Gas turbine engine exhaust nozzle including an infrared...

Power plants – Combustion products used as motive fluid – With exhaust treatment

Reexamination Certificate

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C060S770000, C181S213000

Reexamination Certificate

active

07418813

ABSTRACT:
A method for assembling a gas turbine engine includes mounting a core engine to a vehicle, coupling a fuselage radially outward and around the core engine, coupling an exhaust nozzle to the core engine to channel exhaust gases discharged from the core engine, wherein the exhaust nozzle includes a cowl and a primary nozzle coupled radially inward from the cowl, and coupling an infrared suppression system in flow communication with the engine exhaust nozzle to facilitate suppressing an exhaust infrared signature of the core engine, wherein the infrared suppression system includes a blocking fin having a substantially U-shaped cross-sectional profile and such that a cooling air flowpath is defined between the cowl and the blocking fin.

REFERENCES:
patent: 3027710 (1962-04-01), Maytner
patent: 4077206 (1978-03-01), Ayyagari
patent: 4117671 (1978-10-01), Neal et al.
patent: 4240252 (1980-12-01), Sargisson et al.
patent: 4335801 (1982-06-01), Stachowiak et al.
patent: 4592201 (1986-06-01), Dusa et al.
patent: 4696159 (1987-09-01), Horgan
patent: 4813230 (1989-03-01), Braithwaite
patent: 4819425 (1989-04-01), Farquhar et al.
patent: 5440875 (1995-08-01), Torkelson et al.
patent: 5761900 (1998-06-01), Presz, Jr.
patent: 5775095 (1998-07-01), Zysman et al.
patent: 5794432 (1998-08-01), Dunbar et al.
patent: 5884472 (1999-03-01), Presz et al.
patent: 5943856 (1999-08-01), Lillibridge et al.
patent: 6016651 (2000-01-01), Hammond et al.
patent: 6276127 (2001-08-01), Alberti
patent: 6502383 (2003-01-01), Janardan et al.
patent: 6606854 (2003-08-01), Siefker et al.
patent: 6804948 (2004-10-01), Oishi
patent: 6813877 (2004-11-01), Birch et al.
patent: 6854260 (2005-02-01), Anderson
patent: 6935098 (2005-08-01), Bardagi et al.
patent: 7017331 (2006-03-01), Anderson
patent: 7017332 (2006-03-01), Oishi
patent: 7114323 (2006-10-01), Schlinker et al.
patent: 7240493 (2007-07-01), Seiner
patent: 2003/0182925 (2003-10-01), Lair
patent: 2004/0159092 (2004-08-01), Anderson

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