Solar-powered unmanned aerial vehicle and flying control method thereof
A technology of solar unmanned aerial vehicles and solar battery packs, which is applied in the field of unmanned aerial vehicles, can solve the problems of unmanned aerial vehicles such as short flight time, increased body weight, and short battery life, so as to achieve convenient detection and aerial photography, improve battery life, The effect of high power generation efficiency
Pending Publication Date: 2019-07-05
DONGJUN NEW ENERGY CO LTD
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Problems solved by technology
[0002] The biggest defect of the existing electric energy unmanned aerial vehicle or solar energy and electric energy complementary unmanned aerial vehicle is its short endurance time. If the flight time of the unmanned aerial vehicle is to be increased, the capacity of the battery must be increased, and the capacity of the battery will be increased. The weight of the drone, and when equipped with heavy detection, aerial photography, communication and other equipment, the flight time of the drone will be shorter
[0003] In addition, existing drones use multiple propellers, which are complex in structure and prone to failure
Method used
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[0037] The following is a clear and complete description of the technical solution of the present invention in conjunction with the accompanying drawings. Apparently, the described embodiments are part of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0038] An embodiment of the present invention provides a solar unmanned aerial vehicle, as attached Figure 1-2 As shown, it includes: a fuselage, a solar battery group wing 1 arranged on the fuselage, an equipment box 9 and a landing gear 8; an empennage 10 arranged at the tail of the fuselage; a lifting assembly arranged at the front of the fuselage And the steering assembly, the pulling assembly and the steering assembly only have one propeller 4 .
[0039] The fuselage in this embodiment has a fusela...
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The invention belongs to the technical field of unmanned aerial vehicles, and provides a solar-powered unmanned aerial vehicle and a flying control method thereof. The solar-powered unmanned aerial vehicle comprises a solar battery pack wing, an equipment box and an undercarriage which are arranged on a vehicle body of the unmanned aerial vehicle, and further comprises an empennage arranged at thetail of the vehicle body, a pull-up assembly and a steering assembly, wherein the pull-up assembly and the steering assembly are arranged on the front part of the vehicle body; and the pull-up assembly and the steering assembly are only provided with one propeller. The unmanned aerial vehicle only adopts one propeller, thus the structure of the unmanned aerial vehicle is simplified, and in sunnyweather with the large wind power, the unmanned aerial vehicle can fly at a constant speed and hover in air; and during flying, the solar battery pack wing converts a large amount of solar energy intoelectric energy to charge a storage battery and drive the propeller to rotate, and thus the endurance time of the solar-powered unmanned aerial vehicle is greatly prolonged.
Description
technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a solar-powered unmanned aerial vehicle and a flight control method thereof. Background technique [0002] Existing electric energy unmanned aerial vehicles or solar energy and electric energy complementary unmanned aerial vehicles, short battery life is its biggest defect, if want to increase the flight time of unmanned aerial vehicles, it is bound to increase the capacity of the storage battery, increase the capacity of the storage battery and increase the capacity of the machine. The weight of the drone, and when equipped with heavy detection, aerial photography, communication and other equipment, the flight time of the drone will be shorter. [0003] In addition, existing drones use multiple propellers, which are complex in structure and prone to failure. Contents of the invention [0004] The purpose of the present invention is to provide a so...
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IPC IPC(8): B64C3/00B64C39/02B64D27/24H02J7/35
CPCB64C3/00B64C39/02B64D27/24H02J7/35Y02T50/50
Inventor 莫怀友
Owner DONGJUN NEW ENERGY CO LTD