Combined bracket for launching and transporting unmanned aerial vehicle

Abstract

The invention relates to a combined bracket for launching and transporting an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicle brackets. Comprising a front side base and a rear side base which are fixedly connected, two front side launching racks which are in bilateral symmetry are rotationally arranged on the front side base, two rear side launching racks which are in bilateral symmetry are rotationally arranged on the rear side base, and the two rear side launching racks are each provided with a locking mechanism. The unmanned aerial vehicle is fixedly connected with the rear side launcher through a locking mechanism; the same transportation frame is fixedly arranged on the front side base and the rear side base, the transportation frame comprises a bottom frame, the bottom frame is fixed on the front side base and the rear side base, a front lower support and a rear lower support are arranged on the bottom frame, and a fixed pressing plate is arranged on each lower support; the problems that in the existing unmanned aerial vehicle launching process, a rocket booster collides with a front supporting leg, and the safety is insufficient in the unmanned aerial vehicle transportation process are solved.

Description

Technical Field

[0001] The invention belongs to the technical field of unmanned aerial vehicle brackets, and in particular relates to a combined bracket for launching and transporting unmanned aerial vehicles. Background Art

[0002] At present, there are many ways to launch drones in China, including: taxiing takeoff, catapult takeoff, rocket-assisted takeoff, aerial drop and vertical takeoff. The advantages of rocket-assisted launch are that the entire launch device occupies less space, has lower costs, is less affected by the outside world, and can be deployed quickly, but it also has disadvantages, mainly manifested as follows: (1) The launch pad is a fixed structure, and the front and rear legs cannot be tilted. In this case, the rocket booster is likely to collide with the front legs during launch, and even cause launch failure.

[0003] (2) The UAV launcher and the transport bracket are combined, but after the combination process, the center of mass of the UAV in the transport state is much higher than the center of mass of the UAV in the launch state, resulting in poor transportability. Summary of the invention

[0004] The present invention overcomes the shortcomings of the prior art and proposes a combined bracket for launching and transporting a UAV; it solves the problems of collision between a rocket booster and a front leg during the current UAV launch process and the lack of safety during the UAV transportation process.

[0005] In order to achieve the above object, the present invention is implemented through the following technical solutions.

[0006] A combined bracket for launching and transporting an unmanned aerial vehicle comprises a front base and a rear base which are fixedly connected to each other, two left-right symmetrical front launching racks are rotatably arranged on the front base, and two left-right symmetrical rear launching racks are rotatably arranged on the rear base, a locking mechanism is respectively arranged on the two rear launching racks, and the unmanned aerial vehicle is fixedly connected to the rear launching racks via the locking mechanism; the same transport rack is fixedly arranged on the front base and the rear base, the transport rack comprises a base frame, the base frame is fixed on the front base and the rear base, two front and rear lower supports are arranged on the base frame, and a fixed pressure plate is respectively arranged on each lower support.

[0007] Furthermore, the front launching frame includes a front rotating frame, a front supporting rod, a front supporting seat, and a front inverted fixing seat; a vertical front rotating frame is fixedly arranged in the middle of the left and right edges of the upper end surface of the front base, respectively, and the front supporting rod is a vertically arranged rod-shaped structure, and the lower end of the front supporting rod is rotatably connected to the inner lower end of the front rotating frame through a front rotating pin; a first torsion spring is arranged on the front rotating pin, and when the first torsion spring is in a free state, the front supporting rod is in a horizontal state, and when the first torsion spring is in a stretched state, the front supporting rod is in a vertical state; a front supporting seat is fixedly arranged at the upper end of the front supporting rod, and an arc-shaped supporting groove is provided on the upper end surface of the front supporting seat.

[0008] Furthermore, a first fixing hole that passes through left and right is provided at the upper end of the front rotating frame, and a second fixing hole that passes through left and right is provided in the middle of the front support rod. When the front support rod is in a vertical state inside the front rotating frame, the first fixing hole on the front rotating frame corresponds to the second fixing hole on the front support rod, and the first fixing pin is inserted into the corresponding first fixing hole and second fixing hole, thereby locking the support rod in a vertical state; a front side inversion fixing seat is fixedly provided on the upper end surface of the front side base at the front side of each front rotating frame, and the front side inversion fixing seat is a U-shaped plate structure with an opening upward, and a third fixing hole that passes through left and right is provided on the front side inversion fixing seat; when the front support rod is rotated to a horizontal state, the second fixing hole on the front support rod corresponds to the third fixing hole on the front inversion fixing seat, and the second fixing pin is inserted into the corresponding second fixing hole and third fixing hole, thereby locking the support rod in a horizontal state.

