Modularized vehicle-mounted unmanned aerial vehicle flying platform and vehicle

Abstract

The invention relates to the technical field of vehicle-mounted unmanned aerial vehicles, and provides a modular vehicle-mounted unmanned aerial vehicle releasing platform and a vehicle. The modular vehicle-mounted unmanned aerial vehicle releasing platform comprises a parking apron, a clamping system and a lifting system; the lifting system is detachably arranged at the bottom of the parking apron and used for lifting the parking apron; the clamping system comprises two driving motors and four reduction gearboxes which are detachably arranged at the bottom of the parking apron, the reduction gearboxes at the two ends of a longitudinally-arranged transmission shaft are each provided with a transverse lead screw, the reduction gearboxes at the two ends of a transversely-arranged transmission shaft are each provided with a longitudinal lead screw, and the longitudinal lead screws and the transverse lead screws are each provided with threads with the two ends opposite in direction. The two transverse screw rods are connected with two longitudinal clamping bars arranged above the parking apron; and the two longitudinal screw rods are connected with two transverse clamping bars arranged above the parking apron. The unmanned aerial vehicle flying platform can be quickly mounted and dismounted through the modular design.

Description

Technical Field

[0001] The present invention relates to the technical field of vehicle-mounted unmanned aerial vehicles, and in particular to a modular vehicle-mounted unmanned aerial vehicle launching platform and a vehicle. Background Art

[0002] The statements in this section merely provide background art related to the present invention and do not necessarily constitute prior art.

[0003] At present, the status of vehicle-mounted drone launch platforms shows the trend of technological progress and diversified applications. Vehicle-mounted drone launch platforms are not only more intelligent and integrated in design, but also have found practical application scenarios in multiple industries. Modern vehicle-mounted drone launch platforms are usually equipped with automatic take-off and landing systems, which can realize autonomous take-off and landing of drones and seamless docking with vehicles, which reduces the need for manual intervention and improves operational efficiency; with the help of GPS, inertial measurement unit (IMU), visual sensor and other technologies, vehicle-mounted drone launch platforms can provide accurate location information and flight path planning for drones. Through real-time data transmission, users can monitor the status of drones and mission execution in the car; some high-end models of launch platforms also have windproof, waterproof, low temperature resistance and other functions to ensure that drones can work normally in severe weather conditions.

[0004] However, most of the current vehicle-mounted drone launch platforms have the following defects:

[0005] Location limitations: Currently, most vehicle-mounted drone launch platforms are designed to be installed on the roof. Although this design can provide a relatively open take-off and landing space, it also brings many inconveniences. In addition, the roof platform may not be suitable for some large-sized or special-shaped vehicles, and there are safety hazards in roof operations under severe weather conditions (such as rain and snow). In addition, the roof requires the vehicle to be stopped before the drone can be safely operated, which increases the complexity and time cost of use.

[0006] Lack of universality: The same vehicle cannot be quickly transferred from one location to another for use, or modules cannot be shared between multiple vehicles, which increases R&D costs and cycles and reduces product standardization and market adaptability. Summary of the invention

[0007] In order to address the deficiencies in the prior art, the present invention provides a modular vehicle-mounted UAV launching platform and a vehicle, which achieves the clamping of the UAV through a clamping system, and the apron, the clamping system and the lifting system are detachably connected. The modular design enables the UAV launching platform to be quickly installed and disassembled without being restricted by location and without the need to stop the vehicle, and the UAV can be safely operated.

[0008] In order to achieve the above object, the present invention adopts the following technical solution:

[0009] A first aspect of the present invention provides a modular vehicle-mounted UAV launching platform.

[0010] A modular vehicle-mounted UAV launch platform, including a landing pad, a clamping system and a lifting system;

[0011] The lifting system is detachably arranged at the bottom of the apron and is used to raise and lower the apron;

[0012] The clamping system includes two driving motors and four reduction gearboxes detachably arranged at the bottom of the apron, each driving motor is connected to the two reduction gearboxes through a transmission shaft, the two transmission shafts are arranged vertically, the reduction gearboxes at both ends of the longitudinally arranged transmission shaft are equipped with a transverse screw rod, and the reduction gearboxes at both ends of the transversely arranged transmission shaft are equipped with a longitudinal screw rod, and the longitudinal screw rod and the transverse screw rod both have threads in opposite directions at both ends; the two transverse screw rods are connected to the two longitudinal clamping bars arranged above the apron, and the two longitudinal clamping bars are driven to move toward each other or relative to each other through the rotation of the transverse screw rods, so as to realize the clamping and release of the UAV in one dimension; the two longitudinal screw rods are connected to the two transverse clamping bars arranged above the apron, and the two transverse clamping bars are driven to move toward each other or relative to each other through the rotation of the longitudinal screw rods, so as to realize the clamping and release of the UAV in another dimension.

