VERTICAL TAKEOFF AND LANDING AIRCRAFT Russian patent published in 2017 - IPC B64C29/00 B64C27/08 

Abstract RU 2627220 C1

FIELD: aviation.

SUBSTANCE: aircraft includes a basic frame of a spatial structure, a seat, a cabin, controls, motors, a control system, a remote control system. The basic support frame is made with a central part and with two peripheral clusters on the right and left on the flight. Peripheral clusters can be folded up, down or pushed under the central part. The central part and peripheral clusters of the frame are made with a spatial construction. Each peripheral cluster is made of at least three identical sections connected to each other. Inside each section, there is a motor installation containing at least one engine and at least one horizontal rotation propeller.

EFFECT: increase of fault tolerance, safety, and maintainability of the aircraft of vertical take-off and landing.

24 cl, 34 dwg

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RU 2 627 220 C1

Authors

Igor Chudakov

Shanin Aleksej Viktorovich

Igor Chudakov

Dates

2017-08-04Published

2016-07-26Filed