A vehicle-mounted UAV landing gear lifting and stabilizing device

Through the coordinated work of components such as multi-stage cylinders and lifting and stabilizing mechanisms, the stability problem of the vehicle-mounted UAV landing gear during the lifting process was solved, and the UAV's stable lifting and accurate take-off was achieved.

CN117922871BActive Publication Date: 2025-09-16JIANGXI AOXIANG XINGYUN TECH CO LTD
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Patent Information

Application Number
CN202410270879.5
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-03-11
Publication Date
2025-09-16
Estimated Expiration
2044-03-11

AI Technical Summary

Technical Problem

The existing vehicle-mounted drone landing gear device is difficult to ensure stability during the lifting process, and it is easy for external factors to cause the drone to deviate from the take-off position, affecting normal take-off.

Method used

The vehicle-mounted UAV landing gear lifting and stabilization device consists of a multi-stage cylinder, a connecting frame, a lifting component, a lifting and stabilizing mechanism, and a lifting and pulling mechanism. Through the coordinated work of components such as the connecting plate, rack frame, take-up wheel, and pull rope, the stable lifting and buffering of the landing frame is achieved, ensuring the stability of the UAV during takeoff.

Benefits of technology

The stability of the drone during lifting and lowering is improved, the shaking amplitude is reduced, and the drone can be ensured to take off accurately and avoid direct impact damage.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present invention relates to the technical field of drone landing gear, and in particular to a vehicle-mounted drone landing gear lifting and stabilizing device. The present invention provides a vehicle-mounted drone landing gear lifting and stabilizing device that can reinforce and stabilize during the lifting process and further improve the drone lifting stability. A vehicle-mounted drone landing gear lifting and stabilizing device includes a base, a multi-stage cylinder, a connecting frame, a placement frame, a lifting assembly, and a lifting and stabilizing mechanism. The upper left side of the base is connected to the multi-stage cylinder, the upper end of the multi-stage cylinder telescopic rod is connected to the connecting frame, the placement frame is slidably connected to the connecting frame, the right part of the connecting frame is connected to the lifting assembly, and the connecting frame is provided with a lifting and stabilizing mechanism. The present invention drives the connecting plate to move by the upward movement of the connecting frame, so that the mounting frame drives the adjacent lifting kits to extend synchronously, so that both the front and rear sides of the connecting frame can be supported, reducing the shaking amplitude of the connecting frame during the lifting process and improving the lifting stability of the connecting frame.
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Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicle (UAV) landing gear, and in particular to a vehicle-mounted UAV landing gear lifting and stabilizing device. Background Art

[0002] The landing gear of a drone refers to the structural component that supports the drone when taking off and landing on the ground. It has the important functions of supporting the aircraft, reducing the landing impact, and providing a suspension device. When a vehicle-mounted drone takes off and lands, it needs to rely on a carrier vehicle as a carrier. The existing vehicle-mounted drone landing gear lifting and stabilization device generally drives the drone to a high altitude through simple lifting, allowing the drone to move to a suitable take-off altitude and avoid the drone being restricted by the carrier vehicle. However, the existing device is difficult to ensure the stability of the drone during the lifting process. During the lifting process, it is easy to shake due to external factors, causing the drone to deviate from the original take-off position, affecting the normal take-off of the drone.

[0003] Therefore, in order to solve the above problems, a vehicle-mounted UAV landing gear lifting and stabilization device is now developed, which can reinforce and stabilize the landing gear during the lifting process and further improve the lifting stability of the UAV. Summary of the Invention

[0004] In order to overcome the shortcomings of existing devices that are difficult to ensure the stable lifting of drones, and are easily shaken due to external factors during the lifting process, thereby causing the drone to deviate from the original take-off position and affecting the normal take-off of the drone, the present invention provides a vehicle-mounted drone landing gear lifting and stabilization device that can reinforce and stabilize the lifting process and further improve the lifting stability of the drone.

