| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 12/24/2008 | WO2008155373A1 Non-rotational stabilization of the flame of a premixing burner |
| 12/24/2008 | EP2006606A1 Swirling-free stabilising of the flame of a premix burner |
| 12/24/2008 | EP2005068A1 Gas turbine combustor |
| 12/24/2008 | EP2005067A1 Crack resistant combustor |
| 12/24/2008 | EP1771640B1 Multi-zone tubing assembly and installing method for a transition piece of a gas turbine |
| 12/24/2008 | DE10393125B4 Kühlanordnung eines Übergangsstücks einer Gasturbine Cooling structure of a transition piece of a gas turbine |
| 12/24/2008 | CN101329072A Rear step type flame holder for rotor engine |
| 12/24/2008 | CN100445535C Improved high-temperature turbine nozzle with light decreasement by light reflection and manufactuirng process |
| 12/23/2008 | US7467942 Device and method for flame stabilization in a burner |
| 12/23/2008 | US7467518 Externally fueled trapped vortex cavity augmentor |
| 12/23/2008 | CA2368329C Nickel-base braze material and braze repair method |
| 12/22/2008 | CA2627627A1 Heat shields for use in combustors |
| 12/18/2008 | WO2008153736A2 Turbine engine fuel injector with helmholtz resonator |
| 12/18/2008 | WO2008152964A1 Combustion oscillation detection device mounting structure |
| 12/18/2008 | WO2008151441A1 Fuel nozzle providing shaped fuel spray |
| 12/18/2008 | US20080307793 Brazed Joint Between a Metal Part and a Ceramic Part |
| 12/18/2008 | DE102008022117A1 Method for determining thermoacoustic transfer function of burner of combustion system, particularly combustion chamber of gas turbine, involves forming transfer function by two partial transfer functions |
| 12/18/2008 | CA2690431A1 Fuel nozzle providing shaped fuel spray |
| 12/17/2008 | EP2003399A2 Turbomachine combustion chamber with helical air circulation |
| 12/17/2008 | EP2003398A2 Fuel nozzle providing shaped fuel spray |
| 12/17/2008 | EP2002185A1 Fuel lance for a gas turbine plant and a method of operating a fuel lance |
| 12/17/2008 | CN201166388Y Fork type sound velocity combustor |
| 12/17/2008 | CN101324344A Turbomachine combustion chamber with helical air circulation |
| 12/17/2008 | CN100443806C Tangential standing vortex burning chamber |
| 12/17/2008 | CN100443805C Evaporation pipe type miniature-small-sized engine combustion chamber |
| 12/16/2008 | US7464553 Air-assisted fuel injector for mixer assembly of a gas turbine engine combustor |
| 12/16/2008 | CA2354520C Burner and process for operating gas turbines |
| 12/14/2008 | CA2634615A1 Turbine engine combustion chamber with helicoidal circulation of air |
| 12/11/2008 | DE19721937B4 Vormischbrenner zum Betrieb eines Aggregates zur Erzeugung eines Heissgases Premix burner to operate a unit for generating a hot gas |
| 12/11/2008 | DE19542644B4 Vormischverbrennung Premixed combustion |
| 12/10/2008 | EP1999410A1 Burner for the operation of a heat generator |
| 12/10/2008 | EP1999409A1 Burner arrangement |
| 12/10/2008 | CN101321990A Burner lance |
| 12/10/2008 | CN101319791A Gas flow reflux apparatus of gas-turbine combustor |
| 12/09/2008 | CA2143232C A fuel nozzle for a turbine having dual capability for diffusion and premix combustion and methods of operation |
| 12/04/2008 | WO2008146818A1 Method of preparing through holes in tube body wall surfaces, and tube body structure |
| 12/04/2008 | WO2008091289A3 Instrumented component for use in an operating environment |
| 12/03/2008 | EP1998115A1 Cooling channel for cooling a component carrying a hot gas |
| 12/03/2008 | EP1998114A2 A dynamic control system to implement homogenous mixing of diluent and fuel to enable gas turbine combustion systems to reach and maintain low emission levels |
| 12/03/2008 | EP1998036A2 Resonance driven glow plug torch igniter and ignition method |
| 12/01/2008 | CA2632879A1 A dynamic control system to implement homogenous mixing of diluent and fuel to enable gas turbine combustion systems to reach and maintain low emission levels |
| 11/27/2008 | WO2008142020A1 Gas turbo set and method for controlling a gas turbo set |
| 11/27/2008 | WO2008141959A1 Swirler vane |
| 11/27/2008 | WO2008141955A1 Fuel distributor |
| 11/27/2008 | WO2008141594A2 Combustion burner - combustion chamber |
| 11/26/2008 | EP1995521A1 Swirler vane |
| 11/26/2008 | EP1995433A1 Gas turbo group and method for controlling a gas turbo group |
| 11/26/2008 | EP1994334A1 Combustor and method of operating a combustor |
| 11/26/2008 | EP1994260A2 Gas turbine comprising an adjustable mixing housing |
| 11/26/2008 | EP1356236B1 Premix burner and method for operating such a premix burner |
