An aircraft landing gear installation accessory

Abstract

An aircraft landing gear installation aid, relating to the field of landing gear installation devices, includes a movable base and a lifting component. The upper surface of the movable base is connected to the lower surface of the lifting component, and the lifting component is located at the edge of the movable base. A tilt adjustment component is provided on the side of the lifting component, and the tilt adjustment component is connected to the lifting end of the lifting component. The tilt adjustment component is located directly above the movable base. A clamping and rotating clamping component is provided on the tilt adjustment component, and the lower surface of the clamping and rotating clamping component is connected to the upper surface of the tilt adjustment component. The advantages are: it avoids damage to the clamping components caused by manually prying or striking the landing gear when the two mounting ports on the aircraft require tilting or rotating alignment of the landing gear, or when the positions of the two mounting ports on the aircraft are misaligned with the landing gear during installation. Furthermore, a single person can directly rotate the landing gear, improving installation efficiency.

Description

Technical Field

[0001] This utility model relates to the technical field of landing gear installation devices, and in particular to an auxiliary tool for aircraft landing gear installation. Background Technology

[0002] As is generally known, landing gear is the main load-bearing component of an aircraft when it is parked, taxiing, taking off, or landing. When the landing gear is fully extended or retracted and the cabin door is closed, an installation vehicle is generally required to move and transport the aircraft landing gear during installation.

[0003] The Chinese patent CN211731856U describes an aircraft main landing gear mounting vehicle. This device includes a mounting vehicle body and wheels. Two pairs of wheels are connected to the lower part of the mounting vehicle body. A frame and a first housing are fixed to the upper center and left side of the mounting vehicle body, respectively. A first screw is rotatably connected inside the first housing via a pair of bearings. An adjustment mechanism is installed on the lower outer wall of the first screw. A first adjusting arm is threadedly connected to the upper outer wall of the first screw. A second adjusting arm is rotatably connected to the groove of the first adjusting arm via a rotating shaft. A fixing mechanism is installed inside the second adjusting arm. However, the following problems exist in actual use:

[0004] Aircraft landing gear is typically installed directly onto the aircraft as a landing gear assembly. During installation, the landing gear needs to be aligned with the aircraft mounting ports on both sides of the landing gear. If slight misalignment occurs during the alignment process, the landing gear needs to be tilted to achieve alignment. Alternatively, if there is a slight misalignment where the aircraft mounting ports on both sides of the landing gear are not on the same horizontal plane, installers usually try to align the landing gear by forcibly prying it or by tapping it with a rubber mallet. In this case, the clamping device may damage the clamping parts of the landing gear, or the prying or tapping may damage the parts of the landing gear that are being pried or tapped.

[0005] Therefore, an auxiliary tool for aircraft landing gear installation is proposed. Utility Model Content

[0006] The purpose of this utility model is to overcome the shortcomings of the prior art, solve the problems mentioned in the background art, and provide an auxiliary tool for aircraft landing gear installation.

[0007] To achieve the aforementioned objective, this utility model adopts the following technical solution:

[0008] An aircraft landing gear mounting accessory includes a movable base and a lifting component. The upper surface of the movable base is connected to the lower surface of the lifting component, and the lifting component is located at the edge of the movable base. A tilt adjustment component is provided on the side of the lifting component and is connected to the lifting end of the lifting component. The tilt adjustment component is located directly above the movable base. The bearing portion of the tilt adjustment component is U-shaped, with the end of the U-shape away from the lifting component. The active adjustment end of the tilt adjustment component is located on the upper surface of the bearing portion of the tilt adjustment component near the upper surface of the lifting component. The driven adjustment end of the tilt adjustment component is located on the upper surface of the U-shaped end of the bearing portion of the tilt adjustment component. A rotating clamping component is provided on the tilt adjustment component, and the lower surface of the rotating clamping component is connected to the upper surface of the tilt adjustment component. The bearing portion of the rotating clamping component is U-shaped and corresponds to the bearing portion of the tilt adjustment component.

