Standard Search
About 24 results
https://drivepatents.com/patents/1390129 · 10 Jun 2026
A gas turbine engine (20) is provided that includes fan (28), compressor (30), combustion (32), and turbine (34) sections, a fan bypass air path (38), and a turbine active clearance control system (54). The turbine section has a rotor stage (44) and a turb...
https://drivepatents.com/patents/1397863 · 2 Apr 2025
An engine system comprises a first fuel store, a second fuel store, an engine arranged to produce mechanical power by combustion or oxidation of a fuel in an engine, a fuel distribution system arranged to deliver fuel from the first and second fuel stores ...
https://drivepatents.com/patents/1397861 · 15 Jan 2025
An engine system comprises a first fuel store, a second fuel store, an engine arranged to produce mechanical power by combustion or oxidation of a fuel in an engine, a fuel distribution system arranged to deliver fuel from the first and second fuel stores ...
https://drivepatents.com/patents/1397859 · 18 Dec 2024
An engine system comprises a first fuel store of a first fuel, a second fuel store of a second fuel, an engine arranged to produce mechanical power by combustion or oxidation of fuel in the engine, a fuel distribution system arranged to deliver fuel from t...
https://drivepatents.com/patents/966202 · 17 Dec 2014
A disc shaft center adjusting mechanism in a gas turbine comprises the following: exhaust gas diffusers (13) provided between a bearing case (11) and an interior wall (10) connected to the downstream side of a turbine; a plurality of struts (14) provided i...
https://drivepatents.com/patents/977415 · 19 Mar 2014
A gas turbine that supplies combustion gas generated by supplying fuel to a combustor where the fuel is combusted with compressed air compressed at a compressor to a turbine to acquire rotational power, the gas turbine comprising pressurizing means connect...
https://drivepatents.com/patents/978492 · 12 Feb 2014
The gas turbine jet engine has a housing structure (22) radially surrounding the main flow channel (20), in which a housing gas flow flows in a same direction as a main flow in the main flow channel. The housing structure has an adjustable flow conducting ...
https://drivepatents.com/patents/980921 · 18 Dec 2013
A gas turbine that supplies combustion gas generated by supplying fuel to a combustor where the fuel is combusted with compressed air compressed at a compressor to a turbine to acquire rotational power, the gas turbine comprising pressurizing means connect...
https://drivepatents.com/patents/984633 · 28 Aug 2013
A gas turbine that supplies combustion gas generated by supplying fuel to a combustor where the fuel is combusted with compressed air compressed at a compressor to a turbine to acquire rotational power, the gas turbine comprising pressurizing means connect...
https://drivepatents.com/patents/987682 · 7 Aug 2013
A method of controlling the part-load performance of a turbine (1) includes generating a bypass flow in the turbine (1) by removing a portion of a compressed fluid from a compressor (10) of the turbine (1), determining an operating load of the turbine (1),...