Cooling joint connection for abutting segments in a gas turbine

Rotary kinetic fluid motors or pumps – Including thermal expansion joint

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415139, F01D 2526

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active

058237410

ABSTRACT:
A seal joint including a sealing member for sealing segmented components of a gas turbine engine is spaced from the gas path to provide more effective cooling. The segments include radial extension flanges spacing the seal joint from the gas path. Various cooling arrangements are adaptable to the modified segments to provide for open or closed circuit impingement or convection cooling plus film cooling. Excessive thermal gradients are avoided as the entire corner of the segment is evenly cooled. Moreover, air usage at the joint is bounded by seal leakage with no extra dedicated cooling air.

REFERENCES:
patent: 2863634 (1958-12-01), Chamberlin et al.
patent: 4537024 (1985-08-01), Grosjean
patent: 4650394 (1987-03-01), Weidner
patent: 4676715 (1987-06-01), Imbault et al.
patent: 5158430 (1992-10-01), Dixon et al.
patent: 5167485 (1992-12-01), Starkweather
patent: 5374161 (1994-12-01), Kelch et al.
patent: 5609469 (1997-03-01), Worley et al.
patent: 5634766 (1997-06-01), Cunha et al.

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