| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 04/10/2013 | CN103032903A Combustor |
| 04/10/2013 | CN103032902A Combustion system and method of assembling the same |
| 04/10/2013 | CN103032901A Forward casing with a circumferential sloped surface and a combustor assembly including same |
| 04/10/2013 | CN103032900A Triple annular counter rotating swirler |
| 04/10/2013 | CN103032899A System for fuel injection in fuel nozzle |
| 04/10/2013 | CN103032898A Mixing enhancing device for combustion chamber |
| 04/10/2013 | CN103032897A Turbomachine combustor assembly including combustion dynamics mitigation system |
| 04/10/2013 | CN103032896A Combustor and method for supplying flow to combustor |
| 04/10/2013 | CN103032895A System for cooling multi-tube fuel nozzle |
| 04/10/2013 | CN103032894A System for supplying pressurized fluid to cap assembly of gas turbine combustor |
| 04/10/2013 | CN103032893A Combustor and method for supplying flow to combustor |
| 04/10/2013 | CN103032892A Combustor and method for supplying fuel to combustor |
| 04/10/2013 | CN103032891A Multi-vortex combustion method |
| 04/10/2013 | CN103032890A Film cooled combustion liner assembly |
| 04/10/2013 | CN103032889A Combustion liner for a turbine engine |
| 04/10/2013 | CN103032113A 涡轮系统 Turbine system |
| 04/10/2013 | CN101514815B Gas turbine combustor flame stabilizer |
| 04/09/2013 | US8413448 Air blast fuel injector |
| 04/09/2013 | CA2560561C Methods and apparatuses for assembling a gas turbine engine |
| 04/04/2013 | WO2013046825A1 Combustor tail pipe, gas turbine with tail pipe, and method for manufacturing tail pipe |
| 04/04/2013 | WO2013045802A1 Turbine engine combustion chamber |
| 04/04/2013 | WO2013045792A2 Annular combustion chamber for a turbine engine |
| 04/04/2013 | US20130081401 Impingement cooling of combustor liners |
| 04/04/2013 | US20130081400 Combustor with a pre-nozzle mixing cap assembly |
| 04/04/2013 | US20130081397 Forward casing with a circumferential sloped surface and a combustor assembly including same |
| 04/04/2013 | DE10347588B4 Gleichraum-Gasturbine Constant-volume gas turbine |
| 04/04/2013 | CA2848629A1 Annular combustion chamber for a turbine engine |
| 04/03/2013 | EP2574847A2 Combustion liner for a turbine engine |
| 04/03/2013 | EP2574846A2 A method of operating a combustion chamber |
| 04/03/2013 | EP2574845A2 Combustion system and method of assembling the same |
| 04/03/2013 | EP2574844A2 System for supplying pressured fluid to a cap assembly of a gas turbine combustor |
| 04/03/2013 | CN202852885U Baffling type annular combustion chamber |
| 04/03/2013 | CN202852884U Double-oil-line centrifugal atomization jet device |
| 04/03/2013 | CN202852883U Fuel atomization device |
| 04/03/2013 | CN202852882U Fuel oil atomization device |
| 04/03/2013 | CN202852881U Direct-flow nozzle |
| 04/03/2013 | CN202852880U Double-stage radial swirler |
| 04/03/2013 | CN202852879U Twin-stage radial swirler |
| 04/03/2013 | CN103017203A Fractional combustion chamber |
| 04/03/2013 | CN103017202A System for injecting fuel in gas turbine engine |
| 04/03/2013 | CN103017201A Combustor and method for conditioning flow through a combustor |
| 04/03/2013 | CN103017200A System for directing airflow into combustor |
| 04/03/2013 | CN103017199A Combustor and method for supplying fuel to a combustor |
| 04/02/2013 | US8408004 Resonator assembly for mitigating dynamics in gas turbines |
| 04/02/2013 | CA2593917C Integral heater for fuel conveying member |
| 03/30/2013 | CA2790445A1 Combustion system and method of assembling the same |
| 03/28/2013 | WO2013044197A2 A combustor resonator section with an internalthermal barrier coating and method of fabricating the same |
| 03/28/2013 | WO2013043768A1 Cast manifold for dual fuel stage dry low nox gas turbine engine |
| 03/28/2013 | WO2013043078A1 Combustor cap for damping low frequency dynamics |
| 03/28/2013 | WO2013043076A1 Combustor and method for supplying fuel to a combustor |
| 03/28/2013 | WO2013042049A1 Method for detecting malfunctions in a combustion chamber of a gas turbine plant, and gas turbine plant |
| 03/28/2013 | WO2012168636A3 Annular combustion chamber of a turbomachine |
| 03/28/2013 | US20130078581 Apparatuses for controlling heat for rapid thermal processing of carbonaceous material and methods for the same |
