| Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889) |
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| 01/03/2014 | WO2014004494A1 Real time linearization of a component-level gas turbine engine model for model-based control |
| 01/03/2014 | WO2014004491A1 Sleeve for turbine bearing stack |
| 01/03/2014 | WO2014004347A1 Bearing support for a turbocharger |
| 01/03/2014 | WO2014004344A1 Turbocharger support housing having alignment features |
| 01/03/2014 | WO2014004266A1 Thrust reverser maintenance actuation system |
| 01/03/2014 | WO2014004238A1 Exhaust-gas turbocharger |
| 01/03/2014 | WO2014004122A1 Pre-turbine exhaust case variable area mixing plane |
| 01/03/2014 | WO2014004069A1 Methods and apparatus for co-firing fuel |
| 01/03/2014 | WO2014004001A1 Mistake proof damper pocket seals |
| 01/03/2014 | WO2014003985A1 Valve for controlling flow of a turbomachine fluid |
| 01/03/2014 | WO2014003958A1 Turbine blade platform with u-channel cooling holes |
| 01/03/2014 | WO2014002818A1 Oxidation system for treatment of low-concentration methane gas provided with multiple oxidizers |
| 01/03/2014 | WO2014001230A1 Method for a part load co reduction operation for a sequential gas turbine |
| 01/03/2014 | WO2013181389A3 Ladder seal system for gas turbine engines |
| 01/03/2014 | WO2013165513A3 Counter-rotating low pressure turbine without turbine exhaust case |
| 01/03/2014 | WO2013165511A3 Edm method for multi-lobed cooling hole |
| 01/03/2014 | WO2013165506A3 Cooling hole with crenellation features |
| 01/03/2014 | WO2013165503A3 Cooling hole with enhanced flow attachment |
| 01/03/2014 | WO2013165502A3 Cooling hole with thermo-mechanical fatigue resistance |
| 01/03/2014 | WO2013044197A3 A combustor resonator section with an internal thermal barrier coating and method of fabricating the same |
| 01/02/2014 | US20140003915 Low noise compressor rotor for geared turbofan engine |
| 01/02/2014 | US20140000285 Gas turbine engine turbine vane platform core |
| 01/02/2014 | US20140000284 Cooling apparatus for a mid-turbine frame |
| 01/02/2014 | US20140000283 Cover plate for a component of a gas turbine engine |
| 01/02/2014 | US20140000282 Turbine blade platform with u-channel cooling holes |
| 01/02/2014 | US20140000280 Gas turbine engine turbine blade airfoil profile |
| 01/02/2014 | US20140000279 System and method for operating a precooler in an aircraft |
| 01/02/2014 | US20140000278 Turbomachine thermal energy exchange |
| 01/02/2014 | US20140000276 Turbomachine comprising a privileged injection device and corresponding injection method |
| 01/02/2014 | US20140000275 Lng fuel handling for a gas turbine engine |
| 01/02/2014 | US20140000271 Systems and Methods For Controlling Stoichiometric Combustion In Low Emission Turbine Systems |
| 01/02/2014 | US20140000269 Combustion nozzle and an associated method thereof |
| 01/02/2014 | US20140000268 Igniter for a turbomachine and mounting assembly therefore |
| 01/02/2014 | US20140000267 Transition duct for a gas turbine |
| 01/02/2014 | US20140000266 Gas Turbine Fuel Nozzle End Cover Using Au-Ni Braze and Method Producing Same |
| 01/02/2014 | US20140000264 Combustion burner |
| 01/02/2014 | DE19963099B4 Kühlluftbohrungen in Gasturbinenkomponenten Cooling holes in gas turbine components |
| 01/02/2014 | DE102012210702A1 Method for preheating fuel to be combusted in gas turbine, involves heating fuel by heat exchange with lubricant of gas turbine before injecting fuel into combustion chamber, where fuel flows through heat exchanger on secondary side |
| 01/02/2014 | DE102009053000B4 Fanrückhaltescheibe für ein Strahltriebwerk Fanrückhaltescheibe for a jet engine |
| 01/01/2014 | EP2679785A1 Gas turbine |
| 01/01/2014 | EP2679784A1 Hot water injection for turbomachine |
| 01/01/2014 | EP2679780A1 Diffuser for the exhaust section of a gas turbine and gas turbine with such a diffuser |
| 01/01/2014 | EP2679779A2 Modified rotor component and method for modifing a wear charcteristic of a rotor component in a turbine system |
| 01/01/2014 | EP2679771A1 Systems and methods to control flow in a rotor wheel |
| 01/01/2014 | EP2678543A1 Driveshaft for the gearbox of auxiliary machines of a turbojet engine |
| 01/01/2014 | EP2678542A1 Turbomachine comprising a privileged injection device and corresponding injection method |
| 01/01/2014 | CN103492158A Moulded article |
| 01/01/2014 | CN103486024A Flow and pressure ripple reduction with advance dual gear and bearing face cut |
