Aircraft shaped part assembling frame

Abstract

The utility model provides an aircraft shaped part assembling frame which comprises a machine frame and a positioning mechanism arranged on the machine frame, the positioning mechanism comprises an outer side part positioning assembly, and the outer side part positioning assembly is arranged at one end of the machine frame; the inner side part positioning assembly is arranged at the other end of the rack; the number of the first forming part positioning assemblies is multiple, and the multiple first forming part positioning assemblies are arranged between the inner side part positioning assembly and the outer side part positioning assembly at intervals; the number of the second and third shaping piece positioning assemblies is multiple, the number of the rib assembly positioning assemblies is multiple, the number of the first shaping piece positioning assemblies is multiple, and the multiple rib assembly positioning assemblies are arranged between the inner side piece positioning assembly and the outer side piece positioning assembly at intervals. The first shaping piece positioning assembly, the second shaping piece positioning assembly, the third shaping piece positioning assembly and the rib assembly positioning assembly are arranged in a staggered mode. The problem that manual operation is large in error and low in efficiency is solved.

Description

Technical Field

[0001] This utility model relates to the field of assembly work technology, and more specifically, to an aircraft shaping component assembly rack. Background Technology

[0002] See Figure 1 The aircraft shaping component 10 includes an outer part 11, an inner part 12, a first shaping component 13, a second shaping component 14, a third shaping component 15, and a rib assembly 16. The outer part 11 and the inner part 12 are located at opposite ends of the first shaping component 13. The rib assembly 16 is located on the first shaping component 13. The second shaping component 14 is located on the side of the first shaping component 13 away from the rib assembly 16. The third shaping component 15 is located on the second shaping component 14 and is located on the side away from the first shaping component 13.

[0003] For assembling aircraft components, the existing solution is manual positioning, which involves drawing lines on each part using rulers and compasses for positioning. However, manual operation suffers from large errors and low efficiency. Utility Model Content

[0004] The main objective of this invention is to provide an aircraft shaping component assembly rack to solve the problems of large errors and low efficiency in manual operation in the prior art.

[0005] To achieve the above objectives, according to one aspect of the present invention, an aircraft shaping component assembly rack is provided, comprising a frame and a positioning mechanism disposed on the frame. The positioning mechanism includes an outer component positioning assembly disposed at one end of the frame; an inner component positioning assembly disposed at the other end of the frame; a first shaping component positioning assembly, wherein the number of first shaping component positioning assemblies is multiple, and the multiple first shaping component positioning assemblies are arranged at intervals between the inner component positioning assembly and the outer component positioning assembly; a second and third shaping component positioning assembly, wherein the number of second and third shaping component positioning assemblies is multiple, and the multiple second and third shaping component positioning assemblies are arranged at intervals between the inner component positioning assembly and the outer component positioning assembly; and a rib component positioning assembly, wherein the number of first shaping component positioning assemblies is multiple, and the multiple rib component positioning assemblies are arranged at intervals between the inner component positioning assembly and the outer component positioning assembly, and the first shaping component positioning assembly, the second and third shaping component positioning assembly, and the rib component positioning assembly are staggered.

[0006] Furthermore, the frame includes a frame body; a first body connected to the frame body, wherein an outer part positioning assembly, an inner part positioning assembly, a second and third shaping part positioning assembly, and a portion of the structure of the first shaping part positioning assembly are disposed on the first body; and a second body connected to the frame body, the second body being located above the first body, wherein another portion of the structure of the first shaping part positioning assembly and the rib assembly positioning assembly are disposed on the second body.

[0007] Furthermore, a hollow operating area is formed between the first and second platforms, and the positioning mechanism is located in the hollow operating area.

[0008] Furthermore, the second platform includes an inverted U-shaped beam structure, the ends of which are connected to the first platform and form a hollowed-out operating area.

[0009] Furthermore, the positioning mechanism is detachably and positionably connected to the frame.

[0010] Furthermore, the outer part positioning assembly includes an outer part connecting plate, which is erected on the frame of the machine; and an outer part positioning plate, which is connected to the top of the outer part connecting plate, and has a first abutting surface for positioning the outer part.

