METHOD OF STABILIZING ARTICULATED ROTOR BLADE

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METHOD OF STABILIZING ARTICULATED ROTOR BLADE

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BREON JOSHUA A / PARSONS ERIC S / SUTTON CHRISTOPHER M / ADAMS WILLIAM PAUL / CONTI TIMOTHY JAMES / ANAPOLLE JARED / MEDRANO EVAN

Abstract

A rotor blade for a rotary wing aircraft includes a leading edge and a trailing edge defining a chordwise direction. The leading edge defines a forward end of the rotor blade and the trailing edge defines an aft end of the rotor blade. The rotor blade has a center of gravity and an aerodynamic center along the chordwise direction. The center of gravity is aft of the aerodynamic center.

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Title :

METHOD OF STABILIZING ARTICULATED ROTOR BLADE

Contributors:

BREON JOSHUA A (author) / PARSONS ERIC S (author) / SUTTON CHRISTOPHER M (author) / ADAMS WILLIAM PAUL (author) / CONTI TIMOTHY JAMES (author) / ANAPOLLE JARED (author) / MEDRANO EVAN (author)

Publication date :

2024-02-29

Type of media :

Patent

Type of material :

Electronic Resource

Language :

English

Classification :

IPC:

B64C AEROPLANES , Flugzeuge