Compound helicopter drive means

Fluid reaction surfaces (i.e. – impellers) – Plural impellers having relative movement or independent... – Divergent rotation axes

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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.

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