Compound clearance control engine

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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Details

C060S785000

Reexamination Certificate

active

07823389

ABSTRACT:
A gas turbine engine includes a compressor, combustor, and turbine having a row of blades mounted inside a surrounding turbine shroud. A heat exchanger is used for cooling pressurized air bled from the compressor. A distribution network joins the heat exchanger to the turbine for selectively channeling air from the heat exchanger below the blades and above the shroud for controlling blade tip clearance.

REFERENCES:
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patent: 5205708 (1993-04-01), Plemmons et al.
patent: 5281085 (1994-01-01), Lenahan et al.
patent: 6487491 (2002-11-01), Karpman et al.
patent: 6612114 (2003-09-01), Klingels
patent: 6960060 (2005-11-01), Lee
patent: 7096673 (2006-08-01), Little et al.
patent: 2006/0042266 (2006-03-01), Albers et al.
General Electric Company, “CF6-80C2 Engine Airflow FADEC Control,” on sale and in public use in USA for more than one year before Sep. 1, 2006, two pages.
General Electric Company, “GE90-115B Engine Airflow,” Jun. 2006, three pages, on sale and in public use in USA for more than one year before Mar. 29, 2010.

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