[0011] Furthermore, the outer part positioning plate has a first plate segment and a second plate segment arranged at an angle, and the first plate segment is connected to the outer part connecting plate, and the side surface of the second plate segment facing away from the outer part connecting plate is the first abutting surface.

[0012] Furthermore, the inner component positioning assembly includes a first inner component positioning plate, which is disposed on the frame and is inclined to the first body of the frame; and a second inner component positioning plate, which is disposed on the frame and is parallel to the first inner component positioning plate, with a gap formed between the first inner component positioning plate and the second inner component positioning plate.

[0013] Furthermore, the inner part positioning assembly also includes a third inner part positioning plate. The first inner part positioning plate has a first connecting structure, and the third inner part positioning plate has a second connecting structure that cooperates with the first connecting structure. The third inner part positioning plate is parallel to the first inner part positioning plate.

[0014] Furthermore, the first connecting structure and the second connecting structure are concave and convex to make the first inner side part positioning plate and the third inner side part positioning plate position and cooperate; the first connecting structure is a positioning notch on the first inner side part positioning plate, and the second connecting structure is a positioning protrusion on the third inner side part positioning plate; or the second connecting structure is a positioning notch on the third inner side part positioning plate, and the first connecting structure is a positioning protrusion on the first inner side part positioning plate.

[0015] Furthermore, the third inner part positioning plate is located at the lower edge of the first inner part positioning plate.

[0016] Furthermore, the first shaping element positioning assembly includes an upper positioning unit, the top end of which is connected to the second platform and extends toward the first platform; and a lower positioning unit, the bottom end of which is connected to the first platform and extends toward the second platform, with the upper positioning unit and the lower positioning unit being staggered.

[0017] Furthermore, the upper positioning unit includes a first connecting plate and a second connecting plate arranged in parallel, and the top ends of both the first connecting plate and the second connecting plate are connected to the second platform; the upper positioning unit also includes a third connecting plate, which is disposed at the end of the second connecting plate away from the second platform, and a first shaping placement space is formed between the third connecting plate and the first connecting plate.

[0018] Furthermore, the first connecting plate extends vertically; the second connecting plate includes a vertical segment and a first horizontal segment connected in sequence, with the bottom end of the first connecting plate lower than the first horizontal segment; the third connecting plate includes a second horizontal segment and an inclined segment set at an angle to the second horizontal segment connected in sequence, with the inclined segment gradually approaching the direction of the first connecting plate.

[0019] Furthermore, the upper positioning unit also includes at least two first shaping element positioning elements, and the first shaping element positioning elements are provided on the side of the first connecting plate and the third connecting plate that are close to each other.

[0020] Furthermore, the lower positioning unit includes a first clamping plate, which is erected on the first platform; and a second clamping plate, which is erected on the first platform, with a first shaping gap formed between the first clamping plate and the second clamping plate.

[0021] Furthermore, the second and third shaping component positioning assembly includes a first positioning plate, which is erected on the first body of the frame platform, and one side of the first positioning plate provides a second abutment surface; a clamping plate, which is installed on the second abutment surface, and a positioning space is formed between the clamping plate and the second abutment surface for the second shaping component and the third shaping component to pass through.

[0022] Furthermore, the clamping plate includes a first segment connected in sequence, the first segment being connected to a first positioning plate; a second segment, a positioning space being formed between the second segment and the first positioning plate; and a third segment, the third segment extending toward the first positioning plate and forming an installation gap with the first positioning plate.

[0023] Furthermore, the rib assembly positioning assembly includes a connecting frame connected to the second body of the frame; a clamping member disposed on the connecting frame, forming a space between the connecting frame and the clamping member for clamping the rib assembly; and a connecting member connected to the connecting frame via the connecting member.

