications or additions to the described specific embodiments or use similar methods to replace them, without departing from the spirit of this utility model.

[0053] Although this document frequently uses terms such as 1. main body of the equipment; 2. internal sheet-like core mold assembly; 3. external plate-like connecting block assembly; 4. top surface; 5. side arc-shaped connecting block; 6. first upper arc surface; 7. second upper arc surface; 8. third upper arc surface; 9. first lower bottom surface; 10. second lower bottom surface; 11. side bottom surface; 12. lower bottom surface; 13. top connecting block; 14. bottom connecting block; 15. transverse connecting block; 16. longitudinal connecting block; 17. connecting edge, the possibility of using other terms is not excluded. The use of these terms is merely for the convenience of describing and explaining the essence of this utility model; interpreting them as any additional limitation would contradict the spirit of this utility model.

Claims

1. A molding equipment for a triangular port of an aircraft air intake with a sequential demolding mechanism for convex modules, comprising a main body (1), characterized in that, The equipment body (1) has a hollow internal structure. The two sides of the equipment body (1) are symmetrically distributed. The structure of the equipment body (1) includes an internal sheet-like core mold assembly (2) and an external plate-like connecting block assembly (3). The external plate-like connecting block assembly (3) is fixedly installed on the outside of the internal sheet-like core mold assembly (2), and the inner surface of the external plate-like connecting block assembly (3) is tightly fitted with the outer wall of the internal sheet-like core mold assembly (2). The internal sheet-like core mold assembly (2) includes an upper top surface (4) and a lower bottom surface (12). The upper top surface (4) and the lower bottom surface (12) are integrally formed. The external plate-like connecting block assembly (3) includes a side arc-shaped connecting block (5), a top connecting block (13), and a bottom connecting block (14).

2. The aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism according to claim 1, characterized in that, The top surface (4) includes a first upper arc surface (6), a second upper arc surface (7) and a third upper arc surface (8). One side of the second upper arc surface (7) is fixedly connected to the first upper arc surface (6), and the other side of the second upper arc surface (7) is fixedly connected to the third upper arc surface (8).

3. The aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism according to claim 2, characterized in that, The lower bottom surface (12) includes a first lower bottom surface (9), a second lower bottom surface (10) and a side bottom surface (11). The first lower bottom surface (9) and the second lower bottom surface (10) are fixedly connected, and the side bottom surface (11) is fixed on both sides of the second lower bottom surface (10).

4. The aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism according to claim 3, characterized in that, The two sides of the first lower bottom surface (9) are fixedly connected to the two sides of the first upper arc surface (6), and the two sides of the second lower bottom surface (10) are fixedly connected to the two sides of the second upper arc surface (7) and the third upper arc surface (8) through the side bottom surface (11).

5. The aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism according to claim 4, characterized in that, The side arc-shaped connecting blocks (5) are provided in four sets, and the side arc-shaped connecting blocks (5) are fixedly installed in pairs on one side of the upper top surface (4) and the lower bottom surface (12). One set of side arc-shaped connecting blocks (5) is fixedly installed on one side of the first upper arc surface (6) and the first lower bottom surface (9), and the top of the side arc-shaped connecting blocks (5) is connected by the top connecting block (13). The other set of side arc-shaped connecting blocks (5) is fixedly installed at the junction of the second upper arc surface (7) and the third upper arc surface (8) and the second lower bottom surface (10).

6. The aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism according to claim 5, characterized in that, The bottom connecting block (14) includes a horizontal connecting block (15) and a vertical connecting block (16). There are two sets of horizontal connecting blocks (15) and four sets of vertical connecting blocks (16). Both the horizontal connecting blocks (15) and the vertical connecting blocks (16) are fixed on the bottom surface.

7. The aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism according to claim 6, characterized in that, The longitudinal connecting block (16) is uniformly fixed between the two transverse connecting blocks (15).

8. The aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism according to claim 7, characterized in that, The two sides of the transverse connecting block (15) are fixedly provided with connecting edges (17), and both ends of the longitudinal connecting block (16) are fixedly overlapped on the connecting edges (17) of the transverse connecting block (15).

9. The aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism according to claim 8, characterized in that, One end of the bottom of the side arc-shaped connecting block (5) is fixedly overlapped on the connecting edge (17) of the transverse connecting block (15).

10. The aircraft air intake triangular port forming equipment with a convex module sequential demolding mechanism according to claim 9, characterized in that, The cross-sections of the side arc-shaped connecting block (5), the top connecting block (13), and the bottom connecting block (14) are T-shaped structures.

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