[0009] The rotating clamping component includes a clamping bracket, limiting rods, a push plate, clamping blocks, a bidirectional threaded rod, a coupling, a servo motor, and a rotating assembly. Two push plates and two clamping blocks are provided. The clamping bracket is U-shaped, with the U-shaped end of the clamping bracket away from the lifting component. The lower surface of the clamping bracket is connected to the upper surface of the tilt adjustment component. At least two limiting holes are provided on both sides of the clamping bracket, and the limiting holes on both sides of the clamping bracket correspond to each other. The number of limiting rods corresponds to the number of limiting holes in the clamping bracket. The limiting rods pass through the limiting holes of the clamping bracket and are fixedly connected to one side of the push plate, and the limiting rods are slidably connected to the clamping bracket. The other side of the push plate is connected to the clamping block, and the side of the clamping block near the object being clamped is connected to the rotating assembly. The front and rear parts of the bidirectional threaded rod have opposite rotation directions. The side of the clamping bracket has a pivot hole. One end of the bidirectional threaded rod is rotatably connected to the inner wall of the clamping bracket, and the other end of the bidirectional threaded rod is fixedly connected to one end of the coupling. The other end of the coupling passes through the pivot hole of the clamping bracket and is fixedly connected to the power output end of the servo motor. The coupling is rotatably connected to the clamping bracket. The push plate has a threaded hole, and the two push plates are respectively threaded to the front and rear parts of the bidirectional threaded rod.

[0010] The clamping block includes a clamping inclined block and a clamping flat block. The clamping flat block is fixedly connected to the push plate through the clamping inclined block, and the position where the clamping inclined block is connected to the clamping flat block is higher than the position where the clamping inclined block is connected to the push plate. The rotating component is provided on the surface of the clamping flat block near the object being clamped.

[0011] The rotating assembly includes two sets of rotating wheels, each set having at least two wheels. The two sets of rotating wheels are rotatably connected to the clamping block. The clamping block has a horizontal groove on the side near the object being clamped. The rotating wheel is located in the horizontal groove of the clamping block, and the rotating wheel is in contact with the object being clamped. The rotating wheel is horizontally positioned.

[0012] The tilt adjustment component includes a tilt adjustment bracket and a tilt adjustment assembly. The tilt adjustment bracket is U-shaped, and there are two sets of tilt adjustment assemblies. The upper surface of the tilt adjustment bracket is connected to the lower surface of the clamping bracket through the tilt adjustment assembly. The tilt adjustment bracket is connected to the lifting end of the lifting component.

[0013] The tilt adjustment assembly includes a hydraulic support rod, a hydraulic push rod, a universal ball, a slider, and a hydraulic pump. The bottom end of the hydraulic support rod is fixedly connected to the upper surface of the tilt adjustment bracket, and the hydraulic support rod is located on the upper surface of the tilt adjustment bracket near the lifting component. The top end of the hydraulic support rod is fixedly connected to the universal ball. The lower surface of the clamping bracket is provided with a hemispherical groove, and the universal ball is located in the hemispherical groove of the clamping bracket and is slidably connected to the clamping bracket. The upper surface of the tilt adjustment bracket is provided with a sliding groove away from the lifting component. The bottom end of the slider is located in the sliding groove of the tilt adjustment bracket and is slidably connected to the tilt adjustment bracket. The top end of the slider is rotatably connected to the clamping bracket via a pin. One end of the hydraulic push rod is fixedly connected to the side of the slider near the lifting component, and the other end of the hydraulic push rod is fixedly connected to the tilt adjustment bracket, and the hydraulic push rod is located in the sliding groove of the tilt adjustment bracket. The hydraulic support rod and the hydraulic push rod are respectively connected to the hydraulic pump through hydraulic pipes.

[0014] The slider includes a slider base, a slider support rod, and a spring. The slider base has a groove, and the slider support rod is located in the groove of the slider base and is slidably connected to the slider base. The slider base and the slider support rod are connected by the spring. The bottom end of the slider base is slidably connected to the tilt adjustment bracket, and the top end of the slider support rod is rotatably connected to the clamping bracket.

[0015] Compared with the prior art, the present invention has the following beneficial effects:

[0016] This aircraft landing gear installation accessory avoids damage to the landing gear clamping parts caused by manual prying or knocking when the two mounting ports on the aircraft need to be tilted or rotated for alignment, or when there is vertical misalignment between the two mounting ports and the corresponding landing gear positions. It also avoids damage to the prying or knocking parts caused by prying or knocking. In addition, a single person can directly rotate the landing gear without having to rotate the entire landing gear with the device, reducing manpower and improving installation efficiency. Attached Figure Description

[0017] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0018] Figure 2 This is a side view of the present invention.