[0009] Furthermore, the rear launch frame includes a rear rotating frame, a rear support rod, and a rear inverted fixed seat; two left-right symmetrical vertical rear rotating frames are fixedly arranged on the upper end surface of the rear base along the middle part of the front-to-back direction, and the rear support rod is a vertically arranged rod-shaped structure, and the lower end of the rear support rod is rotatably connected to the inner lower end of the rear rotating frame through a rear rotating pin; a second torsion spring is arranged on the rear rotating pin, and when the second torsion spring is in a free state, the rear support rod is in a horizontal state, and when the second torsion spring is in a stretched state, the rear support rod is in a vertical state.

[0010] Furthermore, a fourth fixing hole is provided at the upper end of the rear rotating frame, which passes through the left and right sides, and a fifth fixing hole is provided at the middle portion of the rear support rod, which passes through the left and right sides. When the rear support rod is in a vertical state inside the rear rotating frame, the fourth fixing hole on the rear rotating frame corresponds to the fifth fixing hole on the rear support rod, and a third fixing pin is inserted into the corresponding fourth fixing hole and fifth fixing hole, thereby locking the support rod in a vertical state; a rear side inversion fixing seat is fixedly provided on the upper end surface of the rear side base at the rear side of each rear rotating frame, and the rear side inversion fixing seat is a U-shaped plate structure with an opening upward, and a sixth fixing hole is provided on the rear side inversion fixing seat; when the rear support rod is rotated to a horizontal state, the fifth fixing hole on the rear support rod corresponds to the sixth fixing hole on the rear inversion fixing seat, and a fourth fixing pin is inserted into the corresponding fifth fixing hole and sixth fixing hole, thereby locking the support rod in a horizontal state.

[0011] Furthermore, the locking mechanism is fixedly arranged at the upper end of the rear support rod; the locking mechanism includes a base plate, an up and down adjustment pad, a movable plate, a movable seat, a fixed seat, and a tensioning screw; two front and rear mounting grooves are arranged on the upper end surface of the base plate, and an up and down adjustment pad is arranged inside each mounting groove; four square array longitudinal grooves are arranged on the base plate, and the four longitudinal grooves extend along the front and back directions, and a fixing bolt passes downward through each longitudinal groove, and a fixing nut is screwed on the lower end of the fixing bolt; the movable plate is arranged at the upper end of the two up and down adjustment pads, and a transverse groove is respectively arranged at the four corners of the movable plate, and the transverse groove extends along the left and right directions, and the four fixing bolts respectively pass through the four transverse grooves of the movable plate.

[0012] Furthermore, the movable seat is a U-shaped block structure that opens forward, and a U-shaped groove is provided in the middle of the front end face of the movable seat, and the movable seat is fixedly arranged on the upper end face of the movable plate; a front fixing hole and a rear limiting groove are provided on the left and right side walls of the U-shaped groove, and the limiting grooves extend along the front and rear directions; a fixing pin or a shear pin is inserted between the fixing holes on both sides, and a nut is screwed on the end of the fixing pin or the shear pin; a limiting pin is inserted between the limiting grooves on both sides, and a nut is screwed on the end of the limiting pin; a tightening through hole that passes through the front and back is provided on the fixed seat, and a tightening screw is inserted inside the tightening through hole, and a handle at one end of the tightening screw contacts the rear end face of the fixed seat, and the other end of the tightening screw passes through the movable seat and extends into the U-shaped groove of the movable seat, and a tightening nut is screwed on the end of the tightening screw away from the handle, and the movable seat and the fixed seat can be fixed in the front and back directions by tightening the tightening nut.

[0013] Furthermore, the chassis includes a front chassis, a rear chassis, and a fixing frame; the front chassis is fixedly arranged at the upper end surface of the front base, and the front chassis is located between the left and right front inverted fixing seats; a transport frame fixing seat is fixedly arranged on the upper end surface of the front base, the front chassis is clamped inside the transport frame fixing seat, and the bolts pass through the transport frame fixing seat and the front chassis and are fixed by nuts, thereby fixing the front chassis to the front base; the rear chassis is fixedly arranged at the upper end surface of the rear base, and the rear chassis is open The frame structure is U-shaped downward, and the rear chassis is located on the outside of the two rear inverted fixing seats; a transport frame fixing seat is fixedly arranged on the upper end surface of the rear base, and the rear chassis is clamped in the inside of the transport fixing seat, and bolts pass through the transport frame fixing seat and the rear chassis and are fixed by nuts, thereby fixing the rear chassis to the rear base; the fixing frame is a frame structure extending along the front and rear directions, the lower side of the front end of the fixing frame is fixedly connected to the upper end of the front chassis, and the lower side of the rear end of the fixing frame is fixedly connected to the upper end of the rear chassis.

