Gas turbine engine and method for reducing turbine engine...

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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Details

C060S039281, C060S039463, C060S742000, C060S039465

Reexamination Certificate

active

08056344

ABSTRACT:
In a turbine engine hydrogen is injected into the combustor in response to a power output level of the turbine engine. In a preferred embodiment, gaseous hydrogen is always injected at low-power operations and switched off at mid-power and high-power operations.

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patent: 5694760 (1997-12-01), Baxter
patent: 5732546 (1998-03-01), Pineo et al.
patent: 6199366 (2001-03-01), Murata et al.
patent: 6609378 (2003-08-01), Scott
patent: 6640548 (2003-11-01), Brushwood et al.
patent: 2004/0226299 (2004-11-01), Drnevich
patent: 2006/0156729 (2006-07-01), Sprouse et al.

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