| 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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| 05/18/2011 | EP2321178A1 Method for making a nacelle de-icing element |
| 05/18/2011 | CN201835920U Residual oil recovery unit of gas turbine jet nozzle |
| 05/18/2011 | CN1971000B 涡轮动叶片和燃气轮机 Turbine rotor blades and turbine |
| 05/18/2011 | CN1690364B Turbulator on the underside of a turbine blade tip turn and related method |
| 05/18/2011 | CN1680684B Method for manufacturing gas turbine and protection device of a gas turbine engine |
| 05/18/2011 | CN102066721A Lean fuel sucking gas turbine system |
| 05/18/2011 | CN102066696A Turbomachine structural casing |
| 05/18/2011 | CN102061998A Fuel nozzle assembly for a gas turbine engine and method of manufacturing the same |
| 05/18/2011 | CN102061997A Premixing apparatus for fuel injection in turbine engine |
| 05/18/2011 | CN102061996A Inlet air processing system of combustion gas turbine |
| 05/18/2011 | CN102061995A Gas inlet cylinder of gas turbine and manufacturing process thereof |
| 05/18/2011 | CN102061994A Method and device for indirectly promoting medium and low temperature solar heat energy grades |
| 05/18/2011 | CN101680662B Gum-like substance monitoring apparatus and detecting method and gas turbine equipment |
| 05/18/2011 | CN101506578B Burner cleaning device |
| 05/17/2011 | US7942009 Gas turbine engine with an air cooled bearing |
| 05/17/2011 | CA2528893C Method for repairing machine part, method for forming restored machine part, method for manufacturing machine part, gas turbine engine, electric discharge machine, method for repairing turbine component, and method for forming restored turbine component |
| 05/17/2011 | CA2469631C Reduced twist carrier |
| 05/17/2011 | CA2306781C Method for producing abrasive tips for gas turbine blades |
| 05/12/2011 | WO2011056928A2 Micro-turbine combustor |
| 05/12/2011 | WO2011056907A2 Variable performance valve |
| 05/12/2011 | WO2011056360A1 Gas turbine starting process |
| 05/12/2011 | WO2011056296A2 Compressed air energy storage system with reversible compressor-expander unit |
| 05/12/2011 | WO2011055815A1 Combustion burner for gas turbine |
| 05/12/2011 | WO2011055779A1 Cylindrical structure and method for manufacturing same |
| 05/12/2011 | WO2011055778A1 Cylindrical structure and method of production thereof |
| 05/12/2011 | WO2011055094A2 Turbo machine electrical connection element |
| 05/12/2011 | WO2011054806A1 Dual flow turbine engine for an aircraft including structural means for stiffening the central casing |
| 05/12/2011 | US20110110761 Gas turbine having an improved cooling architecture |
| 05/12/2011 | US20110107769 Impingement insert for a turbomachine injector |
| 05/12/2011 | US20110107768 Variable Performance Valve |
| 05/12/2011 | US20110107767 Secondary fuel nozzle venturi |
| 05/12/2011 | US20110107766 Combustor assembly for a turbine engine with enhanced cooling |
| 05/12/2011 | US20110107765 Counter rotated gas turbine fuel nozzles |
| 05/12/2011 | US20110107764 Fuel nozzle assembly for a gas turbine engine and method of assembling the same |
| 05/12/2011 | US20110107763 Micro-turbine combustor |
| 05/12/2011 | US20110107736 System for recirculating the exhaust of a turbomachine |
| 05/12/2011 | DE202010017187U1 Mehrteiliges Turboladergehäuse Multipart turbocharger housing |
| 05/12/2011 | DE19648807B4 Verfahren zum Entfernen einer schützenden Beschichtung und Leitfläche A method for removing a protective coating and guide surface |
| 05/12/2011 | DE102010060363A1 Gasturbinenbrennstoffdüsen mit entgegengerichtetem Drall Gas turbine fuel nozzle with contra-twist |
| 05/12/2011 | DE102010038275A1 Steuerung des Toleranzspielraums von Laufschaufeln und Mänteln einer Turbine Control the tolerance margin of blades and a turbine casings |
| 05/12/2011 | DE102010038274A1 Vorrichtung und Verfahren zur Kühlung von Gasturbinen Apparatus and method for cooling gas turbine |
| 05/12/2011 | DE102010037266A1 Pralleinsatz für Strömungsmaschineninjektor Baffle insert for Strömungsmaschineninjektor |
| 05/12/2011 | DE102009052314A1 Dichtanordnung für eine Gasturbine und eine derartige Gasturbine The seal assembly for a gas turbine and a gas turbine such |
| 05/12/2011 | DE102009046076A1 Generatoreinheit, insbesondere für Kraftfahrzeuge Generator unit, in particular for motor vehicles |
| 05/12/2011 | DE102009046066A1 Brenner für eine Turbine und damit ausgerüstete Gasturbine Burner for a turbine and gas turbine equipped therewith |
| 05/12/2011 | DE102005040184B4 Mantelringsegment einer Gasturbine und Verfahren zur Herstellung derselben Shroud segment of a gas turbine and processes for manufacturing the same |
| 05/12/2011 | CA2780270A1 Micro-turbine combustor |
| 05/12/2011 | CA2780209A1 Variable performance valve |
| 05/12/2011 | CA2779411A1 Cylindrical structure and method for manufacturing the same |