[0019] Figure 3 This is a schematic diagram of the side structure of the tilt adjustment component of this utility model when it is lifted up;

[0020] Figure 4 This utility model Figure 2 A schematic diagram of the cross-sectional structure of the slider at point A shown;

[0021] Figure 5 This utility model Figure 2 A schematic diagram of the cross-sectional structure of the hydraulic support rod at point B shown.

[0022] Figure 6 This is a three-dimensional structural diagram of the rotating clamping component of this utility model;

[0023] Figure 7 This is a three-dimensional structural diagram of the clamping block of this utility model;

[0024] Figure 8 This is a cross-sectional structural diagram of the slider of this utility model;

[0025] Figure 9 This is a schematic diagram of the structure of the bidirectional threaded rod of this utility model.

[0026] 1. Movable base; 2. Lifting component; 3. Clamping bracket; 4. Limiting rod; 5. Push plate; 6. Clamping block; 7. Bidirectional threaded rod; 8. Coupling; 9. Servo motor; 10. Clamping inclined block; 11. Clamping flat block; 12. Rotating wheel; 13. Tilt adjustment bracket; 14. Hydraulic support rod; 15. Hydraulic push rod; 16. Universal ball; 17. Slider; 18. Hydraulic pump; 19. Slider base; 20. Slider support rod; 21. Spring. Detailed Implementation

[0027] 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; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0028] Additional aspects and advantages of this invention will be further set forth in the description which follows in conjunction with the accompanying drawings, and in part will be obvious from the description or may be learned by practice of the invention.

[0029] like Figure 1-3 As shown, an aircraft landing gear mounting accessory includes a movable base 1 and a lifting component 2. The upper surface of the movable base 1 is connected to the lower surface of the lifting component 2, and the lifting component 2 is located at the edge of the movable base 1. A tilt adjustment component is provided on the side of the lifting component 2, and the tilt adjustment component is connected to the lifting end of the lifting component 2. The tilt adjustment component is located directly above the movable base 1. The bearing part of the tilt adjustment component is U-shaped, and the end of the U-shape of the bearing part of the tilt adjustment component is away from the lifting component 2. The active adjustment end of the tilt adjustment component is located on the upper surface of the bearing part of the tilt adjustment component near the upper surface of the lifting component 2, and the driven adjustment end of the tilt adjustment component is located on the upper surface of the U-shaped end of the bearing part of the tilt adjustment component. A clamping rotating clamping component is provided on the tilt adjustment component, and the lower surface of the clamping rotating clamping component is connected to the upper surface of the tilt adjustment component. The bearing part of the clamping rotating clamping component is U-shaped, and the bearing part of the clamping rotating clamping component corresponds to the bearing part of the tilt adjustment component.

[0030] like Figure 1 , Figure 6 , Figure 7 and Figure 9As shown, the rotating clamping component includes a clamping bracket 3, limiting rods 4, a push plate 5, a clamping block 6, a bidirectional threaded rod 7, a coupling 8, a servo motor 9, and a rotating assembly. Two push plates 5 and two clamping blocks 6 are provided. The clamping bracket 3 is U-shaped, with the U-shaped end of the clamping bracket 3 away from the lifting component 2. The lower surface of the clamping bracket 3 is connected to the upper surface of the tilt adjustment component. At least two limiting holes are provided on both sides of the clamping bracket 3, and the limiting holes on both sides of the clamping bracket 3 correspond to each other. The number of limiting rods 4 corresponds to the number of limiting holes in the clamping bracket 3. The limiting rods 4 pass through the limiting holes of the clamping bracket 3 and are fixedly connected to one side of the push plate 5. The limiting rods 4 and the clamping bracket 3 are also connected. The sliding connection is used. The other side of the push plate 5 is connected to the clamping block 6. The side of the clamping block 6 near the clamped object is connected to the rotating component. The front and rear of the bidirectional threaded rod 7 have opposite rotation directions of their threads. The side of the clamping bracket 3 is provided with a rotating shaft hole. One end of the bidirectional threaded rod 7 is rotatably connected to the inner wall of the clamping bracket 3. The other end of the bidirectional threaded rod 7 is fixedly connected to one end of the coupling 8. The other end of the coupling 8 passes through the rotating shaft hole of the clamping bracket 3 and is fixedly connected to the power output end of the servo motor 9. The coupling 8 is rotatably connected to the clamping bracket 3. The push plate 5 is provided with a threaded hole. The two push plates 5 are threadedly connected to the front and rear of the bidirectional threaded rod 7, respectively.

