Simple launching device for unmanned aerial vehicle

Abstract

A simple launching device for an unmanned aerial vehicle relates to the technical field of unmanned aerial vehicles and comprises a supporting module and a bunching and releasing module. The binding and releasing module is arranged on the supporting module in the take-off direction of the unmanned aerial vehicle and comprises a binding band ring, a steering engine, a rotating crank and a limiting seat, the limiting seat is provided with a first limiting hole, the steering engine is connected with one end of the rotating crank, and the other end of the rotating crank extends into the first limiting hole of the limiting seat; the bandage ring is used for binding the unmanned aerial vehicle, one end of the bandage ring is in a fixed state, and the other end of the bandage ring sleeves the other end of the rotating crank extending out of the first limiting hole; wherein the rotating crank is driven by the steering engine, so that the other end of the rotating crank is contracted, and the bandage ring is separated from the rotating crank. The unmanned aerial vehicle launcher is simple in structure, convenient to maintain, high in reliability, capable of rapidly launching unmanned aerial vehicles which cannot meet conditions such as taxiing, takeoff and the like, high in universality and capable of meeting requirements of fixed-wing unmanned aerial vehicles of various models.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned aerial vehicle technical field especially, relate to a simple launching device of unmanned aerial vehicle. BACKGROUND

[0002] At present, the launching of fixed-wing unmanned aerial vehicle usually relies on specific boost mode or runway, and these modes have limitations in specific application scenarios. For example, in the environment with complex terrain or limited space, the traditional launching mode may not be feasible or the cost is too high. The utility model aims to provide a novel launching mechanism to adapt to more extensive application requirements and shorten the development cycle of fixed-wing unmanned aerial vehicle. SUMMARY

[0003] The utility model aims at solving above-mentioned problem among the prior art, provide a simple launching device of unmanned aerial vehicle, when taking off, the unmanned aerial vehicle cannot satisfy the sliding run, and the utility model discloses the following technical scheme:

[0004] In order to achieve the above object, the utility model adopts the following technical scheme:

[0005] A simple launching device of unmanned aerial vehicle, including support module and bundle release module, the bundle release module is set on the support module along the direction of unmanned aerial vehicle takeoff, the bundle release module includes binding belt ring, steering wheel, rotating crank and limit seat, the limit seat is equipped with first limit hole, the steering wheel is connected one end of rotating crank, and the other end of rotating crank extends into the first limit hole of limit seat, the binding belt ring is used for binding unmanned aerial vehicle, and one end of binding belt ring is in fixed state, and the other end of binding belt ring is sleeved on the other end of rotating crank extending from the first limit hole, wherein, through the steering wheel drive rotating crank, the other end of rotating crank is retracted to make the binding belt ring separate from rotating crank.

[0006] The bundle release module further includes bundle release base for setting steering wheel, binding belt ring, rotating crank and limit seat.

[0007] One side of the bundle release base is equipped with steering wheel mounting plate for installing steering wheel, and the other side is equipped with fixing ring for fixing one end of binding belt ring.

[0008] The middle part of the bundle release base is annularly recessed.

[0009] The limit seat is U-shaped, and further provided with a second limit hole opposite to the first limit hole.

[0010] The binding belt ring is made of elastic rubber band.

[0011] The bottom of the support module is provided with a suction cup.

[0012] The utility model further includes a height increasing block, the height increasing block is located between the support module and the bundle release module.

[0013] Compared with the prior art, the utility model discloses technical scheme has obtained the beneficial effect is:

[0014] The launching device simple structure is convenient for maintenance, has very high reliability, and can quickly carry out launching task for the unmanned plane that cannot satisfy the condition such as sliding take-off, and also has very strong universality, can satisfy multiple models of fixed wing unmanned plane. BRIEF DESCRIPTION OF DRAWINGS

[0015] Figure 1 It is one of the overall structure schematic diagram of the utility model;

[0016] Figure 2 It is the side view schematic diagram of the utility model;

[0017] Figure 3 It is the second overall structure schematic diagram of the utility model;

[0018] Figure 4 It is one of the structure schematic diagram of the bundle module;

[0019] Figure 5 It is the second structure schematic diagram of the bundle module;

[0020] Figure 6 It is the schematic diagram of the rotating crank of the bundle module in the retracted state;

[0021] Figure 7 It is the schematic diagram of the rotating crank of the bundle module in the extended state.

[0022] Reference signs: suction cup 11, support frame 12, bandage ring 21, rudder 22, bundle base 23, fixed ring 24, rudder mounting plate 25, rotating crank 26, limit seat 27, first limit hole 271, second limit hole 272, heightening block 10. DETAILED DESCRIPTION

[0023] In order to make the technical problem, technical scheme and beneficial effect of the utility model to be solved more clearly, the following is in combination with the drawings and examples, and the utility model is further explained in detail.

[0024] See Figures 1-7 The embodiment of the utility model discloses a simple launching device of unmanned plane, including support module, bundle module, heightening block 10;

[0025] The support module is erected along the direction of take-off of unmanned plane, and the top of support module is used for setting bundle module;The bundle module is set on the support module along the direction of take-off of unmanned plane;The heightening block 10 is located between the support module and bundle module at the front end of the device;

[0026] Specifically, the support module includes a support frame 12 and a suction cup 11. The suction cup 11 is provided at the bottom of the support frame 12 and is used to fix the support frame 12.

