Parachute support and stabilization for helicopter recovery...

Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes

Reexamination Certificate

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C244S139000, C244S140000

Reexamination Certificate

active

08074919

ABSTRACT:
A parachute support system for supporting a helicopter emergency parachute is provided, comprising a parachute support shaft located within a main rotor shaft, said parachute support shaft being rotationally separated from the rest of the helicopter through the use of bearing supports or enclosures. As the parachute support shaft is connected to the main rotor shaft at multiple distinct and distant points, the system described also provides a preferable load path transfer route, such that parachute system malfunction is minimized.

REFERENCES:
patent: 1705489 (1929-03-01), Mladinich
patent: 2812147 (1957-11-01), Trabucco
patent: 3138348 (1964-06-01), Stahmer
patent: 4709881 (1987-12-01), Rafikian et al.
patent: 5386781 (1995-02-01), Day
patent: 5826827 (1998-10-01), Coyaso et al.
patent: 5836544 (1998-11-01), Gentile
patent: 6199799 (2001-03-01), Lai
patent: 7546976 (2009-06-01), Li
patent: 7559506 (2009-07-01), Kissel, Jr.
patent: 2011/0101157 (2011-05-01), Kissel, Jr.
“The Plane with the Parachute—CAPS—Live With It.”—Cirrus Airframe Parachute System website—cirrusaircraft.com/parachute—retrieved on Oct. 6, 2009.

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