A vehicle-mounted UAV landing gear sliding adjustment and positioning device
By designing a sliding adjustment and positioning device for the vehicle-mounted UAV landing gear, and using components such as adjustment and moving mechanisms to achieve automatic and precise positioning of the UAV landing, the problem of adjusting the UAV landing position is solved, and the operational convenience and safety are improved.
Patent Information
- Application Number
- CN202410441126.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2024-04-12
- Publication Date
- 2025-09-12
- Estimated Expiration
- 2044-04-12
AI Technical Summary
Existing drones are difficult to accurately return to their initial position when landing, and the carrying platform is difficult to adjust the landing position with the drone, which makes operation more difficult for operators.
A sliding adjustment and positioning device for the landing gear of a vehicle-mounted UAV is designed, which includes an adjustment mechanism, a moving mechanism, a return mechanism, an anti-slip mechanism and a support mechanism. Components such as a drive motor, a distance sensor and a motor are used to achieve automatic position adjustment and fixation.
It realizes the automatic precise matching and stable fixation of the UAV landing position, reduces the difficulty of operation, and improves the convenience and safety of UAV use.
Smart Images

Figure CN118306597B_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the field of unmanned aerial vehicle (UAV) landing gear, and in particular to a sliding adjustment and positioning device for a vehicle-mounted UAV landing gear. Background Art
[0002] The landing gear of a drone is similar to that of a manned aircraft, but may differ in design and structure, depending on the type, size, and purpose of the drone. When landing, the drone needs to rely on the landing gear for support and cushioning. After taking off, the drone needs to return to the original take-off position. However, for existing drones, it is difficult to accurately return to the initial position, and the existing carrying platform is also difficult to cooperate with the drone to adjust the landing position, which makes the operation more difficult for the operator.
[0003] Therefore, in order to solve the above problems, a vehicle-mounted UAV landing gear sliding adjustment and positioning device is developed to facilitate automatic position adjustment in conjunction with the UAV landing. Summary of the Invention
[0004] In order to overcome the shortcomings of existing devices that make it difficult for drones to accurately return to their initial positions when landing, and that existing carrying platforms are difficult to adjust the landing positions of drones, which increases the difficulty of operation for operators, the present invention provides a vehicle-mounted drone landing gear sliding adjustment and positioning device that is convenient for automatic position adjustment when landing drones.
[0005] The technical solution of the present invention is as follows: A sliding adjustment and positioning device for a vehicle-mounted UAV landing gear includes a base plate, a sliding member is slidingly connected to the base plate, a mounting plate is rotatably connected to the upper part of the sliding member, a placement plate for placing and supporting the UAV is rotatably connected to the upper left side of the mounting plate, and an adjustment mechanism for adjusting the placement plate at multiple angles is provided on the sliding member.
[0006] Preferably, the adjustment mechanism includes gears, the left part of the mounting plate is rotatably connected to a rotating shaft, the right part of the mounting plate is connected to a drive motor, the output shaft of the drive motor is set to face downward, and there are four gears in total, two of which are fixedly mounted on the sliding member and the placement plate respectively, and the other two gears are respectively mounted on the rotating shaft and the output shaft of the drive motor, and a pulley assembly is connected between the rotating shaft and the output shaft of the drive motor.
[0007] Preferably, a moving mechanism is also included, the moving mechanism including a landing gear, the landing gear is placed on the placement plate, the four front, rear, left and right parts of the landing gear are connected with distance sensors for sensing distance data, and corresponding convex plates are also provided at corresponding positions on the placement plate, the front and rear parts of the landing gear are connected with four left-right symmetrical first fixing parts, the first fixing parts are rotatably connected with moving rods for assisting the movement of the landing gear, the moving rods and adjacent first fixing parts are connected with rotating components, the front and rear sides of the landing gear are connected with left-right symmetrical second fixing parts, the second fixing parts are located on the outside of the adjacent first fixing parts, the front and rear symmetrical second fixing parts are also rotatably connected with the moving rods, and the moving rods and adjacent second fixing parts are also connected with the rotating components.