[0014] Furthermore, a lower support is fixedly provided at the front and rear ends of the upper end face of the fixed frame, and the lower support is a "︺"-shaped rod-like structure located in the left and right vertical planes, and a "︺"-shaped lower support groove is provided inside the lower support; the fixed pressure plate is a "︷"-shaped rod-like structure located in the left and right vertical planes, and a "︷"-shaped upper support groove is provided inside the fixed pressure plate; the two ends of the fixed pressure plate are fixedly connected to the two ends of the lower support by bolts and nuts; a lifting ring is fixedly provided on the upper side of the two ends of the fixed pressure plate, and the transport frame and the drone as a whole can be lifted by the four lifting rings on the two fixed pressure plates.

[0015] The beneficial effects of the present invention compared with the prior art are as follows: The invention provides a combined bracket for launching and transporting a drone, and proposes a launcher with both front and rear legs that can be folded forward, which solves the problem of preventing the rocket booster and the front legs from colliding during the launch of the drone. When the drone transport bracket and the launcher are combined, the front and rear legs of the launcher are both folded forward and fixed, so that the center of mass of the drone in the transport state is lower than the center of mass of the drone in the launch state, thereby improving transportation safety. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] The present invention will be further described in detail below in conjunction with the accompanying drawings: Figure 1 It is a schematic diagram of the structure of the launcher when it is in the launching state; Figure 2 It is a schematic diagram of the structure of the launcher after launch; Figure 3 It is a schematic diagram of the structure when the front support rod is in a vertical state; Figure 4 It is a schematic diagram of the structure when the front support rod is in a horizontal state; Figure 5 It is a schematic diagram of the structure when the rear support rod is in a vertical state; Figure 6 It is a schematic diagram of the structure when the rear support rod is in a horizontal state; Figure 7 It is a structural schematic diagram of the locking mechanism; Figure 8 It is a schematic diagram of the structure of the combined bracket when it is in a transport state; Fig. 9 It is a schematic diagram of the structure of the transport rack; Among them, 1 is the front base, 2 is the rear base, 3 is the front launch frame, 4 is the rear launch frame, 5 is the locking mechanism, 6 is the base, 7 is the lower support, 8 is the fixed pressure plate, 9 is the front rotating frame, 10 is the front support rod, 11 is the front support seat, 12 is the reinforcing rod, 13 is the front rotating pin, 14 is the front lodging fixing seat, 15 is the first fixing pin, 16 is the second fixing pin, 17 is the rear rotating frame, 18 is the rear support Rod, 19 is the rear rotating pin, 20 is the rear inverted fixed seat, 21 is the third fixed pin, 22 is the fourth fixed pin, 23 is the bottom plate, 24 is the up and down adjustment pad, 25 is the fixing bolt, 26 is the movable plate, 27 is the movable seat, 28 is the fixed seat, 29 is the shear pin, 30 is the limit pin, 31 is the tightening screw, 32 is the front base frame, 33 is the rear base frame, 34 is the transport frame fixed seat, 35 is the fixed frame, and 36 is the lifting ring. DETAILED DESCRIPTION

[0017] In order to make the technical problems, technical solutions and beneficial effects to be solved by the present invention clearer, the present invention is further described in detail in conjunction with the embodiments and the accompanying drawings. It should be understood that the specific embodiments described herein are only used to explain the present invention and are not intended to limit the present invention. The technical solutions of the present invention are described in detail below in conjunction with the embodiments and the accompanying drawings, but the scope of protection is not limited thereto.

[0018] like Figure 1 As shown in FIG. 9 , the present invention provides a combined bracket for launching and transporting an unmanned aerial vehicle, comprising a front base 1 and a rear base 2 which are fixedly connected to each other, two left-right symmetrical front launch racks 3 are rotatably arranged on the front base 1, and two left-right symmetrical rear launch racks 4 are rotatably arranged on the rear base 2, a locking mechanism 5 is respectively arranged on the two rear launch racks 4, and the unmanned aerial vehicle is fixedly connected to the rear launch racks 4 through the locking mechanism 5; the same transport frame is fixedly arranged on the front base 1 and the rear base 2, and the transport frame comprises a base frame 6, which is fixed on the front base 1 and the rear base 2, and two front and rear lower supports 7 are arranged on the base frame 6, and a fixed pressure plate 8 is respectively arranged on each lower support 7.

[0019] The front base 1 and the rear base 2 are both horizontally arranged square plate structures, and the rear end of the front base 1 is fixedly connected to the front end of the rear base 2.

