Gas turbine shroud structure

Rotary kinetic fluid motors or pumps – Including thermal expansion joint – Resilient

Reexamination Certificate

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Details

C415S137000, C415S138000

Reexamination Certificate

active

06932566

ABSTRACT:
There is disclosed a gas turbine shroud structure comprising: a shroud support component12attached to an inner surface of a gas turbine casing3; a shroud segment14divided in a peripheral direction and supported by the inner surface of the shroud support component; and a heat-resistant restricting spring18held between the shroud segment and shroud support component to urge the shroud segment inwards in a radial direction. The shroud segment14is formed of a ceramic composite material, and includes a coating layer15having heat insulation and impact absorption effect on an inner surface of the segment.

REFERENCES:
patent: 4676715 (1987-06-01), Imbault et al.
patent: 4768924 (1988-09-01), Carrier et al.
patent: 5188507 (1993-02-01), Sweeney
patent: 5192185 (1993-03-01), Leonard
patent: 6113349 (2000-09-01), Bagepalli et al.
patent: 6197424 (2001-03-01), Morrison et al.
patent: 6726448 (2004-04-01), Farrell et al.
patent: 10-103013 (1998-04-01), None
patent: 10-103014 (1998-04-01), None
UK Search Report dated Aug. 22, 2003.

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