Portable unmanned aerial vehicle launching cabin

Abstract

The utility model relates to a portable unmanned aerial vehicle launching cabin which comprises a launching cabin body, the launching cabin body is provided with a placing area used for storing an unmanned aerial vehicle and a power-assisted launching area, a launching supporting frame is arranged in the power-assisted launching area, and a pull rod mechanism is arranged in the launching supporting frame. A deformable energy storage element is arranged on the pull rod mechanism, and a driving mechanism for driving the pull rod mechanism to pull the energy storage element to deform is arranged at the bottom of the pull rod mechanism; when the unmanned aerial vehicle is launched, the pull rod mechanism extrudes the energy storage element so as to generate elastic potential energy, and the energy storage element is directly released and pushes the unmanned aerial vehicle to be launched after generating enough elastic potential energy.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane technical field, concretely relates to a portable unmanned plane launching cabin. BACKGROUND

[0002] With the continuous development of unmanned plane technology and the expansion of application scenarios, the market size of unmanned plane-mounted launch cabin is also growing continuously. Especially in the fields of military, emergency rescue and environmental monitoring, the demand for unmanned plane-mounted launch cabin is increasing, which promotes the development of related industries. In the future, with the continuous progress and innovation of technology, unmanned plane-mounted launch cabin will be more intelligent, integrated and autonomous, and can play an important role in more fields.

[0003] The utility model discloses a kind of unmanned plane-mounted launch cabin, in combination with its specification and drawing, its scheme unmanned plane launch platform is connected with the cabin body by lifting mechanism, the unmanned plane launch platform is used to load and launch unmanned plane, however its scheme does not give its boost when unmanned plane is launched, equivalent to just a cabin body where unmanned plane is parked, and the whole square cabin is too large, which brings inconvenience when using. SUMMARY

[0004] The utility model mainly aims at the problems existing when unmanned plane is launched, and invents a kind of portable unmanned plane launch cabin, when launching unmanned plane, drive arm slides down and drives down pressure arm, and down pressure arm continuously extrudes energy storage element to generate elastic potential energy, and when enough elastic potential energy is generated, drive arm will stop the downward movement trend, and the elastic potential of energy storage element drives unmanned plane launch.

[0005] The utility model discloses the following technical scheme is realized: a kind of portable unmanned plane launch cabin, including launch cabin body, the launch cabin body is equipped with the placement area for storing unmanned plane and boost launch area, the inside of the boost launch area is equipped with launch support frame, the inside of the launch support frame is equipped with pull rod mechanism, the pull rod mechanism is equipped with the energy storage element that can be deformed, the bottom of the pull rod mechanism is equipped with drive mechanism that drive pull rod mechanism and drive energy storage element to generate deformation.

[0006] As preferred, the launch support frame includes a ring-shaped support frame and a rectangular support frame, the ring-shaped support frame is arranged on the top of the rectangular support frame, the middle part of the rectangular support frame is provided with a first support vertical rod and a first support horizontal rod, and the energy storage element is clamped on the first support vertical rod and the first support horizontal rod.

[0007] As preferred, the energy storage element is a metal spring, the middle part of the metal spring passes through the first support vertical rod, and the bottom is attached to the first support horizontal rod.

[0008] As preferred, the pull rod mechanism comprises a driving arm and a pressing arm, the driving arm is capable of sliding relative to the rectangular support frame, the top of the driving arm is provided with the pressing arm, the width of the pressing arm is greater than the diameter of the energy storage element, and the bottom of the driving arm is provided with a plurality of gear grooves.

[0009] As preferred, the surface of the pressing arm is provided with a UAV placing plate, and the bottom of the UAV in the placing area is clamped on the surface of the UAV placing plate.

[0010] As preferred, the second adsorption assembly comprises a second adsorption support arm and an electromagnet, one side of the second adsorption support arm is provided with a plurality of electromagnets, and each electromagnet is electrically connected to a lithium battery.

[0011] As preferred, the driving mechanism comprises a driving motor, a transmission shaft, a motor support plate and a transmission gear, the motor support plate is arranged at the bottom of the launching cabin body, one side of the motor support plate is provided with the driving motor, the driving motor is connected with the transmission shaft at the end of the rotating shaft, the end of the transmission shaft is provided with the transmission gear, and the surface of the transmission gear is provided with an arc-shaped notch.

[0012] As preferred, the top of the launching cabin body is provided with a cabin cover plate, one side of the cabin cover plate is provided with a rotating shaft support block, the top of the launching cabin body is provided with a rotating shaft support plate matched with the rotating shaft support block, and the rotating shaft support block and the rotating shaft support plate are rotatably connected.