[0024] By applying the technical solution of this utility model, the following technical effects are achieved:

[0025] During use, the outer part positioning assembly, inner part positioning assembly, first shaping part positioning assembly, second and third shaping part positioning assembly, and rib assembly positioning assembly are used to position the outer part, inner part, first shaping part, second shaping part, third shaping part, and rib assembly of the aircraft shaping part in sequence. This positions and constrains the position of each part of the aircraft shaping part, which facilitates the subsequent processing of each part and the assembly between parts, thereby improving assembly accuracy and facilitating manufacturing, use, and maintenance. Attached Figure Description

[0026] The accompanying drawings, which form part of this application, are used to provide a further understanding of the present invention. The illustrative embodiments of the present invention and their descriptions are used to explain the present invention and do not constitute an undue limitation of the present invention. In the drawings:

[0027] Figure 1 A schematic diagram of the structure of the aircraft shaping component is shown;

[0028] Figure 2 This paper presents a schematic diagram of the overall structure of the aircraft shaping component assembly frame of this application;

[0029] Figure 3 A schematic diagram of the external component positioning assembly of this application is shown;

[0030] Figure 4 A schematic diagram of the structure of the inner part positioning assembly of this application is shown;

[0031] Figure 5 A schematic diagram of the upper positioning unit of the first shaping element positioning assembly of this application is shown;

[0032] Figure 6 A schematic diagram of the lower positioning unit of the first shaping element positioning assembly of this application is shown;

[0033] Figure 7 A schematic diagram of the structure of the second and third shaping element positioning assembly of this application is shown;

[0034] Figure 8 A schematic diagram of the rib assembly positioning component of this application is shown.

[0035] The above figures include the following reference numerals:

[0036] 10. Aircraft shaping component; 11. Outer part; 12. Inner part; 13. First shaping component; 14. Second shaping component; 15. Third shaping component; 16. Rib assembly; 20. Frame; 21. Frame body; 22. First frame; 23. Second frame; 30. Positioning mechanism; 40. Outer part positioning assembly; 41. Outer part connecting plate; 42. Outer part positioning plate; 50. Inner part positioning assembly; 51. First inner part positioning plate; 52. Second inner part positioning plate; 53. ... 60. Three inner side component positioning plate; 61. First shaping component positioning assembly; 62. Upper positioning unit; 63. First connecting plate; 64. Second connecting plate; 65. Third connecting plate; 66. First shaping component positioning component; 67. Lower positioning unit; 68. First clamping plate; 69. Second and third shaping component positioning assemblies; 70. First positioning plate; 71. Pressing plate; 82. Rib assembly positioning assembly; 83. Connecting frame; 84. Clamping component; 85. Connecting component. Detailed Implementation

[0037] It should be noted that, unless otherwise specified, the embodiments and features described in this application can be combined with each other. The present invention will now be described in detail with reference to the accompanying drawings and embodiments.

[0038] It should be noted that, unless otherwise specified, all technical and scientific terms used in this application have the same meaning as commonly understood by one of ordinary skill in the art to which this application pertains.

[0039] In this utility model, unless otherwise stated, directional terms such as "upper," "lower," "top," and "bottom" are generally used in relation to the direction shown in the accompanying drawings, or in relation to the vertical, perpendicular, or gravitational direction of the component itself; similarly, for ease of understanding and description, "inner" and "outer" refer to the inner and outer contours of each component itself, but the above directional terms are not used to limit this utility model.

[0040] To address the problems of large errors and low efficiency in manual operations in existing technologies, this application provides an aircraft shaping component assembly rack.

[0041] See Figures 2 to 8The aircraft shaping component assembly frame includes an outer part positioning assembly 40, an inner part positioning assembly 50, a first shaping component positioning assembly 60, a second and third shaping component positioning assembly 70, and a rib assembly positioning assembly 80. The outer part positioning assembly 40 is located at one end of the frame 20, and the inner part positioning assembly 50 is located at the other end of the frame 20. There are multiple first shaping component positioning assemblies 60, which are arranged alternately between the inner part positioning assembly 50 and the outer part positioning assembly 40. There are also multiple second and third shaping component positioning assemblies 70, which are arranged alternately between the inner part positioning assembly 50 and the outer part positioning assembly 40. There are also multiple first shaping component positioning assemblies, and multiple rib assembly positioning assemblies 80 are arranged alternately between the inner part positioning assembly 50 and the outer part positioning assembly 40. The first shaping component positioning assembly 60, the second and third shaping component positioning assembly 70, and the rib assembly positioning assembly 80 are staggered.

