Method for operating a partially closed, turbocharged gas...

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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Details

C060S792000, C060S039183, C060S039511

Reexamination Certificate

active

06901759

ABSTRACT:
A gas turbine system includes a gas turbine (1, 2, 3) having a compressor (1) and a turbine (2), which via a common shaft (3) drive a generator (4), and a combustion chamber (6), the exit of which is connected to the entry to the turbine (2) of the gas turbine (1, 2, 3), has a fuel feed (8) and receives combustion air from the exit of the compressor (1) of the gas turbine (1, 2, 3) via the high-pressure side of a recuperator (5), the exit of the turbine (2) and the entry to the compressor (1) of the gas turbine (1, 2, 3) being connected via the low-pressure side of the recuperator (5), and a first exhaust-gas turbocharger (ATL2) which sucks in air being connected to different locations (9, 10) of the low-pressure side of the recuperator (4) via the exit of its compressor (13) and the entry to its turbine (14).

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Search Report from DE 103 07 374.4 (Aug. 28, 2003).
Search Report from GB 0403740.4 (Jun. 17, 2004).
Malmquist, Anders, et al., “Microturbines: speeding the shift to distributed heat and power”, ABB Review, pp 22-30 (Mar. 2003, ABB, Baden, Switzerland).

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