Gas turbine stator
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United States of America Patent
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Oct 31, 2006
Issued Date -
N/A
app pub date -
May 15, 2003
filing date -
Nov 15, 2000
priority date (Note) -
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Abstract
Stator (1) for a gas turbine including a stator structure (2) having a continuous through-duct (3) for a gas through-flow, a circumferential member (6), which is arranged at a radial distance from the stator structure and is operatively coupled to the stator structure, and at least one member for maintaining the distance between the stator structure and the circumferential member. The spacing member has resilient characteristics in the radial direction of the stator.
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