Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
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)
10/2005
10/19/2005CN1683750A Repairing tenons on turbine buckets
10/19/2005CA2501525A1 Anti-rotation lock
10/18/2005USRE38831 Gas turbine having water spray injection control
10/18/2005US6956301 Method and apparatus for controlling output voltages and frequencies of turbine/alternator on common shaft
10/18/2005US6955052 Thermal gas compression engine
10/18/2005US6955040 Controlled pressure fuel nozzle injector
10/18/2005US6955039 Gas turbine control apparatus and gas turbine system using the same
10/18/2005CA2172071C Protective coating
10/16/2005CA2502816A1 Forced air cooling system
10/15/2005CA2502810A1 Turbine shroud cooling system
10/13/2005WO2005095864A1 Multiple burner arrangement for operating a combustion chamber, and method for operating the multiple burner arrangement
10/13/2005WO2005095861A1 Method for the operation of a heat engine, preferably a gas turbine plant
10/13/2005WO2005095860A1 Method for operating a heat engine, preferably a gas turbine installation
10/13/2005WO2005095773A1 Gas turbine featuring partial recuperation, and method for the operation of a gas turbine system
10/13/2005US20050228553 Hybrid Electric Vehicle Energy Management System
10/13/2005US20050227106 Single crystal combustor panels having controlled crystallographic orientation
10/13/2005US20050226728 Device for balancing a rotating part, in particular a turbojet rotor
10/13/2005US20050226714 Method and apparatus for fabricating gas turbine engines
10/13/2005US20050225456 Helicopter tactile exceedance warning system
10/13/2005US20050225303 Gas turbine engine starter-generator exciter starting system and method including a capacitance circuit element
10/13/2005US20050224635 Dual action inlet door and method for use thereof
10/13/2005US20050224487 Welding process
10/13/2005US20050223728 Refrigerator power plant
10/13/2005US20050223712 Vaporization of liquefied natural gas for increased efficiency in power cycles
10/13/2005US20050223690 Centrifugal pump fuel system and method for gas turbine engine
10/13/2005US20050223629 Method of inhibiting deposit formation in a jet fuel at high temperatures
10/13/2005DE102004014118A1 Anordnung zur Abdichtung eines Übergangs zwischen Kühlpassagen zweier Komponenten einer Turbomaschine Arrangement for sealing a transition between cooling passages of two components of a turbomachine
10/13/2005DE102004014117A1 Komponente einer Turbomaschine mit einer Kühlanordnung Component of a turbo engine with a cooling arrangement
10/13/2005DE102004012080A1 Vorrichtung und Verfahren zum Erwärmen eines Gasstroms Device and method for heating a gas stream
10/12/2005EP1584871A2 Single crystal articles having controlled crystallographic orientation
10/12/2005EP1584827A1 Ceramic bushing for a variable vane assembly of a turbomachine
10/12/2005EP1584797A2 A containment apparatus for a gas turbine engine
10/12/2005EP1584795A2 High efficiency stator for the first phase of a gas turbine
10/12/2005EP1584788A2 High efficiency rotor for a gas turbine
10/12/2005EP1584787A2 High efficiency rotor for the first phase of a gas turbine
10/12/2005EP1584785A1 Balancing weight for a rotor, especially for a rotor of a jet engine
10/12/2005EP1584784A1 Assembly device for annular flanges, in particular in turbomachines
10/12/2005EP1584702A1 Deposition repair of hollow items
10/12/2005EP1584402A2 Welding process
10/12/2005EP1485592A4 Gas turbine apparatus
10/12/2005EP1206634A4 Supercharging system for gas turbines
10/12/2005CN1682078A 燃气轮机 Gas turbine
10/12/2005CN1682023A Jet motor or turbine motor
10/12/2005CN1682021A Internally mounted radial flow intercooler for a combustion air charger
10/12/2005CN1682012A Gas turbine pressurizing air supply system
10/12/2005CN1680684A A containment apparatus for a gas turbine engine
10/12/2005CN1680611A Oxidation resistant superalloy and article
