Method and arrangement for providing a gas turbine, and...

Details Method and arrangement for providing a gas turbine, and... Method and arrangement for providing a gas turbine, and...

2005-04-26

2005-04-26

Gartenberg, Ehud (Department: 3746)

Power plants

Combustion products used as motive fluid

Process

C060S039230

Reexamination Certificate

active

06883331

ABSTRACT:
Method and arrangement for providing a gas turbine (1) having a first compressor (2), a combustion chamber (16) and a first turbine (11), the turbine being adapted to drive the compressor via a first shaft (10a,10b). The gas turbine also has a bleed valve (12) arranged upstream of the first turbine for conducting part of a gas compressed by the compressor past it during engine braking. The invention also relates to a method for engine-braking a gas turbine.

REFERENCES:
patent: 3710576 (1973-01-01), Evans et al.
patent: 3893292 (1975-07-01), Amann et al.
patent: 3915587 (1975-10-01), Rannenberg
patent: 5477673 (1995-12-01), Blais et al.
patent: 6122905 (2000-09-01), Liu
patent: 2734318 (1996-11-01), None

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