[0042] During use, the outer part positioning assembly 40, inner part positioning assembly 50, first shaping part positioning assembly 60, second and third shaping part positioning assembly 70, and rib assembly positioning assembly 80 sequentially position the outer part, inner part, first shaping part, second shaping part, third shaping part, and rib assembly of the aircraft shaping part. This positions and constrains the position of each part of the aircraft shaping part, which facilitates the subsequent processing of each part and the assembly between parts, thereby improving assembly accuracy and facilitating manufacturing, use, and maintenance.

[0043] In this application, the frame 20 includes a frame body 21, a first platform 22, and a second platform 23. The first platform 22 is connected to the frame body 21. A portion of the outer part positioning assembly 40, the inner part positioning assembly 50, the second and third shaping part positioning assembly 70, and the first shaping part positioning assembly 60 are disposed on the first platform 22. The second platform 23 is connected to the frame body 21 and is located above the first platform 22. Another portion of the first shaping part positioning assembly 60 and the rib assembly positioning assembly 80 are disposed on the second platform 23.

[0044] Specifically, aircraft shaping components consist of a wide variety of parts. Since different parts have different positions when their positioning is required, the frame 20 is divided into a first platform 22 and a second platform 23. The first platform 22 and the second platform 23 are differentiated by height, and different positioning components are placed on different platforms to facilitate their placement. This allows for adaptation to the different positions of various parts.

[0045] In this application, a hollow operating area is formed between the first body 22 and the second body 23, and the positioning component is located in the hollow operating area.

[0046] Since the first body 22 is located above the second body 23, a space is formed between the first body 22 and the second body 23. This space is a hollowed-out operating area. The positioning mechanism 30 is placed in this area, which facilitates the placement of parts and the subsequent processing of parts.

[0047] In this application, the second platform 23 includes an inverted U-shaped beam structure, the ends of which are connected to the first platform 22 and form a hollowed-out operating area.

[0048] Specifically, by setting the second body 23 as an inverted U-shaped beam structure, it is easier to connect the second body 23 with the frame 21, and to facilitate the installation and disassembly of the second body 23, thereby facilitating the installation of the entire assembly frame.

[0049] In this application, the positioning mechanism 30 is detachably and positionally adjustable connected to the frame 20. This not only facilitates the installation and manufacturing of the entire assembly frame but also makes subsequent maintenance of the frame 20 assembly frame easier. Furthermore, it facilitates the replacement of any faulty positioning component in case of malfunction. If the specifications of the aircraft shaping component change, the new aircraft shaping component can be adapted by modifying the model and position of different positioning components.

[0050] See Figure 3 The outer component positioning assembly 40 includes an outer component connecting plate 41 and an outer component positioning plate 42. The outer component connecting plate 41 is erected on the frame 21 of the frame 20. The outer component positioning plate 42 is connected to the top of the outer component connecting plate 41 and has a first abutting surface for positioning the outer component.

[0051] Specifically, during use, the outer component connecting plate 41 is used to connect with the frame 21 and serves as a connection, while the outer component positioning plate 42 is used to abut against the outer component and serves as a positioning tool for the outer component.

[0052] In this application, the outer part positioning plate 42 has a first plate segment and a second plate segment arranged at an angle, and the first plate segment is connected to the outer part connecting plate 41, and the side surface of the second plate segment facing away from the outer part connecting plate 41 is the first abutting surface.

[0053] Specifically, the outer part positioning plate 42 is divided into different plate segments, each segment serving a different function, which facilitates the installation of the outer part positioning plate 42 without affecting its normal operation.

