Assembly tool for general assembly of landing gear with buffer type skid

Abstract

The utility model belongs to the technical field of a general assembly tool for a skid undercarriage, and discloses a general assembly tool for a skid undercarriage with a buffer. The device specifically comprises a supporting seat which is supported on a supporting surface; the sliding pipe clamping mechanism is used for clamping a sliding pipe of the landing gear with the buffer type skid; the machine body positioning mechanism is arranged on the side, away from the supporting face, of the supporting base. Comprising a fuselage fixing part used for fixing a fuselage joint of the landing gear with the buffer type skid, and a buffer fixing part used for fixing a buffer of the landing gear with the buffer type skid; the machine body fixing parts of the two machine body positioning mechanisms are oppositely arranged; the two machine body positioning mechanisms are each provided with two buffer fixing parts which are symmetrically arranged relative to the positions where the machine body fixing parts of the two machine body positioning mechanisms are located. According to the utility model, through the synergistic effect of the multiple parts for fixing the corresponding parts, the assembly quality and efficiency are improved, the performance of the undercarriage is guaranteed, and the device has important practical application value.

Description

Technical Field

[0001] This utility model belongs to the technical field of skid landing gear assembly tooling, specifically, it relates to a skid landing gear assembly tooling with a buffer. Background Technology

[0002] Landing gear is an accessory device located under an aircraft, used to support the aircraft during takeoff and landing or taxiing on the ground and for ground movement. To improve the shock absorption performance of traditional landing gear, skid landing gear with dampers has been designed in recent years. Skid landing gear with dampers is a common landing gear structure used in aircraft such as helicopters. By adding dampers, it improves the landing gear's ability to absorb landing impact energy, reduces landing overload, and enhances the stability and comfort of the aircraft during landing.

[0003] However, there is currently a lack of final assembly tooling for skid landing gear with shock absorbers, and only traditional landing gear assembly tooling can be used, resulting in low assembly efficiency and insufficient assembly accuracy for skid landing gear with shock absorbers.

[0004] Therefore, there is an urgent need to provide a final assembly fixture that can accurately and quickly assemble skid landing gear with shock absorbers to overcome the above problems.

[0005] In view of the above, this application is hereby submitted. Utility Model Content

[0006] The technical problem to be solved by this utility model is to overcome the shortcomings of the existing technology in terms of low assembly efficiency and low assembly accuracy of skid landing gear with buffers. The purpose is to provide a skid landing gear assembly tooling that can accurately and quickly assemble skid landing gear with buffers.

[0007] To solve the above-mentioned technical problems, the basic concept of the technical solution adopted by this utility model is: a tooling for assembling a skid landing gear with a buffer, comprising:

[0008] A support base, which is supported on a support surface;

[0009] A slide tube clamping mechanism is used to clamp the slide tube of the buffer-type skid landing gear;

[0010] A fuselage positioning mechanism is disposed on the side of the support base away from the support surface; the fuselage positioning mechanism includes a fuselage fixing part for fixing the fuselage connection of the skid landing gear with buffer, and a buffer fixing part for fixing the buffer of the skid landing gear with buffer.

[0011] The fuselage positioning mechanism comprises two opposing units; the fuselage fixing parts of the two fuselage positioning mechanisms are arranged facing each other; each fuselage positioning mechanism is provided with two buffer fixing parts that are symmetrically arranged relative to the position of its own fuselage fixing part.

[0012] According to one embodiment of the present invention, the assembly fixture for the buffer-type skid landing gear includes:

[0013] A sliding tube, comprising two parallel sliding tubes;

[0014] The arched tube has two parallel sections, with the top of each arched tube being the connection point to the fuselage. Each of the two arched tubes is equipped with two buffers that are symmetrically arranged relative to their respective fuselage connection points.

[0015] According to one embodiment of the present invention, four sliding tube clamping mechanisms are provided;

[0016] The four sliding tube clamping mechanisms are located at the four included corner positions of the support.