[0031] like Figure 7 As shown, the clamping block 6 includes a clamping inclined block 10 and a clamping flat block 11. The clamping flat block 11 is fixedly connected to the push plate 5 through the clamping inclined block 10. The position where the clamping inclined block 10 is connected to the clamping flat block 11 is higher than the position where the clamping inclined block 10 is connected to the push plate 5. A rotating component is provided on the surface of the clamping flat block 11 near the object being clamped.

[0032] like Figure 7 As shown, the rotating assembly includes rotating wheels 12. There are two sets of rotating wheels 12, and each set of rotating wheels 12 has at least two wheels. The two sets of rotating wheels 12 are rotatably connected to the clamping block 6. The side of the clamping block 6 near the object being clamped has a horizontal groove. The rotating wheels 12 are located in the horizontal groove of the clamping block 6. The rotating wheels 12 are in contact with the object being clamped, and the rotating wheels 12 are horizontally arranged.

[0033] like Figure 2-5 As shown, the tilt adjustment component includes a tilt adjustment bracket 13 and a tilt adjustment assembly. The tilt adjustment bracket 13 is U-shaped, and there are two sets of tilt adjustment assemblies. The upper surface of the tilt adjustment bracket 13 is connected to the lower surface of the clamping bracket 3 through the tilt adjustment assembly. The tilt adjustment bracket 13 is connected to the lifting end of the lifting component 2.

[0034] like Figure 2-5As shown, the tilt adjustment assembly includes a hydraulic support rod 14, a hydraulic push rod 15, a universal ball 16, a slider 17, and a hydraulic pump 18. The bottom end of the hydraulic support rod 14 is fixedly connected to the upper surface of the tilt adjustment bracket 13, and the hydraulic support rod 14 is located on the upper surface of the tilt adjustment bracket 13 near the lifting component 2. The top end of the hydraulic support rod 14 is fixedly connected to the universal ball 16. The lower surface of the clamping bracket 3 is provided with a hemispherical groove, and the universal ball 16 is located in the hemispherical groove of the clamping bracket 3 and is slidably connected to the clamping bracket 3. The upper surface of the tilt adjustment bracket 13... A sliding groove is provided away from the lifting component 2. The bottom end of the slider 17 is located in the sliding groove of the tilt adjustment bracket 13 and is slidably connected to the tilt adjustment bracket 13. The top end of the slider 17 is rotatably connected to the clamping bracket 3 through a pin. One end of the hydraulic push rod 15 is fixedly connected to the side of the slider 17 near the lifting component 2, and the other end of the hydraulic push rod 15 is fixedly connected to the tilt adjustment bracket 13. The hydraulic push rod 15 is located in the sliding groove of the tilt adjustment bracket 13. The hydraulic support rod 14 and the hydraulic push rod 15 are respectively connected to the hydraulic pump 18 through hydraulic pipes.

[0035] like Figure 8 As shown, the slider 17 includes a slider base 19, a slider support rod 20, and a spring 21. The slider base 19 has a groove, and the slider support rod 20 is located in the groove of the slider base 19 and is slidably connected to the slider base 19. The slider base 19 and the slider support rod 20 are connected by the spring 21. The bottom end of the slider base 19 is slidably connected to the tilt adjustment bracket 13, and the top end of the slider support rod 20 is rotatably connected to the clamping bracket 3.

[0036] The work process is as follows:

[0037] S1. In use, place the landing gear in the corresponding position on the device, start the servo motor 9, which drives the bidirectional threaded rod 7 to rotate via the coupling 8. The threads at the front and rear of the bidirectional threaded rod 7 rotate in opposite directions, causing the two push plates 5 to slide towards each other. The two push plates 5 push the two clamping blocks 6 to slide towards each other, thus clamping the landing gear. Then, move the landing gear below the desired installation position on the aircraft via the movable base 1. Start the lifting component 2, which pushes the clamping bracket 3 via the lifting tilt adjustment bracket 13, lifting the clamped landing gear to the required installation position. When installing the landing gear on the aircraft, align the mounting openings on both sides. When the two mounting ports on the aircraft are in a horizontal position but the landing gear needs to be tilted to align with the mounting ports, the hydraulic pump 18 is activated. The hydraulic support rod 14 lifts the clamping bracket 3 to the side near the lifting component 2. At the same time, the hydraulic push rod 15 retracts synchronously, pulling the slider 17 towards the lifting component 2, so that the clamping bracket 3 forms an inclined surface. This causes the landing gear to tilt and align with the aircraft's mounting ports for installation. This avoids damage to the landing gear clamping parts caused by manual prying or knocking when the landing gear needs to be tilted to align with the mounting ports. It also avoids damage to the knocking or prying parts caused by prying or knocking the landing gear, thus improving installation efficiency.

