Components for a gas turbine engine

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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Details

C060S039530

Reexamination Certificate

active

07854125

ABSTRACT:
An aerofoil assembly including an aerofoil and a spray element that supplies fluid to a gas turbine engine. The aerofoil has a first part with a leading edge when located in the gas turbine engine, and a second part with a trailing edge when located in the gas turbine engine. The first part has features that slide relative to and engage with complementary features of the second part to form a releasable arrangement.

REFERENCES:
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patent: 4887425 (1989-12-01), Vdoviak
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patent: 5899061 (1999-05-01), Bouchez et al.
patent: 6003297 (1999-12-01), Ziegner
patent: 6322322 (2001-11-01), Rhodes et al.
patent: 2004/0120811 (2004-06-01), Darkins et al.
patent: 2008/0203236 (2008-08-01), Mazzola et al.
patent: 2009/0145100 (2009-06-01), Omielan et al.
patent: 102 54 721 (2004-06-01), None
patent: 1 548 231 (2005-06-01), None
patent: WO 2004/111392 (2004-12-01), None

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