Methods and apparatus for operating gas turbine engines

Rotary kinetic fluid motors or pumps – With separating means or guard for solid matter in working...

Reexamination Certificate

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C415S116000, C415S173100, C415S213100

Reexamination Certificate

active

07607885

ABSTRACT:
A method of operating a gas turbine engine is provided. The method includes channeling cooling air towards a shroud hanger assembly such that the cooling air flows through a cavity defined in the shroud hanger assembly, directing the cooling air through a plurality of cooling passages extending from the cavity, and discharging the air from the plurality of cooling passages towards an impingement baffle to facilitate cooling a shroud hanging from the shroud hanger.

REFERENCES:
patent: 4292008 (1981-09-01), Grosjean et al.
patent: 4573865 (1986-03-01), Hsia et al.
patent: 5169287 (1992-12-01), Proctor et al.
patent: 6726446 (2004-04-01), Arilla et al.
patent: 7147432 (2006-12-01), Lowe et al.

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