[0005] The technical solution of the present invention is: a vehicle-mounted unmanned aerial vehicle landing gear lifting and stabilization device, including a base, a multi-stage cylinder, a connecting frame, a placement frame, a lifting assembly, a lifting and stabilizing mechanism and a lifting and pulling mechanism. The multi-stage cylinder is connected to the upper left side of the base, the upper end of the multi-stage cylinder telescopic rod is connected to the connecting frame, the placement frame is slidably connected to the connecting frame, the right part of the connecting frame is connected to the lifting assembly, the connecting frame is provided with a lifting and stabilizing mechanism, and the lifting and stabilizing mechanism is provided with a lifting and pulling mechanism.

[0006] Furthermore, the lifting and stabilizing mechanism includes a lifting kit, a mounting frame and a connecting plate. The upper left side of the base is connected to a front-to-back symmetrical lifting kit, the top of each lifting kit is connected to a mounting frame, and a connecting plate is connected between the tops of the mounting frames, and the connecting plate is connected to the top of the connecting frame.

[0007] Furthermore, the lifting mechanism includes a rack rack, a first mounting seat, a take-up wheel, a gear, a pull rope and a lifting ear. The left side of the placement frame is connected to a front-to-back symmetrical rack rack, the rack rack is connected to a rib plate, the outer side of the upper part of the mounting frame is connected to the first mounting seat, the first mounting seat is rotatably connected to the take-up wheel, the inner side of the take-up wheel is connected to a gear meshing with the adjacent rack rack, a pull rope is wound around the take-up wheel, the upper side of the right part of the placement frame is connected to a front-to-back symmetrical lifting ear, and the pull ropes are connected to the adjacent lifting ears.

[0008] Furthermore, it also includes a buffer mechanism, which includes a mounting plate, a sleeve rod, a sliding rod, a spring, a fixed seat and a push rod. The lower sides of the front and rear parts of the connecting frame are connected to the mounting plates, the upper side of the left part of the mounting plate is connected to the sleeve rod, the sliding rods are slidably connected inside the sleeve rods, and the sliding rods are connected to the adjacent sleeve rods with springs. The upper side of the right part of the mounting plate is rotatably connected to the fixed seat, the lower part of the fixed seat is connected to the push rod, and the left side of the push rod is in contact with the right side of the adjacent sliding rod.

[0009] Furthermore, it also includes a supporting mechanism, which includes a fixed frame, a fixed oblique frame and a sliding member. The lower sides of the front and rear parts of the placement frame are connected to the fixed oblique frame, the outer sides of the installation frame are connected to the fixed frame, and the left sides of the fixed oblique frame are connected to the sliding member. The sliding member is slidably connected to the adjacent fixed frame.

[0010] Furthermore, it also includes a bracket mechanism, which includes a second mounting seat, an adjusting screw and a limit rod. The upper sides of the front and rear parts of the base are connected to the second mounting seat, the upper sides of the left and right parts of the second mounting seat are connected to the limit rod, the second mounting seat is slidably connected between the left and right symmetrical limit rods, the upper middle part of the lower second mounting seat is rotatably connected to the adjusting screw, and the adjusting screw is threadedly connected to the adjacent upper second mounting seat.

[0011] Furthermore, it also includes a wire pressing mechanism, which includes a mounting frame and a pressing member. The right side of the first mounting seat is connected to the mounting frame, and the mounting frame is slidably connected to the pressing member.

[0012] Furthermore, the lifting assembly includes a drive motor and a screw rod. The drive motor is connected to the lower right side of the connecting frame. The output shaft of the drive motor is set to face upward. The screw rod is connected to the output shaft of the drive motor. The screw rod is rotatably connected to the connecting frame.

[0013] Furthermore, the right side of the putter is a curved structure.

[0014] Furthermore, the adjusting screw rods are all provided with a screw handle.

[0015] The beneficial effects are: 1. The present invention drives the connecting plate to move by the upward movement of the connecting frame, so that the mounting frame drives the adjacent lifting kits to extend synchronously, so that both the front and rear sides of the connecting frame can be supported, reducing the shaking amplitude of the connecting frame during the lifting process and improving the lifting stability of the connecting frame.

[0016] 2. The present invention drives the placement frame to move upward and lift through the lifting assembly, so that the rack frame drives the gear to rotate, and the rotation of the gear drives the take-up wheel to rotate, so that the take-up wheel reels the pull rope, thereby maintaining the lifting and reinforcement of the placement frame for a period of time during the process of the placement frame being lifted upward, making the drone more stable during the ascent.

