Gas turbine bleed energy recovery via counter rotating...

Details Gas turbine bleed energy recovery via counter rotating... Gas turbine bleed energy recovery via counter rotating...

2009-06-10

2011-11-22

Waks, Joseph (Department: 2839)

Prime-mover dynamo plants

Turbogenerators

Reexamination Certificate

active

08063501

ABSTRACT:
A gas turbine engine includes a main compressor section for compressing air, a main combustor section positioned downstream of the main compressor section, a main turbine section positioned downstream of the main combustor section, and a spool extending from the main compressor section to the main turbine section. A second turbine is fluidically connected to the main compressor section by a bleed passage. An electrical generator is mechanically driven by both the spool and the second turbine.

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