[0020] The front launching frame 3 includes a front rotating frame 9 , a front supporting rod 10 , a front supporting seat 11 , and a front falling fixing seat 14 .

[0021] A vertical front rotating frame 9 is fixedly arranged in the middle of the left and right edges of the upper end surface of the front base 1. The front rotating frame 9 is a U-shaped plate structure with an opening facing forward. An inclined reinforcing rod 12 is fixedly arranged on the end surfaces of the left and right front rotating frames 9 that are close to each other, and an inclined reinforcing rod 12 is also fixedly arranged on the rear end surfaces of the left and right front rotating frames 9. All the reinforcing rods 12 are fixedly connected to the upper end surface of the front base 1.

[0022] The front support rod 10 is a vertically arranged rod-shaped structure, and the lower end of the front support rod 10 is rotatably connected to the inner lower end of the front rotating frame 9 through the front rotating pin 13; a first torsion spring is arranged on the front rotating pin 13, and when the first torsion spring is in a free state, the front support rod 10 is in a horizontal state, and when the first torsion spring is in a stretched state, the front support rod 10 is in a vertical state.

[0023] A front support seat 11 is fixedly provided at the upper end of the front support rod 10 , and an arc-shaped support groove is provided on the upper end surface of the front support seat 11 .

[0024] A first fixing hole is provided at the upper end of the front rotating frame 9 and passes through the front frame 9, and a second fixing hole is provided at the middle part of the front support rod 10 and passes through the front frame 9. When the front support rod 10 is in a vertical state inside the front rotating frame 9, the first fixing hole on the front rotating frame 9 corresponds to the second fixing hole on the front support rod 10, and the first fixing pin 15 is inserted into the corresponding first fixing hole and second fixing hole, thereby locking the support rod in a vertical state.

[0025] A front side fall fixing seat 14 is fixedly arranged on the upper end surface of the front side base 1 at the front side of each front side rotating frame 9. The front side fall fixing seat 14 is a U-shaped plate structure with an opening upward, and a third fixing hole that passes through the left and right sides is arranged on the front side fall fixing seat 14. When the front side support rod 10 rotates to a horizontal state, the second fixing hole on the front side support rod 10 corresponds to the third fixing hole on the front side fall fixing seat 14, and a second fixing pin 16 is inserted into the corresponding second fixing hole and the third fixing hole, thereby locking the support rod to a horizontal state.

[0026] The rear launch frame 4 includes a rear rotating frame 17 , a rear support rod 18 , and a rear inverted fixing seat 20 .

[0027] Two symmetrical vertical rear rotating frames 17 are fixedly arranged in the middle of the upper end surface of the rear base 2 along the front-to-back direction, and the two rear rotating frames 17 maintain the same spacing with the left and right edges of the upper end surface of the rear base 2. The rear rotating frame 17 is a U-shaped plate structure with an opening facing forward. An inclined reinforcing rod 12 is fixedly arranged on the end surfaces of the left and right rear rotating frames 17 that are close to each other, and an inclined reinforcing rod 12 is also fixedly arranged on the rear end surfaces of the left and right rear rotating frames 17, and all the reinforcing rods 12 are fixedly connected to the upper end surface of the rear base 2.

[0028] The rear support rod 18 is a vertically arranged rod-shaped structure, and the lower end of the rear support rod 18 is rotatably connected to the inner lower end of the rear rotating frame 17 through the rear rotating pin 19; a second torsion spring is arranged on the rear rotating pin 19, and when the second torsion spring is in a free state, the rear support rod 18 is in a horizontal state, and when the second torsion spring is in a stretched state, the rear support rod 18 is in a vertical state.

[0029] A fourth fixing hole is provided at the upper end of the rear rotating frame 17 and passes through the rear side, and a fifth fixing hole is provided at the middle part of the rear support rod 18 and passes through the rear side. When the rear support rod 18 is in a vertical state inside the rear rotating frame 17, the fourth fixing hole on the rear rotating frame 17 corresponds to the fifth fixing hole on the rear support rod 18, and a third fixing pin 21 is inserted into the corresponding fourth fixing hole and fifth fixing hole, thereby locking the support rod in a vertical state.

[0030] A rear side inversion fixing seat 20 is fixedly arranged on the upper end surface of the rear side base 2 at the rear side of each rear side rotating frame 17. The rear side inversion fixing seat 20 is a U-shaped plate-like structure with an opening upward, and a sixth fixing hole that passes through the rear side inversion fixing seat 20 is arranged. When the rear side support rod 18 rotates to a horizontal state, the fifth fixing hole on the rear side support rod 18 corresponds to the sixth fixing hole on the rear side inversion fixing seat 20, and a fourth fixing pin 22 is inserted into the corresponding fifth fixing hole and sixth fixing hole, thereby locking the support rod to a horizontal state.

