| 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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| 05/21/2009 | US20090126337 Retrofit dirt separator for gas turbine engine |
| 05/21/2009 | US20090126335 Cooling structure |
| 05/20/2009 | EP2060759A2 Split gearbox and nacelle arrangement |
| 05/20/2009 | EP2060747A2 Attachment of a bearing supporting a rotor on a turbomachine |
| 05/20/2009 | EP2060742A2 Dual Configuration seal assembly for a rotational assembly |
| 05/20/2009 | DE102007054467A1 Method for preheating fuel in gas and steam power plant, involves guiding steam or condenser water of condenser as heat transfer medium by heat exchanger |
| 05/20/2009 | DE102007052102A1 Verfahren zur Herstellung einer Schmiermittelzuführung eines Axiallagers A method for producing a lubricant feed of an axial bearing |
| 05/20/2009 | DE102007052101A1 Axiallager, insbesondere für einen Turbolader Axial bearing, in particular for a turbocharger |
| 05/20/2009 | CN201241758Y Small-sized gas turbine with air inlet and exhaust valves and free wheel |
| 05/20/2009 | CN101438039A Modular fuel supply device for a gas turbine |
| 05/20/2009 | CN100489396C Mixing swirler |
| 05/20/2009 | CN100489289C Jet engine cabin air bleed cavity sealing device |
| 05/20/2009 | CN100489288C Device for using seal member for releasing air of cabin and sealing cavity |
| 05/20/2009 | CN100489287C Low flow resistance veneer structure |
| 05/20/2009 | CN100489286C Square shape auxiliary flow-disturbing column veneer structure |
| 05/20/2009 | CN100489285C Ancient coin type flow-disturbing column veneer structure |
| 05/20/2009 | CN100489277C Methods and apparatus for cooling gas turbine rotor blades |
| 05/19/2009 | US7533760 Noise reduction tubes |
| 05/19/2009 | US7533534 HPT aerodynamic trip to improve acoustic transmission loss and reduce noise level for auxiliary power unit |
| 05/19/2009 | US7533526 Drive arrangement |
| 05/19/2009 | CA2475146C System and method of cooling steam turbines |
| 05/14/2009 | WO2009060137A2 Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure |
| 05/14/2009 | WO2009031945A3 Gas turbine plant |
| 05/14/2009 | US20090123267 Inlet film cooling of turbine end wall of a gas turbine engine |
| 05/14/2009 | US20090123266 Air sealing element |
| 05/14/2009 | US20090121083 Nacelle Flow Assembly |
| 05/14/2009 | US20090120522 Fuel inlet with crescent shaped passage for gas turbine engines |
| 05/14/2009 | US20090120103 Method and apparatus for sub sea power generation |
| 05/14/2009 | US20090120102 Turbine engine frame having an actuated equilibrating case |
| 05/14/2009 | US20090120101 Organic Matrix Composite Components, Systems Using Such Components, and Methods for Manufacturing Such Components |
| 05/14/2009 | US20090120100 Starter Generator System for a Tip Turbine Engine |
| 05/14/2009 | US20090120099 Anti-icing apparatus and method for aero-engine nose cone |
| 05/14/2009 | US20090120095 Combustion liner thimble insert and related method |
| 05/14/2009 | US20090120093 Turbulated aft-end liner assembly and cooling method |
| 05/14/2009 | US20090120059 Seal for pulse detonation engine |
| 05/14/2009 | DE202009002457U1 Lagergehäuse eines Abgasturboladers An exhaust gas turbocharger bearing housing |
| 05/14/2009 | DE102008037531A1 System zum Verringern der Schwefeloxid-Emissionen, die durch eine Turbomaschine erzeugt werden System for reducing sulfur oxide emissions, which are generated by a turbomachine |
| 05/14/2009 | DE102008037526A1 Verfahren und Systeme zur Montage einer Austrittshaube für eine Turbine Methods and systems for assembling a discharge hood for a turbine |
| 05/14/2009 | CA2700087A1 Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure |
| 05/14/2009 | CA2638541A1 Fuel inlet with crescent shaped passage for gas turbine engines |
| 05/13/2009 | EP1730445B1 Method for operating a heat engine, preferably a gas turbine installation |
| 05/13/2009 | EP1549842A4 A system for catalytic combustion |
| 05/13/2009 | CN201236746Y Air-intake atomizing type vaporization cooling and wet compression system of gas turbine |
| 05/13/2009 | CN101429893A Air cooled gas turbine components and methods of manufacturing and repairing the same |
| 05/13/2009 | CN101429892A Turboshaft engine including means for heating the air entering the power turbine |
| 05/13/2009 | CN100487712C Method and apparatus for modeling gas turbine engine |
| 05/13/2009 | CN100487233C Connection assembly for connecting connector to hook |
| 05/13/2009 | CA2644326A1 Turbojet turbine or compressor stage |
| 05/13/2009 | CA2643773A1 Method for attaching a bearing supporting a rotor on a turbomachine |