[0054] See Figure 4The inner component positioning assembly 50 includes a first inner component positioning plate 51 and a second inner component positioning plate 52. The first inner component positioning plate 51 is disposed on the frame 20 and is inclined between the first inner component positioning plate 51 and the first body 22 of the frame 21 of the frame 20. The second inner component positioning plate 52 is disposed on the frame 20 and is parallel to the first inner component positioning plate 51, and a gap is formed between the first inner component positioning plate 51 and the second inner component positioning plate 52.

[0055] Specifically, both the first inner component positioning plate 51 and the second inner component positioning plate 52 serve to position the inner component. Since the inner component is angled relative to the other parts, the first inner component positioning plate 51 and the second inner component positioning plate 52 also need to be tilted relative to the first body 22 to accommodate the angle of the inner component. Simultaneously, because the inner component needs to connect with the other parts, a gap needs to be formed between the first inner component positioning plate 51 and the second inner component positioning plate 52. This gap allows space for the other parts to be positioned, preventing interference and facilitating the positioning of the inner component. It also provides support during the subsequent assembly of the other parts.

[0056] In this application, the inner side member positioning assembly 50 further includes a third inner side member positioning plate 53. The first inner side member positioning plate 51 has a first connecting structure, and the third inner side member positioning plate 53 has a second connecting structure that cooperates with the first connecting structure. The third inner side member positioning plate 53 is parallel to the first inner side member positioning plate 51.

[0057] Specifically, when the length of the inner part is long, only part of the inner part can abut and be positioned with the first inner part positioning plate 51 and the second inner part positioning plate 52. The first inner part positioning plate 51 and the second inner part positioning plate 52 alone cannot guarantee accurate positioning of the inner part. Therefore, by setting a third inner part positioning component, the length of the inner positioning component is extended to improve the accuracy of positioning the inner part.

[0058] In this application, the first connecting structure and the second connecting structure are concave and convex to make the first inner side member positioning plate 51 and the third inner side member positioning plate 53 position and cooperate; the first connecting structure is a positioning notch on the first inner side member positioning plate 51, and the second connecting structure is a positioning protrusion on the third inner side member positioning plate 53; or the second connecting structure is a positioning notch on the third inner side member positioning plate 53, and the first connecting structure is a positioning protrusion on the first inner side member positioning plate 51.

[0059] In this application, the third inner side member positioning plate 53 is located at the lower edge of the first inner side member positioning plate 51.

[0060] Specifically, by setting protrusions and notches to install the second inner side component positioning plate 52 and the third inner side component positioning plate 53, the stability of the installation of the third inner side component positioning plate 53 can be increased.

[0061] In this application, the first shaping element positioning assembly 60 includes an upper positioning unit 61 and a lower positioning unit 62. The top end of the upper positioning unit 61 is connected to the second platform 23 and extends toward the first platform 22; the bottom end of the lower positioning unit 62 is connected to the first platform 22 and extends toward the second platform 23, and the upper positioning unit 61 and the lower positioning unit 62 are staggered.

[0062] Because the first shaping component is relatively large, the first shaping component positioning assembly 60 cannot be independently mounted on the first platform 22 or the second platform 23. Therefore, the first shaping component positioning assembly 60 is divided into an upper positioning unit 61 and a lower positioning unit 62, which are respectively mounted on the second platform 23 and the first platform 22. By dividing the first shaping component positioning assembly 60 into two parts, the first shaping component can be positioned more effectively, and the positioning accuracy can be increased.

[0063] See Figure 5 The upper positioning unit 61 includes a first connecting plate 611 and a second connecting plate arranged in parallel, and the top ends of the first connecting plate 611 and the second connecting plate 612 are connected to the second platform 23; the upper positioning unit 61 also includes a third connecting plate 613, which is disposed at the end of the second connecting plate 612 away from the second platform 23, and a first shaping placement space is formed between the third connecting plate 613 and the first connecting plate 611.

[0064] In this application, the first connecting plate 611 extends vertically; the second connecting plate 612 includes a vertical segment and a first horizontal segment connected in sequence, and the bottom end of the first connecting plate 611 is lower than the first horizontal segment; the third connecting plate 613 includes a second horizontal segment and an inclined segment set at an angle to the second horizontal segment connected in sequence, and the inclined segment gradually approaches the first connecting plate 611.