[0031] The locking mechanism 5 is fixedly arranged at the upper end of the rear support rod 18. The locking mechanism 5 comprises a bottom plate 23, an upper and lower adjustment pad 24, a moving plate 26, a moving seat 27, a fixed seat 28, and a tightening screw 31.

[0032] The bottom plate 23 is a horizontally arranged square plate-shaped structure, and two front and rear mounting grooves are arranged on the upper end surface of the bottom plate 23, and an up-and-down adjustment pad 24 is arranged inside each mounting groove. Four square array longitudinal grooves are arranged on the bottom plate 23, and the four longitudinal grooves extend along the front-to-back direction. A fixing bolt 25 passes downward inside each longitudinal groove, and a fixing nut is screwed on the lower end of the fixing bolt 25.

[0033] The movable plate 26 is a square plate-like structure arranged horizontally. The movable plate 26 is arranged at the upper ends of the two upper and lower adjustment pads 24. The lower end surface of the movable plate 26 contacts the upper ends of the two upper and lower adjustment pads 24. The height of the movable plate 26 can be adjusted by selecting the upper and lower adjustment pads 24 of different heights. A transverse groove is arranged at each of the four corners of the movable plate 26. The transverse groove extends along the left and right directions, and the transverse groove is connected with the left end surface or the right end surface of the movable plate 26. Four fixing bolts 25 pass through the four transverse grooves of the movable plate 26 respectively. When the fixing nut is loosened, the fixing bolt 25 can slide relatively inside the longitudinal groove of the bottom plate 23 and the transverse groove of the movable plate 26, so that the front, back, left and right positions of the movable plate 26 can be adjusted. When the position of the movable plate 26 is adjusted, the fixing nuts on the four fixing bolts 25 are tightened, so that the movable plate 26 can be fixed to the bottom plate 23.

[0034] The movable seat 27 is a U-shaped block structure with an opening facing forward. A U-shaped groove is provided in the middle of the front end surface of the movable seat 27. The movable seat 27 is fixedly provided on the upper end surface of the movable plate 26. The left and right side walls of the U-shaped groove are provided with a front fixing hole and a rear limiting groove, and the limiting groove extends along the front-back direction. A fixing pin or a shearing pin 29 is inserted between the fixing holes on both sides, and a nut is screwed on the end of the fixing pin or the shearing pin 29. A limiting pin 30 is inserted between the limiting grooves on both sides, and a nut is screwed on the end of the limiting pin 30.

[0035] The fixed seat 28 is a U-shaped block structure that opens forward. A tightening through hole that passes through the front and back is provided on the fixed seat 28. A tightening screw 31 is inserted into the tightening through hole. The handle at one end of the tightening screw 31 contacts the rear end surface of the fixed seat 28. The other end of the tightening screw 31 passes through the movable seat 27 and extends into the U-shaped groove of the movable seat 27. A tightening nut is threadedly connected to the end of the tightening screw 31 away from the handle. By tightening the tightening nut, the movable seat 27 and the fixed seat 28 can be fixed in the front and back directions.

[0036] When the drone is fixed on the locking mechanism 5, a fixing pin is inserted between the two fixing holes, and the fixing pin and the limit pin 30 pass through the fixing part of the drone, thereby fixing the drone to the two locking mechanisms 5; by tightening four fixing nuts and a tightening nut, the moving plate 26 and the moving plate 26 are fixed on the bottom plate 23, thereby ensuring that the drone is firmly fixed. When the drone needs to be launched, the fixing pin is replaced with a shear pin 29. When the turbojet engine is started, the engine thrust is not enough to shear the shear pin 29, and the drone is still parked on the front launcher 3 and the rear launcher 4. When the rocket booster is started, the thrust generated by the booster causes the shear pin 29 to break, and the drone takes off.

[0037] The base frame 6 includes a front base frame 32 , a rear base frame 33 , and a fixing frame 35 .

[0038] The front chassis 32 is fixedly arranged at the upper end surface of the front base 1, and the front chassis 32 is located between the left and right front inverted fixing seats 14. A transport frame fixing seat 34 is fixedly arranged on the upper end surface of the front base 1, and the front chassis 32 is clamped inside the transport frame fixing seat 34. Bolts pass through the transport frame fixing seat 34 and the front chassis 32 and are fixed by nuts, so that the front chassis 32 is fixedly connected to the front base 1.

