Shock absorption undercarriage of surveying and mapping unmanned aerial vehicle for surveying and mapping geographic information

Abstract

The utility model discloses a surveying and mapping unmanned aerial vehicle damping undercarriage for surveying and mapping geographic information, which comprises a base, the upper side of the base is fixedly connected with symmetrical fixing blocks, the upper sides of the fixing blocks are respectively hinged with two ends of a connecting block, the connecting block is triangular, and the two fixing blocks are arranged along the same straight line; the two sides of the upper end of the connecting block are hinged to one ends of first connecting rods respectively, the two sides of the middle of the connecting block are hinged to one ends of second connecting rods respectively, the first connecting rods and the second connecting rods are arranged in parallel, and the other ends of the two first connecting rods are hinged to the two sides of the upper end of a supporting block respectively. The two sides of the lower end of the supporting block are hinged to the other ends of the two second connecting rods correspondingly. The utility model relates to the technical field of damping equipment of unmanned aerial vehicles, in particular to a damping undercarriage of a surveying and mapping unmanned aerial vehicle for surveying and mapping geographic information, which can effectively absorb and buffer impact force generated during landing of the unmanned aerial vehicle and can perform buffering and damping protection on the unmanned aerial vehicle.

Description

Technical Field

[0001] The utility model relates to the technical field of shock-absorbing equipment for unmanned aerial vehicles (UAVs), and in particular to a shock-absorbing landing gear for a surveying and mapping UAV used for surveying and mapping geographic information. Background Art

[0002] In the field of surveying and mapping, drones are widely used for data collection due to their flexibility and efficiency. However, during takeoff and landing, the impact of landing can damage the drone and its onboard precision instruments, affecting data accuracy and equipment lifespan. Traditional drone landing gear designs often lack effective shock absorption mechanisms, resulting in vibrations generated during landing being directly transmitted to the drone platform, compromising surveying accuracy and equipment safety. Utility Model Content

[0003] The technical problem to be solved by the utility model is to provide a shock-absorbing landing gear for a surveying and mapping UAV for surveying and mapping geographic information, which can effectively absorb and buffer the impact force generated when the UAV lands, and provide buffering and shock-absorbing protection for the UAV.

[0004] A shock-absorbing landing gear for a surveying and mapping UAV for surveying and mapping geographic information comprises a base, the upper side of which is fixedly connected to symmetrical fixing blocks, the upper sides of which are respectively hinged to the two ends of a connecting block, the connecting block being triangular in shape, and the two fixing blocks being arranged along the same straight line;

[0005] The two sides of the upper end of the connecting block are respectively hinged to one end of the connecting rod 1, and the two sides of the middle part of the connecting block are respectively hinged to one end of the connecting rod 2. The connecting rod 1 and the connecting rod 2 are arranged in parallel. The other ends of the two connecting rods 1 are respectively hinged to the two sides of the upper end of the support block, and the two sides of the lower end of the support block are respectively hinged to the other ends of the two connecting rods 2. The upper sides of the two connecting rods 1 are fixedly connected to the drone platform support block, and the upper side of the drone platform support block is fixedly connected to the drone support platform;

[0006] The second connecting rod and the first connecting rod are connected to the buffer assembly.

[0007] As a further limitation of the present technical solution, the buffer assembly includes a sleeve, the lower ends of the sleeves are hinged on both sides of the connecting rod 2, the round rod of the connecting rod is inserted into each of the sleeves, the outer end hinge block of each connecting rod is hinged to the corresponding connecting rod 1, each sleeve is fixed to one end of the spring 1, and the other end of each spring 1 is fixedly connected to the outer end hinge block of the connecting rod, and each spring 1 is respectively ringed around the corresponding sleeve and the round rod of the connecting rod.

[0008] As a further limitation of this technical solution, when the UAV support platform is parallel to the ground, the angle between the axis of the sleeve and the ground is degrees.

[0009] As a further limitation of the present technical solution, one side of the connecting rod 2 is fixedly connected to a fixed shaft, the fixed shaft is hingedly connected to the outer end of the moving rod, the round shaft of the moving rod is inserted into the limiting cylinder, the lower end of the limiting cylinder is hinged to a limiting block, and the limiting block fixes the base.

[0010] As a further limitation of the present technical solution, the lower part of the limiting cylinder is fixed with a second spring, the upper end of the second spring is fixed with an outer end of the moving rod, and the second spring is encircled by the limiting cylinder and the moving rod.

