Aviation engine

Abstract

The invention discloses an aviation engine, and belongs to the technical field of aviation. The aviation engine comprises a first power source, a second power source and a starter, wherein the first power source is provided with a first shaft; the second power source is provided with a second shaft; the starter is separately connected to the first shaft and the second shaft movably; the first shaft and the second shaft are separately connected to a rotor wing of an unmanned aerial vehicle; the rotated first shaft and the rotated second shaft are started for pressing pre-injected comburent, so that mechanical dynamic energy is generated for driving the first shaft and the second shaft to continuously rotate, and rotor rings of the unmanned aerial vehicle are driven to rotate through the first shaft and the second shaft. The aviation engine is applied to the unmanned aerial vehicle; the first power source and the second power source are arranged for combusting the pre-injected comburent to generate mechanical dynamic energy, so that power is provided for rotating the rotor rings, a conventional electric flight mode of increasing endurance time by supplying power through batteries or increasing quantity of batteries is replaced, and therefore, the unmanned aerial vehicle applying the aviation engine has characteristics of long endurance time and high load-bearing capacity.

Description

technical field [0001] The invention belongs to the field of aviation technology, in particular to an aeroengine. Background technique [0002] Aircraft (English abbreviation: Unmanned Aerial Vehicle) is a kind of unmanned aircraft mainly controlled by radio remote control or by its own program. [0003] Aircraft in the prior art are mostly electric aircraft, which mainly use main components such as batteries, electric regulators, motors, flight controllers, and propellers. The flight control of the aircraft is realized by changing the speed of each propeller. However, due to the limitation of battery energy density, this type of electric aircraft generally has a very short flight time and has the disadvantage of poor endurance performance, and the method of simply increasing the number of batteries to increase its flight time will also greatly reduce its flight time. load capacity. Contents of the invention [0004] The invention provides an aero-engine, which is applie...

AI Technical Summary

Problems solved by technology

However, due to the limitation of battery energy density, this type of electric aircraft generally has a very short flight time and has the disadvantage of poor endurance performance, and the method of simply increasing the number of batteries to increase its flight time will also greatly reduce its flight time. load capacity

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