Helicopter having a fusilage section and a tail section...

Details Helicopter having a fusilage section and a tail section... Helicopter having a fusilage section and a tail section...

2007-10-09

2007-10-09

Dinh, Tien (Department: 3644)

Aeronautics and astronautics

Aircraft, heavier-than-air

Helicopter or auto-rotating wing sustained, i.e., gyroplanes

Reexamination Certificate

active

10849132

ABSTRACT:
A helicopter having: a flow control device provided at one of a lower portion of a side surface of a fuselage and a portion on a lower surface of the fuselage near the side surface and extending downward.

REFERENCES:
patent: 1361222 (1920-12-01), Berliner
patent: 2413625 (1946-12-01), Hays
patent: 2466821 (1949-04-01), Owen
patent: 3103327 (1963-09-01), Parry
patent: 3420472 (1969-01-01), Boudes
patent: 3774220 (1973-11-01), Martin et al.
patent: 4055303 (1977-10-01), Brown
patent: 4708305 (1987-11-01), Kelley et al.
patent: 5209430 (1993-05-01), Wilson et al.
patent: 5437419 (1995-08-01), Schmitz
patent: 5918832 (1999-07-01), Zerweckh
patent: 6086016 (2000-07-01), Meek
patent: 6352220 (2002-03-01), Banks et al.
patent: 2002/0125368 (2002-09-01), Phelps et al.

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