About 75 results
https://drivepatents.com/patents/1391993 · 21 Jan 2026
Nozzle assembly (1000), combustor(100) and gas turbine (10). Fuel and compressed air are discharged to a combustion chamber (120a) of the combustor of the gas turbine. The nozzle assembly includes a nozzle body, (1100), a plurality of injection nozzles (12...
https://drivepatents.com/patents/1387930 · 21 Jan 2026
A system includes a variable displacement pump (VDP (102)) in fluid communication with an inlet line (104) and with an outlet line (106). The VDP (102) includes a variable displacement mechanism (108) configured to vary pressure to the outlet line (106). A...
https://drivepatents.com/patents/1387929 · 31 Dec 2025
A system includes a variable displacement pump (VDP (102)) in fluid communication with an inlet line (104) and with an outlet line (106). The VDP (102) includes a variable displacement mechanism (108) configured to vary pressure to the outlet line (106). A...
https://drivepatents.com/patents/1396300 · 26 Nov 2025
The present application discloses a computer implemented method (4090) of determining a fleetwide fuel allocation for a plurality of missions carried out by a plurality of aircraft, the plurality of missions being supplied with fuel from a fuel source comp...
https://drivepatents.com/patents/1392755 · 29 Oct 2025
A combustor including an annular liner (206, 208), a dome wall (202), a combustion chamber, at least one fuel cup (204) and at least one dilution passage (212). The fuel cup (204) being provided on the dome wall (202) and being fluidly coupled to the combu...
https://drivepatents.com/patents/1388128 · 8 Oct 2025
A combustor nozzle (1400), a combustor including the combustor nozzle (1400), and a gas turbine including the combustor are disclosed. The combustor nozzle (1400) may include a plurality of mixing tubes (1420) through which air and fuel flow, a multi-tube ...
https://drivepatents.com/patents/1394773 · 24 Sep 2025
A hollow nozzle (110) including a tubular nozzle casing (111) and a plurality of rotary vanes (112) arranged radially along an inner surface of an inlet of the nozzle casing, through which compressed air is introduced, forming a hollow center (1) at the ce...
https://drivepatents.com/patents/1391048 · 10 Sep 2025
An injector (38) for a gas turbine engine (20) includes an annular gas nozzle (42), a hydrogen feed conduit (50), and a disc (58). The annular gas nozzle (42) is disposed along a central nozzle axis (A2) and includes a forward face (44), a frustoconical in...
https://drivepatents.com/patents/1398162 · 10 Sep 2025
A turbine engine (10) comprises a compressor section (12), a combustion section (14), and a turbine section (16) in serial flow arrangement, the combustion section (14) having a combustor (30) with a fuel mixer (90). The fuel mixer (90) comprises an outer ...
https://drivepatents.com/patents/1399660 · 10 Sep 2025
A fluid delivery system includes a main pump (102) disposed in a primary fluid line (104) configured to receive a low pressure fluid on a low pressure side (106) and output a high pressure fluid on a high pressure side (108) to provide flow from the fluid ...