| 11/26/2008 | EP1250555B1 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines |
| 11/26/2008 | CN101313178A A combustion apparatus |
| 11/26/2008 | CN101311630A Method and apparatus for controlling the combustion in a gas turbine |
| 11/26/2008 | CN100436945C Fuel pre-evaporation and premix perforated pipe |
| 11/25/2008 | US7457710 Apparatus and method for testing combustion |
| 11/25/2008 | US7454914 Helical channel for distributor and method |
| 11/20/2008 | WO2008138971A2 Cool flame combustion |
| 11/20/2008 | WO2008138828A1 Device and method for measuring acoustic vibrations in a fluid flow and a gas turbine installation with such a device |
| 11/20/2008 | WO2008138815A1 Burner component for a gas turbine burner |
| 11/20/2008 | WO2008138797A2 Pressure dynamics reduction within a gas turbine engine |
| 11/19/2008 | EP1992878A1 Fuel distributor |
| 11/19/2008 | EP1992875A2 Fuel nozzle |
| 11/19/2008 | EP1706672B1 Premixing burner arrangement and method for operating a combustion chamber |
| 11/19/2008 | CN101309728A 燃料喷射器 Fuel injector |
| 11/19/2008 | CN101307916A Gas turbine combustion-chamber for combusting ethanol fuel |
| 11/19/2008 | CN101307915A Gas turbine preevaporation combustion-chamber for combusting ethanol fuel |
| 11/19/2008 | CN101307442A Method for making high-temperature articles |
| 11/18/2008 | US7451600 Gas turbine engine combustor with improved cooling |
| 11/18/2008 | US7451599 Fuel manifold inlet tube |
| 11/18/2008 | CA2629043A1 Stress reduction feature to improve fuel nozzle sheath durability |
| 11/18/2008 | CA2459986C Main burner, method and apparatus |
| 11/16/2008 | CA2629184A1 Interface between a combustor and fuel nozzle |
| 11/16/2008 | CA2625133A1 Redundant mounting system for an internal fuel manifold |
| 11/15/2008 | CA2588626A1 A process for producing static components for a gas turbine engine |
| 11/13/2008 | WO2008137201A1 Cooling holes for gas turbine combustor liner having a non-uniform diameter therethrough |
| 11/13/2008 | US20080276618 Method and system for porous flame holder for hydrogen and syngas combustion |
| 11/13/2008 | DE102008022669A1 Brennstoffdüse und Verfahren für deren Herstellung Fuel nozzle, and methods for their preparation |
| 11/13/2008 | CA2685342A1 Cooling holes for gas turbine combustor liner having a non-uniform diameter therethrough |
| 11/12/2008 | EP1990581A2 A method and system for porous flame holder for hydrogen and syngas combustion |
| 11/12/2008 | EP1990580A1 Burner component for a gas turbine burner |
| 11/12/2008 | EP1990579A1 Device and method for measuring acoustic oscillations in the fluid flow and gas turbine facility with such a device |
| 11/12/2008 | EP1990521A1 Pressure dynamics reduction within a gas turbine engine |
| 11/12/2008 | EP1989486A1 Gas turbine burner and method of operating a gas turbine burner |
| 11/12/2008 | EP1588102B1 Heat shield element, combustion chamber and gas turbine |
| 11/12/2008 | CN101303131A Fuel nozzle and method of fabricating the same |
| 11/12/2008 | CN100432536C Recuperated gas turbine engine system and method employing catalytic combustion |
| 11/12/2008 | CN100432531C Burner |
| 11/11/2008 | US7448218 Premix burner and method for burning a low-calorie combustion gas |
| 11/11/2008 | US7448216 Methods and apparatus for operating gas turbine engine combustors |
| 11/06/2008 | WO2008133034A1 Gas turbine combustor |
| 11/06/2008 | WO2008108813A3 Combustor assembly for gas turbine engine |
| 11/06/2008 | US20080271457 Cooling Holes For Gas Turbine Combustor Having A Non-Uniform Diameter Therethrough |
| 11/06/2008 | DE102006045946B4 Verbrennungskammer, die ein äußeres Gehäuse, ein Flammrohr, Kraftstoffdüsen, eine Zündkerze und Ionisierungskammer mit darin aufgestellten Elektroden enthält und sich dadurch kennzeichnet, daß ihre Ionisierungskammer mit Drehbarkeit ausgeführt ist Combustion chamber, comprising an outer casing, a flame tube, fuel jets, a spark plug and ionization chamber with electrodes set out therein and thereby indicates that their ionization chamber is carried out with rotatability |
| 11/05/2008 | EP1988338A1 Systems and methods for installing cooling holes in a combustion liner |
| 11/05/2008 | EP1987286A1 A swirler for use in a burner of a gas turbine engine |
| 11/05/2008 | CN101298918A Systems and methods for installing cooling holes in a combustion liner |
| 11/04/2008 | CA2366704C Gas turbine combustor |
| 10/30/2008 | WO2008131432A1 Multi-point injection mixer |
| 10/30/2008 | WO2008129652A1 Gas turbine power generating apparatus and method of starting the same |
| 10/30/2008 | WO2008128955A1 Swirler |