10/12/2005CN1680068A Deposition repair of hollow items
10/12/2005CN1680066A Welding process
10/11/2005USRE38815 Method and apparatus for the destruction of volatile organic compounds
10/11/2005US6953283 Foil bearing
10/11/2005US6952925 Optimizing inlet air for gas turbines
10/09/2005CA2502796A1 High efficiency rotor for the first phase of a gas turbine
10/09/2005CA2502793A1 High efficiency rotor for the second phase of a gas turbine
10/06/2005WO2005093327A1 Combustion chamber for a gas turbine and associated operating method
10/06/2005US20050222822 Sensor malfunction detection system for gas-turbine engine
10/06/2005US20050221946 Gas turbine gearbox
10/06/2005US20050220621 Composite integrally bladed rotor
10/06/2005US20050220611 Hybrid seal and system and method incorporating the same
10/06/2005US20050220610 Sealing device and method for turbomachinery
10/06/2005US20050220609 Ceramic-based bushing for a variable-pitch vane system in a turbomachine
10/06/2005US20050220384 Rotor recentering after decoupling
10/06/2005US20050218261 Air intake structure for aircraft engine
10/06/2005US20050217530 Gas generator and turbojet fitted with such a generator for starting
10/06/2005US20050217277 Cavity on-board injection for leakage flows
10/06/2005US20050217276 Method and apparatus for reducing gas turbine engine emissions
10/06/2005US20050217272 Deoiler for a lubrication system
10/06/2005US20050217270 Fuel injector head
10/06/2005US20050217269 Controlled pressure fuel nozzle injector
10/06/2005US20050217236 Centrifugal pump fuel system and method for gas turbine engine
10/06/2005US20050217110 Deposition repair of hollow items
10/06/2005US20050217096 Seal removal tool
10/06/2005DE102004016221A1 Cooling system for HP turbine of aviation jet engine has low pressure chamber for receiving of LP compressed air for additional cooling of guide vane segments and means for dilution-free cross-over of HP and LP compressed air flows
10/06/2005DE102004012944A1 Throttle element for fluid systems, esp. for a cooling system fitted into esp. exhaust housing of heat engine has axial fluid bore and parts for detachable fixing of a plug for the bore
10/06/2005CA2503800A1 Deposition repair of hollow items
10/05/2005EP1582703A2 Deoiler for a lubrication system
10/05/2005EP1582702A1 Air intake structure for an airplane engine
10/05/2005EP1582701A1 Air intake structure for an airplane engine
10/05/2005EP1582700A2 Seal assembly for a turbomachine
10/05/2005EP1582699A2 Hybrid seal for a gas turbine
10/05/2005EP1582697A1 Cavity on-board injection for leakage flows
10/05/2005EP1582289A1 Apparatus and method for repairing tenons on turbine buckets
10/05/2005EP1208293A4 A method and apparatus for vaporizing liquid gas in a combined cycle power plant
10/05/2005EP1144141B1 Multipiece core assembly
10/05/2005CN1678816A Recirculation structure for a turbocompressor
10/05/2005CN1676976A Hybrid seal assembly and system and method incorporating the same
10/05/2005CN1676902A Controlled pressure fuel nozzle system
10/05/2005CN1676884A Erosion and wear resistant protective structures for turbine engine components
10/04/2005US6951444 Turbine and a turbine vane for a turbine
10/04/2005US6951112 Methods and apparatus for assembling gas turbine engines
10/04/2005US6951110 Annular recuperator design
10/04/2005US6951108 Gas turbine engine combustor can with trapped vortex cavity
10/04/2005CA2314285C Piping support of gas turbine steam cooled combustor
10/04/2005CA2234831C Microcomponent chemical process sheet architecture
10/02/2005CA2502813A1 Improved fuel injector head
09/2005
09/29/2005WO2005091272A1 Assembly for reducing noise in turbofan engines
09/29/2005WO2005090156A1 Annular acoustic panel
09/29/2005WO2005089949A1 Air/oil separation system and method
09/29/2005US20050215390 Reduced twist carrier
09/29/2005US20050214124 Apparatus and methods for repairing tenons on turbine buckets
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