[0008] Preferably, a return mechanism is also included, the return mechanism includes a drive motor, the drive motor is connected to the lower left side of the base plate by bolts, the output shaft of the drive motor is set to face right, a screw is connected to the output shaft of the drive motor, the lower side and the right side of the base plate are both connected to bearing seats, the screw is rotatably connected to the bearing seat, and the screw is threadedly connected to the sliding member.
[0009] Preferably, an anti-skid mechanism is further included, the anti-skid mechanism including a rotating frame, the left and right parts of the landing gear are both rotatably connected to the rotating frame, the left and right parts of the landing gear are correspondingly connected to fixed rings, the fixed rings are both located on the front sides of adjacent rotating frames, a torsion spring is connected between the rotating frame and the adjacent fixed rings, two left-right symmetrical conical parts are connected to the placement plate, and the rotating frame is connected to a fixed column pushed by the adjacent conical parts.
[0010] Preferably, a support mechanism is further included, wherein the support mechanism includes a support frame, the support frame is connected to the mounting plate, and two rolling rods in contact with the base plate are rotatably connected to the front and rear sides of the support frame.
[0011] Preferably, a blocking component is further included, and each of the rotating components is connected to the blocking component for dust protection.
[0012] Preferably, the pulley assembly includes two pulleys and a transmission belt, the pulleys are connected to the lower part of the rotating shaft and the output shaft of the driving motor, and the transmission belt is wound between the pulleys.
[0013] Preferably, the rotating components include a motor and a transmission wheel, the motor is installed on the inner side of the first fixing member by means of a connecting plate, and the transmission wheels that mesh with each other are connected to corresponding positions of the motor output shaft and the moving rod.
[0014] Preferably, both the left and right parts of the screw rod are provided with limiting rings for limiting the sliding member.
[0015] By adopting the above technical solution, the beneficial effects of the present invention are:
[0016] 1. The present invention relies on the automation performance of the drive motor to enable the placement plate and the mounting plate to be automatically rotated and adjusted, respectively, with the sliding member and the rotating shaft as the center of the circle, so as to quickly match the landing point of the drone. Compared with traditional technologies, the drone no longer needs to perform precise fixed-point landing, which improves the convenience of using the drone.
[0017] 2. The distance sensor of the present invention detects the corresponding convex plate on the placement plate to calculate whether the UAV landing gear is in the correct position. When the distance sensor detects that there is a certain error in the data information, the distance sensors on the left and right sides will correspondingly start the rotating components on the first fixing part, and the sensors on the front and rear sides will correspondingly start the rotating components on the second fixing part. In this way, the final position of the landing gear is automatically adjusted so that the landing gear can be located in the correct parking position, thereby improving the convenience of operation. 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 structural schematic diagram of the adjustment mechanism of the present invention.
[0020] Figure 3 It is a partial three-dimensional structural schematic diagram of the adjustment mechanism of the present invention.
[0021] Figure 4 It is a schematic diagram of the three-dimensional structure of the moving mechanism of the present invention.
[0022] Figure 5 It is a schematic diagram of the three-dimensional structure of the return mechanism of the present invention.
[0023] Figure 6 It is a schematic diagram of the three-dimensional structure of the anti-slip 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 partial three-dimensional structural schematic diagram of the present invention.
[0026] Explanation of the accompanying drawings: 1_base plate, 2_sliding member, 3_mounting plate, 4_placing plate, 5_adjusting mechanism, 51_gear, 52_rotating shaft, 53_driving motor, 54_pulley assembly, 6_moving mechanism, 61_landing gear, 62_distance sensor, 63_first fixing member, 64_rotating assembly, 65_moving rod, 66_second fixing member, 7_returning mechanism, 71_driving motor, 72_screw rod, 73_bearing seat, 8_anti-slip mechanism, 81_rotating frame, 82_fixing ring, 83_torsion spring, 84_fixing column, 85_conical member, 9_support mechanism, 91_support frame, 92_rolling rod, 10_blocking assembly. DETAILED DESCRIPTION
[0027] The present invention will be further described below with reference to the accompanying drawings and specific embodiments.
[0028] Example 1
[0029] A vehicle-mounted UAV landing gear sliding adjustment and positioning device, such as Figure 1 As shown, it includes base plates 1, 1 and 2, a sliding member 2 is slidably connected to the base plate 1, the upper part of the sliding member 2 is rotatably connected to a mounting plate 3, the upper left side of the mounting plate 3 is rotatably connected to a placement plate 4 for placing and supporting the drone, and the sliding member 2 is provided with an adjustment mechanism 5 for adjusting the placement plate 4 at multiple angles.
