Unmanned aerial vehicle empennage mounting vehicle

Abstract

The utility model discloses an unmanned aerial vehicle empennage mounting vehicle which comprises a base, a supporting column is fixedly connected to the middle of the upper end of the base, a first hydraulic cylinder is hinged to the supporting column, a supporting rod is hinged to the upper end of the supporting column, and the output end of the first hydraulic cylinder is hinged to the supporting rod. The end, away from the supporting column, of the supporting rod is fixedly connected with a first rotating rod, and the supporting rod is rotationally connected with a second hydraulic cylinder through the first rotating rod. According to the empennage mounting vehicle, the hydraulic cylinders, the motors, the half gears, the clamping rods, the universal wheels and the like are adopted, the mounting vehicle can move and change the direction conveniently through the universal wheels, the supporting columns, the supporting rods and the second hydraulic cylinders are rotationally connected, so that the empennage mounting vehicle can change the mounting angle conveniently, clamping and mounting of empennages of different models are achieved through the second motors, the half gears and the clamping rods, and mounting is convenient. Therefore, the unmanned aerial vehicle empennage is mechanically mounted, and workers are prevented from being injured.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a vehicle for installing a tail wing of an unmanned aerial vehicle. Background Art

[0002] Most of the current large drones have a V-shaped tail structure. The tail is located at the rear section of the fuselage and is fixed to the fuselage with bolts after the intersection holes of the tail and the intersection holes of the fuselage are aligned.

[0003] The tail of existing large UAVs is usually very heavy and installed at a high position. The traditional manual lifting method requires the participation of multiple operators, and the operators who lift the tail outside need to stand at a high position to maintain the installation posture of the tail. This installation method has high labor intensity and great safety risks. If the operation is improper, the tail is easy to slide from a high altitude and cause damage, which also threatens the personal safety of the operator. Therefore, in order to solve the above problems, the utility model proposes a UAV tail installation vehicle. Utility Model Content

[0004] The purpose of the utility model is to provide a UAV tail wing installation vehicle to solve the problems raised in the above background technology.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a UAV tail wing mounting vehicle, comprising a base, a support column is fixedly connected to the middle of the upper end of the base, a first hydraulic cylinder is hingedly connected to the support column, a support rod is hingedly connected to the upper end of the support column, an output end of the first hydraulic cylinder is hingedly connected to the support rod, an end of the support rod away from the support column is fixedly connected to a first rotating rod, the support rod is rotatably connected to a second hydraulic cylinder via the first rotating rod, a first motor fixedly connected to the second hydraulic cylinder is provided on one side of the first rotating rod, and an output end of the first motor is fixedly connected to the first rotating rod;

[0006] The output end of the second hydraulic cylinder is fixedly connected to a connecting plate, and a symmetrical fixing plate is fixedly connected to the connecting plate on the side away from the second hydraulic cylinder, a long plate is fixedly connected between the fixing plates, and a second motor is fixedly connected to one side of the middle of the long plate, and two output ends of the second motor are fixedly connected to a rotating shaft, and the ends of the two rotating shafts away from the second motor are fixedly connected to a first half gear, and the two first half gears are meshed with the second half gears, and the two second half gears are fixedly connected by a second rotating rod, and the second rotating rod is rotatably connected to the two fixing plates, and the first half gear and the second half gear are fixedly connected to a fixing rod, and the other end of the fixing rod is rotatably connected to a clamping rod via a rotating shaft, and the middle part of the clamping rod is rotatably connected to a symmetrical limiting rod via a rotating shaft, and the other end of the limiting rod is rotatably connected to the fixing plate via a rotating shaft.

[0007] Preferably, universal wheels are fixedly connected to the lower end of the base on all sides, and a push handle is fixedly connected to the upper end of the base on one side of the support column.

[0008] Preferably, a detachable clamp is fixedly connected to the clamping end of the clamping rod.