[0013] As preferred, the side wall surface of the launching cabin body is rotatably connected with a cabin erecting support leg, and the setting is for adjusting the angle of the whole launching cabin body when some special ground is adjusted.

[0014] Compared with the prior art, the utility model has the advantages that: 1. when launching the UAV, the driving arm slides downwards to drive the pressing arm, the pressing arm continuously extrudes the energy storage element to generate elastic potential energy, when enough elastic potential energy is generated, the driving arm stops the downward movement trend, and the elastic potential energy of the energy storage element is directly released to push the UAV to launch; 2. in the process that the transmission gear drives the driving arm, whenever the arc-shaped notch position is reached, the transmission relationship between the transmission gear and the driving arm disappears immediately, and then the driving arm immediately disappears the downward movement trend, the structure design is ingenious, the automatic reset function can be realized, and convenience is brought to use. BRIEF DESCRIPTION OF DRAWINGS

[0015] Figure 1 It is a perspective view of the utility model;

[0016] Figure 2 It is a sectional view of the utility model;

[0017] Figure 3 It is a partial sectional view of the utility model;

[0018] Figure 4 is the sectional view of the utility model after being loaded into the unmanned aerial vehicle;

[0019] Figure 5 is the partial sectional view of the utility model;

[0020] Figure 6 is the schematic view when the utility model is used.

[0021] Marked in the figure: 1, launch cabin body; 11, placement area; 12, power-assisted launch area; 13, pivot support plate; 2, launch support frame; 21, annular support frame; 22, rectangular support frame; 23, first support vertical pole; 24, first support horizontal pole; 3, drive pull rod mechanism; 31, drive arm; 32, press-down arm; 311, tooth groove; 4, energy storage element; 5, drive mechanism; 51, drive motor; 52, transmission shaft; 53, transmission gear; 54, motor support plate; 531, arc-shaped cutout; 6, unmanned aerial vehicle placement plate; 7, cabin cover plate; 71, pivot support block; 8, cabin erecting support leg. DETAILED DESCRIPTION

[0022] The utility model will be further described in connection with the embodiments shown in the drawings:

[0023] As Figures 1 to 6As shown, a portable unmanned aerial vehicle launch cabin includes a launch cabin body 1, which is provided with a placement area 11 for storing unmanned aerial vehicles and a power-assisted launch area 12, four wings of the unmanned aerial vehicle have elastic folding function, and the four wings will be immediately unfolded when the unmanned aerial vehicle leaves the placement area 11. The inside of the power-assisted launch area 12 is provided with a launch support frame 2, the launch support frame 2 includes an annular support frame 21 and a rectangular support frame 22, the annular support frame 21 is arranged at the top of the rectangular support frame 22, the middle part of the rectangular support frame 22 is provided with a first support vertical rod 23 and a first support horizontal rod 24, and the energy storage element 4 is clamped on the first support vertical rod 23 and the first support horizontal rod 24. The energy storage element 4 is a metal spring, the middle part of the metal spring passes through the first support vertical rod 23 and the bottom part is attached to the first support horizontal rod 24. The inside of the launch support frame 2 is provided with a pull rod mechanism 3, the pull rod mechanism 3 is provided with an energy storage element 4 capable of deforming, the pull rod mechanism 3 includes a driving arm 31 and a pressing arm 32, the driving arm 31 can slide relative to the rectangular support frame 22, the top of the driving arm 31 is provided with the pressing arm 32, the width of the pressing arm 32 is greater than the diameter of the energy storage element 4, which is arranged to facilitate the pressing arm 32 to generate a limiting effect on the energy storage element 4, the bottom of the driving arm 31 is provided with a plurality of tooth grooves 311, the surface of the pressing arm 32 is provided with an unmanned aerial vehicle placement plate 6, the bottom of the unmanned aerial vehicle in the inside of the placement area 11 is clamped on the surface of the unmanned aerial vehicle placement plate 6, after the arrangement, the driving arm 31 slides downward to drive the pressing arm 32 to slide, the pressing arm 32 continuously extrudes the energy storage element 4 during displacement to generate elastic potential energy, the first support horizontal rod 24 plays a supporting role during the deformation of the energy storage element 4, and when sufficient elastic potential energy is generated, the driving arm 31 stops the downward movement trend, the elastic potential energy of the energy storage element 4 is directly released and pushes the unmanned aerial vehicle placement plate 6, and the unmanned aerial vehicle placement plate 6 launches the unmanned aerial vehicle on the surface thereof to the outside of the entire launch cabin body 1.