[0030] It should be noted that after the drone takes off, it needs to return to the original take-off position. However, for existing drones to land, it is difficult to return to the initial position accurately. Therefore, when the drone is landing, this device can be used to receive the drone. First, the sliding part 2 sliding on the bottom plate 1 is used to adjust the overall position of the placement plate 4. Then, the adjustment mechanism 5 is controlled to operate according to the landing state of the drone, so that the adjustment mechanism 5 drives the placement plate 4 to perform corresponding rotation adjustment, so that the position of the placement plate 4 can match the final landing position of the drone, thereby achieving the effect of automatically adjusting the receiving position.
[0031] like Figure 1-Figure 3 As shown, the adjusting mechanism 5 includes a gear 51, a rotating shaft 52 is rotatably connected to the left part of the mounting plate 3, and a driving motor 53 is connected to the right part of the mounting plate 3. The output shaft of the driving motor 53 is set to face downward. There are four gears 51, two of which are fixedly mounted on the sliding member 2 and the placement plate 4 respectively, and the other two gears 51 are respectively mounted on the rotating shaft 52 and the output shaft of the driving motor 53. A pulley assembly 54 is connected between the rotating shaft 52 and the output shaft of the driving motor 53. The pulley assembly 54 includes two pulleys and a transmission belt. Pulleys are connected to the lower part of the rotating shaft 52 and the output shaft of the driving motor 53, and a transmission belt is wound around the pulleys.
[0032] It should be noted that when the drone is landing, in order to ensure that the placement plate 4 can be accurately aligned with the final landing point of the drone, the drive motor 53 can be controlled so that the output shaft of the drive motor 53 starts to rotate, thereby causing the output shaft of the drive motor 53 to drive the pulley assembly 54 to operate. At this time, the two gears 51 on the right will begin to interact with each other, so that the mounting plate 3 starts to move in a circular motion with the sliding member 2 as the center. At the same time, under the action of the pulley assembly 54, the two gears 51 on the left will also begin to interact with each other, so that the placement plate 4 rotates accordingly. During this rotation process, the placement plate 4 can always remain relatively stationary, so that the display angle of the placement plate 4 will not change, which is convenient for matching and docking with the landing point of the drone.
[0033] like Figure 1 and Figure 4 As shown, the mobile mechanism 6 is also included. The mobile mechanism 6 includes a landing gear 61. The landing gear 61 is placed on the placement plate 4. The four parts of the landing gear 61, front, back, left, and right, are connected to distance sensors 62 for sensing distance data. Corresponding convex plates are also provided at corresponding positions on the placement plate 4. The front and back parts of the landing gear 61 are connected to four left-right symmetrical first fixing members 63. The first fixing members 63 are rotatably connected to a moving rod 65 for assisting the landing gear 61 to move. The moving rod 65 is connected to the adjacent first fixing member 63. The rotating assembly 64 and the front and rear sides of the landing gear 61 are connected with left-right symmetrical second fixing parts 66, and the second fixing parts 66 are located on the outside of the adjacent first fixing parts 63. The front and rear symmetrical second fixing parts 66 are also rotatably connected with a moving rod 65, and the moving rod 65 and the adjacent second fixing parts 66 are also connected with a rotating assembly 64. The rotating assembly 64 includes a motor and a transmission wheel. The motor is installed on the inner side of the first fixing part 63 by means of a connecting plate, and the corresponding positions of the motor output shaft and the moving rod 65 are connected with mutually meshing transmission wheels.
[0034] It should be noted that the landing gear 61 is directly installed on the drone. After the drone completes landing, the distance sensor 62 is used to detect the corresponding protruding plate on the placement plate 4 to calculate whether the drone landing gear 61 is in the correct position. When the distance sensor 62 detects that there is a certain error in the data information, the distance sensors 62 on the left and right sides will correspondingly start the rotating components 64 on the first fixing part 63, and the sensors on the front and rear sides will correspondingly start the rotating components 64 on the second fixing part 66. After the rotating components 64 on the first fixing part 63 are started, they will drive the front and rear moving rods 65 to rotate, thereby causing the landing gear 61 to move in the left and right directions. After the transmission components on the second fixing part 66 are started, they will drive the left and right moving rods 65 to rotate, thereby causing the landing gear 61 to move in the front and rear directions. In this way, the final position of the landing gear 61 is automatically adjusted so that the landing gear 61 can be located in the correct parking position, thereby improving the convenience of operation.
