Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes
Reexamination Certificate
2011-06-28
2011-06-28
Lee, Benjamin P (Department: 3641)
Aeronautics and astronautics
Aircraft, heavier-than-air
Helicopter or auto-rotating wing sustained, i.e., gyroplanes
C244S017230, C244S060000
Reexamination Certificate
active
07967239
ABSTRACT:
A drive system for a high speed rotary-wing aircraft includes a combiner gearbox in meshing engagement with a main gearbox. The combiner gearbox is driven by one or more engines such that a main rotor system and a translational thrust system are driven thereby. The engine drives the combiner gearbox and thus the main gearbox through an overrunning clutch. The drive system permits the main rotor system RPM to be controlled by offloading power to the translational thrust system during a high speed flight profile.
REFERENCES:
patent: 2041789 (1936-05-01), Stalker
patent: 2420764 (1947-05-01), Zuck
patent: 2644533 (1953-07-01), Maillard et al.
patent: 2698147 (1954-12-01), Hovgard
patent: 2731215 (1956-01-01), Avery
patent: 2959373 (1960-11-01), Zuck
patent: 3506219 (1970-04-01), Mouille et al.
patent: 3628755 (1971-12-01), Nagler
patent: 4488851 (1984-12-01), Young
patent: 4531692 (1985-07-01), Mateus
patent: 5738301 (1998-04-01), Francois et al.
patent: 6065718 (2000-05-01), Piasecki
patent: 6086016 (2000-07-01), Meek
patent: 7434764 (2008-10-01), Lappos et al.
Cotton Bryan Saxon
Gmirya Yuriy Z.
Tully, Jr. Thomas L.
Carlson & Gaskey & Olds PC
Lee Benjamin P
Sikorsky Aircraft Corporation
LandOfFree
Rotor drive and control system for a high speed rotary wing... does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Rotor drive and control system for a high speed rotary wing..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rotor drive and control system for a high speed rotary wing... will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-2621110