[0039] The rear chassis 33 is fixedly arranged at the upper end surface of the rear base 2. The rear chassis 33 is a U-shaped frame structure with an opening downward, and is located outside the two rear side inverted fixing seats 20. A transport frame fixing seat 34 is fixedly arranged on the upper end surface of the rear base 2. The rear chassis 33 is clamped inside the transport fixing seat 28. Bolts pass through the transport frame fixing seat 34 and the rear chassis 33 and are fixed by nuts, thereby fixing the rear chassis 33 to the rear base 2.

[0040] The fixing frame 35 is a frame structure extending along the front-to-back direction. The front lower side of the fixing frame 35 is fixedly connected to the upper end of the front base frame 32 , and the rear lower side of the fixing frame 35 is fixedly connected to the upper end of the rear base frame 33 .

[0041] The lower support 7 is fixedly provided at the front and rear ends of the upper end face of the fixed frame 35, and the lower support 7 is a "︺"-shaped rod-like structure located in the left and right vertical planes, and a "︺"-shaped lower support groove is provided inside the lower support 7. The fixed pressure plate 8 is a "︷"-shaped rod-like structure located in the left and right vertical planes, and a "︷"-shaped upper support groove is provided inside the fixed pressure plate 8. The two ends of the fixed pressure plate 8 are fixedly connected to the two ends of the lower support 7 by bolts and nuts. A lifting ring 36 is fixedly provided on the upper side of the two ends of the fixed pressure plate 8, and the transport frame and the drone can be lifted as a whole through the four lifting rings 36 on the two fixed pressure plates 8.

[0042] The working principle of the present invention is: When the drone needs to be transported, the front support rod 10 and the rear support rod 18 are both in a horizontal state, and the two front support rods 10 are fixed inside the two front inverted fixing seats 14 by the second fixing pins 16, and the two rear support rods 18 are fixed inside the two rear inverted fixing seats 20 by the fourth fixing pins 22. Then, the front support frame and the rear support frame are both inverted, which will not interfere with the transportation of the drone, and can also lower the center of gravity of the combined bracket during transportation, thereby improving the stability during transportation.

[0043] During transportation, the front and rear reinforcement rings of the UAV are respectively clamped into the lower support grooves of the two front and rear lower supports 7 of the transport frame, and then the two fixed pressure plates 8 are fixed to the two lower supports 7, thereby fixing the UAV on the transport frame.

[0044] Before transporting to the designated location for launch, the transport frame is separated from the front base 1 and the rear base 2, and then the transport frame and the UAV are hoisted as a whole using four lifting rings 36, so that the transport frame is separated from the front base 1 and the rear base 2. Then the second fixing pin 16 and the fourth fixing pin 22 are removed, the front support rod 10 and the rear support rod 18 are rotated upward to a vertical state, and the rear support rod 18 is fixed to the rear rotating frame 17 by the third fixing pin 21. Then the UAV is parked on the front support seat 11 and the locking mechanism 5, so that the front side of the UAV is engaged with the front support seat 11 at the upper end of the front support rod 10, so that the front support rod 10 is also in a vertical state under the action of the UAV.

[0045] When the drone is fixed on the locking mechanism 5, a fixing pin is inserted between the two fixing holes, and the fixing pin and the limit pin 30 pass through the fixing part of the drone, thereby fixing the drone to the two locking mechanisms 5; by tightening four fixing nuts and a tightening nut, the moving plate 26 and the moving plate 26 are fixed on the bottom plate 23, thereby ensuring that the drone is firmly fixed. When the drone needs to be launched, the fixing pin is replaced with a shear pin 29. When the turbojet engine is started, the engine thrust is not enough to shear the shear pin 29, and the drone is still parked on the front launcher 3 and the rear launcher 4. When the rocket booster is started, the thrust generated by the booster causes the shear pin 29 to break, and the drone is separated from the locking mechanism 5 and completes takeoff. When the drone takes off, the front support seat 11 is out of contact with the drone, so that the front support rod 10 is rotated downward to a horizontal state under the action of the first torsion spring, so that the booster of the drone will not collide with the front support rod 10.

[0046] It will be apparent to those skilled in the art that the invention is not limited to the details of the exemplary embodiments described above and that the invention can be implemented in other specific forms without departing from the spirit or essential features of the invention. Therefore, the embodiments should be considered exemplary and non-limiting in all respects, and the scope of the invention is defined by the appended claims rather than the foregoing description, and it is intended that all variations falling within the meaning and scope of the equivalent elements of the claims be included in the invention. Any reference numeral in a claim should not be considered as limiting the claim to which it relates.