[0013] Furthermore, the lifting system includes four lifting screws and four electromagnetic fixing sleeves. The four electromagnetic fixing sleeves are detachably arranged at the four corners of the bottom of the apron. An electromagnetic fixing sleeve matching with it is sleeved on the outside of each lifting screw. The lifting screw is driven by the torque output by the driving motor and realizes linear motion by cooperating with the thread of the electromagnetic fixing sleeve, thereby causing the apron to rise and fall.

[0014] Furthermore, the transmission shaft is connected to the reduction gearbox via a coupling.

[0015] Furthermore, the ends of the transverse screw rod and the longitudinal screw rod away from the reduction box are detachably connected to the bottom of the apron through L-shaped fixing pieces.

[0016] Furthermore, the transverse screw rod is connected to the longitudinal clamping rod through a sliding part, and each transverse screw rod is configured with two symmetrically arranged sliding parts, and the sliding part includes a threaded sleeve and a V-shaped part. The threaded sleeve is sleeved on the outside of the transverse screw rod, and the V-shaped part connects the threaded sleeve and the longitudinal clamping rod. The transverse screw rod rotates, driving the threaded sleeve to move, and then driving the longitudinal clamping rod to move.

[0017] Furthermore, the longitudinal screw rod is connected to the transverse clamping rod through a sliding part, and each longitudinal screw rod is configured with two symmetrically arranged sliding parts, and the sliding part includes a threaded sleeve and a V-shaped part. The threaded sleeve is sleeved on the outside of the longitudinal screw rod, and the V-shaped part connects the threaded sleeve and the transverse clamping rod. The rotation of the longitudinal screw rod drives the threaded sleeve to move, and then drives the transverse clamping rod to move.

[0018] Furthermore, one end of the two transverse screw rods close to the reduction box connected thereto is connected to a longitudinal clamping rod; and one end of the two transverse screw rods away from the reduction box connected thereto is connected to another longitudinal clamping rod.

[0019] Furthermore, one end of the two longitudinal screw rods close to the reduction box connected thereto is connected to a transverse clamping rod; and one end of the two longitudinal screw rods away from the reduction box connected thereto is connected to another transverse clamping rod.

[0020] Furthermore, the two longitudinal clamping bars and the two transverse clamping bars form a rectangle parallel to the apron.

[0021] A second aspect of the present invention provides a vehicle, comprising a vehicle body and a modular vehicle-mounted UAV launching platform as described in the first aspect and arranged on the vehicle body.

[0022] Compared with the prior art, the present invention has the following beneficial effects:

[0023] 1. The modular vehicle-mounted UAV launch platform described in the present invention clamps the UAV through a clamping system, and the apron, clamping system and lifting system are detachably connected. The modular design enables the UAV launch platform to be quickly installed and disassembled without being restricted by location and without stopping the vehicle, and the UAV can be safely operated.

[0024] 2. The modular vehicle-mounted drone launch platform described in the present invention has a modular design that enables the drone launch platform to be quickly installed and disassembled, thereby: allowing the platform to be flexibly moved between different locations such as the roof, front cabin luggage box, and trunk, thereby improving the vehicle's space utilization efficiency and the adaptability of drone launches; ensuring that the drone launch platform is compatible with vehicles of different models and sizes, without the need to customize a dedicated platform for each model, reducing costs and improving versatility and scalability; without the need for complex tools or professional skills, greatly shortening the preparation and recovery time of the drone, and improving the efficiency of emergency response and mission execution; independent replacement and maintenance, without the need for large-scale transformation of the entire platform, which not only reduces maintenance costs, but also shortens maintenance time and improves the platform's availability; it can reduce the workload of repeated design, speed up the introduction of new products, and reduce costs due to standardized production. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] The drawings in the specification, which constitute a part of the present invention, are used to provide a further understanding of the present invention. The exemplary embodiments and descriptions of the present invention are used to explain the present invention and do not constitute improper limitations on the present invention.

