A power plant comprises at least one main air compressor (12) and at least one gas turbine assembly. The assembly comprises a turbine combustor (32) for mixing compressed ambient gas flow (26) with a recirculated low oxygen content gas flow (50) and a fuel...

At least one main air compressor (12) makes a compressed ambient gas flow (26, 66). The compressed ambient gas flow (26, 66) is delivered to both master and slave turbine combustors (32, 72) at a pressure that is greater than or substantially equal to an o...

At least one main air compressor (12) makes a compressed ambient gas flow (26). The compressed ambient gas flow (26) is delivered to a turbine combustor (32) at a pressure that is greater than or substantially equal to an output pressure delivered to the t...

Ambient air is compressed into a compressed ambient gas flow (26) with a main air compressor (12). The compressed ambient gas flow (26) having a compressed ambient gas flow rate is delivered to a turbine combustor (32) and mixed with a fuel stream (28) hav...

A main air compressor (12) delivers a compressed ambient gas flow (26) with a compressed ambient gas flow rate to a turbine combustor (32). A fuel stream (28) with a flow rate is delivered to the turbine combustor (32) and mixed with the compressed ambient...

The method involves controlling an exhaust gas stream (21) by a control element for cooling the gas stream by a cooler (27) before the gas stream is mixed with ambient air (2) to a suction flow (3). The exhaust gas stream is provided to avoid condensation ...

The present application provides a stoichiometric exhaust gas recovery turbine system (10). The stoichiometric exhaust gas recovery turbine system (10) may include a main compressor (15) for compressing a flow of ambient air (20), a turbine (40), and a sto...

The method involves dividing exhaust gases (19) into effluent stream (21) by exhaust gas divider (29), for recirculation into intake flow of gas turbine (6), and exhaust gas stream (20) for transfer to surroundings. The target concentration of component in...

A method of operation of a gas turbine engine system and a gas turbine engine system (50,120,130,200) are provided that include a first gas turbine engine (52). The first gas turbine engine (52) has a first compressor (80) configured to intake air and to p...