| 05/12/2009 | US7530757 Rotor coupling having insulated structure |
| 05/09/2009 | CA2643614A1 Means of blocking rotation of an axis supporting a suspension component of a turboshaft |
| 05/07/2009 | WO2009056699A2 Seal having a large compression range |
| 05/07/2009 | WO2008139096A4 Helicopter turboshaft engine comprising a gas generator and a free turbine |
| 05/07/2009 | US20090116953 Turbine airfoil with platform cooling |
| 05/07/2009 | US20090114178 Fuel injection device including plasma-inducing electrode arrays |
| 05/07/2009 | US20090113893 Pilot mixer for mixer assembly of a gas turbine engine combustor having a primary fuel injector and a plurality of secondary fuel injection ports |
| 05/07/2009 | DE112007001504T5 Stromerzeugung Power generation |
| 05/07/2009 | DE102008037503A1 Automatikimpuls-Patronenreinigungssystem und -Verfahren Automatic pulse cartridge cleaning system and method |
| 05/07/2009 | DE102008037501A1 Gasturbinen mit nachgiebigen Sehnengelenkdichtungen Gas turbines with flexible chordal hinge seals |
| 05/07/2009 | DE102007051865A1 Brennkammer mit Zünder für Gasturbinen Combustion chamber with igniter for gas turbines |
| 05/07/2009 | DE102007051845A1 Turbolader und Verfahren zum Erzeugen eines Vordralls vor einem Verdichter des Turboladers Turbocharger and method for generating a pre-whirl in front of a compressor of the turbocharger |
| 05/07/2009 | DE102007051844A1 Turbolader mit einem Verdichtergehäuse zum Einstellen eines Vordralls Turbocharger with a compressor housing for setting a pre-swirl |
| 05/07/2009 | CA2696837A1 Seal having a large compression range |
| 05/06/2009 | EP2056023A1 Annular combustion chamber for a gas turbine engine |
| 05/06/2009 | EP2055938A1 Current-protected driver circuit for ignition exciter unit |
| 05/06/2009 | EP2055905A2 Power turbine test apparatus |
| 05/06/2009 | EP2055899A2 Systems and methods for controlling seal clearance in a turbine engine |
| 05/06/2009 | EP1146989A4 Laser drilling holes in a cylindrical workpiece |
| 05/06/2009 | CN100484836C Air guiding flap, process for adjusting the position of the air guiding flap and ram air system including the air guiding flap |
| 05/06/2009 | CN100484679C Welding process |
| 05/05/2009 | US7527481 Ejector pump for a fuel system for a gas turbine engine |
| 05/05/2009 | US7527220 Aircraft engine mount |
| 05/05/2009 | US7527068 Valve with swirling coolant |
| 05/05/2009 | US7526926 Method for efficient nonsynchronous LNG production |
| 05/05/2009 | US7526921 Auxiliary power unit with integral firebox |
| 05/05/2009 | US7526920 Method of operating an atomizing arrangement |
| 05/05/2009 | US7526862 Method of manufacturing a hollow blade for a turbomachine |
| 04/30/2009 | WO2009055041A2 Low shock strength propulsion system |
| 04/30/2009 | WO2009054050A1 Method for demounting blade ring and member for demounting blade ring |
| 04/30/2009 | WO2009007564A3 Turbojet engine for aircraft |
| 04/30/2009 | WO2008127467A3 Ceramic-encased hot surface igniter system for jet engines |
| 04/30/2009 | US20090110549 Gas turbines having flexible chordal hinge seals |
| 04/30/2009 | US20090110545 Systems and Methods for Controlling Seal Clearance In A Turbine Engine |
| 04/30/2009 | US20090107557 Low shock strength inlet |
| 04/30/2009 | US20090107149 Current-protected driver circuit for ignition exciter unit |
| 04/30/2009 | US20090107148 Annular combustion chamber of a gas turbine engine |
| 04/30/2009 | US20090107147 Gas turbine fuel injector with removable pilot liquid tube |
| 04/30/2009 | US20090107106 Gas Turbine Engine Systems Involving Hydrostatic Face Seals |
| 04/30/2009 | DE19855708B4 Rohrkammerdämpfer Pipe chamber damper |
| 04/30/2009 | DE102007051498A1 Kraftstoffzumesseinheit für ein Flugzeugtriebwerk Fuel metering unit for an aircraft engine |
| 04/30/2009 | CA2703602A1 Low shock strength propulsion system |
| 04/30/2009 | CA2643672A1 Annular combustion chamber for gas turbine engines |
| 04/30/2009 | CA2641881A1 Sequential stiffness support for bearing assemblies and method of fabrication |
| 04/30/2009 | CA2639026A1 Abradable rim seal for low pressure turbine engine |
| 04/29/2009 | EP2053206A2 Gas turbine oil scavenging system |
| 04/29/2009 | CN101421156A Inlet distortion and recovery control system |
| 04/29/2009 | CN101418724A System for delivering air from a multi-stage compressor to a turbine portion of a gas turbine engine |
| 04/29/2009 | CN101418723A Internal waverider-derived hypersonic inlet with ordered inlet and outlet shape and design method |
| 04/29/2009 | CN101417592A Improvement for rotorcraft equipped with turboshaft engines |
| 04/29/2009 | CN100482928C Seal device |