Apparatus and method for reducing the heat rate of a gas...

Power plants – Combustion products used as motive fluid – Plural combustion products generators in ring coaxial with...

Reexamination Certificate

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C060S722000

Reexamination Certificate

active

07047723

ABSTRACT:
The present invention provides an apparatus and method for reducing the pressure loss of air prior to entering a combustion system, such that, for a known combustion system having a predetermined pressure loss, the resulting fluid entering the turbine has a higher supply pressure that will result in more efficient turbine and increased engine output. Significant enhancements include the addition of a plurality of deflector assemblies to direct the air from a compressor outlet towards an exposed single-wall transition duct to provide direct cooling to a first panel of the transition duct.

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patent: 2003/0010014 (2003-01-01), Bland et al.

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