[0011] Compared with the prior art, the advantages and positive effects of the present invention are:

[0012] (1) The design of connecting rod 1 and connecting rod 2 achieves stable support when the UAV lands, reducing the vibration of the equipment caused by the impact force. The design of the buffer component, including the sleeve, spring 1 and spring 2, can effectively absorb and buffer the impact force generated when the UAV lands, protecting the UAV and the equipment it carries from damage.

[0013] (2) The triangular connecting blocks and symmetrically arranged fixing blocks provide a more stable structural support, making the landing gear less likely to deform when subjected to impact force. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] The drawings described herein are used to provide a further understanding of this application and constitute a part of this application. The illustrative embodiments of this application and their descriptions are used to explain this application and do not constitute an undue limitation on this application. Obviously, the drawings described below are only some embodiments of the utility model. For those of ordinary skill in the art, other drawings can be obtained based on these drawings without inventive effort. In the drawings:

[0015] Figure 1 This is a schematic diagram of the three-dimensional structure of the utility model Figure 1 ;

[0016] Figure 2 This is a schematic diagram of the three-dimensional structure of the utility model Figure 2 ;

[0017] Figure 3 It is a schematic diagram of a partial three-dimensional structure of the utility model;

[0018] Figure 4 This is a schematic diagram of the three-dimensional structure of the utility model Figure 3 .

[0019] In the figure: 1. UAV support platform; 2. Connecting rod 1; 3. Connecting rod; 4. Spring 1, 6. Sleeve; 7. Base; 8. Limit block; 9. Fixed block; 10. Connecting block; 11. Connecting rod 2; 12. UAV platform support block; 13. Limit cylinder, 14. Spring 2, 15. Moving rod, 16. Fixed shaft, 17. Support block. DETAILED DESCRIPTION

[0020] The following is combined with Figure 1-4 The utility model is further described with reference to the accompanying drawings and implementation methods.

[0021] A shock-absorbing landing gear for a surveying and mapping UAV for surveying and mapping geographic information includes a base 7, the upper side of which is fixedly connected to symmetrical fixing blocks 9, the upper sides of which are respectively hinged to the two ends of a connecting block 10, the connecting block 10 being triangular in shape, and the two fixing blocks 9 being arranged along the same straight line;

[0022] The two sides of the upper end of the connecting block 10 are respectively hinged to one end of the connecting rod 1 2, and the two sides of the middle part of the connecting block 10 are respectively hinged to one end of the connecting rod 2 11. The connecting rod 1 2 and the connecting rod 2 11 are arranged in parallel. The other ends of the two connecting rods 1 2 are respectively hinged to the two sides of the upper end of the support block 17, and the two sides of the lower end of the support block 17 are respectively hinged to the other ends of the two connecting rods 2 11. The upper sides of the two connecting rods 1 2 are fixedly connected to the drone platform support block 12, and the upper side of the drone platform support block 12 is fixedly connected to the drone support platform 1;

[0023] The connecting rod 2 11 and the connecting rod 1 2 are connected to the buffer assembly.

[0024] In this embodiment, when the drone lands on the drone support platform 1, due to the action of gravity, the connecting rod 1 2 and the connecting rod 2 11 swing, the support block 17 moves, and the buffer assembly buffers the force applied to the drone support platform 1, thereby achieving the stability of the connecting rod 1 2 and the connecting rod 2 11.

[0025] The buffer assembly includes a sleeve 6, and the lower ends of the sleeves 6 are hinged on both sides of the connecting rod 2 11. The round rod of the connecting rod 3 is inserted into each of the sleeves 6. The outer end hinge block of each connecting rod 3 is hinged to the corresponding connecting rod 1 2. Each of the sleeves 6 fixes one end of the spring 1 4, and the other end of each spring 1 4 is fixedly connected to the outer end hinge block of the connecting rod 3. Each spring 1 4 is respectively sleeved around the corresponding sleeve 6 and the round rod of the connecting rod 3.

[0026] When the UAV support platform 1 is parallel to the ground, the angle between the axis of the sleeve 6 and the ground is 30 degrees.

[0027] In this embodiment, the connecting rod 1 swings to drive the connecting rod 3 to move, the connecting rod 3 moves along the sleeve 6 and drives the sleeve 6 to swing, and the spring 1 4 produces elastic deformation to achieve a buffering function.

[0028] One side of the connecting rod 11 is fixedly connected to a fixed shaft 16, and the fixed shaft 16 is hingedly connected to the outer end of the moving rod 15. The round axis of the moving rod 15 is inserted into the limiting cylinder 13, and the lower end of the limiting cylinder 13 is hinged to a limiting block 8, and the limiting block 8 fixes the base 7.