[0065] Specifically, during use, the first shaping component is located within the placement space and is positioned by the third connecting plate 613 and the first connecting plate 611 together. The positioning of the upper part of the first shaping component is achieved through the first connecting plate 611 and the third connecting plate 613.

[0066] In this application, the upper positioning unit 61 also includes at least two first shaping element positioning elements 614, and the first shaping element positioning elements 614 are provided on the side of the first connecting plate 611 and the third connecting plate 613 that are close to each other.

[0067] Specifically, by further positioning the first shaping component using the first shaping component positioning component 614, the stability of the first shaping component placement can be improved.

[0068] See Figure 6 The lower positioning unit 62 includes a first clamping plate 621 and a second clamping plate 622. The first clamping plate 621 is erected on the first platform 22. The second clamping plate 622 is erected on the first platform 22, and a first shaping gap is formed between the first clamping plate 621 and the second clamping plate 622.

[0069] Specifically, the lower positioning unit 62 mainly supports and positions the first shaping component. Since the first shaping component also needs to cooperate with other parts, a gap needs to be formed between the first clamping plate 621 and the second clamping plate 622 for the setting of other parts.

[0070] See Figure 7 The second and third shaping component positioning assembly 70 includes a first positioning plate 71 and a pressing plate 72. The first positioning plate 71 is erected on the first platform 22 of the frame 20, and one side of the first positioning plate 71 provides a second abutment surface. The pressing plate 72 is installed on the second abutment surface, and a positioning space is formed between the pressing plate 72 and the second abutment surface for the second shaping component and the third shaping component to pass through.

[0071] Specifically, during use, the second and third shaping parts abut against the first positioning plate 71 to position the parts; at the same time, the clamping plate 72 plays an auxiliary fixing role, increasing the stability of the second and third shaping parts.

[0072] In this application, the clamping plate 72 includes a first segment, a second segment, and a third segment connected in sequence. The first segment is connected to the first positioning plate 71. A positioning space is formed between the second segment and the first positioning plate 71. The third segment extends toward the first positioning plate 71 and forms an installation gap with the first positioning plate 71.

[0073] Specifically, the first section mainly serves as a connection, connecting the clamping plate 72 and the first positioning plate 71; the second section serves as a limit and clamping function; and the third section mainly serves as a clearance function.

[0074] See Figure 8 The rib assembly positioning assembly 80 includes a connecting frame 81, a clamping member 82, and a connecting member 83. The connecting frame 81 is connected to the second frame 21 of the frame 20. The clamping member 82 is disposed on the connecting frame 81, and a space for clamping the rib assembly is formed between the connecting frame 81 and the clamping member 82. The clamping member 82 is connected to the connecting frame 81 through the connecting member 83.

[0075] Specifically, the clamping member 82 and the connecting frame 81 together position and clamp the rib assembly, which is located in the space formed between the connecting member 83 and the clamping member 82, thus achieving the positioning of the rib assembly.

[0076] Different positioning components are used to position different parts of the aircraft shaping assembly. These positioning components are set on a frame 20 to achieve simultaneous positioning of different parts of the aircraft shaping assembly. This not only facilitates the processing of different parts, but also facilitates the subsequent assembly of these parts.

[0077] As can be seen from the above description, the embodiments of this utility model achieve the following technical effects:

[0078] 1. During use, the outer part positioning assembly 40, inner part positioning assembly 50, first shaping part positioning assembly 60, second and third shaping part positioning assembly 70 and rib assembly positioning assembly 80 sequentially position the outer part, inner part, first shaping part, second shaping part, third shaping part and rib assembly of the aircraft shaping part. The position of each part of the aircraft shaping part is positioned and constrained, which facilitates the subsequent processing of each part and the assembly between parts, thereby improving the assembly accuracy and facilitating manufacturing, use and maintenance.

