About 32 results
https://drivepatents.com/patents/1388134 · 26 Mar 2025
A gas turbine engine (10) configured to combust gaseous hydrogen fuel comprises a combustor (20) comprising an annular combustion chamber outer casing (36) surrounding an inner combustor case (34) and a fuel manifold (42) configured to provide gaseous fuel...
https://drivepatents.com/patents/1394385 · 19 Mar 2025
Die Erfindung betrifft eine Düsenvorrichtung (1) zur Zugabe von Kraftstoff (14) in eine Brennkammer einer Gasturbinenanordnung umfassend - einen Düsenhauptkörper (1a) mit Düsenöffnungen zur Einspritzung des Kraftstoffes in die Brennkammer, - einen Dü...
https://drivepatents.com/patents/965535 · 31 Dec 2014
A segment of a fluid manifold includes a flexible thermal shield with an insulation space defined inboard of the thermal shield to provide thermal isolation from conditions external to the thermal shield. The thermal shield includes a helically corrugated ...
https://drivepatents.com/patents/966079 · 17 Dec 2014
Combustion equipment for use in a gas turbine engine. The combustion equipment has an inner case and an outer case, wherein the outer case encloses the inner case so that a cavity is located between the inner and outer cases. The combustion equipment also ...
https://drivepatents.com/patents/970021 · 17 Sep 2014
A gas turbine engine comprises a combustor (16). The combustor (16) comprises an annular combustor chamber formed between an inner liner (20) and an outer liner (30) spaced apart from the inner liner (20). An annular fuel manifold (40) has fuel nozzles dis...
https://drivepatents.com/patents/973824 · 11 Jun 2014
A fuel nozzle (70) for a gas turbine (10) generally includes a main body (72) having an upstream end (78) axially separated from a downstream end (80). The main body at least partially defines a fuel supply passage (86) that extends through the upstream en...
https://drivepatents.com/patents/974304 · 28 May 2014
A gas turbine combustor (3) includes: multiple gaseous fuel nozzles (9) to inject gaseous fuel; a manifold (17) to distribute gaseous fuel to the multiple gaseous fuel nozzles; a burner flange (11) to secure a burner (200) to an end cover (6); and a burner...
https://drivepatents.com/patents/974624 · 21 May 2014
A fuel supply system supplies fuel to a plurality of combustion sectors (70,74) of a combustion section of a gas turbine. Each of the combustion sectors includes at least two combustors. The fuel supply system generally includes a fuel distribution manifol...
https://drivepatents.com/patents/986709 · 18 Sep 2013
A combustor 14 includes a combustion chamber 38 and a casing 28 that circumferentially surrounds the combustion chamber to at least partially define an annular passage 56 between the casing 28 and the combustion chamber 38. A fuel plenum 72 extends radiall...
https://drivepatents.com/patents/988888 · 10 Jul 2013
A fuel distribution manifold (116) comprises an outer shell (130) having an inner surface (152). The outer shell (130) defines an inlet (134) for receiving fuel from a parent supply (120) line, a base (140) opposite the inlet (134), a central manifold axis...