[0026] Figure 1 This is a structural diagram of a modular vehicle-mounted UAV launch platform according to Embodiment 1 of the present invention;

[0027] Figure 2 It is a structural schematic diagram of a lifting system according to Embodiment 1 of the present invention;

[0028] Figure 3 A cross-sectional view of a driving structure of a lifting system according to Embodiment 1 of the present invention;

[0029] Figure 4 It is a cross-sectional view of the lifting structure of Example 1 of the present invention;

[0030] Figure 5 Schematic diagram of a clamping system according to Embodiment 1 of the present invention;

[0031] Figure 6 This is a cross-sectional view of the driving structure of the clamping system of Example 1 of the present invention. DETAILED DESCRIPTION

[0032] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0033] It should be noted that the following detailed descriptions are exemplary and are intended to provide further explanation of the present invention. Unless otherwise specified, all technical and scientific terms used herein have the same meanings as those commonly understood by those skilled in the art to which the present invention belongs.

[0034] It should be noted that the terms used herein are only for describing specific embodiments and are not intended to limit exemplary embodiments according to the present invention. As used herein, unless the context clearly indicates otherwise, the singular form is also intended to include the plural form. In addition, it should be understood that when the terms "comprising" and / or "including" are used in this specification, it indicates the presence of features, steps, operations, devices, components and / or combinations thereof.

[0035] In the present invention, terms such as "upper", "lower", "left", "right", "front", "back", "vertical", "horizontal", "side", "bottom", etc. indicate directions or positional relationships based on the directions or positional relationships shown in the accompanying drawings. They are relational words determined only for the convenience of describing the structural relationships of the various parts or elements of the present invention, and do not specifically refer to any part or element in the present invention and should not be understood as limitations on the present invention.

[0036] In the present invention, terms such as "fixed connection", "connected", "connection", etc. should be understood in a broad sense, indicating that it can be fixedly connected, integrally connected or detachably connected; it can be directly connected or indirectly connected through an intermediate medium. Relevant scientific research or technical personnel in this field can determine the specific meanings of the above terms in the present invention according to specific circumstances, and they should not be understood as limiting the present invention.

[0037] In the absence of conflict, the embodiments of the present invention and the features of the embodiments may be combined with each other.

[0038] Example 1

[0039] Embodiment 1 of the present invention provides a modular vehicle-mounted UAV launch platform.

[0040] This embodiment provides a modular vehicle-mounted UAV launch platform, such as Figure 1 As shown, it includes a base plate 1, a helipad 2, a lifting system 3 and a clamping system 4.

[0041] In this embodiment, the direction of the long side of the bottom plate 1 is the X-axis direction, the direction of the width is the Y-axis direction, and the direction of the vertical axis to the bottom plate 1 is the Z-axis direction.

[0042] like Figure 2 , Figure 3 and Figure 4 As shown, the lifting system 2 includes two first drive motors 32 , four first reduction gearboxes 33 , two first transmission shafts 34 , four lifting screw rods 36 , four electromagnetic fixing sleeves 31 and four first couplings 35 .

[0043] The four corners of the bottom plate 1 are respectively detachably connected to a first reduction box 33 . Specifically, threaded holes are provided at the four corners of the bottom plate 1 , and the first reduction box 33 is detachably connected to the bottom plate 1 by bolts.

[0044] Two first drive motors 32 are detachably connected to the base plate 1 . Every two first reduction gearboxes 33 and one first drive motor 32 are located on the same axis and parallel to the Y axis. The two first drive motors 32 are also detachably connected to the base plate 1 by bolts.

[0045] Each first drive motor 32 is connected to a first transmission shaft 34, which passes through the first drive motor 32 and is connected to a first reduction box 33 at both ends. Specifically, the end of the first transmission shaft 34 is connected to an output shaft (the output shaft in the Y-axis direction) of the first reduction box 33 through a first coupling 35. Figure 3 shown.

[0046] like Figure 4As shown, each first reduction box 33 is equipped with a lifting screw 36 in the Z-axis direction thereof, and the lifting screw 36 is provided with an electromagnetic fixing sleeve 31 matching therewith on the outside, and the electromagnetic fixing sleeve 31 can be detachably fixed to the bottom of the apron 2 .

