Unmanned aerial vehicle provided with auxiliary lifting mechanism

A technology of unmanned aerial vehicles and power mechanisms, applied in the field of unmanned aerial vehicles, can solve the problems of reduced endurance, unfavorable energy saving and environmental protection, and large overall weight of unmanned aerial vehicles, so as to improve the effective utilization rate, improve endurance and reduce energy consumption Effect

Inactive Publication Date: 2017-06-13
珠海卡特瑞科农林航空装备研究所有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

It can be seen from the above that the overall weight of the UAV is relatively large. On the premise of not calculating the weight of the load part, the energy consumed by it to overcome ...

Method used

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  • Unmanned aerial vehicle provided with auxiliary lifting mechanism
  • Unmanned aerial vehicle provided with auxiliary lifting mechanism
  • Unmanned aerial vehicle provided with auxiliary lifting mechanism

Examples

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Embodiment Construction

[0022] An unmanned aerial vehicle with an auxiliary lifting mechanism, such as figure 1 , 2 , embodiment one shown in 3 and Figure 4 In the shown embodiment two, it includes a fuselage, a load mechanism 80 (an agricultural spraying box in the figure) and a power mechanism; the fuselage includes a frame 10, and several wings arranged on the frame 10 arm 20, the rotor device arranged at both ends of the wing arm 20, and the control mechanism arranged on the frame 10, the described rotor device includes a rotor motor 30 and a propeller 40; mechanism, the auxiliary lifting mechanism can generate buoyancy to float upwards in the air, and it is a bladder that contains gas and the density of the gas in it is smaller than that of air. The bladder is a balloon 90, The gas in it is hydrogen or helium. In addition, the buoyancy of the auxiliary lifting mechanism is not greater than the self-gravity of the fuselage, so that before the load mechanism of the drone is mounted on the fusel...

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Abstract

The invention relates to an unmanned aerial vehicle provided with an auxiliary lifting mechanism. The unmanned aerial vehicle provided with the auxiliary lifting mechanism comprises a fuselage, a load mechanism and a power mechanism, wherein the fuselage comprises a rack, a plurality of wing arms arranged on the rack, rotor wing devices arranged at the two ends of the wing arms and a control mechanism arranged on the rack, and each rotor wing device comprises a rotor wing motor and a propeller; and the unmanned aerial vehicle also comprises an auxiliary lifting mechanism which is connected and fixed on the fuselage, the auxiliary lifting mechanism can produce buoyancy force for floating upwards in air and is a bladder including gas inside, and the density of the gas inside the bladder is lower than the density of the air, and the buoyancy force of the auxiliary lifting mechanism is not more than the self gravity of the fuselage. The unmanned aerial vehicle provided by the invention has the advantages that the partial gravity of the fuselage is helped to be cancelled by virtue of the auxiliary lifting mechanism connected with the fuselage, so that the unmanned aerial vehicle is easier to take off and lift off and quickly enters a working condition, the energy consumption of a power mechanism is reduced, the cruising capability of the unmanned aerial vehicle is improved, the effective utilization rate of energy is increased, and energy conservation and environmental protection are realized.

Description

[0001] 【Technical field】 [0002] The invention relates to an unmanned aerial vehicle, in particular to an unmanned aerial vehicle with an auxiliary lifting mechanism. [0003] 【Background technique】 [0004] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. Due to its low cost, good cost-effectiveness, good maneuverability, and convenient use, it is currently used in aerial photography, agriculture, plant protection, selfie, express transportation, disaster relief, observing wild animals, monitoring infectious diseases, surveying and mapping, news reports, It is widely used in power inspection, disaster relief, film and television shooting and other fields. [0005] A UAV generally includes a body part, a control part, a power part and a load part; the body part is a frame, and a plurality of wing arms arranged on the frame; The rotor; the control part is the control mechanism arr...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C39/02B64B1/40
CPCB64B1/40B64C27/08B64C39/02B64U10/30B64U10/10B64U50/19
Inventor 黄彰标
Owner 珠海卡特瑞科农林航空装备研究所有限公司
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