[0035] Example 2
[0036] On the basis of Example 1, Figure 1 and Figure 5 As shown, it also includes a return mechanism 7, which includes a drive motor 71. The drive motor 71 is connected to the lower left side of the base plate 1 by bolts. The output shaft of the drive motor 71 is set to face right. The output shaft of the drive motor 71 is connected to a screw rod 72. The lower side and the right side of the base plate 1 are both connected to a bearing seat 73. The screw rod 72 is rotatably connected to the bearing seat 73, and the screw rod 72 is threadedly connected to the sliding member 2. The left and right parts of the screw rod 72 are both provided with limit rings for limiting the sliding member 2.
[0037] It should be noted that when the drone operation is completed, in order to effectively store the placement plate 4, the drive motor 71 can be started. The rotation of the output shaft of the drive motor 71 will drive the screw 72 to rotate, so that the sliding member 2 slides along the bottom plate 1, thereby achieving the effect of driving the placement plate 4 back to the original position.
[0038] like Figure 1 and Figure 6 As shown, an anti-skid mechanism 8 is also included, and the anti-skid mechanism 8 includes a rotating frame 81. The left and right parts of the landing gear 61 are rotatably connected to the rotating frame 81. The left and right parts of the landing gear 61 are correspondingly connected to fixed rings 82. The fixed rings 82 are located in front of adjacent rotating frames 81. Torsion springs 83 are connected between the rotating frames 81 and the adjacent fixed rings 82. Two left-right symmetrical conical parts 85 are connected to the placement plate 4, and the rotating frames 81 are connected to fixed columns 84 pushed by adjacent conical parts 85.
[0039] It should be noted that when the drone drives the landing gear 61 to stop on the placement plate 4, the position of the landing gear 61 may not be the exact position at this time, so the landing gear 61 will start to automatically adjust its position. During the adjustment process, the fixed column 84 will be affected by the adjacent conical part 85, thereby causing the rotating frame 81 to begin to flip outward, and the torsion spring 83 will be deformed under force, thereby causing the outer side of the rotating frame 81 to contact the placement plate 4, increasing the friction between the landing gear 61 and the placement plate 4, and preventing the drone from accidentally sliding after docking.
[0040] like Figure 1 and Figure 7 As shown, it also includes a support mechanism 9, which includes a support frame 91. The support frame 91 is connected to the mounting plate 3, and two rolling rods 92 in contact with the base plate 1 are rotatably connected to the front and rear sides of the support frame 91.
[0041] It should be noted that as the mounting plate 3 begins to move in a circle with the sliding member 2 as the center, the support frame 91 will drive the rolling rod 92 to move continuously, so that the rolling rod 92 can continuously adjust the contact position with the base plate 1, so that the mounting plate 3 can always be supported, thereby improving the load-bearing stability of the mounting plate 3.
[0042] like Figure 1 and Figure 8 As shown, a blocking component 10 is also included, and each rotating component 64 is connected to a blocking component 10 for dust protection.
[0043] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and are not intended to limit the scope of protection of the present invention. Although the present invention has been described in detail with reference to preferred embodiments, those skilled in the art should understand that the technical solutions of the present invention may be modified or replaced by equivalents without departing from the essence and scope of the technical solutions of the present invention.