Claims

1. A combined bracket for launching and transporting unmanned aerial vehicles, characterized in that: The invention comprises a front base (1) and a rear base (2) which are fixedly connected to each other, two left-right symmetrical front launch racks (3) are rotatably arranged on the front base (1), and two left-right symmetrical rear launch racks (4) are rotatably arranged on the rear base (2), and a locking mechanism (5) is respectively arranged on the two rear launch racks (4), and the unmanned aerial vehicle and the rear launch racks (4) are fixedly connected via the locking mechanism (5); the same transport frame is fixedly arranged on the front base (1) and the rear base (2), and the transport frame comprises a bottom frame (6), the bottom frame (6) is fixed on the front base (1) and the rear base (2), and two front and rear lower supports (7) are arranged on the bottom frame (6), and a fixed pressure plate (8) is respectively arranged on each lower support (7).

2. The combined bracket for launching and transporting a UAV according to claim 1, characterized in that: The front launch frame (3) comprises a front rotating frame (9), a front supporting rod (10), a front supporting seat (11), and a front falling fixed seat (14); a vertical front rotating frame (9) is fixedly arranged at the middle of the left and right edges of the upper end surface of the front base (1), the front supporting rod (10) is a vertically arranged rod-shaped structure, and the lower end of the front supporting rod (10) is rotatably connected to the inner lower end of the front rotating frame (9) through a front rotating pin (13); a first torsion spring is arranged on the front rotating pin (13); when the first torsion spring is in a free state, the front supporting rod (10) is in a horizontal state, and when the first torsion spring is in a stretched state, the front supporting rod (10) is in a vertical state; a front supporting seat (11) is fixedly arranged at the upper end of the front supporting rod (10), and an arc-shaped supporting groove is arranged on the upper end surface of the front supporting seat (11).

3. The combined bracket for launching and transporting a UAV according to claim 2, characterized in that: A first fixing hole extending leftward and rightward is provided at the upper end of the front rotating frame (9), and a second fixing hole extending leftward and rightward is provided at the middle of the front supporting rod (10). When the front supporting rod (10) is in a vertical state inside the front rotating frame (9), the first fixing hole on the front rotating frame (9) corresponds to the second fixing hole on the front supporting rod (10), and a first fixing pin (15) is inserted into the corresponding first fixing hole and second fixing hole, thereby locking the supporting rod in a vertical state. A front base is provided at the front side of each front rotating frame (9). (1) A front side fall fixing seat (14) is fixedly arranged on the upper end surface, and the front side fall fixing seat (14) is a U-shaped plate-like structure with an opening upward, and a third fixing hole penetrating from left to right is arranged on the front side fall fixing seat (14); when the front side support rod (10) is rotated to a horizontal state, the second fixing hole on the front side support rod (10) corresponds to the third fixing hole on the front side fall fixing seat (14), and a second fixing pin (16) is inserted into the corresponding second fixing hole and the third fixing hole, thereby locking the support rod into a horizontal state.

4. The combined bracket for launching and transporting a UAV according to claim 3, characterized in that: The rear launch frame (4) comprises a rear rotating frame (17), a rear support rod (18), and a rear inverted fixed seat (20); two left-right symmetrical vertical rear rotating frames (17) are fixedly arranged on the upper end surface of the rear base (2) along the middle part of the front-back direction; the rear support rod (18) is a vertically arranged rod-shaped structure; the lower end of the rear support rod (18) is rotatably connected to the inner lower end of the rear rotating frame (17) through a rear rotating pin (19); a second torsion spring is arranged on the rear rotating pin (19); when the second torsion spring is in a free state, the rear support rod (18) is in a horizontal state; when the second torsion spring is in a stretched state, the rear support rod (18) is in a vertical state.

5. The combined bracket for launching and transporting a UAV according to claim 4, characterized in that: A fourth fixing hole is provided at the upper end of the rear rotating frame (17) and is passed through to the left and right. A fifth fixing hole is provided at the middle of the rear support rod (18) and is passed through to the left and right. When the rear support rod (18) is in a vertical state inside the rear rotating frame (17), the fourth fixing hole on the rear rotating frame (17) corresponds to the fifth fixing hole on the rear support rod (18). A third fixing pin (21) is inserted into the corresponding fourth fixing hole and fifth fixing hole, thereby locking the support rod in a vertical state. A rear side fall-down fixing seat (20) is fixedly arranged on the upper end surface of each base (2), and the rear side fall-down fixing seat (20) is a U-shaped plate-like structure with an opening facing upward, and a sixth fixing hole is arranged on the rear side fall-down fixing seat (20) and passes through the rear side. When the rear side support rod (18) is rotated to a horizontal state, the fifth fixing hole on the rear side support rod (18) corresponds to the sixth fixing hole on the rear side fall-down fixing seat (20), and a fourth fixing pin (22) is inserted into the corresponding fifth fixing hole and the sixth fixing hole, thereby locking the support rod into a horizontal state.