[0079] 2. Aircraft shaping components consist of a wide variety of parts. Since different parts have different positions when their positioning is required, the frame 20 is divided into a first platform 22 and a second platform 23. The first platform 22 and the second platform 23 are differentiated by height, and different positioning components are placed on different platforms to facilitate their placement. This allows for adaptation to the different positions of various parts.

[0080] Obviously, the embodiments described above are only some embodiments of this utility model, and not all embodiments. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort should fall within the protection scope of this utility model.

[0081] It should be noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to limit the exemplary embodiments according to this application. As used herein, the singular form is intended to include the plural form as well, unless the context clearly indicates otherwise. Furthermore, it should be understood that when the terms "comprising" and / or "including" are used in this specification, they indicate the presence of features, steps, operations, devices, components, and / or combinations thereof.

[0082] It should be noted that the terms "first," "second," etc., used in the specification, claims, and accompanying drawings of this application are used to distinguish similar objects and are not necessarily used to describe a specific order or sequence. It should be understood that such data can be interchanged where appropriate so that the embodiments of this application described herein can be implemented in sequences other than those illustrated or described herein.

[0083] The above are merely preferred embodiments of this utility model and are not intended to limit the scope of this utility model. Various modifications and variations can be made to this utility model by those skilled in the art. Any modifications, equivalent substitutions, or improvements made within the spirit and principles of this utility model should be included within the protection scope of this utility model.

Claims

1. An aircraft forming component assembly rack, characterized in that, Includes a frame (20) and a positioning mechanism (30) disposed on the frame (20), the positioning mechanism (30) comprising: An outer part positioning assembly (40) is disposed at one end of the frame (20); An inner component positioning assembly (50) is disposed at the other end of the frame (20); The first shaping element positioning component (60) is a plurality of the first shaping element positioning components (60), and the plurality of the first shaping element positioning components are arranged at intervals between the inner side component positioning component (50) and the outer side component positioning component (40). The second and third shaping component positioning assembly (70) is a plurality of the second and third shaping component positioning assemblies (70), and the plurality of the second and third shaping component positioning assemblies (70) are arranged at intervals between the inner component positioning assembly (50) and the outer component positioning assembly (40); Rib assembly positioning component (80), the number of the first shaping component positioning components is multiple, the multiple rib assembly positioning components (80) are arranged at intervals between the inner side component positioning component (50) and the outer side component positioning component (40), and the first shaping component positioning component (60), the second and third shaping component positioning components (70) and the rib assembly positioning component (80) are staggered.

2. The aircraft forming component assembly frame according to claim 1, characterized in that, The rack (20) includes: Frame (21); The first platform (22) is connected to the frame (21), and a portion of the outer part positioning component (40), the inner part positioning component (50), the second and third shaping component positioning component (70) and the first shaping component positioning component (60) are arranged on the first platform (22). The second platform (23) is connected to the frame (21). The second platform (23) is located above the first platform (22). Another part of the structure of the first shaping component positioning assembly (60) and the rib component positioning assembly (80) are disposed on the second platform (23). A hollow operating area is formed between the first platform (22) and the second platform (23), and the positioning mechanism (30) is located in the hollow operating area; The second platform (23) includes an inverted U-shaped beam structure, the ends of which are connected to the first platform (22) and form the hollowed-out operating area.

3. The aircraft forming component assembly frame according to claim 1, characterized in that, The outer component positioning assembly (40) includes: An outer component connecting plate (41) is erected on the frame (21) of the machine frame (20); An outer part positioning plate (42) is connected to the top of the outer part connecting plate (41). The outer part positioning plate (42) has a first abutting surface for positioning the outer part. The outer part positioning plate (42) has a first plate segment and a second plate segment arranged at an angle, and the first plate segment is connected to the outer part connecting plate (41), and the side surface of the second plate segment facing away from the outer part connecting plate (41) is the first abutting surface.

