Aircraft starter generator for variable frequency (vf) electrical system
AssigneeHamilton Sundstrand Corporation
InventorsMagdy A. Kandil, Keith R. Magnus, Don Baker
Life of this patent
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Abstract
A starter-generator for an aircraft engine comprises a variable dynamoelectric machine alternatively operable as a motor or as a generator, having a rotor. A support motor is coupled to the variable dynamoelectric machine to assist the machine. A torque converter selectively couples and decouples the rotor to the engine, coupling the rotor to the engine at some point when the dynamoelectric machine is operated as a motor. The engine may be started by the dynamoelectric machine when operated as a motor through a first power train including the torque converter and may drive the dynamoelectric machine as a generator through a second power train.
Claims20
A starter-generator for an engine comprising:
- a variable frequency dynamoelectric machine alternatively operable as a motor or as a generator, said variable frequency dynamoelectric machine having a rotor
- a torque converter for selectively coupling and decoupling said rotor to an aircraft engine, said torque converter for coupling said rotor to the engine when said variable frequency dynamoelectric machine is operated as a motor,
- a coupling for interconnecting said rotor and the engine at about the same speed when said rotor and the engine are coupled and operating to decouple said rotor from the engine for a speed of said rotor greater than a speed of the engine;
- and
- wherein the engine (a) may be started by said variable frequency dynamoelectric machine when operated as a motor through a first power train including said torque converter and (b) may drive said variable frequency dynamoelectric machine as a generator to create an electrical output of a frequency varying with the speed of the engine through a second power train including said coupling.
A starter-generator for an engine comprising:
- a variable frequency dynamoelectric machine alternatively operable as a motor or as a generator, said variable frequency dynamoelectric machine having a rotor;
- a torque converter for selectively coupling and decoupling said rotor to an aircraft engine, said torque converter for coupling said rotor to an engine when said variable frequency dynamoelectric machine is operated as a motor;
- a support motor coupled to said variable frequency dynamoelectric machine for assisting said variable frequency dynamoelectric machine in reaching a predetermined speed;
- a first coupling for interconnecting the engine and said torque converter and operating to decouple the engine from said torque converter for a speed of the engine greater than a speed of said torque converter;
- a second coupling for interconnecting said rotor and the engine at about the same speed when said rotor and the engine arm coupled and operating to decouple said rotor from said engine for a speed of said rotor greater than the speed or the engine;
- wherein the engine (a) may be started by said variable frequency dynamoelectric machine when operated as a motor through a first power train including said torque converter and said first coupling and (b) may drive said variable frequency dynamoelectric machine as a generator to create an electrical output of a frequency varying with the speed of the engine through a second power train including said second coupling;
- and
- wherein said torque converter decouples said rotor from said engine until said variable frequency dynamoelectric machine reaches said predetermined speed and couples said rotor to said engine after reaching said predetermined speed.
Dependencies are inferred from the claim text.