[0017] The two slide tube clamping mechanisms are arranged in a direction parallel to the two body fixing parts of the body positioning mechanisms and facing each other, for clamping the same slide tube.

[0018] According to one embodiment of the present invention, the sliding tube clamping mechanism includes:

[0019] A base plate having an oblong hole; the base plate is mounted on the support bracket by means of bolts passing through the oblong hole.

[0020] The first middle plate is disposed on the side of the base plate away from the support.

[0021] The second middle plate is connected to the first middle plate by an adjusting bolt; by rotating the adjusting bolt, the distance between the second middle plate and the first middle plate increases or decreases; the side of the second middle plate away from the support is provided with an arc-shaped groove.

[0022] The top plate is connected to the second middle plate by bolts; the top plate is located at the end of the second middle plate away from the support base; the top plate has an arc-shaped groove on the side facing closer to the second middle plate, and the arc-shaped groove of the top plate and the arc-shaped groove of the middle plate cooperate to clamp the slide tube of the skid landing gear with buffer.

[0023] According to one embodiment of the present invention, the fuselage positioning mechanism further includes:

[0024] A support column, wherein the support column is disposed on the side of the support base away from the support surface;

[0025] The first horizontal column is perpendicular to the support column; the first horizontal column is located at the end of the support column away from the support base; the fuselage fixing part is located at the midpoint of the first horizontal column, and the buffer fixing part is located at both ends of the first horizontal column.

[0026] According to one embodiment of the present invention, the fuselage fixing part includes:

[0027] A fuselage fixing plate is disposed on the side of the first cross column facing the support base and extending towards the fuselage positioning mechanism disposed on the other side.

[0028] The first reinforcing rib is a right-angled triangular structure; one right-angled side of the first reinforcing rib is connected to the side of the first crossbar facing the fuselage positioning mechanism located on the other side, and the other right-angled side is connected to the side of the fuselage fixing plate facing away from the support.

[0029] According to one embodiment of the present invention, the buffer fixing part includes:

[0030] A buffer fixing plate is disposed on the side of the first cross column facing closer to the support bracket and extending towards the fuselage positioning mechanism disposed on the other side; the extension length of the buffer fixing plate is the same as the extension length of the fuselage fixing plate.

[0031] The second reinforcing rib is a right-angled triangular structure; one right-angled side of the second reinforcing rib is connected to the side of the first crossbar facing the fuselage positioning mechanism located on the other side, and the other right-angled side is connected to the side of the buffer fixing plate facing away from the support.

[0032] According to one embodiment of the present invention, the fuselage positioning mechanism further includes:

[0033] The second horizontal column is disposed at the end of the support column away from the first horizontal column; the projection of the first horizontal column covers the projection of the second horizontal column in a direction parallel to the axis of the support column.

[0034] A horizontal column is arranged horizontally; the horizontal column is connected to the side of the second horizontal column away from the support column; the axis of the horizontal column, the axis of the second horizontal column, and the axis of the support column are perpendicular to each other; the fuselage positioning mechanism is connected to the support bracket through the horizontal column.

[0035] According to an embodiment of the present utility model, the horizontal column includes a first connecting plate arranged horizontally;

[0036] The first connecting plate is arranged on one side of the horizontal column away from the second cross column; the first connecting plate is connected to the support pedestal by means of bolt connection.

[0037] According to an embodiment of the present utility model, the support pedestal includes:

[0038] A bearing column, which is a "day" - shaped and horizontally placed frame structure;

[0039] Support columns, multiple support columns are provided, and the multiple support columns support the bearing column on a support surface; the multiple support columns are arranged in a rectangular array.

[0040] After adopting the above - mentioned technical solution, the present utility model has the following beneficial effects compared with the prior art:

[0041] In the present utility model, by providing components (a fuselage positioning mechanism) for connecting the landing gear at corresponding positions of the simulated fuselage and positioning (a slide - tube clamping mechanism) of the corresponding constraint parts, it is convenient to carry out assembly operations, ensuring the accuracy and efficiency of the landing gear component assembly.

