Combustion chamber of a gas turbine engine with an upstream...

Details Combustion chamber of a gas turbine engine with an upstream... Combustion chamber of a gas turbine engine with an upstream...

2006-09-01

2009-11-17

Casaregola, Louis J (Department: 3741)

Power plants

Combustion products used as motive fluid

Having mounting or supporting structure

C060S752000

Reexamination Certificate

active

07617688

ABSTRACT:
The present invention is concerned with an annular combustion chamber of a gas turbine engine with an external annular wall and an internal annular wall, including an upstream fairing for separating the gas stream at the inlet of the chamber into a combustion stream and a bypass stream which bypasses the inlet of the chamber, the fairing including an annular wall forming a cap, which includes a downstream portion for fastening to a wall of the chamber and an upstream portion forming an edge of the flow cross section for the combustion stream, wherein the upstream portion is continued into at least one additional downstream portion for fastening to the wall of the chamber.

REFERENCES:
patent: 6449952 (2002-09-01), Emilianowicz et al.
patent: 0 564 171 (1993-10-01), None
patent: 1 251 312 (2002-10-01), None
patent: 1 265 031 (2002-12-01), None
patent: 1 398 571 (2004-03-01), None

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