About 14 results
https://drivepatents.com/patents/1397351 · 6 Aug 2025
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 (520) to a combustor (16) of the gas turbine engine via a c...
https://drivepatents.com/patents/1397359 · 6 Aug 2025
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 line (410) configured to supply fuel from the fuel tank to...
https://drivepatents.com/patents/1395938 · 7 Aug 2024
L'invention concerne un ensemble propulsif (4) comprenant une nacelle (6) et un moteur (9) arrangé à l'intérieur de la nacelle (6) et alimenté en carburant par une canalisation d'apport (5a) en carburant, le moteur (9) comportant une chambre de combust...
https://drivepatents.com/patents/970836 · 27 Aug 2014
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), ethane (C2H6), propane (C3H8), butane (C4H10), carbon di...
https://drivepatents.com/patents/971582 · 6 Aug 2014
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 one inlet damper and at least one outlet damper of an e...
https://drivepatents.com/patents/974010 · 4 Jun 2014
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. A generator unit (60) is driven by the rotational move...
https://drivepatents.com/patents/984445 · 28 Aug 2013
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 transfers heat from the inlet air to the fuel by consuming e...
https://drivepatents.com/patents/987209 · 21 Aug 2013
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 (15) for distributing a feedwater. Further included is a ...
https://drivepatents.com/patents/988321 · 24 Jul 2013
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 ejector/educator (150) in communication with the flow of fue...
https://drivepatents.com/patents/993808 · 16 Jan 2013
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 in each of the combustion chambers; at least one heat e...