A detachable UAV auxiliary aircraft
An unmanned aerial vehicle, a separate technology, applied in the field of rotorcraft, can solve problems such as single function, crash, machine damage, etc., and achieve the effect of good flight performance, strong endurance and safety.
Active Publication Date: 2019-06-11
SHANGHAI UNIVERSITY OF ELECTRIC POWER
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AI Technical Summary
Problems solved by technology
[0003] 1. Today's drones have a single functional structure
The structure and function of existing drones are often relatively single, and most of them use an integrated fuselage assembly, which is not flexible and convenient enough in design
[0004] 2. Today's drones have insufficient battery life
Due to the limitation of battery power, the existing drones often cannot meet the requirements of most users.
[0005] 3. Today's drones have a small range
Due to the lack of endurance or the limitation of the remote control signal sending and receiving distance, the range of today's drones is relatively small
[0006] 4. Today’s drones are prone to crashes
Because the battery power is not enough to return to the landing environment, or because the UAV fails, it will often cause crashes. Even if some existing UAVs are equipped with self-rescue devices such as self-rescue parachutes, this hard landing method will still cause serious damage to the aircraft. Some damage to the machine
[0007] 5. Today's drones cannot take off and land in certain environments
Existing UAVs cannot take off and land freely under the special environment of water surface, muddy ground or no-fly zone, which greatly limits the scope of application of UAVs today
Method used
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[0039] Such as Figure 1-Figure 10 As shown, the detachable UAV auxiliary aircraft includes a remote controller 15, an airborne platform assembly 11, a quadrotor aircraft assembly 13 and a detachable connector 6, an airborne platform assembly 11 and a quadrotor aircraft assembly 13 are connected by detachable connectors 6, the airborne platform assembly 11 includes the airborne platform frame, the airborne platform light 5 and the fixed mechanical arm module, the airborne platform frame is disc-shaped, and the airborne platform light 5 It is installed on the edge of the support of the airborne platform, and the fixed manipulator module is installed on the upper part of the frame of the airborne platform. The fixed robot arm module includes fixed robot arm 1, fixed robot arm recovery slot 2, chute 4 and moving roller 3, such as Figure 5 As shown, the fixed mechanical arm 1 is located in the fixed mechanical arm recovery groove 2, and the fixed mechanical arm 1 is provided wit...
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The invention relates to a detachable UAV auxiliary aircraft. The detachable UAV auxiliary aircraft includes a remote controller and a quadrotor aircraft assembly. The detachable UAV auxiliary aircraft also includes a detachable connector, machine Carrier platform assembly and pan-tilt camera, the airborne platform assembly is connected to the quadrotor aircraft assembly through a detachable connector, and the pan-tilt camera is installed at the bottom of the quadrotor aircraft assembly; the quadrotor aircraft assembly is used as a drone alone Or it can be used as a UAV auxiliary aircraft after being connected with the airborne platform assembly. When the UAV breaks down, it can be used as a UAV rescue machine to bring it back to the ground. Compared with the prior art, the present invention has the advantages of detachable design, can be used not only as a drone but also as a drone rescue machine, and has high rescue safety.
Description
technical field [0001] The invention relates to a rotorcraft, in particular to a detachable drone auxiliary aircraft. Background technique [0002] UAVs are developing rapidly, and various types of UAVs emerge in endlessly, but the structure and function of UAVs in the market today are single, and there is a lack of an unmanned aerial vehicle that can provide auxiliary functions for UAVs and serve UAVs. There are still many technical problems in existing drones, some of which are listed below: [0003] 1. Today's drones have a single functional structure. The structure and function of existing UAVs are often relatively simple, and most of them use an integrated fuselage assembly, which is not flexible and convenient in design. [0004] 2. Today's drones have insufficient battery life. Due to the limitation of the battery power of the existing drones, the battery life often cannot meet the requirements of most users. [0005] 3. Today's drones have a small range. Due to ...
Claims
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IPC IPC(8): B64D5/00B64D47/00B64C27/08
CPCB64C27/08B64D5/00B64D47/00B64U10/10B64U10/13B64U50/19B64U2101/00B64U80/82
Inventor 薛阳王舒郑梦秋杨天宇郑蓉张亚飞王琳
Owner SHANGHAI UNIVERSITY OF ELECTRIC POWER