[0017] 3. The present invention squeezes the fixing seat through the lower right side of the placement rack, so that the fixing seat drives the push rod to flip upward, thereby causing the push rod to squeeze the right side of the sliding rod, and then the spring is compressed. The placement rack is relieved and buffered as a whole by the buffering force of the spring, thereby preventing the placement rack from being directly reset and damaged. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic diagram of the three-dimensional structure of the present invention.

[0019] Figure 2 It is a partial three-dimensional structural schematic diagram of the present invention.

[0020] Figure 3 It is a schematic diagram of the three-dimensional structure of the lifting and stabilizing mechanism of the present invention.

[0021] Figure 4 It is a schematic diagram of the three-dimensional structure of the lifting mechanism of the present invention.

[0022] Figure 5 It is a schematic diagram of the three-dimensional structure of the buffer mechanism of the present invention.

[0023] Figure 6 It is a partial cross-sectional three-dimensional structural diagram of the buffer mechanism of the present invention.

[0024] Figure 7 It is a schematic diagram of the three-dimensional structure of the support mechanism of the present invention.

[0025] Figure 8 It is a schematic diagram of the three-dimensional structure of the bracket mechanism of the present invention.

[0026] Figure 9 It is a schematic diagram of the three-dimensional structure of the wire pressing mechanism of the present invention.

[0027] Figure 10 It is a partial three-dimensional structural schematic diagram of the wire pressing mechanism of the present invention.

[0028] In the accompanying drawings: 1-base, 2-multi-stage cylinder, 3-connecting frame, 4-placing frame, 5-lifting assembly, 6-lifting and stabilizing mechanism, 61-lifting kit, 62-mounting frame, 63-connecting plate, 7-lifting mechanism, 71-rack frame, 72-first mounting seat, 73-take-up wheel, 74-gear, 75-pull rope, 76-lifting ear, 8-buffer mechanism, 81-mounting plate, 82-sleeve rod, 83-sliding rod, 84-spring, 85-fixed seat, 86-push rod, 9-support mechanism, 91-fixed frame, 92-fixed oblique frame, 93-sliding member, 10-bracket mechanism, 101-second mounting seat, 102-adjusting screw rod, 103-limiting rod, 11-wire pressing mechanism, 111-mounting frame, 112-down pressure member. DETAILED DESCRIPTION

[0029] The present invention will be described in detail below with reference to the accompanying drawings and specific embodiments.

[0030] A vehicle-mounted UAV landing gear lifting and stabilization device, such as Figure 1 and Figure 2 As shown, it includes a base 1, a multi-stage cylinder 2, a connecting frame 3, a placement frame 4, a lifting component 5, a lifting and stabilizing mechanism 6 and a lifting mechanism 7. The multi-stage cylinder 2 is connected to the upper left side of the base 1, and the telescopic rod of the multi-stage cylinder 2 is set to face upward. The upper end of the telescopic rod of the multi-stage cylinder 2 is connected to the connecting frame 3. The placement frame 4 for placing the drone is slidably connected to the connecting frame 3. The right part of the connecting frame 3 is connected to a lifting component 5 for driving the placement frame 4 to automatically lift and lower. The lifting component 5 includes a driving motor and a screw rod. The driving motor is connected to the lower right side of the connecting frame 3. The output shaft of the driving motor is set to face upward. The output shaft of the driving motor is connected to the screw rod, and the screw rod is rotatably connected to the connecting frame 3. The connecting frame 3 is provided with a lifting and stabilizing mechanism 6 for stabilizing the lifting of the placement frame 4. The lifting and stabilizing mechanism 6 is provided with a lifting mechanism 7 for lifting and reinforcing the suspended position on the right side of the placement frame 4.

[0031] When the lifting frame 4 is lifted up, the lifting stabilization mechanism 6 will stabilize the connecting frame 3 in the front and rear directions, and the lifting mechanism 7 will pull the suspended position on the right side of the placing frame 4 to ensure the overall stability of the placing frame 4, avoid violent shaking during the lifting of the placing frame 4, and improve the stability of the drone's take-off operation.