[0047] like Figure 5 and Figure 6 As shown, the clamping system 4 includes four second couplings 47, eight sliding members 48, two second drive motors 49, four second reduction gearboxes 45, two second transmission shafts 46, two transverse screw rods 43, two longitudinal screw rods 44, two transverse clamping rods 41 and two longitudinal clamping rods 42.

[0048] The two second drive motors 49 are detachably arranged at the middle of the long side edge or the short side edge of the bottom surface of the apron 2 , and each second drive motor 49 is connected to a second transmission shaft 46 , and the second transmission shaft 46 passes through the second drive motor 49 .

[0049] For the second transmission shaft 46 connected to the second drive motor 49 arranged in the middle of the long side edge of the bottom surface of the apron 2, a second reduction box 45 is connected to its two ends respectively (the second transmission shaft 46 is connected to the X-direction output shaft of the second reduction box 45 through a second coupling 47), and each second reduction box 45 is equipped with a transverse screw 43 in its Y-axis direction.

[0050] For the second transmission shaft 46 connected to the second drive motor 49 arranged in the middle of the short side edge of the bottom surface of the apron 2, a second reduction box 45 is connected to its two ends respectively (the second transmission shaft 46 is connected to the Y-direction output shaft of the second reduction box 45 through a second coupling 47), and each second reduction box 45 is equipped with a longitudinal screw 44 in its X-axis direction.

[0051] The ends of the transverse screw rod 43 and the longitudinal screw rod 44 away from the reduction gear box are detachably connected to the bottom surface of the apron 2 through an L-shaped fixing piece. Specifically: a threaded hole is provided at one end of the L-shaped fixing piece to be fixedly connected to the bottom surface of the apron 2, and a limiting hole is provided at the other end. The ends of the transverse screw rod 43 and the longitudinal screw rod 44 away from the reduction gear box are arranged in the limiting hole.

[0052] Each transverse screw rod 43 is configured with two sliding members 48 , and each longitudinal screw rod 44 is also configured with two sliding members 48 .

[0053] The sliding member 48 includes a threaded sleeve and a shaped member. Specifically, the threaded sleeve includes a cylindrical sleeve with threads adapted to the transverse screw rod 43 and the longitudinal screw rod 44. A connecting block is fixed to the outside of the cylindrical sleeve, and the connecting block is parallel to the apron 2. The shaped member includes a horizontal block, a vertical block and an inclined block. The horizontal block is parallel to the apron 2, the vertical block is perpendicular to the apron 2, and the inclined block is connected between the horizontal block and the vertical block, and the inner angles of the horizontal block and the vertical block are large. At 90 degrees less than 180 degrees, the horizontal block, vertical block and oblique block are in the same plane (XZ or YZ plane), forming a component similar to the Chinese-Fang shape; the connecting block is connected to the end of the vertical block of the Chinese-Fang shape part and is perpendicular to the Chinese-Fang shape part, and the central axis of the cylindrical sleeve is parallel to the Chinese-Fang shape part; the horizontal block of the Chinese-Fang shape part is detachably connected to the horizontal clamping bar 41 or the longitudinal clamping bar 42. After connection, the horizontal clamping bar 41 or the longitudinal clamping bar 42 is perpendicular to the Chinese-Fang shape part.

[0054] Each transverse screw rod 43 is equipped with two symmetrically arranged sliding members 48, and each longitudinal screw rod 44 is also equipped with two symmetrically arranged sliding members 48. The end of the transverse block of the V-shaped member faces the edge of the apron.

[0055] The two sliding members 48 disposed at the same end of the two transverse screw rods 43 are detachably connected to a longitudinal clamping rod 42 ; the two sliding members 48 disposed at the same end of the two longitudinal screw rods 44 are detachably connected to a transverse clamping rod 41 .

[0056] After assembly, the base plate 1 is parallel to the apron 2, and the central axes coincide with each other.