[0042] The following further describes in detail the specific embodiments of the present utility model with reference to the accompanying drawings. Description of the Drawings

[0043] The accompanying drawings, as a part of the present utility model, are used to provide a further understanding of the present utility model. The schematic embodiments and descriptions thereof of the present utility model are used to explain the present utility model, but do not constitute an improper limitation to the present utility model. Obviously, the accompanying drawings in the following description are only some embodiments, and those of ordinary skill in the art can also obtain other drawings based on these drawings without creative efforts. In the drawings:

[0044] Figure 1 is a schematic structural diagram of an assembly tool for the overall assembly of a buffer - type skid landing gear with a buffer - type skid landing gear clamped in an embodiment of the present utility model;

[0045] Figure 2 is Figure 1 a schematic structural diagram in a front - view perspective;

[0046] Figure 3 is Figure 1 a schematic structural diagram in a side - view perspective;

[0047] Figure 4 is Figure 1A structural diagram from a top-down view;

[0048] Figure 5 This is a schematic diagram of the fuselage positioning mechanism of the landing gear assembly tooling with buffer skid in this embodiment of the present invention.

[0049] Figure 6 for Figure 5 A structural diagram from a frontal view;

[0050] Figure 7 A schematic diagram of the slide tube clamping mechanism for the assembly tooling of the skid landing gear with buffer;

[0051] Figure 8 for Figure 7 A structural diagram from a frontal view;

[0052] Figure 9 for Figure 7 A structural schematic diagram from a top view and a cross-sectional view at the specified BB position;

[0053] Figure 10 This is a cross-sectional view of the slide tube clamping mechanism installed on the landing gear assembly tooling with a buffer skid, according to an embodiment of the present invention.

[0054] Description of main components in the diagram:

[0055] 1. Support bracket; 11. Bearing column; 12. Column; 121. Column base; 2. Slide tube clamping mechanism; 21. Base plate; 211. Waist-shaped hole; 22. First middle plate; 23. Second middle plate; 231. Middle plate arc groove; 232. Positioning groove; 24. Top plate; 241. Top plate arc groove; 25. Adjusting bolt; 3. Skid landing gear with buffer; 31. Slide tube; 32. Fuselage connection; 33. Buffer; 34. Arched tube; 4. Fuselage positioning mechanism; 41. Fuselage fixing part; 411. Fuselage fixing plate; 412. First reinforcing rib; 42. Buffer fixing part; 421. Buffer fixing plate; 422. Second reinforcing rib; 43. Support column; 44. First cross column; 45. Second cross column; 46. Horizontal column; 461. First connecting plate; 462. Second connecting plate; 463. Third connecting plate.

[0056] It should be noted that these accompanying drawings and textual descriptions are not intended to limit the scope of the present invention in any way, but rather to illustrate the concept of the present invention to those skilled in the art by referring to specific embodiments. Detailed Implementation

[0057] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions in the embodiments will be clearly and completely described below with reference to the accompanying drawings. The following embodiments are used to illustrate this utility model, but are not intended to limit the scope of this utility model.

[0058] In the description of this utility model, it should be noted that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "inner", and "outer" indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, 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. Therefore, they should not be construed as limitations on this utility model.

[0059] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "joining" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0060] like Figures 1 to 10 As shown, the present invention provides a skid-mounted landing gear assembly fixture with a buffer, comprising:

[0061] Support bracket 1 supports the overall assembly tooling of the buffer-type skid landing gear on the support surface; the support surface can be the ground or a placement surface at a certain limited area.