Claims
1. A vehicle-mounted UAV landing gear sliding adjustment and positioning device, characterized in that: The invention comprises a bottom plate (1), a sliding member (2) is slidably connected to the bottom plate (1), a mounting plate (3) is rotatably connected to the upper portion of the sliding member (2), a placement plate (4) for placing and supporting a drone is rotatably connected to the upper left side of the mounting plate (3), and an adjustment mechanism (5) for adjusting the placement plate (4) at multiple angles is provided on the sliding member (2); The adjusting mechanism (5) includes a gear (51), the left portion of the mounting plate (3) is rotatably connected to a rotating shaft (52), the right portion of the mounting plate (3) is connected to a driving motor (53), the output shaft of the driving motor (53) is arranged to face downward, there are four gears (51), two of which are fixedly mounted on the sliding member (2) and the placement plate (4), respectively, and the other two gears (51) are mounted on the rotating shaft (52) and the output shaft of the driving motor (53), respectively, and a pulley assembly (54) is connected between the rotating shaft (52) and the output shaft of the driving motor (53); The mobile mechanism (6) includes a landing gear (61), the landing gear (61) is placed on the placement plate (4), and the landing gear (61) is connected to four positions, front, back, left, and right, of the landing gear (61) with distance sensors (62) for sensing distance data. The placement plate (4) is also provided with corresponding convex plates at corresponding positions. The front and back sides of the landing gear (61) are connected to two left-right symmetrical first fixing members (63), and the first fixing members (63) are rotatably connected to each other to assist the landing gear (61) in moving. A movable rod (65), a rotating assembly (64) is connected between the movable rod (65) and the adjacent first fixing member (63), and the front and rear sides of the landing gear (61) are connected to left-right symmetrical second fixing members (66), the second fixing members (66) are located outside the adjacent first fixing member (63), and the movable rod (65) is also rotatably connected between the front and rear symmetrical second fixing members (66), and the rotating assembly (64) is also connected between the movable rod (65) and the adjacent second fixing member (66); The invention also includes a return mechanism (7), wherein the return mechanism (7) includes a drive motor (71), the drive motor (71) is connected to the lower left side of the base plate (1) by a bolt, the output shaft of the drive motor (71) is set to face right, and the output shaft of the drive motor (71) is connected to a screw rod (72), the lower side and the right side of the base plate (1) are both connected to a bearing seat (73), the screw rod (72) is rotatably connected to the bearing seat (73), and the screw rod (72) is threadedly connected to the sliding member (2).
2. The sliding adjustment and positioning device for a vehicle-mounted UAV landing gear according to claim 1, characterized in that: The invention also includes an anti-skid mechanism (8), wherein the anti-skid mechanism (8) includes a rotating frame (81), and the left and right parts of the landing gear (61) are both rotatably connected to the rotating frame (81), and the left and right parts of the landing gear (61) are respectively connected to fixed rings (82), and the fixed rings (82) are both located in front of the adjacent rotating frames (81). A torsion spring (83) is connected between the rotating frame (81) and the adjacent fixed ring (82), and the placement plate (4) is connected to two left-right symmetrical conical members (85), and the rotating frame (81) is connected to a fixed column (84) pushed by the adjacent conical members (85).
3. The sliding adjustment and positioning device for a vehicle-mounted UAV landing gear according to claim 2, characterized in that: The invention also includes a support mechanism (9), wherein the support mechanism (9) includes a support frame (91), the support frame (91) is connected to the mounting plate (3), and the support frame (91) is rotatably connected to a rolling rod (92) in contact with the bottom plate (1) on both the front and rear sides.
4. The sliding adjustment and positioning device for a vehicle-mounted UAV landing gear according to claim 3, characterized in that: It also includes a blocking component (10), and each of the rotating components (64) is connected to the blocking component (10) for dustproof shielding.
5. The sliding adjustment and positioning device for a vehicle-mounted UAV landing gear according to claim 4, characterized in that: The pulley assembly (54) includes two pulleys and a transmission belt. The pulleys are connected to the lower part of the rotating shaft (52) and the output shaft of the driving motor (53), and the transmission belt is wound between the pulleys.
6. The sliding adjustment and positioning device for a vehicle-mounted UAV landing gear according to claim 5, characterized in that: The rotating assembly (64) includes a motor and a transmission wheel. The motor is mounted on the inner side of the first fixing member (63) by means of a connecting plate. The motor output shaft and the movable rod (65) are connected to the transmission wheels at corresponding positions thereof.
7. The sliding adjustment and positioning device for a vehicle-mounted UAV landing gear according to claim 6, characterized in that: The left and right sides of the screw rod (72) are both provided with limiting rings for limiting the position of the sliding member (2).
Citation Information
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