| 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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| 08/21/2008 | WO2008076471A3 Aircraft engine inlet pivotable barrier filter |
| 08/21/2008 | WO2008073826A3 Monolithic acoustically-treated engine nacelle inlet panels |
| 08/21/2008 | US20080196974 Device and method of standby lubrification for an engine |
| 08/21/2008 | US20080196383 Airframe mounted electric motor driven lubrication pump control deoil system |
| 08/21/2008 | DE102007008296A1 Verfahren zur automatischen Regelung einer oder mehrerer Feuerungstemperaturen einer Gasturbinenanlage und Verfahren zur Bestimmung des Wassergehalts im Abgas einer Gasturbinenanlage A method for automatically controlling one or more combustion temperatures of a gas turbine system and method for determining the water content in the exhaust gas of a gas turbine plant |
| 08/21/2008 | CA2621725A1 Apparatus and process for emergency lubrication of engines |
| 08/20/2008 | EP1959114A2 Multi-speed gearbox for low spool driven auxiliary component |
| 08/20/2008 | EP1959113A1 Method of taking auxiliary energy on an airplane jet engine and jet engine equipped to implement such a method |
| 08/20/2008 | EP1959104A1 Insulating system |
| 08/20/2008 | EP1959102A2 Gas turbine with turbo generator |
| 08/20/2008 | EP1825114B1 Tip turbine engine with a heat exchanger |
| 08/20/2008 | CN101245713A 废气涡轮 Turbocharged |
| 08/20/2008 | CN100412333C Method and apparatus for actuating fuel trim valves in a gas turbine |
| 08/19/2008 | US7413399 Method and apparatus for distributing fluid into a turbomachine |
| 08/19/2008 | US7412834 Annular combustion chamber for a turbomachine with an improved inner fastening flange |
| 08/19/2008 | US7412833 Method of cooling centerbody of premixing burner |
| 08/19/2008 | US7412831 Integral cooling system for rotary engine |
| 08/19/2008 | US7412819 Turbojet architecture with two fans at the front |
| 08/19/2008 | CA2413640C Process for rejuvenating a diffusion aluminide coating |
| 08/19/2008 | CA2406430C Method for removing metal cladding from airfoil substrate |
| 08/19/2008 | CA2328555C Hot air evacuation device for the nose inlet cowl of a jet engine, with de-icing system |
| 08/14/2008 | WO2008041964A8 Infrared suppression system |
| 08/14/2008 | US20080190114 Gas turbine engine component cooling scheme |
| 08/14/2008 | US20080190113 Gas turbine combustor and fuel supply method for same |
| 08/14/2008 | US20080190112 Gas turbine combustor and fuel supply method for same |
| 08/14/2008 | US20080190094 Combination Power Plant and Method For the Cooling Thereof |
| 08/14/2008 | US20080190093 System for deicing the nose cone of an aircraft turbojet with oil |
| 08/14/2008 | US20080190091 Bifurcated oil scavenging bearing compartment within a gas turbine engine |
| 08/14/2008 | DE19717267B4 Verfahren zur Aufbereitung von tiefgekühltem Flüssiggas A method for treating liquefied gas |
| 08/14/2008 | CA2620806A1 Oil-based de-icing system for the nose cone of an aircraft turbine engine |
| 08/14/2008 | CA2619168A1 Impeller rear cavity thrust adjustor |
| 08/13/2008 | EP1956215A2 Gas turbine engine with insulated cooling circuit |
| 08/13/2008 | EP1956214A2 Vapour cooling system for a gas turbine engine |
| 08/13/2008 | EP1956195A2 Heater for the surface of a gas turbine component |
| 08/13/2008 | EP1956116A1 Removal of thermal barrier coatings |
| 08/13/2008 | EP1954919A1 Device for absorbing sound in power plants |
| 08/13/2008 | EP1444417B1 Turbine blade cooling system and method of cooling a turbine blade |
| 08/13/2008 | EP1257349B1 A heat exchanger for cooling and for a pre-cooler for turbine intake air conditioning |
| 08/13/2008 | CN201100174Y Anti-sliding structure of Ti alloy supporter for gas turbine dynamic device |
| 08/13/2008 | CN101243242A Compressor, compressor wheel, cleaning attachment and exhaust turbocharger |
| 08/13/2008 | CN100410496C High efficiency stator for the first phase of a gas turbine |
| 08/13/2008 | CN100410494C High efficiency rotor for a gas turbine |
| 08/13/2008 | CN100410404C Precipitation reinforced Ni-Fe-Cr alloy and its production method |
| 08/12/2008 | US7410343 Gas turbine |
| 08/12/2008 | US7409832 Gas turbine power generator plant with mutually independent cooling air channels from intake to exhaust |
| 08/12/2008 | US7409831 Provision of sealing in a jet engine for bleeding air to the cabin using a tube with a double ball joint |
| 08/12/2008 | CA2468134C Device for supplying secondary air in a gas turbine engine |
| 08/12/2008 | CA2397612C Gas and steam turbine installation |
| 08/12/2008 | CA2337311C Methods and apparatus for reducing heat load in combustor panels |
| 08/07/2008 | WO2008093447A1 Low noise aircraft |
