Gas turbine engine shroud sealing arrangement

Details Gas turbine engine shroud sealing arrangement Gas turbine engine shroud sealing arrangement

2007-05-15

2007-05-15

Look, Edward K. (Department: 3745)

Rotary kinetic fluid motors or pumps

Bearing, seal, or liner between runner portion and static part

Resilient, flexible, or resiliently biased

C415S170100

Reexamination Certificate

active

11034764

ABSTRACT:
A ring seal is mounted in the annular gap between a shroud platform overhanging portion and the surrounding shroud support to minimize cooling air leakage through the shroud.

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