| 03/28/2013 | US20130074514 Systems and methods involving improved fuel atomization in air blast fuel nozzles of gas turbine engines |
| 03/28/2013 | US20130074510 Combustor and method for supplying fuel to a combustor |
| 03/28/2013 | US20130074507 Combustion liner for a turbine engine |
| 03/28/2013 | US20130074506 Turbine burner |
| 03/28/2013 | US20130074505 System for directing airflow into a combustor |
| 03/28/2013 | US20130074504 System for injecting fuel in a gas turbine engine |
| 03/28/2013 | US20130074503 System for supplying pressurized fluid to a cap assembly of a gas turbine combustor |
| 03/28/2013 | US20130074502 Transition piece of combustor, gas turbine having the same, and producing method for transition piece |
| 03/28/2013 | US20130074501 Combustor resonator section with an internal thermal barrier coating and method of fabricating the same |
| 03/27/2013 | EP2573469A2 Combustor and Method for Supplying Fuel to a Combustor |
| 03/27/2013 | EP2573468A2 System for injecting fuel in a gas turbine engine |
| 03/27/2013 | EP2573467A2 Turbine combustor and method for temperature control and damping a portion of a combustor |
| 03/27/2013 | EP2573466A2 System for directing airflow into a combustor |
| 03/27/2013 | EP2573465A2 Combustor and method for conditioning flow through a combustor |
| 03/27/2013 | EP2573464A2 Combustion sections of gas turbine engines with convection shield assemblies |
| 03/27/2013 | CN202835446U 发动机火焰筒 Engine flame tube |
| 03/27/2013 | CN202835445U Centrifuge atomizing spray nozzle |
| 03/27/2013 | CN202835444U Swirler and offcenter atomizing nozzle with spiral groove |
| 03/27/2013 | CN202835443U Centrifugal atomizing nozzle |
| 03/27/2013 | CN202835442U Structure preventing carbon from being deposited on jet nozzle |
| 03/27/2013 | CN103003552A Fuel nozzle, gas turbine combustor equipped with same, and gas turbine equipped with this gas turbine combustor |
| 03/27/2013 | CN102997281A System and method for conditioning a working fluid in a combustor |
| 03/27/2013 | CN102997280A Combustion fuel nozzle assembly in gas turbine and method to turn fuel flow |
| 03/27/2013 | CN102997279A Fuel injector |
| 03/27/2013 | CN102165262B Stepped swirler for dynamic control |
| 03/27/2013 | CN102119299B Multistage gas furnace having split manifold |
| 03/27/2013 | CN101737805B Low-cost inside diameter-variable combustion chamber and design and test method thereof |
| 03/27/2013 | CN101709656B Coupling method for improving blade cooling efficiency and combustion efficiency of interstage/afterburner/channel combustion chambers |
| 03/27/2013 | CN101309728B Fuel injector |
| 03/27/2013 | CN101243287B Premix burner with mixing section |
| 03/26/2013 | US8402763 Combustor headend guide vanes to reduce flow maldistribution into multi-nozzle arrangement |
| 03/21/2013 | WO2013039095A1 Gas turbine |
| 03/21/2013 | WO2013037503A1 Flame holder having reduced thermal stresses for a gas turbine burner |
| 03/21/2013 | WO2012016748A3 Gas turbine combustion chamber |
| 03/21/2013 | US20130067927 System and method for controlling combustion instabilities in gas turbine systems |
| 03/21/2013 | US20130067925 Method for operating a combustion device |
| 03/21/2013 | US20130067923 Combustor and method for conditioning flow through a combustor |
| 03/21/2013 | US20130067921 Fuel injector |
| 03/21/2013 | DE102011082884A1 Brenner und Gasturbine mit einem solchen Brenner Burner and the gas turbine having such a burner |
| 03/21/2013 | CA2853557A1 Flame holder having reduced thermal stresses for a gas turbine burner |
| 03/20/2013 | EP2570730A2 System and method for controlling combustion instabilites in gas turbine systems |
| 03/20/2013 | EP2570729A2 System and method for conditioning a working fluid in a combustor |
| 03/20/2013 | EP2570728A1 Fuel injector |
| 03/20/2013 | EP2570727A2 Systems and methods of pressure drop control in fluid circuits through swirling flow mitigation |
| 03/20/2013 | CN202813443U Lean pre-mixing combustion room of gas turbine |
| 03/20/2013 | CN202813442U Head level spacing sleeve of gas turbine combustor and gas turbine combustor |
| 03/20/2013 | CN202813441U Cracking gas fuel injection device for chemical regenerative cycle |