Gas turbine and gas turbine high temperature section cooling...

Details Gas turbine and gas turbine high temperature section cooling... Gas turbine and gas turbine high temperature section cooling...

2006-01-31

2006-01-31

Gartenberg, Ehud (Department: 3746)

Power plants

Combustion products used as motive fluid

Process

C060S806000

Reexamination Certificate

active

06990815

ABSTRACT:
A gas turbine including a compressor, combustor and turbine further includes (1) a cooling air system for supplying part of air compressed by a compressor to a high temperature section of the turbine, (2) a heat exchanger for exchanging heat of part of air compressed by the compressor, this heat exchanger being mounted on the cooling air system, and (3) a system for adjusting the air temperature downstream from the heat exchanger in conformity to the operation period of the turbine.

REFERENCES:
patent: 3163004 (1964-12-01), Spillmann et al.
patent: 6367242 (2002-04-01), Uematsu et al.
patent: 10-196316 (1998-07-01), None

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