| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 05/16/2012 | CN102458756A 缩小开口直径的方法 The method of narrowing the opening diameter |
| 05/10/2012 | WO2012045029A8 Dual fuel aircraft engine control system and method for operating same |
| 05/10/2012 | WO2012025682A3 Combustion chamber for an aircraft engine, and method for attaching an injection system in a combustion chamber of an aircraft engine |
| 05/10/2012 | US20120111012 Ultra low emissions gas turbine combustor |
| 05/10/2012 | US20120110974 Late lean injection with adjustable air splits |
| 05/10/2012 | DE102011055109A1 Anlage zum Lenken des Luftstroms in einer Kraftstoffdüsenanordnung System for directing the air flow in a fuel nozzle assembly |
| 05/10/2012 | DE102011055053A1 Eigenschwingungen ausführende Brennstoffinjektionsstrahlen Natural oscillations exporting fuel injection jets |
| 05/10/2012 | DE102011055024A1 System und Verfahren zur Verbrennungsdynamiksteuerung durch akustische Steuerung/Unterdrückung von Brennstoffdurchflussschwankungen an einer Brennstoffeinspritzstelle System and method for controlling combustion dynamics by acoustic control / suppression of fuel flow fluctuations to a fuel injection point |
| 05/09/2012 | EP2450533A1 Seal arrangement |
| 05/09/2012 | EP2449310A1 Burner, in particular for gas turbines |
| 05/09/2012 | EP2245314B1 Diffuser for turbine engine including indented annular webs |
| 05/09/2012 | CN102444911A Combustor with lean pre-nozzle fuel injection system |
| 05/09/2012 | CA2756371A1 Seal arrangement |
| 05/08/2012 | US8172568 Combustor |
| 05/08/2012 | US8171740 Annular rich-quench-lean gas turbine combustors with plunged holes |
| 05/03/2012 | WO2012057994A2 Gas turbine combustor with mounting for helmholtz resonators |
| 05/03/2012 | WO2012057908A2 Substrate with shaped cooling holes and methods of manufacture |
| 05/03/2012 | WO2012057282A1 Gas turbine and gas turbine plant provided with same |
| 05/03/2012 | WO2009148682A3 Fuel distributor and method of manufacturing |
| 05/03/2012 | WO2009148680A3 Unitary conduit for transporting fluids and method of manufacturing |
| 05/03/2012 | WO2009126403A3 Swirlers and method of manufacturing |
| 05/03/2012 | US20120102960 Gas turbine engine systems involving cooling of combustion section liners |
| 05/03/2012 | US20120102959 Substrate with shaped cooling holes and methods of manufacture |
| 05/03/2012 | DE102011054872A1 Turbomaschine mit Kontrollsystem zur Kohlenstoffdioxid (CO2)-Konzentrierung und Verfahren Turbo engine control system for carbon dioxide (CO2) -Konzentrierung and procedures |
| 05/03/2012 | DE102011054859A1 Vormischdüse Premix |
| 05/03/2012 | CA2815104A1 Substrate with shaped cooling holes and methods of manufacture |
| 05/02/2012 | EP2446194A1 Combustion chamber arrangement for damping thermo-acoustic oscillations, gas turbine and method of operating such a gas turbine |
| 05/02/2012 | EP1673575B1 Gas turbine engine with an aerodynamic trip |
| 05/02/2012 | CN202209695U Turboshaft engine backflow combustion chamber with novel flame tube cooling structure |
| 05/02/2012 | CN102434893A Combustor liner concentric support and method |
| 05/02/2012 | CN102434892A Combustion liner stop blocks having insertable wear features and related methods |
| 05/02/2012 | CN101235970B Gas turbine combusting device possessing upstream injection device |
| 05/02/2012 | CN101220965B Airfoil, sleeve, and method for assembling a combustor assembly |
| 04/26/2012 | WO2010030309A3 Combustor assembly comprising a combustor device, a transition duct and a flow conditioner |
| 04/26/2012 | WO2009126701A3 Repairable fuel nozzle and a method of repairing |
| 04/26/2012 | DE102011054553A1 Brennstoffdüse für eine Brennkammer Fuel for a combustion chamber |
| 04/26/2012 | DE102011053400A1 Einrichtung und Verfahren für eine Brennkammereinrichtung Apparatus and method for a combustor |
| 04/26/2012 | DE102011052673A1 Duale weiche Durchlässe aufweisende Düse Dual soft passages having nozzle |
| 04/26/2012 | DE102011050491A1 Vorrichtung und Filterungssysteme in Bezug auf Brennkammern in Verbrennungsturbinen Apparatus and filtering systems in terms of combustion chambers in combustion turbines |
| 04/26/2012 | DE102007004394B4 Brenner zum Verbrennen eines Vorgemischs für eine Gasturbine Burner for burning a premix for a gas turbine |
| 04/25/2012 | CN202203988U 涡轴发动机的回流燃烧室 Turboshaft engine combustion chamber reflux |
| 04/25/2012 | CN202203987U 涡轴发动机的回流燃烧室火焰筒冷却结构 Turboshaft engine combustor liner cooling structure reflux |
| 04/25/2012 | CN101910730B 燃气轮机的燃烧器 A gas turbine combustor |
| 04/25/2012 | CN101765742B 用于运行预混合式燃烧器的方法 The method used to run premixed burners |
| 04/24/2012 | CA2513048C Gas turbine floating collar arrangement |
| 04/24/2012 | CA2509797C Gas turbine engine combustion chamber set-up with integrated high-pressure turbine distributor |