[0009] Preferably, the second motor is a dual-shaft motor.

[0010] Preferably, the first half gear and the second half gear are symmetrically arranged.

[0011] Compared with the prior art, the beneficial effects of the utility model are as follows: the utility model adopts a hydraulic cylinder, a motor, a half gear, a clamping rod, a universal wheel, etc., and the universal wheel facilitates the movement and change of direction of the installation vehicle. The support column, the support rod and the second hydraulic cylinder are rotatably connected, so as to facilitate the tail wing installation vehicle to change the installation angle. The second motor, the half gear and the clamping rod are used to realize the clamping and installation of different types of tail wings, thereby realizing the mechanical installation of the UAV tail wing and avoiding injuries to workers. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] Figure 1 It is a schematic diagram of the structure of the utility model;

[0013] Figure 2 It is a structural schematic diagram of the clamping device of the utility model;

[0014] Figure 3 It is a cross-sectional structural schematic diagram of the clamping device of the utility model;

[0015] Figure 4 It is a structural schematic diagram of the support rod of the utility model.

[0016] In the figure: 1. base; 2. universal wheel; 3. push handle; 4. support column; 5. first hydraulic cylinder; 6. support rod; 61. first rotating rod; 7. first motor; 8. second hydraulic cylinder; 9. connecting plate; 10. fixed plate; 11. long board; 12. second motor; 13. rotating shaft; 14. first half gear; 15. second half gear; 16. second rotating rod; 17. fixed rod; 18. clamping rod; 181. chuck; 19. limit rod. DETAILED DESCRIPTION

[0017] See also Figure 1-4The utility model provides a technical solution: a UAV tail wing mounting vehicle, comprising a base 1, a support column 4 is fixedly connected to the middle of the upper end of the base 1, a first hydraulic cylinder 5 is hingedly connected to the support column 4, a support rod 6 is hingedly connected to the upper end of the support column 4, an output end of the first hydraulic cylinder 5 is hingedly connected to the support rod 6, an end of the support rod 6 away from the support column 4 is fixedly connected to a first rotating rod 61, the support rod 6 is rotatably connected to a second hydraulic cylinder 8 through the first rotating rod 61, a first motor 7 fixedly connected to the second hydraulic cylinder 8 is provided on one side of the first rotating rod 61, and an output end of the first motor 7 is fixedly connected to the first rotating rod 61;

[0018] The output end of the second hydraulic cylinder 8 is fixedly connected to a connecting plate 9, and a symmetrical fixing plate 10 is fixedly connected to the side of the connecting plate 9 away from the second hydraulic cylinder 8. A long plate 11 is fixedly connected between the fixing plates 10, and a second motor 12 is fixedly connected to one side of the middle of the long plate 11. The two output ends of the second motor 12 are fixedly connected to a rotating shaft 13, and the ends of the two rotating shafts 13 away from the second motor 12 are fixedly connected to a first half gear 14, and the two first half gears 14 are meshed and connected with a second half gear 15. The two second half gears 15 are fixedly connected through a second rotating rod 16, and the second rotating rod 16 is rotatably connected to the two fixing plates 10. The first half gear 14 and the second half gear 15 are fixedly connected to a fixing rod 17, and the other end of the fixing rod 17 is rotatably connected to a clamping rod 18 through a rotating shaft, and the middle part of the clamping rod 18 is rotatably connected to a symmetrical limiting rod 19 through a rotating shaft, and the other end of the limiting rod 19 is rotatably connected to the fixing plate 10 through a rotating shaft.

[0019] Furthermore, universal wheels 2 are fixedly connected to the lower end of the base 1, and a push handle 3 is fixedly connected to one side of the support column 4 at the upper end of the base 1, so as to facilitate the movement and direction change of the installation vehicle.

[0020] Furthermore, a detachable clamp 181 is fixedly connected to the clamping end of the clamping rod 18, so that the clamp 181 can be replaced easily.