[0024] In the embodiment, the bottom of the pull rod mechanism 3 is provided with a driving mechanism 5 for driving the pull rod mechanism 3 to pull the energy storage element 4 to deform, the driving mechanism 5 comprises a driving motor 51, a transmission shaft 52, a motor support plate 54 and a transmission gear 53, the motor support plate 54 is arranged at the bottom of the launching cabin body 1, one side of the motor support plate 54 is provided with the driving motor 51, the end of the rotating shaft of the driving motor 51 is connected with the transmission shaft 52, the end of the transmission shaft 52 is provided with the transmission gear 53, and the surface of the transmission gear 53 is provided with an arc-shaped notch 531.

[0025] The working principle and the use method of the utility model:

[0026] First, open the cabin cover plate 7, then adjust the cabin erection support leg 8 until the appropriate angle, then the rotating shaft of the driving motor 51 drives the transmission shaft 52, the transmission shaft 52 drives the transmission gear 53 to rotate simultaneously, because the surface of the transmission gear 53 is provided with teeth, so the transmission gear 53 can continuously drive the driving arm 31 to move downwards through the tooth groove 311, when the driving arm 31 slides downwards, the pressing arm 32 is driven to slide, the pressing arm 32 continuously extrudes the energy storage element 4 to generate elastic potential energy in the displacement process, the first support cross bar 24 plays a supporting role in the deformation process of the energy storage element 4, when the arc-shaped notch 531 is reached, the transmission relationship between the transmission gear 53 and the driving arm 31 disappears immediately, so the driving arm 31 stops the downward movement trend, the elastic potential energy of the energy storage element 4 is directly released and pushes the unmanned aerial vehicle placing plate 6, and the unmanned aerial vehicle placing plate 6 launches the unmanned aerial vehicle on the surface to the outside of the whole launching cabin body 1.

[0027] The specific embodiments described herein are merely illustrative of the spirit of the present application. Those skilled in the art of the present application can make various modifications or supplements to the described specific embodiments or replace them with similar ways, but will not deviate from the spirit of the present application or exceed the scope defined by the appended claims.

Claims

1. A portable unmanned aerial vehicle (UAV) launch pod, comprising a launch pod body (1), characterized in that, The launch cabin body (1) is provided with a placement area (11) for storing UAVs and an assist launch area (12). The assist launch area (12) is provided with a launch support frame (2). The launch support frame (2) is provided with a pull rod mechanism (3). The pull rod mechanism (3) is provided with a deformable energy storage element (4). The bottom of the pull rod mechanism (3) is provided with a drive mechanism (5) that drives the pull rod mechanism (3) to pull the energy storage element (4) to generate deformation.

2. The portable UAV launch pod according to claim 1, characterized in that, The launch support frame (2) includes an annular support frame (21) and a rectangular support frame (22). The annular support frame (21) is located on the top of the rectangular support frame (22). The rectangular support frame (22) has a first support vertical rod (23) and a first support horizontal rod (24) in the middle. The energy storage element (4) is attached to the first support vertical rod (23) and the first support horizontal rod (24).

3. The portable UAV launch pod according to claim 2, characterized in that, The energy storage element (4) is a metal spring, with the middle part of the metal spring passing through the first support vertical rod (23) and the bottom part attached to the first support horizontal rod (24).

4. The portable UAV launch pod according to claim 3, characterized in that, The lever mechanism (3) includes a drive arm (31) and a lowering arm (32). The drive arm (31) can slide relative to the rectangular support frame (22). The top of the drive arm (31) is provided with a lowering arm (32). The width of the lowering arm (32) is greater than the diameter of the energy storage element (4). The bottom of the drive arm (31) is provided with several toothed grooves (311).

5. The portable UAV launch pod according to claim 4, characterized in that, The surface of the lower pressure arm (32) is provided with a drone placement plate (6), and the bottom of the drone inside the placement area (11) is stuck on the surface of the drone placement plate (6).

6. The portable UAV launch pod according to claim 4, characterized in that, The drive mechanism (5) includes a drive motor (51), a transmission shaft (52), a motor support plate (54), and a transmission gear (53). The motor support plate (54) is located at the bottom of the launch cabin body (1). A drive motor (51) is provided on one side of the motor support plate (54). The drive shaft (52) is connected to the end of the shaft of the drive motor (51). A transmission gear (53) is provided at the end of the transmission shaft (52). An arc-shaped cut (531) is provided on the surface of the transmission gear (53).

7. The portable unmanned aerial vehicle launch pod according to claim 6, characterized in that, The launch cabin body (1) is provided with a cabin cover plate (7) on the top. A pivot support block (71) is provided on one side of the cabin cover plate (7). A pivot support plate (13) adapted to the pivot support block (71) is provided on the top of the launch cabin body (1). The pivot support block (71) and the pivot support plate (13) are rotatably connected.

8. The portable UAV launch pod according to claim 7, characterized in that, The launch cabin body (1) has rotatably connected cabin support legs (8) on its side wall surface.

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