Fluid reaction surfaces (i.e. – impellers) – Plural impellers having relative movement or independent... – Divergent rotation axes
Patent
1975-11-17
1976-08-31
Blix, Trygve M.
Fluid reaction surfaces (i.e., impellers)
Plural impellers having relative movement or independent...
Divergent rotation axes
416169R, 416170R, 244 1719, B64C 2722
Patent
active
039778126
ABSTRACT:
Compound helicopters, those having a rotor blade and a small wing, possess rear propulsion propeller adjacent to the tail rotor. The tail gearbox is driven through a drive train coupled to the main rotor drive shaft. In such aircraft the tail rotor is in operation when the propulsion propeller is turning, and vice versa. A mechanism is provided herein for stopping or feathering the tail rotor when driving the propulsion propeller, or for stopping the propulsion propeller when the tail rotor is in operation.
REFERENCES:
patent: 1154769 (1915-09-01), Hertzberg
patent: 2401365 (1946-06-01), Mercier
patent: 2771143 (1956-11-01), Campbell
patent: 2838913 (1958-06-01), Peterson et al.
patent: 2890604 (1959-06-01), Campbell
patent: 3190414 (1965-06-01), Maurer et al.
patent: 3468192 (1969-09-01), Nasvytis
patent: 3540680 (1970-11-01), Peterson
patent: 3679033 (1972-07-01), Wagner
patent: 3851546 (1974-12-01), Kepple et al.
Barefoot Galen L.
Blix Trygve M.
The United States of America as represented by the Secretary of
Wilson, Jr. Norman L.
LandOfFree
Compound helicopter drive means does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Compound helicopter drive means, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Compound helicopter drive means will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1813031