[0038] S2, when the two mounting ports on the aircraft are in a horizontal position but the landing gear needs to be rotated to align with the mounting ports, the landing gear can be rotated manually. The landing gear is held by two sets of rotating wheels 12 horizontally set on the two clamping blocks 6. It is already clamped in the vertical direction. The rotating wheels 12 are rotatably connected, so the manual can easily rotate it. This avoids the waste of manpower caused by having to rotate the entire device when the landing gear needs to be rotated to align with the mounting ports, thereby improving efficiency.

[0039] S3. When the two mounting ports on the aircraft are misaligned with the landing gear positions, first start the hydraulic pump 18 to tilt the landing gear. Then adjust the landing gear position so that the center of the landing gear is at the center of the misaligned mounting ports. Then manually rotate the landing gear to align the mounting ports. This avoids damage to the clamping parts of the landing gear when the two mounting ports on the aircraft are misaligned and the landing gear is forcibly pried or knocked. It also avoids damage to the pried or knocked parts when the landing gear is pried or knocked, thus improving installation efficiency.

[0040] The landing gear tilt angle is adjusted by using a hydraulic support rod 14 and a hydraulic push rod 15. To reduce the impact force when adjusting the landing gear tilt angle, the oil inside the hydraulic rod itself is a good buffer medium. The clamping block 6 adopts a structure with a clamping inclined block 10 and a clamping flat block 11. When clamping the aircraft landing gear, it forms a "V" shape, which can provide better support for the landing gear. The slider 17 adopts a structure with a slider base 19, a slider support rod 20 and a spring 21. It can provide a certain degree of self-adaptation during the adjustment of the landing gear tilt angle, and also play a buffering role.

[0041] The parts of this utility model not described in detail are prior art. Although this utility model has been specifically shown and introduced in conjunction with preferred embodiments, there are many methods and approaches to implement this technical solution. The above description is only a preferred embodiment of this utility model. However, those skilled in the art should understand that various changes in form and detail can be made to this utility model without departing from the spirit and scope of this utility model as defined by the appended claims, and all such changes shall be within the protection scope of this utility model.

Claims

1. An aircraft landing gear mounting accessory, comprising a movable base (1) and a lifting component (2), wherein the upper surface of the movable base (1) is connected to the lower surface of the lifting component (2), and the lifting component (2) is located at the edge of the movable base (1), characterized in that: The lifting component (2) has a tilt adjustment component on its side, and the tilt adjustment component is connected to the lifting end of the lifting component (2). The tilt adjustment component is located directly above the movable base (1). The bearing part of the tilt adjustment component is "U"-shaped, and the end of the "U"-shaped bearing part of the tilt adjustment component is far away from the lifting component (2). The active adjustment end of the tilt adjustment component is located on the upper surface of the bearing part of the tilt adjustment component near the lifting component (2). The driven adjustment end of the tilt adjustment component is located on the upper surface of the "U"-shaped end of the bearing part of the tilt adjustment component. The tilt adjustment component has a clamping rotating clamping component, and the lower surface of the clamping rotating clamping component is connected to the upper surface of the tilt adjustment component. The bearing part of the clamping rotating clamping component is "U"-shaped, and the bearing part of the clamping rotating clamping component corresponds to the bearing part of the tilt adjustment component.

