FIXED OR CONTROLLED PROPELLER BLADE TIP (WINGLET) Russian patent published in 2015 - IPC B64C11/20 B64C27/473 B63H1/16 

Abstract RU 2546337 C1

FIELD: transport.

SUBSTANCE: blade tip made as and winglet represents blade profile divided into upper and lower parts. Each part of end winglet can have fixed or adjustable angle of attack independent from angle of attack of the other part.

EFFECT: lower power losses of propeller drive, improved blade aerodynamics, increased lifting and pulling force and propeller efficiency.

1 dwg

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RU 2 546 337 C1

Authors

Beloglazov Sergej Nesterovich

Dates

2015-04-10Published

2014-02-04Filed