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

Gas turbine engine driven auxiliary electric power unit with turbine speed controlled in response to generator output current

Patent 5635768 Issued on June 3, 1997. Estimated Expiration Date: Icon_subject April 28, 2015. 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

3342999

3764815

Turbine inlet temperature control apparatus and method
Patent #: 4219738
Issued on: 08/26/1980
Inventor: Griesinger

Control apparatus for controlling surge in air compressor-driven system
Patent #: 4309871
Issued on: 01/12/1982
Inventor: Venema

Electronic phase shift and speed governor
Patent #: 4399397
Issued on: 08/16/1983
Inventor: Kleinschmidt, Jr.

Power plant with a gas turbine for operation of a generator
Patent #: 4421989
Issued on: 12/20/1983
Inventor: Brannstrom

Closed cycle gas turbine for gaseous production
Patent #: 4434613
Issued on: 03/06/1984
Inventor: Stahl

Synchronization fuel control for gas turbine-driven AC generator by use of maximum and minimum fuel signals
Patent #: 4492874
Issued on: 01/08/1985
Inventor: Near

Rapid power response turbine
Patent #: 4529887
Issued on: 07/16/1985
Inventor: Johnson

Protection of gas engine or turbine from damage by changes in operating characteristics
Patent #: 4959896
Issued on: 10/02/1990
Inventor: Bolin, et al.

More ...

Inventors

Assignee

Application

No. 430373 filed on 04/28/1995

US Classes:

290/40C, Control in response to generator and prime mover conditions290/52TURBOGENERATORS

Examiners

Primary: Stephan, Steven L.
Assistant: Cuneo, Christopher

Attorney, Agent or Firm

Foreign Patent References

  • 60187721 JP. 02/13/1986
  • 60257795 JP. 05/13/1986
  • 1032606 GB. 06/13/1966
  • 2141785 GB. 01/13/1985
  • 2205207 GB. 11/13/1988

International Classes

H02P 009/04
F02C 009/56

Foreign Application Priority Data

1994-04-30 GB

Abstract

A gas turbine engine driven auxiliary electric power unit which includes a turbine (9), an air compressor (7) for supplying compressed air to the turbine and driven by the turbine, fuel supplying means (2) for supplying gaseous fuel to the turbine, a generator (10) driven by the turbine for generating electrical output power which is fed to a main electric user supply (14), first detecting means (15) for monitoring turbine shaft speed, second detecting means (19) for monitoring the output power of the generator, first modulating means (16,18,13) for modulating the turbine shaft speed to cause it to coincide with a predetermined shaft speed (17) by means of controlling current flow from the generator to the main electric user supply, and second modulating means (20,22,23) for modulating the flow of gaseous fuel which is supplied from the fuel supplying means to the turbine so as to cause the monitored output power to coincide with a predetermined output power (21).

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