| 08/07/2008 | WO2008092845A2 A gas turbine |
| 08/07/2008 | WO2008092252A1 Gas turbine engine fuel control system |
| 08/07/2008 | WO2008092184A1 Boring machine for turbine casings |
| 08/07/2008 | WO2008059169A3 Aircraft leading edge |
| 08/07/2008 | WO2008059169A2 Aircraft leading edge |
| 08/07/2008 | DE10361644B4 Luftleitklappe eines Luftfahrzeuges mit Regelung der auf sie wirkenden Druckkräfte, und Stauluftsystem mit einer solchen Luftleitklappe Air guiding an aircraft with control of the pressure forces acting on them, and ram air system with such a flow-rate control |
| 08/07/2008 | CA2670272A1 Metal/polymer laminate ducting and method of making same |
| 08/06/2008 | EP1953364A1 Gas turbine engine with a starter mounted on the gear unit |
| 08/06/2008 | EP1953352A2 Method and system for increasing modified Wobbe index control range of fuel gas |
| 08/06/2008 | EP1953268A1 Thermal barrier coatings with low thermal conductivity comprising lanthanide sesquioxides |
| 08/06/2008 | EP1953267A1 Thermal barrier coatings with low thermal conductivity comprising lanthanide sesquioxides |
| 08/06/2008 | EP1539573B1 Torsionally de-coupled engine mount system |
| 08/06/2008 | EP1497476B1 Process of masking cooling holes of a gas turbine component |
| 08/06/2008 | CN201096019Y Heavy duty burning machine assembly overturning support |
| 08/06/2008 | CN101235753A Distributed architecture for a gas turbine starter/generator |
| 08/06/2008 | CN101235730A Gas turbine engine with a gearbox-mounted starter |
| 08/06/2008 | CN101235728A Impingement cooled bucket shroud, turbine rotor incorporating the same, and cooling method |
| 08/06/2008 | CN101235327A Class natural gas combination circulation |
| 08/06/2008 | CN100408823C Connector assembly for mounting a gas turbine engine |
| 08/06/2008 | CN100408726C High temp-resistant article and its manufacturing method |
| 08/06/2008 | CN100408146C Configuration and process for carbonyl removal |
| 08/05/2008 | US7407368 Turbine shroud segment |
| 08/05/2008 | CA2418842C Method for converting thermal energy into mechanical work |
| 08/05/2008 | CA2399210C Welding superalloy articles |
| 07/31/2008 | WO2008089925A2 Hydrodynamic drive of a high-pressure compressor shaft of a gas turbine engine |
| 07/31/2008 | US20080179466 Dual Flow APU Inlet and Associated Systems and Methods |
| 07/31/2008 | US20080178604 Process for Optimizing the Energy of a Combined Heat and Power Generation Site |
| 07/31/2008 | US20080178598 Device for injecting a mixture of air and fuel, and combustion chamber and turbomachine both equipped with such a device |
| 07/31/2008 | DE102008005943A1 Guide blade sealing device for gas turbo group, has compressor and turbine guide blades and axially limiting hot spot segments, which are connected among each other in gas-tight manner using temperature-resistant skeletal laminations |
| 07/31/2008 | DE102007004274A1 Gasturbinentriebwerk, insbesondere Flugtriebwerk Gas turbine engine, in particular aircraft engine |
| 07/31/2008 | CA2619326A1 Distributed architecture for a gas turbine starter-generator |
| 07/30/2008 | EP1950392A1 Device for assembling two units, for example for a turbomachine stator |
| 07/30/2008 | EP1948921A2 Methods and apparatus for a fluid inlet |
| 07/30/2008 | CN201093150Y Adjustable supporting structure |
| 07/30/2008 | CN201092868Y Dedusting desalination injection mechanism for turbine rotor vane |
| 07/30/2008 | CN101230988A Operating method for coal gasification combined cycle power plant |
| 07/30/2008 | CN101230802A Variable coupling of high pressure rotor and low pressure rotor of turbofan engine |
| 07/30/2008 | CN101230801A Regulation of the temperature of hot gas of a gas turbine |
| 07/30/2008 | CN101230800A Holding device and system for turbine rotor |
| 07/30/2008 | CN101230790A Control system based on forecasting model for heavy gas turbine |
| 07/30/2008 | CN100406684C Gas turbo group |
| 07/30/2008 | CN100406683C Recirculation structure for a turbocompressor |
| 07/30/2008 | CN100406678C Method and equipment for assembling rotary machine |
| 07/30/2008 | CA2619146A1 Apparatus for cooling electrical equipment in a turbine engine |
| 07/30/2008 | CA2619142A1 Gas turbine engine with a gearbox-mounted starter |
| 07/29/2008 | US7404986 Physical vapor deposition is augmented by chemical vapor deposition from one or more organometallic compounds, preferably refractory metal carbonyls, to deposit coatings and repair material on superalloy turbine engine parts |
| 07/29/2008 | US7404678 Rotor recentering after decoupling |
| 07/29/2008 | US7404294 Gas turbine and a method for controlling a gas turbine |
| 07/29/2008 | US7404287 Gas turbine, combined cycle plant and compressor |
| 07/29/2008 | US7404286 Orbiting combustion nozzle engine |