[0062] The slide tube clamping mechanism 2 is used to clamp the slide tube 31 of the buffer-type skid landing gear 3;

[0063] The fuselage positioning mechanism 4 is disposed on the side of the support 1 away from the support surface; the fuselage positioning mechanism 4 includes a fuselage fixing part 41 for fixing the fuselage connection 32 of the skid landing gear 3 with buffer, and a buffer fixing part 42 for fixing the buffer 33 of the skid landing gear 3 with buffer.

[0064] The fuselage positioning mechanism 4 is provided in two opposite directions; the fuselage fixing parts 41 of the two fuselage positioning mechanisms 4 are arranged facing each other; each fuselage positioning mechanism 4 is provided with two buffer fixing parts 42 that are symmetrically arranged relative to the position of its own fuselage fixing part 41.

[0065] In this utility model, by setting a support base to support the support surface, a stable foundation is provided for the entire assembly fixture, ensuring that the fixture will not shift or shake during the assembly process, thereby ensuring the smooth progress of the assembly work.

[0066] The slide tube clamping mechanism can firmly clamp the slide tube of the landing gear with a shock absorber, preventing the slide tube from moving or wobbling during assembly. This is crucial for improving assembly accuracy. Only when the position of the slide tube is precisely fixed can the subsequent connections between various components be ensured to be accurate, reducing assembly errors caused by slide tube position deviations, thereby improving the overall assembly quality of the landing gear.

[0067] The fuselage positioning mechanism is located on the side of the support base away from the support surface. It includes a fuselage fixing part for securing the fuselage connection of the skid-mounted landing gear with a buffer, and a buffer fixing part for securing the buffer. Furthermore, there are two opposing fuselage positioning mechanisms, with their fuselage fixing parts facing each other, and each mechanism has two buffer fixing parts symmetrically positioned relative to their respective fuselage fixing parts. This structural design allows for precise positioning and fixing of both the landing gear fuselage connection and the buffer simultaneously. On one hand, the two opposing fuselage fixing parts stably secure the fuselage connection from both sides, ensuring the accuracy of the fuselage's position during assembly and making the connection between the fuselage and other components smoother and more precise. On the other hand, the symmetrically positioned buffer fixing parts accurately position the buffer, allowing it to be accurately installed in the designated location and precisely fitted with the fuselage and skid-mounted landing gear. Since the buffer plays a crucial role in shock absorption and cushioning in a skid-mounted landing gear with a buffer, its installation accuracy directly affects the performance of the landing gear. This precise positioning and fixing method can greatly improve the installation accuracy of the buffer, thereby enhancing the overall shock absorption and cushioning performance of the landing gear.

[0068] In one specific embodiment of this example, the fuselage connection 32 is connected to the fuselage fixing part 41 by means of bolts;

[0069] The buffer 33 is connected to the buffer fixing part 42 by bolts.

[0070] Please see the appendix Figure 1 To be continued Figure 4 In one specific embodiment of this invention, the assembly fixture for the landing gear with buffer skid includes:

[0071] Slide tube 31, wherein the slide tube 31 comprises two parallel tubes;

[0072] An arched tube 34 is provided with two parallel arched tubes 34, the top of which is the fuselage connection 32; each of the two arched tubes 34 is provided with two buffers 33 arranged symmetrically relative to the location of its fuselage connection 32.

[0073] Please see the appendix Figure 1 Appendix Figure 2 and attached Figure 4 In one specific embodiment of this example, four sliding tube clamping mechanisms 2 are provided;

[0074] The four sliding tube clamping mechanisms 2 are arranged at the four included corner positions of the support 1;

[0075] The two slide tube clamping mechanisms 2 are arranged in a direction parallel to the two body fixing parts 41 of the body positioning mechanism 4 facing each other, and are used to clamp the same slide tube 31.

[0076] Please see the appendix Figure 7 To be continued Figure 10 In one specific embodiment of this invention, the slide tube clamping mechanism 2 includes:

[0077] The base plate 21 is provided with a waist-shaped hole 211; the base plate 21 is installed on the support bracket 1 by means of bolts passing through the waist-shaped hole 211.