[0032] like Figure 1 and Figure 3 As shown, the lifting and stabilizing mechanism 6 includes a lifting kit 61, a mounting frame 62 and a connecting plate 63. The upper left side of the base 1 is connected to the front and rear symmetrical lifting kits 61, the tops of the lifting kits 61 are connected to the mounting frames 62, and the connecting plates 63 are connected between the tops of the mounting frames 62. The connecting plates 63 are connected to the top of the connecting frame 3.

[0033] It should be noted that when the multi-stage cylinder 2 is started and the connecting frame 3 begins to lift upward, as the connecting frame 3 moves upward, the connecting frame 3 will drive the connecting plate 63 to move upward synchronously. At this time, the connecting plate 63 will drive the front and rear mounting frames 62 to move upward, thereby causing the lifting kit 61 to begin to extend, and the mounting frame 62 is supported by the extension movement of the lifting kit 61, so that the connecting frame 3 can maintain stability during the lifting process. In summary, the upward movement of the connecting frame 3 drives the connecting plate 63 to move, so that the mounting frame 62 drives the adjacent lifting kits 61 to extend synchronously, so that both the front and rear sides of the connecting frame 3 can be supported, reducing the shaking amplitude of the connecting frame 3 during the lifting process, and improving the stability of the lifting of the connecting frame 3.

[0034] like Figure 1 and Figure 4As shown, the lifting mechanism 7 includes a rack rack 71, a first mounting seat 72, a take-up wheel 73, a gear 74, a pull rope 75 and a lifting ear 76. The left side of the placement frame 4 is connected to a front-to-back symmetrical rack rack 71, and a rib is connected to the rack rack 71. The outer side of the upper part of the mounting frame 62 is connected to the first mounting seat 72, and the first mounting seat 72 is rotatably connected to the take-up wheel 73. The inner side of the take-up wheel 73 is connected to a gear 74 that meshes with the adjacent rack rack 71. The take-up wheel 73 is wound with a pull rope 75 for lifting and reinforcing the placement frame 4. The upper right side of the placement frame 4 is connected to a front-to-back symmetrical lifting ear 76, and the pull rope 75 is connected to the adjacent lifting ear 76.

[0035] When the lifting lever 74 is in the upright position, the pull rope 75 is pulled up to lift the lifting eye 76, thereby providing support for the right side of the lifting lever 4, thereby preventing the right side of the lifting lever 4 from floating and causing a decrease in stability. At the same time, as the lifting lever 4 begins to lift up, the lifting lever 4 drives the rack rack 71 to move upward, thereby causing the rack rack 71 to contact with the gear 74. After the rack rack 71 contacts with the gear 74, as the rack rack 71 moves upward, the gear 74 begins to rotate, thereby causing the take-up wheel 73 to start rotating synchronously. When the take-up wheels 73 start rotating, the pull rope 75 is reeled in, so that the pull rope 75 is always kept taut, thereby preventing the pull rope 75 from loosening and causing the right side of the lifting lever 4 to lose its support. When the lifting lever 4 is lifted to more than half the height of the connecting frame 3, the drone is about to enter the take-off position, and the rack rack 71 is When the lifting assembly 5 is controlled, the rack 4 starts to slide downward and reset. At this time, with the cooperation of the rack 71 and the gear 74, the reeled rope 75 will be released, so that the rope 75 returns to the taut state. In summary, the lifting assembly 5 drives the rack 4 to move upward and lift, so that the rack 71 drives the gear 74 to rotate, and the rotation of the gear 74 drives the take-up wheel 73 to rotate, so that the take-up wheel 73 rewinds the rope 75, thereby maintaining the lifting and reinforcement of the rack 4 for a period of time during the upward lifting of the rack 4, making the drone more stable during the ascent.

[0036] like Figure 1 、 Figure 5 and Figure 6As shown, a buffer mechanism 8 is also included, which includes a mounting plate 81, a sleeve rod 82, a sliding rod 83, a spring 84, a fixed seat 85 and a push rod 86. The lower sides of the front and rear parts of the connecting frame 3 are connected to the mounting plate 81, the upper left side of the mounting plate 81 is connected to the sleeve rod 82, the sliding rod 83 is slidably connected inside the sleeve rod 82, and the sliding rod 83 is connected to the adjacent sleeve rod 82 with a spring 84 for buffering. The upper right side of the mounting plate 81 is rotatably connected to the fixed seat 85, and the lower part of the fixed seat 85 is connected to the push rod 86 for pushing the sliding rod 83. The right side of the push rod 86 is a curved surface structure, and the left side of the push rod 86 is in contact with the right side of the adjacent sliding rod 83.

