Aircraft generator starter-drive

Machine element or mechanism – Elements – Gear casings

Patent

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Details

123179AS, 123179R, F16H 4704

Patent

active

043154425

ABSTRACT:
This invention relates to a hydraulic control system for an aircraft starter-drive mechanism that includes a generator that can be driven as a motor drivingly connected through a differential, which is mutually connected to first and second hydraulic units and to an engine drive shaft during a start mode. The hydraulic control system includes a control valve arrangement, cooperatively coupled to the first and second hydraulic units, and operative in the starting mode to control flow between the hydraulic units, to thereby divide the delivery of rotary power from the generator/motor to the engine drive shaft through the differential and the hydraulic units.

REFERENCES:
patent: 3274855 (1966-09-01), Reynolds
patent: 3365981 (1968-01-01), Gantzer
patent: 3786696 (1974-01-01), Aleem
patent: 4046029 (1977-09-01), Sugden
patent: 4252035 (1981-02-01), Cordner

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