[0078] The first middle plate 22 is disposed on the side of the base plate 21 away from the support 1;

[0079] The second middle plate 23 is connected to the first middle plate 22 by adjusting bolt 25; by rotating the adjusting bolt 25, the distance between the second middle plate 23 and the first middle plate 22 increases or decreases; the side of the second middle plate 23 away from the support 1 is provided with a middle plate arc-shaped groove 231; the height (thickness in the vertical direction) of the second middle plate 23 is the same as the height of the highest point of the first middle plate 22;

[0080] The top plate 24 is connected to the second middle plate 23 by bolts. The top plate 24 is located at the end of the second middle plate 23 away from the support 1. The top plate 24 has an arc-shaped groove 241 on the side facing closer to the second middle plate 23. The arc-shaped groove 241 on the top plate and the arc-shaped groove 231 on the middle plate cooperate to clamp the slide tube 31 of the skid landing gear 3 with buffer.

[0081] In one specific embodiment of this example, the base plate 21 is a rectangular plate (length greater than width), and the oblong hole 211 is provided along the length direction of the base plate 21;

[0082] The base plate 21 is also provided with bolt holes, and is connected to the support 1 by bolts.

[0083] In one specific embodiment of this invention, the first middle plate 22 is an "L"-shaped plate; the first middle plate 22 includes a lower plate and a vertical plate;

[0084] The lower plate is connected to the base plate 21;

[0085] The vertical plate is perpendicular to the lower plate, and the adjusting bolt 25 passes through the vertical plate of the first middle plate 22 and connects to the second middle plate 23.

[0086] In one specific embodiment of this example, a positioning groove 232 is provided on the second middle plate 23, and the head end (nut end) of the adjusting bolt 25 is disposed in the positioning groove 232.

[0087] In one specific embodiment of this example, a mating nut (shown in the figure, with units marked) is installed on the threaded end of the adjusting bolt 25 (the other end relative to the head end);

[0088] The mating nut, in conjunction with the adjusting bolt, determines the distance between the first middle plate 22 and the second middle plate 23, thereby achieving a certain dimensional adjustment.

[0089] The flexible tooling solution provided by this utility model can make corresponding adaptive adjustments according to the landing gear model by setting the adjustment nut 25 (fine adjustment) and the waist-shaped hole 211 (coarse adjustment) to ensure the accuracy of limit and positioning.

[0090] In one specific embodiment of this example, the slide tube 31 is a tubular structure with both ends raised and the middle straight;

[0091] The top plate 24 and the second middle plate 23 clamp the straight middle portion of the slide tube 31.

[0092] Please see the appendix Figure 1 To be continued Figure 6 In one specific embodiment of this invention, the fuselage positioning mechanism 4 further includes:

[0093] Support column 43, the support column 43 is disposed on the side of the support base 1 away from the support surface;

[0094] The first horizontal column 44 is perpendicular to the support column 43; the first horizontal column 44 is located at the end of the support column 43 away from the support base 1; the fuselage fixing part 41 is located at the midpoint of the first horizontal column 44; and the buffer fixing part 42 is located at both ends of the first horizontal column 44.

[0095] Please see the appendix Figure 2 Appendix Figure 3 Appendix Figure 5 and attached Figure 6 In one specific embodiment of this invention, the fuselage fixing part 41 includes:

[0096] The fuselage fixing plate 411 is disposed on the side of the first cross column 44 facing the support base 1 and extending in the direction (inward) towards the fuselage positioning mechanism 4 disposed on the other side.

[0097] The first reinforcing rib 412 is a right-angled triangular structure; one right-angled side of the first reinforcing rib 412 is connected to the side (inner side) of the first horizontal column 44 facing the fuselage positioning mechanism 4 located on the other side, and the other right-angled side is connected to the side (upper side) of the fuselage fixing plate 411 facing away from the support 1.

