Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes
Patent
1994-08-30
1996-12-31
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft, heavier-than-air
Helicopter or auto-rotating wing sustained, i.e., gyroplanes
415119, 416203, B64C 2782
Patent
active
055886183
ABSTRACT:
A flow-straightener with stationary vanes and aerodynamic profile is mounted downstream of the rotor with blades in the transverse duct passing through the fairing at the tail of the helicopter. The blades of the rotor are distributed angularly about the axis of the rotor with uneven azimuth modulation, such that any angle between two arbitrary blades of the rotor is different from any angle between two arbitrary vanes of the flow-straightener.
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Proceedings of the nineteenth european rotorcraft forum 14 Sep. 1993, CERNOBBIO : "A new generation of fenestron fan-in-fin tail rotor on EC 135".
"Noise Reduction by Applying Modulation Principles" by Donald Ewald et al, published in The Journal of Acoustical Society of America, vol. 49, No. 5, 1971, pp. 1381-1385.
Arnaud Gilles L.
Arnaud Remy E.
Marze Henri-James R.
Routhieau Vincent Jean-Luc
Barefoot Galen L.
Eurocopter France
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