U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Brushless starter-generator with independently controllable exciter field

Patent 7301311 Issued on November 27, 2007. Estimated Expiration Date: Icon_subject February 22, 2026. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

3676764

3823357

3908161

Quadrature axis field brushless exciter
Patent #: 4093869
Issued on: 06/06/1978
Inventor: Hoffmann, et al.

Starter motor-alternator apparatus
Patent #: 4219739
Issued on: 08/26/1980
Inventor: Greenwell

Aircraft engine starting with synchronous ac generator
Patent #: 4473752
Issued on: 09/25/1984
Inventor: Cronin

System and method employing a digital computer for automatically synchronizing a gas turbine or other electric power plant generator with a power system
Patent #: 4536126
Issued on: 08/20/1985
Inventor: Reuther

Starter-generator for engines
Patent #: 4743776
Issued on: 05/10/1988
Inventor: Baehler ,   et al.

Starter generator system with two stator exciter windings
Patent #: 4743777
Issued on: 05/10/1988
Inventor: Shilling ,   et al.

Inverter operated turbine engine starting system
Patent #: 4786852
Issued on: 11/22/1988
Inventor: Cook

More ...

Inventors

Assignee

Application

No. 11360116 filed on 02/22/2006

US Classes:

322/59, With excitation winding and/or circuit control322/29, Speed or frequency of generator322/37, Electrical conditions in circuit other than that of generator being controlled322/46, Combined permanent magnet and wound field structure290/31, Starting and generating dynamo318/718, Induced voltage in field winding322/10, WITH PHYSICAL STARTING AND/OR STOPPING OF THE GENERATOR322/68, Short circuiting of field winding290/52, TURBOGENERATORS290/1CDrive gearing

Examiners

Primary: Ponomarenko, Nicholas

Attorney, Agent or Firm

International Class

H02P 9/44

Abstract

A starter-generator system supplies a controllable torque to a gas turbine engine, to thereby assist in starting the gas turbine engine, by independently controlling excitation frequency and/or voltage magnitude. The starter-generator includes a multi-phase exciter stator, a rotationally mounted multi-phase exciter rotor, a multi-phase main stator, a rotationally mounted multi-phase main rotor, and an exciter controller. The rotationally mounted multi-phase exciter rotor has a plurality of exciter rotor windings wound thereon that, upon excitation thereof with a rotating electromagnetic exciter flux generated by the exciter stator, have non-rectified excitation currents induced therein. The rotationally mounted multi-phase main rotor has a plurality of main rotor windings wound thereon that are electrically connected to receive the non-rectified excitation currents induced in the exciter rotor windings and that, upon excitation thereof with a rotating electromagnetic flux and in response to the non-rectified excitation currents supplied thereto, have currents induced therein that generate a main rotor torque to thereby cause the multi-phase main rotor and the multi-phase exciter rotor to rotate. The exciter controller is electrically coupled to at least the exciter stator and is configured to selectively supply the electrical excitation thereto, to thereby selectively control the generated main rotor torque.

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