[0098] Please see the appendix Figure 1 Appendix Figure 2 Appendix Figure 3 Appendix Figure 5 and attached Figure 6 In one specific embodiment of this invention, the buffer fixing part 42 includes:

[0099] The buffer fixing plate 421 is disposed on the side of the first cross column 44 facing closer to the support 1 and extending towards the fuselage positioning mechanism 4 disposed on the other side (inward side); the extension length of the buffer fixing plate 421 is the same as the extension length of the fuselage fixing plate 411.

[0100] The second reinforcing rib 422 is a right-angled triangular structure; one right-angled side of the second reinforcing rib 422 is connected to the side (inner side) of the first crossbar 44 facing the fuselage positioning mechanism 4 located on the other side, and the other right-angled side is connected to the side (upper side) of the buffer fixing plate 421 facing away from the support 1.

[0101] Please see the appendix Figure 1 To be continued Figure 6 In one specific embodiment of this invention, the fuselage positioning mechanism 4 further includes:

[0102] The second horizontal column 45 is disposed at the end of the support column 43 away from the first horizontal column 44; along a direction parallel to the axis of the support column 43, the projection of the first horizontal column 44 covers the projection of the second horizontal column 45.

[0103] A horizontal column 46 is arranged horizontally; the horizontal column 46 is connected to the side of the second horizontal column 45 away from the support column 43; the axis of the horizontal column 46, the axis of the second horizontal column 45 and the axis of the support column 43 are perpendicular to each other; the fuselage positioning mechanism 4 is connected to the support bracket 1 through the horizontal column 46.

[0104] Please see the appendix Figure 1 Appendix Figure 4 To be continued Figure 6 In one specific embodiment of this example, the horizontal column 46 includes a horizontally arranged first connecting plate 461;

[0105] The first connecting plate 461 is disposed on the side of the horizontal column 46 away from the second horizontal column 45; the first connecting plate 461 is connected to the support 1 by bolt connection.

[0106] In one specific embodiment of this example, the first connecting plate 461 is positioned at the midpoint of the horizontal column 46.

[0107] Please see the appendix Figure 1 To be continued Figure 6 In one specific embodiment of this example, the horizontal column 46 further includes a horizontally arranged second connecting plate 462 and a third connecting plate 463;

[0108] The second connecting plate 462 and the third connecting plate 463 are disposed at the upper end of the horizontal column 46; the second connecting plate 462 and the third connecting plate 463 are both disposed on the side of the horizontal column 46 away from the second horizontal column 45; the second connecting plate 462 and the third connecting plate 463 are also connected to the support 1 by bolts.

[0109] In terms of position, the second connecting plate 462 and the third connecting plate 463 are symmetrically distributed relative to the first connecting plate 461.

[0110] In one specific embodiment of this example, reinforcing ribs are provided between the first connecting plate 461 and the horizontal column 46, between the second connecting plate 462 and the horizontal column 46, and between the third connecting plate 463 and the horizontal column 46.

[0111] In a specific implementation manner of this embodiment, reinforcing rib plates are provided between the first cross-column 44 and the support column 43, and between the second cross-column 45 and the support column 43.

[0112] It should be noted that the selection of specific components and the determination of dimensions correspond to the landing gear (dimension specifications) of corresponding occasions and corresponding models. Therefore, the dimensions of components are not significantly limited in this application.

[0113] Please refer to Appendix Figure 1 to Appendix Figure 4 , in a specific implementation manner of this embodiment, the support support 1 includes:

[0114] A bearing column 11, which is a "day"-shaped, horizontally placed frame structure;

[0115] Column 12, there are multiple columns 12, and the multiple columns 12 support the bearing column 11 on the support surface; the multiple columns 12 are arranged in a rectangular array.

[0116] Please refer to Appendix Figure 1 and Appendix Figure 4 , in a specific implementation manner of this embodiment, the first connecting plate 461 is connected to the middle column of the "day"-shaped bearing column 11;

[0117] The horizontal column 46 is vertically arranged with the middle column of the "day"-shaped bearing column 11.

