#F02C7/224

REHEAT ASSEMBLY FOR A GAS TURBINE ENGINE

The foregoing describes a reheat assembly for a gas turbine engine. The reheat assembly comprises a support duct section, a vaporiser and a heat shield. The support duct section comprises a core side …

DRIVE·5d ago·2 min read

F02C7/224 ROLLS ROYCE PLC [GB]

FUEL MANAGEMENT SYSTEM

There is provided a fuel management system (500A) for a gas turbine engine (10), the fuel management system (500A) comprising a fuel supply line (510) configured to supply fuel from a system inlet (52…

DRIVE·Aug 6·1 min read

F02C7/224 ROLLS ROYCE PLC [GB]

FUEL MANAGEMENT SYSTEM

There is provided a fuel management system (400A) for a gas turbine engine. The fuel management system comprises: a fuel tank (41) configured to store fuel for the gas turbine engine; a fuel supply li…

DRIVE·Aug 6·2 min read

F02C7/224 ROLLS ROYCE PLC [GB]

AIR FLOW AIDED LNG VAPORIZER AND COMPRESSION SYSTEM

Embodiments of the present disclose relate to a system of distributing fuel gas. The system of distributing fuel gas includes a vaporizer and compression system (VCS). The VCS includes a vaporizer, a …

DRIVE·Feb 20·1 min read

F02C7/224 Texas Fueling Services, Inc.

INTEGRATED FUEL CELL AND ENGINE COMBUSTOR ASSEMBLY

An engine assembly includes a combustor, a fuel cell stack integrated with the combustor, and a pre-burner system fluidly connected to the fuel cell stack. The fuel cell stack is configured to direct …

DRIVE·Nov 10·1 min read

F02C7/224 General Electric Company

INTEGRATED FUEL CELL AND ENGINE COMBUSTOR ASSEMBLY

An engine assembly includes a combustor, a fuel cell stack integrated with the combustor, the fuel cell stack configured (i) to direct fuel and air exhaust from the fuel cell stack into the combustor …

DRIVE·Nov 10·1 min read

F02C7/224 General Electric Company

Method for adjusting a natural gas temperature for a fuel supply line of a gas turbine engine and gas turbine

The method for adjusting a natural gas temperature for a fuel supply line (6) of a gas turbine engine (1) comprises measuring by infrared analysis the natural gas percentage content of methane (CH4), …

DRIVE·Aug 27·1 min read

F02C7/224 ALSTOM TECHNOLOGY LTD [CH]

Method of operating a fuel heating system

A method 400 of operating a fuel heating system is provided. The method includes performing 404 pre-ignition diagnostic checks on a plurality of components of the fuel heating system, wherein at least…

DRIVE·Aug 6·1 min read

F02C7/224 GEN ELECTRIC [US]

Power plant and method for generating electric power

The power plant (100) has a burner unit (10), in which thermal energy is produced by burning a fuel. A turbine unit (50) is provided, in which a rotational movement is produced with the thermal energy…

DRIVE·Jun 4·1 min read

F02C7/224 LUMENION AG [CH]

Gas turbine inlet system with solid-state heat pump

A gas turbine inlet system (20) includes a first passage (22) that delivers inlet air to a compressor (12), a second passage (28) that delivers fuel to a combustor (14), and a heat pump (26) that tran…

DRIVE·Aug 28·1 min read

F02C7/224 GEN ELECTRIC [US]

Fuel heating system for power plant

A fuel heating system (10) for a power plant includes a fuel source for a gas turbine system (12), wherein the fuel source contains a fuel at a first temperature. Also included is a feedwater source (…

DRIVE·Aug 21·1 min read

F02C7/224 GEN ELECTRIC [US]

Liquid fuel heating system

The present invention provides a liquid fuel heating system (100) for heating a flow of fuel (20) for a gas turbine engine (12). The liquid fuel system (100) may include a flow of steam (135), an ejec…

DRIVE·Jul 24·1 min read

F02C7/224 GEN ELECTRIC [US]

Systems and methods for bulk temperature variation reduction of a gas turbine through can-to-can fuel temperature modulation

A gas turbine (10) includes a plurality of combustion chambers (14); at least one fuel nozzle (16, 18, 20) for each of the combustion chambers; at least one fuel line (34, 36, 38) for each fuel nozzle…

DRIVE·Jan 16·1 min read

F02C7/224 GEN ELECTRIC [US]

Systems and methods for modified Wobbe index control with constant fuel temperature

The present application provides a gas turbine engine system (100) for combusting a flow of fuel (160). The gas turbine engine system (100) may include a combustor (140) and a fuel system (150) for pr…

DRIVE·Jan 9·1 min read

F02C7/224 GEN ELECTRIC [US]

Heat exchanger

A heat exchanger is provided for warming fuel prior to introduction of the fuel to an engine, the heat exchanger including: a fuel inlet and a fuel outlet; a heat exchange matrix having heat transfer …

DRIVE·Jan 2·1 min read

F02C7/224 ROLLS ROYCE PLC [GB]

AN ARRANGEMENT FOR PREPARATION OF LIQUID FUEL FOR COMBUSTION AND A METHOD OF PREPARING LIQUID FUEL FOR COMBUSTION

The invention relates to a preparation of liquid fuel for combustion, particularly for ignition, in the burners of a gas turbine. The invention provides a source of heated liquid fuel, particularly he…

DRIVE·Aug 15·1 min read

F02C7/224 SIEMENS AG [DE]

Aircraft with a preheating device for a fluid/fluid heat exchanger thereof

The aircraft has a heat exchanger exchanging heat between first fluid e.g. fuel, and second fluid e.g. oil. A preheating device preheats the first fluid in upstream from narrow pipes (22) of the excha…

DRIVE·Dec 7·1 min read

F02C7/224 AIRBUS OPERATIONS SAS [FR]