6. The combined bracket for launching and transporting a UAV according to claim 5, characterized in that: The locking mechanism (5) is fixedly arranged at the upper end of the rear support rod (18); the locking mechanism (5) comprises a base plate (23), an upper and lower adjustment pad (24), a movable plate (26), a movable seat (27), a fixed seat (28), and a tensioning screw (31); two front and rear mounting grooves are arranged on the upper end surface of the base plate (23), and an upper and lower adjustment pad (24) is arranged inside each mounting groove; four square array longitudinal grooves are arranged on the base plate (23), the four longitudinal grooves extend along the front and rear directions, a fixing bolt (25) passes downward inside each longitudinal groove, and a fixing nut is screwed on the lower end of the fixing bolt (25); the movable plate (26) is arranged at the upper end of the two upper and lower adjustment pads (24), and a transverse groove is respectively arranged at the four corners of the movable plate (26), and the transverse groove extends along the left and right directions, and the four fixing bolts (25) respectively pass through the four transverse grooves of the movable plate (26).

7. The combined bracket for launching and transporting a UAV according to claim 6, characterized in that: The movable seat (27) is a U-shaped block structure with an opening facing forward. A U-shaped groove is provided in the middle of the front end surface of the movable seat (27). The movable seat (27) is fixedly provided on the upper end surface of the movable plate (26). A front fixing hole and a rear limiting groove are provided on the left and right side walls of the U-shaped groove. The limiting groove extends along the front-back direction. A fixing pin or a shearing pin (29) is inserted between the fixing holes on both sides. A nut is screwed to the end of the fixing pin or the shearing pin (29). A limiting pin (30) is inserted between the limiting grooves on both sides. The limiting pin (30) ) is threadedly connected to the end of the movable seat (27) with a nut; a tightening through hole extending from front to back is provided on the fixed seat (28), a tightening screw (31) is inserted into the tightening through hole, a handle at one end of the tightening screw (31) contacts the rear end surface of the fixed seat (28), the other end of the tightening screw (31) passes through the movable seat (27) and extends into the U-shaped groove of the movable seat (27), a tightening nut is threadedly connected to the end of the tightening screw (31) away from the handle, and by tightening the tightening nut, the movable seat (27) and the fixed seat (28) can be fixed in the front-to-back direction.

8. The combined bracket for launching and transporting a UAV according to claim 5, characterized in that: The chassis (6) comprises a front chassis (32), a rear chassis (33), and a fixing frame (35); the front chassis (32) is fixedly arranged at the upper end surface of the front base (1), and the front chassis (32) is located between the left and right front inverted fixing seats (14); a transport frame fixing seat (34) is fixedly arranged on the upper end surface of the front base (1), and the front chassis (32) is clamped inside the transport frame fixing seat (34), and bolts pass through the transport frame fixing seat (34) and the front chassis (32) and are then fixed by nuts, thereby fixing the front chassis (32) to the front base (1); the rear chassis (33) is fixedly arranged at the upper end surface of the rear base (2), and the rear chassis (33) is fixedly arranged between the left and right front inverted fixing seats (14); ) is a U-shaped frame structure with an opening facing downward, and the rear base frame (33) is located outside the two rear inverted fixed seats (20); a transport frame fixing seat (34) is fixedly arranged on the upper end surface of the rear base (2), and the rear base frame (33) is clamped inside the transport fixing seat (28), and bolts pass through between the transport frame fixing seat (34) and the rear base frame (33) and are fixed by nuts, thereby fixing the rear base frame (33) and the rear base (2) together; the fixing frame (35) is a frame structure extending along the front-to-back direction, and the front lower side of the fixing frame (35) is fixedly connected to the upper end of the front base frame (32), and the rear lower side of the fixing frame (35) is fixedly connected to the upper end of the rear base frame (33).

9. The combined bracket for launching and transporting a UAV according to claim 8, characterized in that: A lower support (7) is fixedly provided at the front and rear ends of the upper end face of the fixing frame (35), respectively; the lower support (7) is a "︺"-shaped rod-shaped structure located in the left and right vertical planes, and a "︺"-shaped lower support groove is provided inside the lower support (7); the fixed pressure plate (8) is a "︷"-shaped rod-shaped structure located in the left and right vertical planes, and a "︷"-shaped upper support groove is provided inside the fixed pressure plate (8); the two ends of the fixed pressure plate (8) are fixedly connected to the two ends of the lower support (7) by bolts and nuts; a lifting ring (36) is fixedly provided on the upper side of the two ends of the fixed pressure plate (8), and the transport frame and the drone can be lifted as a whole by four lifting rings (36) on the two fixed pressure plates (8).

Images