[0118] In a specific implementation manner of this embodiment, the bottom plate 21 of the sliding pipe clamping mechanism 2 is connected and arranged at the four corner positions of the "day"-shaped bearing column 11.

[0119] Please refer to Appendix Figure 1 to Appendix Figure 4 , in a specific implementation manner of this embodiment, a column base 121 is provided at one end (the end close to the support surface) of the column 12 far from the bearing column 11;

[0120] In the projection along the direction parallel to the axis of the column 12, the projection of the column base​​​​​In one specific embodiment of this example, multiple columns 12 are provided, and the multiple columns 12 support the endpoints and midpoints of the multiple columns of the bearing column 11.

[0123] The diagram shows that there are nine columns 12.

[0124] By applying the assembly fixture provided in this application, simultaneous assembly of left and right symmetrical parts can be achieved. It provides corresponding component positioning (sliding tube clamping mechanism 2) and corresponding simulated positions of fuselage connection positions (fuselage positioning mechanism 4), ensuring assembly accuracy and efficiency.

[0125] The above description is merely a preferred embodiment of the present utility model and is not intended to limit the present utility model in any way. Although the present utility model has been disclosed above with reference to a preferred embodiment, it is not intended to limit the present utility model. Any person skilled in the art can make some modifications or alterations to the above-described technical content to create equivalent embodiments without departing from the scope of the present utility model. The implementation schemes in the above embodiments can also be further combined or replaced. Any simple modifications, equivalent changes and alterations made to the above embodiments based on the technical essence of the present utility model without departing from the scope of the present utility model shall still fall within the scope of the present utility model.

Claims

1. A tooling for assembling a skid landing gear with a buffer, characterized in that, include: Support (1), the support (1) is supported on the support surface; The slide tube clamping mechanism (2) is used to clamp the slide tube (31) of the buffer-type skid landing gear (3); The fuselage positioning mechanism (4) is disposed on the side of the support base (1) away from the support surface; the fuselage positioning mechanism (4) includes a fuselage fixing part (41) for fixing the fuselage connection (32) of the skid landing gear (3) with buffer, and a buffer fixing part (42) for fixing the buffer (33) of the skid landing gear (3); Among them, the fuselage positioning mechanism (4) is provided in two opposite directions; the fuselage fixing parts (41) of the two fuselage positioning mechanisms (4) are arranged facing each other; each of the two fuselage positioning mechanisms (4) is provided with two buffer fixing parts (42) that are symmetrically arranged relative to the position of their own fuselage fixing parts (41).

2. The assembly tooling for a skid-mounted landing gear with a buffer as described in claim 1, characterized in that, The assembly fixture for the skid landing gear with buffer includes: The slide tube (31) comprises two parallel tubes; An arched tube (34) has two parallel arched tubes. The top of the arched tube (34) is the fuselage connection point (32). Both arched tubes (34) are provided with two buffers (33) that are symmetrically arranged relative to their fuselage connection points (32).

3. The assembly fixture for a skid-mounted landing gear with a buffer as described in claim 2, characterized in that, The slide tube clamping mechanism (2) is provided in four parts; The four sliding tube clamping mechanisms (2) are arranged at the four included angle positions of the support (1); Two slide tube clamping mechanisms (2) are arranged in a direction parallel to the two fuselage positioning mechanisms (4) and facing each other, for clamping the same slide tube (31).