4. The aircraft forming component assembly frame according to claim 1, characterized in that, The inner member positioning assembly (50) includes: The first inner side component positioning plate (51) is disposed on the frame (20) and is inclined between the first inner side component positioning plate (51) and the first body (22) of the frame (21) of the frame (20); The second inner part positioning plate (52) is disposed on the frame (20), and the second inner part positioning plate (52) is parallel to the first inner part positioning plate (51), and a gap is formed between the first inner part positioning plate (51) and the second inner part positioning plate (52). The inner component positioning assembly (50) further includes a third inner component positioning plate (53). The first inner component positioning plate (51) has a first connecting structure, and the third inner component positioning plate (53) has a second connecting structure that cooperates with the first connecting structure. The third inner component positioning plate (53) is parallel to the first inner component positioning plate (51).

5. The aircraft forming component assembly frame according to claim 4, characterized in that, The third inner side component positioning plate (53) is located at the lower edge of the first inner side component positioning plate (51). The first connecting structure and the second connecting structure are in a concave-convex fit so that the first inner side component positioning plate (51) and the third inner side component positioning plate (53) are positioned and fitted together. The first connecting structure is a positioning notch on the first inner side member positioning plate (51), and the second connecting structure is a positioning protrusion on the third inner side member positioning plate (53); or The second connecting structure is the positioning notch on the third inner side member positioning plate (53), and the first connecting structure is the positioning protrusion on the first inner side member positioning plate (51).

6. The aircraft forming component assembly frame according to claim 2, characterized in that, The first shaping element positioning assembly (60) includes: The upper positioning unit (61) is connected to the second platform (23) at its top and extends toward the first platform (22); The lower positioning unit (62) is connected to the first platform (22) at its bottom end and extends toward the second platform (23), and the upper positioning unit (61) and the lower positioning unit (62) are staggered.

7. The aircraft forming component assembly frame according to claim 6, characterized in that, The upper positioning unit (61) includes a first connecting plate (611) and a second connecting plate (612) arranged side by side, and the top ends of the first connecting plate (611) and the second connecting plate (612) are both connected to the second platform (23). The upper positioning unit (61) further includes a third connecting plate (613), which is disposed at the end of the second connecting plate (612) away from the second platform (23), and a first shaping placement space is formed between the third connecting plate (613) and the first connecting plate (611). The first connecting plate (611) extends vertically; The second connecting plate (612) includes a vertical section and a first horizontal section connected in sequence, and the bottom end of the first connecting plate (611) is lower than the first horizontal section; The third connecting plate (613) includes a second horizontal segment and an inclined segment set at an angle to the second horizontal segment, which are connected in sequence, and the inclined segment gradually moves closer to the first connecting plate (611); The upper positioning unit (61) further includes at least two first shaping element positioning elements (614), and the first shaping element positioning elements (614) are provided on the side of the first connecting plate (611) and the third connecting plate (613) that are close to each other.

8. The aircraft forming component assembly rack according to claim 6, characterized in that, The lower positioning unit (62) includes: The first card plate (621) is placed upright on the first platform (22); The second card plate (622) is placed on the first platform (22), and a first shaping gap is formed between the first card plate (621) and the second card plate (622).

9. The aircraft shaping component assembly rack according to any one of claims 1 to 8, characterized in that, The second and third shaping element positioning assembly (70) includes: The first positioning plate (71) is placed on the first platform (22) of the frame (20), and one side of the first positioning plate (71) provides a second abutment surface. A clamping plate (72) is installed on the second abutting surface, and a positioning space is formed between the clamping plate (72) and the second abutting surface for the passage of the second shaping member and the third shaping member; The clamping plate (72) comprises the following sequentially connected components: The first segment is connected to the first positioning plate (71); The second segment, the positioning space is formed between the second segment and the first positioning plate (71); The third segment extends toward the first positioning plate (71) and forms an installation gap with the first positioning plate (71).

10. The aircraft shaping component assembly rack according to any one of claims 1 to 8, characterized in that, The rib assembly positioning component (80) includes: A connecting frame (81) is connected to the second body (23) of the frame (20); A clamping member (82) is disposed on the connecting frame (81), and a space for clamping rib assembly is formed between the connecting frame (81) and the clamping member (82); The connector (83) is used to connect the clamping member (82) to the connecting frame (81).

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