[0021] Furthermore, the second motor 12 is a dual-shaft motor, so that one motor controls the rotation of the two first half gears 14 .

[0022] Furthermore, the first half gear 14 and the second half gear 15 are symmetrically arranged, so as to facilitate the synchronous movement of the fixing rod 17, the clamping rod 18 and the limiting rod 19, thereby achieving clamping.

[0023] Specifically, when the utility model is used, the installation vehicle is first pushed to the required place by the universal wheel 2 and the push handle 3, and then the second hydraulic cylinder 8 is turned on, the second hydraulic cylinder 8 will drive the connecting plate 9 to move, and then the clamp 181 is moved to a suitable position, and then the second motor 12 is turned on, the second motor 12 will drive the rotating shaft 13 and the first half gear 14 to rotate, and the first half gear 14 will drive the second half gear 15 to rotate, and then under the joint action of the first half gear 14, the second half gear 15, the fixing rod 17, the clamping rod 18 and the limiting rod 19, the symmetrical clamping rods 18 will approach each other until the tail of the drone is clamped, and then the first hydraulic cylinder 5 and the first motor 7 are turned on to adjust the installation angle of the installation vehicle, and then the tail of the drone is moved to the tail of the drone, and then the tail is fixed by bolts, and then the push handle 3 is pulled to move the installation vehicle away.

Claims

1. A UAV tail wing mounting vehicle, comprising a base (1), characterized in that: A support column (4) is fixedly connected to the middle of the upper end of the base (1), a first hydraulic cylinder (5) is hingedly connected to the support column (4), a support rod (6) is hingedly connected to the upper end of the support column (4), an output end of the first hydraulic cylinder (5) is hingedly connected to the support rod (6), an end of the support rod (6) away from the support column (4) is fixedly connected to a first rotating rod (61), the support rod (6) is rotatably connected to a second hydraulic cylinder (8) via the first rotating rod (61), a first motor (7) fixedly connected to the second hydraulic cylinder (8) is provided on one side of the first rotating rod (61), and an output end of the first motor (7) is fixedly connected to the first rotating rod (61); The output end of the second hydraulic cylinder (8) is fixedly connected to a connecting plate (9), a side of the connecting plate (9) away from the second hydraulic cylinder (8) is fixedly connected to a symmetrical fixing plate (10), a long plate (11) is fixedly connected between the fixing plates (10), a middle side of the long plate (11) is fixedly connected to a second motor (12), two output ends of the second motor (12) are fixedly connected to a rotating shaft (13), ends of the two rotating shafts (13) away from the second motor (12) are fixedly connected to a first half gear (14), and the two first half gears (14) are meshed. A second half gear (15) is connected, and the two second half gears (15) are fixedly connected via a second rotating rod (16), and the second rotating rod (16) is rotationally connected to the two fixed plates (10). The first half gear (14) and the second half gear (15) are both fixedly connected to a fixing rod (17), and the other end of the fixing rod (17) is rotationally connected to a clamping rod (18) via a rotating shaft, and the middle part of the clamping rod (18) is rotationally connected to a symmetrical limiting rod (19) via a rotating shaft, and the other end of the limiting rod (19) is rotationally connected to the fixed plate (10) via a rotating shaft.

2. The UAV tail wing installation vehicle according to claim 1, characterized in that: Universal wheels (2) are fixedly connected to the lower end of the base (1) on all sides, and a push handle (3) is fixedly connected to the upper end of the base (1) on one side of the support column (4).

3. The UAV tail wing installation vehicle according to claim 1, characterized in that: A detachable clamp (181) is fixedly connected to the clamping end of the clamping rod (18).

4. The UAV tail wing installation vehicle according to claim 1, characterized in that: The second motor (12) is a dual-shaft motor.

5. The UAV tail wing installation vehicle according to claim 1, characterized in that: The first half gear (14) and the second half gear (15) are symmetrically arranged.

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