1
Keller Jakob Dr, Sattelmayer Thomas Dr, Styner Daniel: Process for combustion of liquid fuel in a burner.. Bbc Brown Boveri & Cie, June 28, 1989: EP0321809-A1 (171 worldwide citation)

In the premix combustion of liquid fuel in a burner without premixing section, there is formed in the interior (14) of the burner a conical liquid fuel column (5) which widens in the direction of flow and which is surrounded by a rotating combustion air flow (15) which flows tangentially into the bu ...


2
Colin Wilkes, Milton B Hilt: Dual stage-dual mode low nox combustor. General Electric Company, Jerome C Squillaro, October 6, 1981: US04292801 (119 worldwide citation)

An improved dual stage-dual mode combustor capable of reduced emissions of nitrogen oxide from a combustion turbine is disclosed. The combustor includes two combustion chambers separated by a throat region. Fuel is initially introduced and ignited in the first chamber. Thereafter, fuel is introduced ...


3
Pfefferle William C: Catalytically-supported thermal combustion. Engelhard Minerals & Chemicals Corporation, December 30, 1975: US3928961 (119 worldwide citation)

A method for the catalytically-supported thermal combustion of carbonaceous fuel comprising the adiabatic combustion of at least a portion of the fuel admixed with air in the presence of a solid oxidation catalyst at an operating temperature substantially above the instantaneous auto-ignition temper ...


4
Alexander A Belokon, George L Touchton: Recuperated gas turbine engine system and method employing catalytic combustion. MES International, Alston & Bird, March 7, 2006: US07007487 (108 worldwide citation)

A recuperated gas turbine engine system and associated method employing catalytic combustion, wherein the combustor inlet temperature can be controlled to remain above the minimum required catalyst operating temperature at a wide range of operating conditions from full-load to part-load and from hot ...


5
Richard Sterling Tuthill, William Theodore Bechtel II, Jeffrey Arthur Benoit, Stephen Hugh Black, Robert James Bland, Guy Wayne DeLeonardo, Stefan Martin Meyer, Joseph Charles Taura, John Luigi Battaglioli: Swozzle based burner tube premixer including inlet air conditioner for low emissions combustion. General Electric Company, Nixon & Vanderhye P C, August 27, 2002: US06438961 (108 worldwide citation)

A burner for use in a combustion system of a heavy-duty industrial gas turbine includes a fuel/air premixer having an air inlet, a fuel inlet, and an annular mixing passage. The fuel/air premixer mixes fuel and air into a uniform mixture for injection into a combustor reaction zone. The burner also ...


6
Narendra D Joshi, Edward E Ekstedt, Michael J Epstein: Air fuel mixer for gas turbine combustor. General Electric Company, James P Davidson, Jerome C Squillaro, October 12, 1993: US05251447 (100 worldwide citation)

An air fuel mixer is disclosed having a mixing duct, a shroud surrounding the upstream end of the mixing duct having contained therein a fuel manifold in flow communication with a fuel supply and control means, a set of inner and outer counter-rotating swirlers adjacent the upstream end of the mixin ...


7
Sturgess Geoffrey John, Hoffman Jacob Sherman, Vdoviak John William, Hirschkron Robert: Air blast fuel atomizer. General Electric Company, November 21, 1972: US3703259 (97 worldwide citation)

An air blast fuel atomizer for establishing a highly atomized fuel dispersion at the confluence of two counter-rotating air swirls, wherein a uniform concentration of fuel is disposed on a circumferential shroud and directed to the atomization forces at the lip of the shroud.


8
Narendra D Joshi, Frederick E Moreno: Staged low NOx premix gas turbine combustor. PruTech II, Flehr Hohbach Test Albritton & Herbert, May 29, 1990: US04928481 (93 worldwide citation)

In a staged low NOx lean premix hot wall gas turbine combustor, the interior wall of the combustor is maintained at or near the flame temperature to provide stable operation over a wide range of heat release values. One or more stages of the staged combustor includes a Stirred Reactor region followe ...


9
Narendra D Joshi, Eric J Kress: Dual fuel mixer for gas turbine combustor. General Electric Company, Jerome C Squillaro, David L Narciso, October 4, 1994: US05351477 (91 worldwide citation)

A dual fuel mixer is disclosed having a mixing duct, a shroud surrounding the upstream end of the mixing duct having contained therein a gas fuel manifold and a liquid fuel manifold in flow communication with a gas fuel supply and a liquid fuel supply, respectively, and control means, a set of inner ...


10
Lohmann Robert P, Markowski Stanley J: Swirl combustor with vortex burning and mixing. United Aircraft Corporation, McCarthy Jack N, March 25, 1975: US3872664 (88 worldwide citation)

This disclosure sets forth an engine wherein the combustion section includes a combustor with a main combustion burner having a hot fluid injected thereinto from a pilot burner. A multiplicity of swirling jets of a cooler oxidizer fluid are directed into the combustor for engaging with the hot pilot ...



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