| 05/12/2011 | CA2779409A1 Cylindrical structure and method for manufacturing the same |
| 05/12/2011 | CA2779253A1 Dual flow turbine engine for an aircraft including structural means for stiffening the central casing |
| 05/12/2011 | CA2777285A1 Turbo machine electrical connection element |
| 05/11/2011 | EP2320067A2 Aircraft starter generator |
| 05/11/2011 | EP2320050A2 Gas turbine compressor and method of operation |
| 05/11/2011 | EP2320031A1 Floating brush seal assembly |
| 05/11/2011 | EP2318683A2 Acoustic attenuation panel for aircraft engine nacelle |
| 05/11/2011 | EP2318679A1 Inner wall for the nacelle of a turbine engine |
| 05/11/2011 | EP2318666A1 Fixed vane assembly for a turbine engine having a reduced weight, and turbine engine including at least one such fixed vane assembly |
| 05/11/2011 | CN102057194A Multi-way valve of a fuel system of a gas turbine |
| 05/11/2011 | CN102057145A Method for rinsing a fuel system of a gas turbine and associated fuel system |
| 05/11/2011 | CN102057144A Method of depositing a coating for improving laminar flow |
| 05/11/2011 | CN102054218A Turbine operation degradation determination system and method |
| 05/11/2011 | CN102052157A System and method to insulate turbines and associated piping |
| 05/11/2011 | CN102052156A Apparatus and method for turbine engine cooling |
| 05/11/2011 | CN102052155A System for ice and/or frost prevention using guided wave energy |
| 05/11/2011 | CN102052154A Gas turbine system to inhibit coke formation and methods of use |
| 05/11/2011 | CN102052145A 内燃发动机 Internal combustion engine |
| 05/11/2011 | CN101255801B High back pressure internal combustion steam turbine |
| 05/10/2011 | US7938230 Device for lubricating a component in an assembly of parts |
| 05/10/2011 | US7937951 System for cooling the impeller of a centrifugal compressor |
| 05/10/2011 | US7937950 Device for fastening a sequentially operated burner in a gas turbine arrangement |
| 05/10/2011 | US7937949 Emergency power engine restart system |
| 05/10/2011 | US7937946 Small gas turbine engine with lubricated bearings |
| 05/10/2011 | US7937944 System for ventilating a combustion chamber wall |
| 05/10/2011 | US7937930 Semiclosed Brayton cycle power system with direct heat transfer |
| 05/10/2011 | US7937929 Exhaust duct with bypass channel |
| 05/10/2011 | CA2611612C Internally mounted fuel manifold with support pins |
| 05/05/2011 | WO2011053411A1 Adiabatic compressed air energy storage system with liquid thermal energy storage |
| 05/05/2011 | WO2011053402A1 Reinforced thermal energy storage pressure vessel for an adiabatic compressed air energy storage system |
| 05/05/2011 | WO2011051598A2 Turbine engine starter/generator, and method for the control thereof |
| 05/05/2011 | US20110106680 Turbine operation degradation determination system and method |
| 05/05/2011 | US20110103939 Turbine rotor blade tip and shroud clearance control |
| 05/05/2011 | US20110100020 Apparatus and method for turbine engine cooling |
| 05/05/2011 | US20110100019 Apparatus and methods for fuel nozzle frequency adjustment |
| 05/05/2011 | US20110100018 Operational control system of gas turbine |
| 05/05/2011 | US20110100017 Open Cycle Gas Turbine System Having An Enhanced Combustion Efficiency |
| 05/05/2011 | US20110100016 Apparatus and methods for fuel nozzle frequency adjustment |
| 05/05/2011 | US20110100015 Gas turbine system to inhibit coke formation and methods of use |
| 05/05/2011 | US20110099969 Hybrid multichannel porous structure for hydrogen separation |
| 05/05/2011 | DE102010046596A1 Exhaust turbocharger for internal combustion engine of passenger car, has bearing part formed from material that exhibits higher expansion coefficient than material of bearing element, where element is formed in region that surrounds part |
| 05/05/2011 | DE102009051848A1 Brennkraftmaschine Internal combustion engine |
| 05/05/2011 | DE102009051554A1 Verfahren zum Erzeugen eines Einlaufbelags an einer Strömungsmaschine A method for generating a run-in coating on a turbomachine |
| 05/05/2011 | DE102009051307A1 Charging device, particularly exhaust gas turbocharger, comprises shaft mounted over two roller bearings, where two roller bearings are arranged in cartridge or socket |
| 05/05/2011 | DE102009013150B4 Bauteil zum Einsatz in Heißgasströmungen Component for use in streams of hot gas |
| 05/05/2011 | DE102008028025B4 Hitzeschildanordnung Heat shield assembly |
| 05/05/2011 | DE10041413B4 Verfahren zum Betrieb einer Kraftwerksanlage Method for operating a power plant |
| 05/05/2011 | CA2779155A1 Turbine engine starter/generator, and method for the control thereof |
| 05/04/2011 | EP2317461A1 Turbine operation degradation determination system and method |
| 05/04/2011 | EP2317270A1 Heat exchanging partition wall |
| 05/04/2011 | EP2317176A1 Planetary gear reduction system |