A tiltable active propulsion system suitable for miniature short-distance/vertical take-off and landing aircraft

Abstract

The invention provides a tiltable active power system of a miniature short distance / vertical take-off and landing aircraft, which is characterized in that it comprises: a fuselage (6), wings (71, 72), empennages (8, 9), propellers (2), the independently tiltable power system (1) for driving the propeller (2), so as to realize its vertical / short take-off and landing performance.

Description

technical field [0001] The invention relates to a power system scheme suitable for tilting active force adopted by miniature short-distance / vertical take-off and landing aircraft Background technique [0002] As far as the current situation is concerned, the STOL / VTOL aircraft is still in the experimental and trial stage of research and exploration. Considering the convenience of control and transmission, most of this type of aircraft adopt electric solutions—using electric motors as the power source. However, due to the technical limitations of the battery itself, the payload of electric aircraft is small, and the range / duration is short, which is difficult to pay. various practical applications. Contents of the invention [0003] The present invention is based on the application research of miniature short-distance / vertical take-off and landing aircraft, combined with the engineering background, and comprehensively considers the power requirements, control requirements ...

AI Technical Summary

Problems solved by technology

Considering the convenience of control and transmission, most of this type of aircraft adopt electric solutions—using electric motors as the power source. However, due to the technical limitations of the battery itself, the payload of electric aircraft is small, and the range / duration is short, which is difficult to pay. practical applications

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