[0037] The cam 85 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83, and the cam 86 is pressed against the bottom edge of the support 83,

[0038] like Figure 1 and Figure 7 As shown, it also includes a support mechanism 9, which includes a fixed frame 91, a fixed oblique frame 92 and a sliding member 93. The lower sides of the front and rear parts of the placement frame 4 are connected to the fixed oblique frame 92 for improving the bearing capacity of the placement frame 4. The outer side of the mounting frame 62 is connected to the fixed frame 91, and the left side of the fixed oblique frame 92 is connected to the sliding member 93. The sliding member 93 is slidably connected to the adjacent fixed frame 91.

[0039] It should be noted that when the placement rack 4 is raised or lowered, it will drive the fixed inclined rack 92 to move synchronously, so that the sliding members 93 all slide along the adjacent fixed racks 91, and during the raising and lowering process of the placement rack 4, the placement rack 4 is supported by the fixed inclined rack 92.

[0040] like Figure 1 and Figure 8As shown, it also includes a bracket mechanism 10, the bracket mechanism 10 includes a second mounting seat 101, an adjusting screw rod 102 and a limiting rod 103, the front and rear upper sides of the base 1 are connected to the second mounting seat 101, the left and right upper sides of the second mounting seat 101 are connected to the limiting rod 103, and the left and right symmetrical limiting rods 103 are slidably connected with the second mounting seat 101, the upper second mounting seat 101 is used to support the mounting plate 81, and the middle upper side of the lower second mounting seat 101 is rotatably connected to the adjusting screw rod 102, the adjusting screw rod 102 is provided with a screw handle, and the adjusting screw rod 102 is threadedly connected to the adjacent upper second mounting seat 101.

[0041] It should be noted that in order to avoid the right part of the mounting plate 81 being in a suspended state without support, the second mounting seat 101 on the upper side is adjusted by rotating the adjusting screw 102, so that the second mounting seat 101 on the upper side can adjust the support position to ensure that the second mounting seat 101 on the upper side can be fitted with the mounting plate 81, thereby achieving the supporting effect on the mounting plate 81.

[0042] like Figure 1 、 Figure 9 and Figure 10 As shown, it also includes a wire pressing mechanism 11, which includes a mounting frame 111 and a pressing member 112. The right side of the first mounting seat 72 is connected to the mounting frame 111, and the mounting frame 111 is slidably connected to the pressing member 112 for pressing the adjacent pull rope 75.

[0043] It should be noted that by sliding the pressing member 112 to squeeze the adjacent pull ropes 75, the corresponding pull ropes 75 can always be kept taut, preventing the pull ropes 75 from loosening due to unexpected reasons, resulting in a weakening of the pulling and reinforcing ability of the placement rack 4.

[0044] The above description is merely a specific embodiment of the present invention, but the scope of protection of the present invention is not limited thereto. Any modifications or substitutions that can be easily conceived by a person skilled in the art within the technical scope disclosed in the present invention should be included within the scope of protection of the present invention. Therefore, the scope of protection of the present invention should be based on the scope of protection of the claims.