[0029] A second spring 14 is fixed to the lower portion of the limiting cylinder 13 , and an upper end of the second spring 14 is fixed to the outer end of the moving rod 15 . The second spring 14 surrounds the limiting cylinder 13 and the moving rod 15 .

[0030] In this embodiment, the other end of the connecting rod 2 11 realizes the support and shock-absorbing and buffering functions through a buffer support assembly composed of a limit cylinder 13, a movable rod 15 and a spring 2 14. When the connecting rod 1 2 and the connecting rod 2 11 swing downward, the spring 2 14 undergoes elastic deformation, and the movable rod 15 moves in the limit cylinder 13 to realize the buffering and shock-absorbing function.

[0031] During use, the UAV lands on the UAV support platform 1. Due to the action of gravity, the connecting rod 2 swings downward, and the connecting rod 2 drives the connecting rod 11 to swing through the support block 17. The connecting rod 11 drives the moving rod 15 to move in the limit cylinder 13, and the spring 2 14 undergoes elastic deformation. At the same time, the connecting rod 2 drives the connecting rod 3 to move, and the connecting rod 3 moves along the sleeve 6 and drives the sleeve 6 to swing. The spring 1 4 produces elastic deformation. The elastic deformation of the spring 1 4 and the spring 2 14 buffers the vibration force and gravity, thereby realizing the shock absorption function.

[0032] The above disclosure is only a specific embodiment of the present invention, but the present invention is not limited thereto. Any changes that can be conceived by those skilled in the art should fall within the scope of protection of the present invention.

Claims

1. A shock-absorbing landing gear for a surveying and mapping UAV for surveying and mapping geographic information, comprising a base (7), characterized by: The upper side of the base (7) is fixedly connected to a symmetrical fixed block (9), the upper side of the fixed block (9) is hinged to the two ends of a connecting block (10), the connecting block (10) is triangular in shape, and the two fixed blocks (9) are arranged along the same straight line; The upper ends of the connecting block (10) are hinged to one end of the connecting rod 1 (2) on both sides, and the middle parts of the connecting block (10) are hinged to one end of the connecting rod 2 (11) on both sides. The connecting rod 1 (2) and the connecting rod 2 (11) are arranged in parallel. The other ends of the two connecting rods 1 (2) are hinged to the upper ends of the support block (17) on both sides, and the lower ends of the support block (17) are hinged to the other ends of the two connecting rods 2 (11) on both sides. The upper sides of the two connecting rods 1 (2) are fixedly connected to the UAV platform support block (12), and the upper side of the UAV platform support block (12) is fixedly connected to the UAV support platform (1). The second connecting rod (11) and the first connecting rod (2) are connected to the buffer assembly.

2. The shock-absorbing landing gear for a surveying and mapping UAV for surveying and mapping geographic information according to claim 1 is characterized by: The buffer assembly includes a sleeve (6), the lower ends of the sleeves (6) are hinged on both sides of the connecting rod (11), the round rod of the connecting rod (3) is inserted into each sleeve (6), the outer end hinge block of each connecting rod (3) is hinged to the corresponding connecting rod (2), each sleeve (6) fixes one end of the spring (4), the other end of each spring (4) is fixedly connected to the outer end hinge block of the connecting rod (3), and each spring (4) is respectively sleeved on the corresponding sleeve (6) and the round rod of the connecting rod (3).

3. The shock-absorbing landing gear for a surveying and mapping UAV for surveying and mapping geographic information according to claim 2 is characterized by: When the UAV support platform (1) is parallel to the ground, the angle between the axis of the sleeve (6) and the ground is 30 degrees.

4. The shock-absorbing landing gear for a surveying and mapping UAV for surveying and mapping geographic information according to claim 3 is characterized by: One side of the second connecting rod (11) is fixedly connected to a fixed shaft (16), the fixed shaft (16) is hingedly connected to the outer end of the moving rod (15), the circular shaft of the moving rod (15) is inserted into the limiting cylinder (13), the lower end of the limiting cylinder (13) is hingedly connected to a limiting block (8), and the limiting block (8) fixes the base (7).

5. The shock-absorbing landing gear for a surveying and mapping UAV for surveying and mapping geographic information according to claim 4 is characterized by: The lower part of the limiting cylinder (13) is fixed with a second spring (14), the upper end of the second spring (14) is fixed with the outer end of the moving rod (15), and the second spring (14) is encircled around the limiting cylinder (13) and the moving rod (15).

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