| 01/01/2014 | CN103485896A Anti-siphon structure in oil suction inlet of lubricating oil pump |
| 01/01/2014 | CN103485895A Ultrahigh rotation speed centrifugal ventilator |
| 01/01/2014 | CN103485894A Thermally actuated assembly for a gas turbine system and method of controlling a cooling airflow path |
| 01/01/2014 | CN103485893A Method, system and apparatus for enhanced off line compressor and turbine cleaning |
| 01/01/2014 | CN102322353B Method for increasing thermal efficiency of cycle of combustion turbine |
| 01/01/2014 | CN102235267B Gas turbine engine modified by using retired turbofan engine through low-pressure crest truncation |
| 01/01/2014 | CN102220903B Method for raising cyclic thermal performance of gas turbine based on combustion-reforming of methane |
| 01/01/2014 | CN102213142B Method for increasing thermal efficiency of reheating cycle of gas turbine based on methane reformation |
| 01/01/2014 | CN101952558B Fastening device for an exhaust-gas turbocharger |
| 12/31/2013 | US8616007 Structural attachment system for transition duct outlet |
| 12/31/2013 | US8616006 Advanced optics and optical access for laser ignition for gas turbines including aircraft engines |
| 12/31/2013 | US8616002 Gas turbine premixing systems |
| 12/31/2013 | CA2701748C Sealing segment and sealing-segment arrangement |
| 12/31/2013 | CA2644099C Impingement cooled structure |
| 12/31/2013 | CA2557047C Fuel nozzle for gas turbine engines |
| 12/27/2013 | WO2013192540A1 Turbine engine combustor wall with non-uniform distribution of effusion apertures |
| 12/27/2013 | WO2013192525A1 Liquid fuel turbine engine for reduced oscillations |
| 12/27/2013 | WO2013192523A1 Gas fuel turbine engine for reduced oscillations |
| 12/27/2013 | WO2013192378A1 Spherical-link end damper system with near constant engagement |
| 12/27/2013 | WO2013192373A1 Bulb seal with metal backed fastener |
| 12/27/2013 | WO2013192064A1 Two-piece duct assembly |
| 12/27/2013 | WO2013192063A1 Four bar drive mechanism for bleed system |
| 12/27/2013 | WO2013192055A1 Four bar bracket |
| 12/27/2013 | WO2013191954A1 Method of reducing combustion induced oscillations in a turbine engine |
| 12/27/2013 | WO2013191941A1 Exhaust-gas turbocharger |
| 12/27/2013 | WO2013191937A1 Compressor cover for turbochargers |
| 12/27/2013 | WO2013191889A1 Turbomachine flow stability enhancement device control |
| 12/27/2013 | WO2013191877A1 Airfoil including adhesively bonded shroud |
| 12/27/2013 | WO2013191850A1 Metallic rails on composite fan case |
| 12/27/2013 | WO2013191843A1 Intershaft seal with centrifugal compensation |
| 12/27/2013 | WO2013191195A1 Vane linking portion structure, and jet engine using same |
| 12/27/2013 | WO2013191070A1 Fan case for aircraft engine |
| 12/27/2013 | WO2013189883A1 Seal between static turbine parts |
| 12/27/2013 | WO2013165521A3 Gas turbine engine with fan-tied inducer section and multiple low pressure turbine sections |
| 12/27/2013 | WO2013165509A3 Multi-lobed cooling hole |
| 12/27/2013 | WO2013165508A3 Multi-lobed cooling hole array |
| 12/27/2013 | WO2013165505A3 Composite fan containment case assembly |
| 12/27/2013 | WO2013162665A3 Engine hot section vane with tapered flame holder surface |
| 12/27/2013 | CA2875928A1 Fan case for aircraft engine |
| 12/27/2013 | CA2875746A1 Seal between static turbine parts |
| 12/26/2013 | US20130344318 Formation of Corrosion-Resistant Coating |
| 12/26/2013 | US20130343900 Process for producing a run-in coating |
| 12/26/2013 | US20130341872 Channeled spring seal for sealing an air gap between moving plates |
| 12/26/2013 | US20130341426 Flexible leaf spring seal for sealing an air gap between moving plates |
| 12/26/2013 | US20130340439 Systems and Methods for De-Icing a Gas Turbine Engine Inlet Screen and Dehumidifying Inlet Air Filters |
| 12/26/2013 | US20130340438 Method of reducing combustion induced oscillations in a turbine engine |
| 12/26/2013 | US20130340436 Gas fuel turbine engine for reduced oscillations |
| 12/26/2013 | US20130340404 Hot egr driven by turbomachinery |
| 12/25/2013 | EP2677140A2 Conical light fod momentum particle separator protector |
| 12/25/2013 | EP2676023A1 Process for cooling the turbine stage and gas turbine having a cooled turbine stage |
| 12/25/2013 | EP2084378B1 Bearing structure of turbocharger |
| 12/25/2013 | CN203362322U Fuel supply switching system for gas turbine generator sets |