Claims

1. A vehicle-mounted UAV landing gear lifting and stabilization device, characterized by: The utility model comprises a base (1), a multi-stage cylinder (2), a connecting frame (3), a placement frame (4), a lifting component (5), a lifting and stabilizing mechanism (6) and a lifting and pulling mechanism (7), wherein the upper left side of the base (1) is connected to the multi-stage cylinder (2), the upper end of the telescopic rod of the multi-stage cylinder (2) is connected to the connecting frame (3), the placement frame (4) is slidably connected to the connecting frame (3), the right side of the connecting frame (3) is connected to the lifting component (5) for driving the placement frame (4) to automatically lift, the connecting frame (3) is provided with a lifting and stabilizing mechanism (6) for stabilizing the lifting of the placement frame (4), and the lifting and stabilizing mechanism (6) is provided with a lifting and pulling mechanism (7) for lifting and reinforcing the suspended position of the right side of the placement frame (4); The lifting and stabilizing mechanism (6) includes a lifting kit (61), a mounting frame (62) and a connecting plate (63). The upper left side of the base (1) is connected to the lifting kit (61) which is symmetrical in front and back. The tops of the lifting kits (61) are connected to the mounting frames (62). The tops of the mounting frames (62) are connected to the connecting plates (63). The connecting plates (63) are connected to the tops of the connecting frames (3). The lifting mechanism (7) includes a rack rack (71), a first mounting seat (72), a take-up wheel (73), a gear (74), a pull rope (75) and a lifting lug (76). The left side of the placement frame (4) is connected to a front-back symmetrical rack rack (71), the rack rack (71) is connected to a rib plate, the outer side of the upper portion of the mounting frame (62) is connected to the first mounting seat (72), the first mounting seat (72) is rotatably connected to the take-up wheel (73), the inner side of the take-up wheel (73) is connected to a gear (74) meshing with the adjacent rack rack (71), a pull rope (75) is wound around the take-up wheel (73), the upper side of the right portion of the placement frame (4) is connected to a front-back symmetrical lifting lug (76), and the pull rope (75) is connected to the adjacent lifting lug (76); The buffer mechanism (8) is also included. The buffer mechanism (8) includes a mounting plate (81), a sleeve rod (82), a sliding rod (83), a spring (84), a fixed seat (85) and a push rod (86). The lower sides of the front and rear parts of the connecting frame (3) are connected to the mounting plate (81). The upper left side of the mounting plate (81) is connected to the sleeve rod (82). The sleeve rod (82) is slidably connected to the sliding rod (83). The sliding rod (83) is connected to the adjacent sleeve rod (82) with a spring (84). The upper right side of the mounting plate (81) is rotatably connected to the fixed seat (85). The lower part of the fixed seat (85) is connected to the push rod (86). The right side of the push rod (86) is a curved surface structure. The left side of the push rod (86) is in contact with the right side of the adjacent sliding rod (83). The invention also includes a support mechanism (9), which includes a fixed frame (91), a fixed oblique frame (92) and a sliding member (93). The lower sides of the front and rear parts of the placement frame (4) are connected to the fixed oblique frame (92), the outer sides of the installation frame (62) are connected to the fixed frame (91), and the left sides of the fixed oblique frame (92) are connected to the sliding member (93). The sliding member (93) is slidably connected to the adjacent fixed frame (91).

2. The vehicle-mounted UAV landing gear lifting and stabilization device according to claim 1, characterized in that: The bracket mechanism (10) further comprises a second mounting seat (101), an adjusting screw rod (102) and a limiting rod (103); the upper sides of the front and rear parts of the base (1) are both connected to the second mounting seat (101); the upper sides of the left and right parts of the second mounting seat (101) are both connected to the limiting rod (103); the upper side of the middle part of the lower second mounting seat (101) is rotatably connected to the adjusting screw rod (102); and the adjusting screw rod (102) is threadedly connected to the adjacent upper second mounting seat (101).

3. The vehicle-mounted UAV landing gear lifting and stabilization device according to claim 2, characterized in that: The invention also includes a wire pressing mechanism (11), which includes a mounting frame (111) and a pressing member (112). The right side of the first mounting seat (72) is connected to the mounting frame (111), and the mounting frame (111) is slidably connected to the pressing member (112).

4. The vehicle-mounted UAV landing gear lifting and stabilization device according to claim 3, characterized in that: The lifting assembly (5) includes a drive motor and a screw rod. The drive motor is connected to the lower right side of the connecting frame (3). The output shaft of the drive motor is set to face upward. The screw rod is connected to the output shaft of the drive motor. The screw rod is rotatably connected to the connecting frame (3).

5. The vehicle-mounted UAV landing gear lifting and stabilization device according to claim 4, characterized in that: The adjusting screw rod (102) is provided with a screw handle.

Citation Information

Patent Citations

  • Auxiliary take-off device of unmanned aerial vehicle

    CN111392058A

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