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Aircraft rescue unmanned plane

A technology of unmanned aerial vehicles and aircraft, applied in the field of unmanned aerial vehicles, can solve problems such as forced landings or crashes, increased safety hazards, losses and social impacts, and achieve high efficiency, reduce the incidence of air accidents, and have strong mobility. Effect

Active Publication Date: 2017-01-04
山东森亚信息科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the development of the aviation industry, the number of aircraft has increased, resulting in an increase in the number of accidents and potential safety hazards. It is difficult to rescue when problems occur during flight, and it is easy to cause forced landings or crashes, causing huge losses and social impact. , it becomes particularly important to reduce the probability of such accidents, so there is an urgent need for an aircraft rescue drone

Method used

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Embodiment Construction

[0014] The technical solutions of the present invention will be further specifically described below through the embodiments and in conjunction with the accompanying drawings.

[0015] like figure 1 , figure 2 , image 3 As shown, an aircraft rescue drone includes a frame 1, a propulsion device 2, and a grabbing mechanism 3, and is characterized in that: the propulsion device 2 is installed below the two main wings 102 of the frame 1; The grabbing mechanism 3 is installed above the two fuselages 101 of the frame 1;

[0016] The frame 1 includes 2 fuselages 101, 2 main wings 102, 2 auxiliary wings 103, a base plate 104, 2 main rudder surfaces 105, 2 auxiliary rudder surfaces 106, an energy storage module 107, a rear wheel 108, two front wheels 109, a control unit 110, and a fuel tank 111, the two fuselages 101 are fixedly connected through the base plate 104; the two main wings 102 are respectively fixedly installed on the sides of the two fuselages 101; The two auxiliarie...

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Abstract

The invention provides an aircraft rescue unmanned plane which comprises a machine frame, a propulsion device and a grabbing mechanism. The unmanned plane is characterized in that the propulsion device is installed below two main wings of the machine frame; and the grabbing mechanism is installed above two fuselages. The machine frame comprises the two fuselages, the two main wings, two auxiliary wings, a bottom plate, two main control surfaces, two auxiliary control surfaces, an energy storage module, a rear wheel, two front wheels, a control unit and a fuel tank, wherein the two fuselages are fixedly connected through the bottom plate. The aircraft rescue unmanned plane has high flexibility, and can quickly fly to the bottom of the aircraft to be rescued and fix the aircraft through the grabbing mechanism, so that the aircraft can land safely. The aircraft rescue unmanned plane has high efficiency, and lowers the air accident incidence rate.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to an aircraft rescue unmanned aerial vehicle. Background technique [0002] With the development of the aviation industry, the number of aircraft has increased, resulting in an increase in the number of accidents and potential safety hazards. It is difficult to rescue when problems occur during flight, and it is easy to cause forced landings or crashes, causing huge losses and social impact. , It becomes particularly important to reduce the probability of this type of accident, so there is an urgent need for a kind of aircraft rescue unmanned aerial vehicle. Contents of the invention [0003] In view of the above problems, the present invention provides an aircraft rescue UAV, which has strong maneuverability and can quickly fly to the bottom of the aircraft to be rescued, and fix the aircraft by a grabbing mechanism to make it land safely. [0004] The technical solution...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02
CPCB64C39/02B64U10/25B64U2101/00
Inventor 不公告发明人
Owner 山东森亚信息科技有限公司
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