4. The assembly fixture for a skid-mounted landing gear with a buffer as described in claim 3, characterized in that, The slide tube clamping mechanism (2) includes: A base plate (21) is provided with a waist-shaped hole (211); the base plate (21) is installed on the support bracket (1) by means of bolts passing through the waist-shaped hole (211); The first middle plate (22) is disposed on the side of the base plate (21) away from the support (1); The second middle plate (23) is connected to the first middle plate (22) by an adjusting bolt (25); by rotating the adjusting bolt (25), the distance between the second middle plate (23) and the first middle plate (22) increases or decreases; the second middle plate (23) is provided with an arc-shaped groove (231) on the side away from the support (1); The top plate (24) is connected to the second middle plate (23) by bolts. The top plate (24) is located at the end of the second middle plate (23) away from the support base (1). The top plate (24) has an arc-shaped groove (241) on the side facing closer to the second middle plate (23). The arc-shaped groove (241) on the top plate and the arc-shaped groove (231) on the middle plate cooperate to clamp the slide tube (31) of the skid landing gear (3) with buffer.

5. The assembly fixture for a skid-mounted landing gear with a buffer as described in claim 2, characterized in that, The fuselage positioning mechanism (4) further includes: A support column (43) is disposed on the side of the support base (1) away from the support surface; The first horizontal column (44) is arranged perpendicularly to the support column (43); the first horizontal column (44) is located at the end of the support column (43) away from the support base (1); the fuselage fixing part (41) is located at the midpoint of the first horizontal column (44), and the buffer fixing part (42) is located at both ends of the first horizontal column (44).

6. The assembly fixture for a skid-mounted landing gear with a buffer as described in claim 5, characterized in that, The fuselage fixing part (41) includes: The fuselage fixing plate (411) is disposed on the side of the first cross column (44) facing the support base (1) and extends towards the fuselage positioning mechanism (4) disposed on the other side. The first reinforcing rib (412) is a right-angled triangular structure; one right-angled side of the first reinforcing rib (412) is connected to the side of the first crossbar (44) facing the fuselage positioning mechanism (4) located on the other side, and the other right-angled side is connected to the side of the fuselage fixing plate (411) facing away from the support (1).

7. The assembly fixture for a skid-mounted landing gear with a buffer as described in claim 6, characterized in that, The buffer fixing part (42) includes: A buffer fixing plate (421) is disposed on the side of the first cross column (44) facing closer to the support base (1) and extending towards the fuselage positioning mechanism (4) disposed on the other side; the extension length of the buffer fixing plate (421) is the same as the extension length of the fuselage fixing plate (411). The second reinforcing rib (422) is a right-angled triangular structure; one right-angled side of the second reinforcing rib (422) is connected to the side of the first crossbar (44) facing the fuselage positioning mechanism (4) located on the other side, and the other right-angled side is connected to the side of the buffer fixing plate (421) facing away from the support (1).

8. The assembly fixture for a skid-mounted landing gear with a buffer as described in claim 5, characterized in that, The fuselage positioning mechanism (4) further includes: The second horizontal column (45) is disposed at the end of the support column (43) away from the first horizontal column (44); along a direction parallel to the axis of the support column (43), the projection of the first horizontal column (44) covers the projection of the second horizontal column (45). A horizontal column (46), the horizontal column (46) being horizontally arranged; the horizontal column (46) is connected to a side of the second cross column (45) away from the support column (43); the axes of the horizontal column (46), the second cross column (45), and the support column (43) are perpendicular to each other pairwise; the fuselage positioning mechanism (4) is connected to the support base (1) through the horizontal column (46).

9. The assembly fixture for a skid-mounted landing gear with a buffer as described in claim 8, characterized in that, The horizontal column (46) includes a first connecting plate (461) arranged horizontally; The first connecting plate (461) is arranged on a side of the horizontal column (46) away from the second cross column (45); the first connecting plate (461) is connected to the support base (1) by means of bolt connection.

10. A landing gear assembly fixture with a buffer skid as described in any one of claims 1-9, characterized in that, The support base (1) includes: A bearing column (11), the bearing column (11) being a "day"-shaped, horizontally placed frame structure; Columns (12), there are multiple columns (12), and the multiple columns (12) support the bearing column (11) on a support surface; the multiple columns (12) are arranged in a rectangular array.

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