MULTIPLE CONTROL LOOP ACCELERATION OF TURBOALTERNATOR AFTER REACHING SELF-SUSTAINING SPEED PREVIOUS TO REACHING SYNCHRONOUS SPEED

Title:

MULTIPLE CONTROL LOOP ACCELERATION OF TURBOALTERNATOR AFTER REACHING SELF-SUSTAINING SPEED PREVIOUS TO REACHING SYNCHRONOUS SPEED

Document Type and Number:

WIPO Patent Application WO2004025100

Kind Code:

A3

Abstract:

The invention is a method of operating a turboalternator when turbine speed is between synchronous speed and self-sustaining speed. A control system (40) adjusts a fuel valve (44) in response to a signal from an exhaust gas temperature sensor (42).

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Inventors:

HARTZHEIM ANTHONY A (US)

Application Number:

PCT/US2003/029326

Publication Date:

August 12, 2004

Filing Date:

September 15, 2003

Export Citation:

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Assignee:

ELLIOTT ENERGY SYSTEMS INC (US)
HARTZHEIM ANTHONY A (US)

International Classes:

F01D15/10; F02C9/28; (IPC1-7): F02C7/26; F02C9/26

Foreign References:

US4627234A	1986-12-09
US5157918A	1992-10-27
US6487096B1	2002-11-26
US6612112B2	2003-09-02

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