Methods for regulating gas turbine engine fluid flow

Power plants – Combustion products used as motive fluid – For nominal other than power plant output feature

Reexamination Certificate

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Reexamination Certificate

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06986257

ABSTRACT:
A method enables a gas turbine engine to be operated. The method includes directing fluid flow from a source into an inlet of a valve, channeling the fluid flow entering an inlet portion of the valve towards an outlet portion of the valve such that a direction of the fluid flow is changed within the inlet portion, and controlling the amount of fluid flow entering the outlet portion of the valve by selectively positioning a valve disk coupled within the inlet portion of the valve by a valve disk axle. The method also comprises channeling the fluid flow from the inlet portion of the valve through the outlet portion of the valve and into a fluid supply pipe, wherein the valve outlet portion has a substantially right cylindrical shape such that a direction of fluid entering the body outlet portion remains substantially constant therethrough.

REFERENCES:
patent: 2837270 (1958-06-01), Chapman
patent: 4916893 (1990-04-01), Rodgers
patent: 5396760 (1995-03-01), Hines
patent: 6722137 (2004-04-01), Proctor et al.

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