Control apparatus for a starter/generator system
First Claim
1. A starter/generator system for an engine, comprising:
- a starter/generator including an exciter generator with a DC winding; and
a controller, for providing AC power to said exciter generator during a start mode of operation and DC power to said exciter generator during a generate mode of operation.
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Accused Products
Abstract
A control apparatus (202) for a starter/generator (110) of an aircraft electrical power system is provided. During a start mode of operation, AC power is provided by the control apparatus (202) to an exciter stator (114) of the starter/generator (110) which is combined with controlled AC power supplied by a start converter (106) to a main stator (116) of the starter/generator (110) to rotate and start an aircraft engine. Alternatively, during a generate mode of operation after engine start, the control apparatus (202) provides DC power to the starter/generator (110) to produce a regulated voltage output from the starter/generator (110).
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Citations
12 Claims
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1. A starter/generator system for an engine, comprising:
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a starter/generator including an exciter generator with a DC winding; and
a controller, for providing AC power to said exciter generator during a start mode of operation and DC power to said exciter generator during a generate mode of operation. - View Dependent Claims (2, 3, 4, 5, 6)
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7. A controller for a starter/generator, comprising:
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a logic circuit for receiving input signals and generating output signals based on said input signals;
a switching circuit for providing AC power to an exciter stator of a starter/generator system during a start mode of operation and DC power to said exciter stator during a generate mode of operation based on said output signals. - View Dependent Claims (8, 9, 10, 11, 12)
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Specification