[0027] The beam release module includes a beam release base 23, a strap ring 21, a steering gear 22, a rotating crank 26 and a limit seat 27;

[0028] The traction base 23 is used to accommodate the servo 22, the strap ring 21, the rotating crank 26, and the limit seat 27. One side of the traction base 23 is provided with a servo mounting plate 25 for mounting the servo 22, and the other side is provided with a fixing ring 24 for fixing one end of the strap ring 21. The middle portion of the traction base 23 is annularly recessed.

[0029] The limiting seat 27 is U-shaped and has a first limiting hole 271 and a second limiting hole 272 opposite to the first limiting hole 271 at the U-shaped portion. The servo 22 is connected to one end of the rotating crank 26, and the other end of the rotating crank 26 extends into the first limiting hole 271 of the limiting seat 27.

[0030] The strap ring 21 is used to bind the drone. One end of the strap ring 21 is connected to the fixing ring 24 in a fixed state, and the other end of the strap ring 21 is sleeved on the other end of the rotating crank 26 extending from the first limiting hole 271.

[0031] The servo 22 drives the rotating crank 26 to cause the other end of the rotating crank 26 to contract, thereby separating the strap ring 21 from the rotating crank 26 .

[0032] In this embodiment, the strap ring 21 can be made of cloth material, and more preferably made of elastic rubber band.

[0033] The working principle of this utility model is as follows:

[0034] 1. Tie the drone to the support module with the harness module. The support module is placed on a mobile vehicle such as a car or boat. As the vehicle / boat moves, when the drone reaches its takeoff speed, the harness module releases the drone and the drone takes off with its own lift.

[0035] 2. The principle of the harness release module releasing the restraint on the drone is as follows: since the strap ring 21 is placed on the rotating crank 26 extending from the first limiting hole 271, the drone is restrained. When the rotating crank 26 is driven by the servo 22, the other end of the rotating crank 26 contracts, thereby separating the strap ring 21 from the rotating crank 26, and the strap ring 21 releases the drone.

[0036] 3、When the unmanned aerial vehicle is fixed, the rotating crank 26 is driven by the steering engine 22 to make the other end of the rotating crank 26 extend from the first limiting hole 271, then the band ring 21 is hooked on the rotating crank 26, so that the band ring 21 binds the unmanned aerial vehicle, further, the rotating crank 26 can continue to extend until the second limiting hole 272;

[0037] 4、The purpose of the heightening block 10 is to pad the unmanned aerial vehicle, two binding modules arranged along the take-off direction of the unmanned aerial vehicle are used in the embodiment, the binding module in the front part of the unmanned aerial vehicle is padded by the heightening block 10, so that the unmanned aerial vehicle obtains a certain angle when taking off, and the take-off of the unmanned aerial vehicle is facilitated.

[0038] 5、For different unmanned aerial vehicles, the middle part of the binding base 23 can be provided with an annular recess in the embodiment.

[0039] The launching device has simple structure, is convenient to maintain, has high reliability, can quickly perform a launching task for the unmanned aerial vehicle which cannot meet the conditions such as sliding take-off, and has strong universality and can meet the unmanned aerial vehicles of various models.

[0040] It should be explained that: first, in the description of the utility model, it should be explained that unless otherwise provided and limited, the terms "installation", "connection", "connection" should be understood broadly, which can be mechanical connection or electrical connection, can be the communication between the two elements, can be directly connected, "up", "down", "left", "right" and the like are only used to indicate the relative position relationship, when the absolute position of the described object changes, the relative position relationship can change. Secondly: the embodiment of the utility model disclosed in the embodiment of the utility model only relates to the structure related to the embodiment of the disclosure, other structures can refer to the general design, under the condition of no conflict, the same embodiment and different embodiments of the utility model can be combined with each other. Finally, the above is only the preferred embodiment of the utility model, the protection scope of the utility model is not limited to the above-mentioned embodiment, and the technical solutions under the idea of the utility model belong to the protection scope of the utility model.

Claims

1. A simple launch device for a UAV, characterized by: It includes a support module and a bundling module; the bundling module is arranged on the support module along the take-off direction of the drone; the bundling module includes a strap ring, a servo, a rotating crank and a limit seat, the limit seat is provided with a first limit hole, the servo is connected to one end of the rotating crank, and the other end of the rotating crank extends into the first limit hole of the limit seat; the strap ring is used to bind the drone, one end of the strap ring is in a fixed state, and the other end of the strap ring is sleeved on the other end of the rotating crank extending from the first limit hole; wherein, the rotating crank is driven by the servo to cause the other end of the rotating crank to contract so that the strap ring is separated from the rotating crank.

2. The simple launch device for unmanned aerial vehicles according to claim 1, characterized in that: The bundle release module also includes a bundle release base for arranging a servo, a strap ring, a rotating crank and a limit seat.

3. The simple launch device for unmanned aerial vehicles according to claim 2, characterized in that: One side of the bundle base is provided with a servo mounting plate for installing a servo, and the other side is provided with a fixing ring for fixing one end of the strap ring.

4. The simple launch device for unmanned aerial vehicles according to claim 2, characterized in that: The middle portion of the beam-releasing base is arranged in an annular recess.

5. The simple launch device for unmanned aerial vehicles according to claim 1, characterized in that: The limiting seat is U-shaped and further provided with a second limiting hole opposite to the first limiting hole.

6. The simple launch device for unmanned aerial vehicles according to claim 1, characterized in that: The strap ring is made of an elastic rubber band.

7. The simple launch device for unmanned aerial vehicles according to claim 1, characterized in that: A suction cup is provided at the bottom of the supporting module.

8. The simple launch device for unmanned aerial vehicles according to claim 1, characterized in that: It also includes a heightening block, which is arranged at the front end of the device and located between the supporting module and the beam releasing module.

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