2. The aircraft landing gear installation accessory according to claim 1, characterized in that: The rotating clamping component includes a clamping bracket (3), a limiting rod (4), a push plate (5), a clamping block (6), a bidirectional threaded rod (7), a coupling (8), a servo motor (9), and a rotating assembly. Two push plates (5) and two clamping blocks (6) are provided. The clamping bracket (3) is U-shaped, with the U-shaped end of the clamping bracket (3) away from the lifting component (2). The lower surface of the clamping bracket (3) is connected to the upper surface of the tilt adjustment component. At least two limiting holes are provided on both sides of the clamping bracket (3), and the limiting holes on both sides of the clamping bracket (3) correspond to each other. The number of limiting rods (4) corresponds to the number of limiting holes in the clamping bracket (3). The limiting rods (4) pass through the limiting holes of the clamping bracket (3) and are fixedly connected to one side of the push plate (5), and the limiting rods (4) slide against the clamping bracket (3). The push plate (5) is connected to the clamping block (6) on the other side. The side of the clamping block (6) near the object being clamped is connected to the rotating assembly. The front and rear of the bidirectional threaded rod (7) have opposite rotation directions. The side of the clamping bracket (3) has a rotating shaft hole. One end of the bidirectional threaded rod (7) is rotatably connected to the inner wall of the clamping bracket (3). The other end of the bidirectional threaded rod (7) is fixedly connected to one end of the coupling (8). The other end of the coupling (8) passes through the rotating shaft hole of the clamping bracket (3) and is fixedly connected to the power output end of the servo motor (9). The coupling (8) is rotatably connected to the clamping bracket (3). The push plate (5) has a threaded hole. The two push plates (5) are threadedly connected to the front and rear of the bidirectional threaded rod (7) respectively.

3. The aircraft landing gear installation accessory according to claim 2, characterized in that: The clamping block (6) includes a clamping inclined block (10) and a clamping flat block (11). The clamping flat block (11) is fixedly connected to the push plate (5) through the clamping inclined block (10). The position where the clamping inclined block (10) is connected to the clamping flat block (11) is higher than the position where the clamping inclined block (10) is connected to the push plate (5). The rotating component is provided on the surface of the clamping flat block (11) near the object being clamped.

4. An aircraft landing gear installation accessory according to claim 2 or 3, characterized in that: The rotating assembly includes rotating wheels (12), and there are two sets of rotating wheels (12). Each set of rotating wheels (12) has at least two wheels. The two sets of rotating wheels (12) are rotatably connected to the clamping block (6). The clamping block (6) has a horizontal groove on the side near the object being clamped. The rotating wheels (12) are located in the horizontal groove of the clamping block (6). The rotating wheels (12) are in contact with the object being clamped, and the rotating wheels (12) are horizontally arranged.

5. The aircraft landing gear installation accessory according to claim 2, characterized in that: The tilt adjustment component includes a tilt adjustment bracket (13) and a tilt adjustment assembly. The tilt adjustment bracket (13) is U-shaped. The tilt adjustment assembly is provided in two sets. The upper surface of the tilt adjustment bracket (13) is connected to the lower surface of the clamping bracket (3) through the tilt adjustment assembly. The tilt adjustment bracket (13) is connected to the lifting end of the lifting component (2).

6. The aircraft landing gear installation accessory according to claim 5, characterized in that: The tilt adjustment assembly includes a hydraulic support rod (14), a hydraulic push rod (15), a universal ball (16), a slider (17), and a hydraulic pump (18). The bottom end of the hydraulic support rod (14) is fixedly connected to the upper surface of the tilt adjustment bracket (13), and the hydraulic support rod (14) is located on the upper surface of the tilt adjustment bracket (13) near the lifting component (2). The top end of the hydraulic support rod (14) is fixedly connected to the universal ball (16). The lower surface of the clamping bracket (3) is provided with a hemispherical groove. The universal ball (16) is located in the hemispherical groove of the clamping bracket (3) and is slidably connected to the clamping bracket (3). The upper surface of the tilt adjustment bracket (13) is away from the lifting component (2). The lifting component (2) is provided with a sliding groove. The bottom end of the slider (17) is located in the sliding groove of the tilt adjustment bracket (13) and is slidably connected to the tilt adjustment bracket (13). The top end of the slider (17) is rotatably connected to the clamping bracket (3) through a pin. One end of the hydraulic push rod (15) is fixedly connected to the side of the slider (17) near the lifting component (2). The other end of the hydraulic push rod (15) is fixedly connected to the tilt adjustment bracket (13). The hydraulic push rod (15) is located in the sliding groove of the tilt adjustment bracket (13). The hydraulic support rod (14) and the hydraulic push rod (15) are respectively connected to the hydraulic pump (18) through hydraulic pipes.

7. The aircraft landing gear installation accessory according to claim 6, characterized in that: The slider (17) includes a slider base (19), a slider support rod (20), and a spring (21). The slider base (19) has a groove. The slider support rod (20) is located in the groove of the slider base (19) and is slidably connected to the slider base (19). The slider base (19) and the slider support rod (20) are connected by the spring (21). The bottom end of the slider base (19) is slidably connected to the tilt adjustment bracket (13). The top end of the slider support rod (20) is rotatably connected to the clamping bracket (3).

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