[0057] The lifting system 2 is started, and the first drive motor 32 is started. By precisely controlling the synchronous movement of each component, the apron 2 is smoothly lifted until it reaches the preset height. Specifically, after power is turned on, the first drive motor 32 responds and starts to operate as a power source; the first drive motor 32 drives the first transmission shaft 34 to rotate, and through the coupling 35 (the main functions of the coupling are: transmitting torque, compensating for axial, radial or angular centering errors between the two shafts during actual installation, absorbing vibration and impact, ensuring the smooth operation of the two shafts, and facilitating connection and disassembly ) is transmitted to the first reduction box 33, that is, the torque generated by the first drive motor 32 is efficiently transmitted to the first reduction box 33 via the first transmission shaft 34 and the coupling 35, ensuring the continuity and stability of power transmission; the worm gear mechanism inside the first reduction box 33 accurately controls the conversion of torque, converts high-speed rotation into low-speed and high-torque output, and drives the rotation of the lifting screw 36; the lifting screw 36 is driven by the torque output of the first reduction box 33, and through the cooperation of its thread and the electromagnetic fixing sleeve 31, it realizes linear motion, prompting the apron 2 to rise smoothly to the specified height. The micro switch built into the first reduction box 33 plays a key role. When the electromagnetic fixing sleeve 31 drops to the lowest point, the micro switch is triggered. By clearing the count of the Hall sensor, the precise control of the rising process of the apron 2 is realized, ensuring the smoothness of its movement and effectively preventing the occurrence of displacement errors and irregular movements.

[0058] After the apron 2 reaches the designated position, the clamping system 4 is immediately started, and the transverse clamping rod 43 and the longitudinal clamping rod 44 move along the predetermined trajectory according to the threaded guide of the screw rod to complete the precise clamping of the target. Specifically: after the second drive motor 49 is started, the torque generated is efficiently transmitted to the second reduction box 45 through the second transmission shaft 46 and the second coupling 47. The gear design inside the second reduction box 45 converts high-speed rotation into low-speed and high-torque output. This conversion process is a key step in achieving precise control and high-torque output; the converted torque is transmitted to the transverse screw rod 43 or the longitudinal screw rod 44 through the worm gear mechanism to rotate it, wherein the longitudinal screw rod 43 and the transverse screw rod 44 both have a unique design of opposite-direction threads at both ends to ensure the precise movement of the clamping rod; the transverse clamping rod 41 is fixed to the threaded sleeve 48 by screw connection The purpose is to facilitate installation and disassembly. The threaded sleeve 48 is connected to the longitudinal screw rod 44. Through the rotation (forward or reverse) of the longitudinal screw rod 44, the two threaded sleeves 48 at both ends move toward each other or relative to each other, and the transverse clamping rod 41 can move toward each other or relative to each other along the thread, so as to achieve the clamping and release of the UAV; the longitudinal clamping rod 42 is fixed to the threaded sleeve 48 by screwing, and the threaded sleeve 48 is connected to the transverse screw rod 43. Similarly, through the rotation of the transverse screw rod 43, the two threaded sleeves 48 at both ends move toward each other or relative to each other, and the longitudinal clamping rod 42 can move toward each other or relative to each other, so as to achieve the clamping and release action of the UAV in another dimension; through the coordinated work of the longitudinal clamping rod 42 and the transverse clamping rod 43, the UAV can be accurately clamped and positioned, ensuring the stability and accuracy of the operation.

[0059] The entire process reflects the high degree of coordination and precise cooperation among the components, ensuring the safety and efficiency of the operation.

[0060] The modular vehicle-mounted UAV launch platform provided in this embodiment has the following advantages:

[0061] Position adaptability: Traditional drone launch platforms are usually fixed in a certain position of the vehicle, such as the roof or trunk, which limits the space utilization of the vehicle and the flexibility of drone launch. The modular design allows the platform to be flexibly moved between different positions such as the roof, front cabin trunk, trunk, etc., improving the space utilization efficiency of the vehicle and the adaptability of drone launch. The drone can be operated safely without stopping the vehicle.

[0062] Rapid Deployment: The modular design enables the drone launch platform to be quickly installed and disassembled without the need for complex tools or specialized skills, greatly shortening the preparation and recovery time of the drone and improving the efficiency of emergency response and mission execution.

[0063] Versatility and compatibility: The modular design ensures that the drone launch platform is compatible with vehicles of different models and sizes, eliminating the need to customize a dedicated platform for each vehicle type, reducing costs and improving versatility and scalability.

[0064] Easy maintenance: Independent replacement and repair without large-scale reconstruction of the entire platform, which not only reduces maintenance costs, but also shortens repair time and improves platform availability.

[0065] Reduce development costs: Modular design can reduce the workload of repeated design, speed up the introduction of new products, and reduce costs due to standardized production.

