Gas turbine combustion chamber and air guidance method...

Details Gas turbine combustion chamber and air guidance method... Gas turbine combustion chamber and air guidance method...

2005-01-04

2005-01-04

Kim, Ted (Department: 3746)

Power plants

Combustion products used as motive fluid

Combustion products generator

C060S756000, C060S757000, C060S758000, C060S760000

Reexamination Certificate

active

06837053

ABSTRACT:
In order to provide a method of air guidance and a design for a gas turbine combustion chamber which permits improved cooling and reduced pressure losses and which avoids the overcooling phenomena by specific reaction to hot spots, a gas turbine combustion chamber includes a casing and at least one hollow element. The at least one hollow element is in connection with air guidance regions of the combustion chamber via at least two openings. As such, a tangential through-flow exists with a subsequent axial flow to the burner.

REFERENCES:
patent: H001380 (1994-12-01), Halila et al.
patent: 5467815 (1995-11-01), Haumann
patent: 5737922 (1998-04-01), Schoenman
patent: 6047552 (2000-04-01), Gross
patent: 6276142 (2001-08-01), Putz
patent: 0 624 757 (1994-05-01), None
patent: WO9909354 (1999-02-01), None

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