About 28 results
https://drivepatents.com/patents/1386857 · 11 Feb 2026
A system includes a plurality of injectors (106) each having a respective main circuit (132) configured to be connected in fluid communication with one manifold for supplying fuel to each injector in the plurality of injectors. Each injector (160) in the p...
https://drivepatents.com/patents/1395844 · 22 Oct 2025
A valve having a first segment (220) between a first outer wall (220A) and a first inner wall (220B) and has a first outer port (225A) near the first outer wall and a side port (225B) between the first inner and outer walls; a second segment (230) between ...
https://drivepatents.com/patents/972939 · 2 Jul 2014
An electric-generating gas turbine includes a compressor (103) configured to compress air, a combustor (112) configured to generate combustion gas by mixing and combusting the air compressed by the compressor (103) and fuel, a turbine (114) configured to b...
https://drivepatents.com/patents/985626 · 13 Mar 2013
A method is provided for modifying a fuel control system for a gas turbine (10) having a standard unloading sequence and a pre-defmed minimum inlet pressure requirement associated with the standard unloading sequence to allow the gas turbine to operate ove...
https://drivepatents.com/patents/992722 · 27 Feb 2013
A fuel divider included in a fuel supply device of a gas turbine engine includes a movable member which is movable according to a fuel pressure at a fuel entrance, opens only a pilot port when the fuel pressure at the fuel entrance is lower than a first pr...
https://drivepatents.com/patents/993258 · 6 Feb 2013
In a fuel supply device of a gas turbine engine of the present invention, a fuel divider 66 includes a fuel entrance E1 into which the fuel supplied from a collecting fuel passage 63 is introduced; a pilot port 76 connected to the pilot fuel passage 64; a ...
https://drivepatents.com/patents/994920 · 19 Dec 2012
A flow divider assembly (130) includes a dividing valve (220) and a balancing valve (270). The dividing valve includes a dividing cavity (222) configured to receive a flow of fuel and a piston device (250) arranged within the dividing cavity and selectivel...
https://drivepatents.com/patents/995221 · 12 Dec 2012
A fuel supply device of a gas turbine engine of the present invention includes a fuel divider 66 which divides fuel supplied from a collecting fuel passage 63 to feed the fuel to a pilot fuel passage 64 and to a main fuel passage 65. The fuel divider 66 in...
https://drivepatents.com/patents/996762 · 24 Oct 2012
A gas turbine engine (10) includes a plurality of fuel injectors (24, 26; 44, 46, 48; 66, 68, 70, 72; 74, 76, 78, 80, 82, 84, 86, 88) grouped operatively by stages in a multistage combustor (12; 12'; 12"). A fuel system (30; 30'; 30") for the gas turbine e...
https://drivepatents.com/patents/997071 · 17 Oct 2012
A flow divider valve for a gas turbine engine fuel supply system is provided. The flow divider valve is configured, whenever fuel pressure at its inlet port is between a first predetermined pressure and a second predetermined pressure, to supply the fuel t...