[0066] Example 2

[0067] Embodiment 2 of the present invention provides a vehicle, including a vehicle body and a modular vehicle-mounted UAV launching platform as described in Embodiment 1 and arranged on the vehicle body.

[0068] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and variations. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention.

Claims

1. A modular vehicle-mounted UAV launch platform, characterized by: Including the apron, gripping system and lifting system; The lifting system is detachably arranged at the bottom of the apron and is used to raise and lower the apron; The clamping system includes two driving motors and four reduction gearboxes detachably arranged at the bottom of the apron, each driving motor is connected to the two reduction gearboxes through a transmission shaft, the two transmission shafts are arranged vertically, the reduction gearboxes at both ends of the longitudinally arranged transmission shaft are equipped with a transverse screw rod, and the reduction gearboxes at both ends of the transversely arranged transmission shaft are equipped with a longitudinal screw rod, and the longitudinal screw rod and the transverse screw rod both have threads in opposite directions at both ends; the two transverse screw rods are connected to the two longitudinal clamping bars arranged above the apron, and the two longitudinal clamping bars are driven to move toward each other or relative to each other through the rotation of the transverse screw rods, so as to realize the clamping and release of the UAV in one dimension; the two longitudinal screw rods are connected to the two transverse clamping bars arranged above the apron, and the two transverse clamping bars are driven to move toward each other or relative to each other through the rotation of the longitudinal screw rods, so as to realize the clamping and release of the UAV in another dimension.

2. A modular vehicle-mounted UAV launch platform as claimed in claim 1, characterized in that: The lifting system includes four lifting screws and four electromagnetic fixing sleeves. The four electromagnetic fixing sleeves are detachably arranged at the four corners of the bottom of the apron. A matching electromagnetic fixing sleeve is sleeved on the outside of each lifting screw. The lifting screw is driven by the torque output by the driving motor and cooperates with the thread of the electromagnetic fixing sleeve to achieve linear motion, thereby causing the apron to rise and fall.

3. The modular vehicle-mounted UAV launch platform according to claim 1, characterized in that: The transmission shaft is connected to the reduction box through a coupling.

4. The modular vehicle-mounted UAV launch platform according to claim 1, characterized in that: The ends of the transverse screw rod and the longitudinal screw rod away from the reduction box are detachably connected to the bottom of the apron through L-shaped fixing pieces.

5. The modular vehicle-mounted UAV launch platform according to claim 1, characterized in that: The transverse screw rod is connected to the longitudinal clamping rod through a sliding part. Each transverse screw rod is configured with two symmetrically arranged sliding parts. The sliding part includes a threaded sleeve and a V-shaped part. The threaded sleeve is sleeved on the outside of the transverse screw rod. The V-shaped part connects the threaded sleeve and the longitudinal clamping rod. The rotation of the transverse screw rod drives the threaded sleeve to move, and then drives the longitudinal clamping rod to move.

6. The modular vehicle-mounted UAV launch platform according to claim 1, characterized in that: The longitudinal screw rod is connected to the transverse clamping rod through a sliding part. Each longitudinal screw rod is configured with two symmetrically arranged sliding parts. The sliding part includes a threaded sleeve and a V-shaped part. The threaded sleeve is sleeved on the outside of the longitudinal screw rod. The V-shaped part connects the threaded sleeve and the transverse clamping rod. The rotation of the longitudinal screw rod drives the threaded sleeve to move, and then drives the transverse clamping rod to move.

7. The modular vehicle-mounted UAV launch platform according to claim 1, characterized in that: One end of the two transverse screw rods close to the reduction box connected thereto is connected to a longitudinal clamping rod; and one end of the two transverse screw rods away from the reduction box connected thereto is connected to another longitudinal clamping rod.

8. The modular vehicle-mounted UAV launch platform according to claim 1, characterized in that: One end of the two longitudinal screw rods close to the reduction box connected thereto is connected to a transverse clamping rod; and one end of the two longitudinal screw rods away from the reduction box connected thereto is connected to another transverse clamping rod.

9. The modular vehicle-mounted UAV launch platform according to claim 1, characterized in that: The two longitudinal clamping bars and the two transverse clamping bars form a rectangle parallel to the apron.

10. A vehicle, characterized in that: It comprises a vehicle body and a modular vehicle-mounted UAV launching platform as described in any one of claims 1 to 9 arranged on the vehicle body.

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