| 04/24/2012 | CA2494943C Diffuser for jet turbine engine |
| 04/24/2012 | CA2478876C Air/fuel injection system with cold-plasma generation capability |
| 04/24/2012 | CA2466759C Fuel nozzle sheath retention ring |
| 04/19/2012 | WO2012049035A1 Combustion device with pulsed fuel split |
| 04/19/2012 | WO2012048913A1 Impingement cooled end plate with thermal decoupling for a jet pilot |
| 04/19/2012 | US20120090291 Internal combustion engine |
| 04/18/2012 | EP2442033A1 Anchoring segment for combustion chamber and combustion chamber outer shell |
| 04/18/2012 | EP2442032A1 Wear segment in the turbine stator vane anchoring of the external shell of an annular combustion chamber |
| 04/18/2012 | EP2442031A1 Combustion device with pulsed fuel split |
| 04/18/2012 | EP2442030A1 Axial stage for a burner with a stabilised jet |
| 04/18/2012 | EP2442029A1 Impingement cooled head plate with thermal decoupling for a jet pilot |
| 04/18/2012 | EP2440852A1 Drive for a turbine and drive method |
| 04/18/2012 | EP2440851A1 Heat shield element arrangement comprising screw threading means and method for installing a heat shield element |
| 04/18/2012 | EP2440367A1 Method for reducing the diameter of an opening |
| 04/18/2012 | CN102422083A 燃烧器 Burner |
| 04/17/2012 | US8156746 Lean direct injection atomizer for gas turbine engines |
| 04/17/2012 | US8156724 Combustion chamber |
| 04/17/2012 | CA2714525C Swirl generator |
| 04/12/2012 | WO2012045706A1 Gas-turbine combustion chamber with fuel nozzle, burner with such a fuel nozzle and fuel nozzle |
| 04/12/2012 | DE19948674B4 Verbrennungseinrichtung, insbesondere für den Antrieb von Gasturbinen Combustion device, in particular for the propulsion of gas turbines |
| 04/12/2012 | DE102011054308A1 Brennkammer mit einem Magerbetrieb-Vordüsen-Brennstoffeinspritzsystem Combustion chamber with a lean operation fuel injection system pre-orifices |
| 04/12/2012 | DE102011054259A1 Flammenverträgliche Primärdüsenkonstruktion Compatible flames primary nozzle design |
| 04/12/2012 | DE102011054251A1 Vorrichtung und Verfahren zur Modifizierung einer Brennkammerdüse An apparatus and method for modifying a Brennkammerdüse |
| 04/11/2012 | EP2439452A2 Gas turbine combustor |
| 04/11/2012 | EP2439448A1 Method and device for detecting liquid fuel leakage in a gas turbine system combustion assembly |
| 04/11/2012 | EP2439447A1 Fuel nozzle, gas turbine combustion chamber and burner with such a fuel nozzle |
| 04/11/2012 | EP2439389A1 Method for manufacturing combustor constituent member, combustor constituent member, gas turbine combustor, and gas turbine |
| 04/11/2012 | EP2438357A2 Burner, operating method and assembly method |
| 04/11/2012 | CN102414514A 预混合燃烧器 Premixed burner |
| 04/11/2012 | CN102414513A 旋流器、燃烧腔以及改进混合的燃气涡轮 Cyclone, combustion chamber and improved hybrid gas turbine |
| 04/11/2012 | CN101382298B Outer sidewall retention scheme for a singlet first stage nozzle |
| 04/11/2012 | CN101307442B Method for making high-temperature articles |
| 04/10/2012 | CA2557440C Dual conduit fuel manifold for gas turbine engine |
| 04/05/2012 | WO2012045029A1 Dual fuel aircraft engine control system and method for operating same |
| 04/05/2012 | WO2012043073A1 Air recovery-type cooling structure for air-cooled gas turbine combustor |
| 04/05/2012 | WO2012041906A1 Burner for a gas turbine |
| 04/05/2012 | WO2012041839A1 Burner for a gas turbine |
| 04/05/2012 | WO2009126485A3 Method of assembling a fuel nozzle |
| 04/05/2012 | US20120079827 Air-cooled swirlerhead |
| 04/05/2012 | DE102011054174A1 Turbomaschine mit einem Mischrohrelement mit einem Wirbelgenerator Turbo engine with a mixing tube member having a vortex generator |
| 04/05/2012 | CA2812256A1 Dual fuel aircraft engine control system and method for operating same |
| 04/04/2012 | EP2436983A1 Jet burner |
| 04/04/2012 | EP2436982A1 An igniter |
| 04/04/2012 | EP2436979A1 Burner for a gas turbine |
| 04/04/2012 | EP2436977A1 Burner for a gas turbine |
| 04/04/2012 | EP2435681A1 Stabilizing a gas turbine engine via incremental tuning |
| 04/04/2012 | CN102401398A Fuel injection assembly for use in turbine engines and method of assembling same |
| 04/04/2012 | CN102401397A Apparatus and method for mixing fuel in gas turbine nozzle |
| 04/04/2012 | CN101726005B 三重漩涡燃气轮机燃烧室 Triple swirl gas turbine combustor |
| 04/03/2012 | US8146372 Gas turbine combustion chamber having inner and outer walls subdivided into sectors |
| 04/03/2012 | US8146365 Fuel nozzle providing shaped fuel spray |
| 04/03/2012 | CA2495169C Side-fed shielded internal fuel manifold inlet tube |
| 03/29/2012 | WO2012039611A1 Combustor with a single limited fuel-air mixing burner and recuperated micro gas turbine |
| 03/29/2012 | WO2012038404A1 Burner with low nox emissions |