#F01D13/02

AIRCRAFT ENGINE, GAS TURBINE INTAKE THEREFORE, AND METHOD OF GUIDING EXHAUST GASSES

A gas turbine intake (16) has a swirl housing (42) having a tangential inlet (58) fluidly connecting an exhaust conduit, an annular outlet (52) defined around a central axis (36) and fluidly connectin…

DRIVE·May 6·2 min read

F01D13/02 PRATT & WHITNEY CANADA [CA]

COMBINED CYCLE POWER GENERATION METHODS

A power generation system including a gas turbine is disclosed. The power generation system includes a steam supply system including a high-temperature high pressure superheater and a high-temperature…

DRIVE·Jan 28·1 min read

F01D13/02 GENERAL ELECTRIC TECHNOLOGY GMBH [CH]

Power plant and method of use

A power plant arrangement and method of operation are provided. The power plant arrangement comprises at least one main air compressor (12) and one or more gas turbine assemblies. Each assembly compri…

DRIVE·Feb 27·1 min read

F01D13/02 GEN ELECTRIC [US]

Power plant start-up method

Ambient air is compressed into a compressed ambient gas flow (26) and delivered to a turbine combustor (32). An exhaust port is opened. A turbine shaft (22) is rotated at an ignition speed and a fuel …

DRIVE·Feb 27·1 min read

F01D13/02 GEN ELECTRIC [US]

METHOD FOR CONTROLLING A POWER PLANT

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

DRIVE·Feb 27·1 min read

F01D13/02 GEN ELECTRIC [US]

Turbo recuperator device

A device and method for recuperating a gas turbine engine comprises a compressor [10] being configured to receive a coolant fluid stream, to compress the coolant fluid stream and to discharge the comp…

DRIVE·Jul 7·2 min read

F01D13/02 GEN ELECTRIC [US]