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)
11/2002
11/20/2002EP1258618A2 System and method for monitoring engine performance in a gas turbine engine
11/20/2002EP1258617A2 Methods and apparatus for detecting turbine engine flameout
11/20/2002EP1258599A2 Assembly method and apparatus for maintaining rotor assembly tip clearances
11/20/2002EP1258545A1 Method for isothermal brazing of single crystal components
11/20/2002EP1258312A2 Repair of a single crystal nickel based superalloy article
11/20/2002EP1257680A1 Iron base high temperature alloy
11/20/2002EP1257373A1 Device and method for casting a workpiece and workpiece
11/20/2002EP1257349A1 A heat exchanger for cooling and for a pre-cooler for turbine intake air conditioning
11/20/2002EP1107867A4 Removal of thermal barrier coatings
11/20/2002CN1380487A 燃气轮机 Gas turbine
11/20/2002CN1380486A Method for manufacturing turbine blade and turbine blade
11/20/2002CN1094559C Method for total-power operating of gas turbine generating station using supplemental compressed air when high external temp. or low air density
11/19/2002US6481969 Apparatus and methods for balancing turbine rotors
11/19/2002US6481967 Gas turbine moving blade
11/19/2002US6481212 Combustion turbine cooling media supply system and related method
11/19/2002CA2269889C Jet engine booster structure
11/14/2002WO2002090741A1 Method for cooling a gas turbine and gas turbine installation
11/14/2002WO2002090723A1 Arrangement for mounting two coaxial shaftlines
11/14/2002WO2002090721A1 Power generation apparatus
11/14/2002WO2002090039A1 Method of repairing a turbin blade tip
11/14/2002US20020168537 Article having turbulation and method of providing turbulation on an article
11/14/2002US20020168263 Seal element for sealing a gap and combustion turbine having a seal element
11/14/2002US20020166586 Fluid metering device
11/14/2002US20020166324 Integrated turbine power generation system having low pressure supplemental catalytic reactor
11/14/2002US20020166317 Methods and systems for preventing gas turbine engine lube oil leakage
11/14/2002US20020166231 Method for applying diffusion aluminide coating on a selective area of a turbine engine component
11/14/2002DE10122305A1 Engine for an airplane has a lattice, net or perforated sheet arranged in front of the intake region
11/13/2002EP1256635A1 Method for applying diffusion aluminide coating on a selective area of a turbine engine component
11/13/2002EP1255921A1 Modular gas turbine power plant
11/13/2002EP1214172A4 Laser cladding a turbine engine vane platform
11/13/2002CN1379170A Combustion turbine
11/13/2002CN1379167A Moulded article formed into flow guiding ring
11/13/2002CN1379166A Sealing element for sealing gap and combustion turbine possessing said sealing element
11/13/2002CN1378890A Method for making turbine vanes
11/12/2002US6479097 Sound lining for ducts
11/12/2002US6478553 High thrust turbocharger rotor with ball bearings
11/12/2002US6478537 Pre-segmented squealer tip for turbine blades
11/12/2002US6478304 Sealing ring for non-hermetic fluid seals
11/12/2002US6478289 Apparatus and methods for controlling the supply of water mist to a gas-turbine compressor
11/12/2002US6477852 Heat and electric power supply system and operation method thereof
11/12/2002US6477773 Methods for disassembling, replacing and assembling parts of a steam cooling system for a gas turbine
11/08/2002CA2383468A1 Method for applying diffusion aluminide coating on a selective area of a turbine engine component
11/07/2002WO2002089536A1 Method for plasma-catalytic conversion of fuels that can be used in an internal combustion engine or a gas turbine into a synthetic gas and the plasma-catalytic converter used for same
11/07/2002WO2002088602A1 Turbine premixing combustor
11/07/2002WO2002088601A1 Combustion chamber, in particular of a gas turbine
11/07/2002WO2002088531A1 Method of operating a gas turbine
11/07/2002WO2002068867A3 Control strategy for flexible catalytic combustion system
11/07/2002US20020164246 Gas turbine with axially mutually displaceable guide parts
11/07/2002US20020162914 Aircraft system architecture
11/07/2002US20020162220 Method of repairing a turbine blade tip
11/07/2002CA2445492A1 Method for plasma catalytic conversion of fuels usable in an internal combustion engine or gas turbine into a synthetic gas and the plasma catalytic converter therefor
11/06/2002EP1255032A1 Air intake and flying vehicle, in particular a missile, with such air intake
11/06/2002EP1255024A2 Methods and systems for preventing gas turbine engine lube oil leakage
11/06/2002EP1255023A1 Mounting assembly of two coaxial shafts
11/06/2002EP1254967A1 Improved plasma sprayed thermal bond coat system
11/06/2002EP1254738A2 Automated system for repairing components
11/06/2002EP1253986A1 Method and arrangement for producing casting moulds from metal
11/06/2002EP1123422B1 Electron beam physical vapor deposition apparatus and method
11/06/2002CN1378039A 燃气轮机 Gas turbine
11/06/2002CN1378036A Turbomachine
11/06/2002CN1378035A Turbine blade and method for producing turbine blade
11/06/2002CN1093912C Treating device for liquid and gaseous fuels
11/05/2002US6475642 Oxidation-resistant coatings, and related articles and processes
11/05/2002US6475289 Cleaning of internal passages of airfoils
11/05/2002US6474941 Variable stator vane bushing
11/05/2002US6474315 Electron stimulation via photon emitting radiation
11/05/2002CA2229915C Gas turbine stationary blade
11/01/2002WO2002090742A1 Gas turbine power generation facility
10/2002
10/31/2002WO2002086299A1 Air turbine starter with seal assembly
10/31/2002WO2002086294A1 Mobile installation for silencing and cleaning exhaust gases of an internal combustion engine
10/31/2002WO2002086292A1 Turbine or compressor device and method for assembling the device
10/31/2002WO2002086291A1 Blade for a turbine comprising a cooling air deflector
10/31/2002WO2002078010A8 A nuclear power plant and method of operating the same
10/31/2002WO2002048525A3 System to feed cooling air into a gas turbine rotor
10/31/2002WO2001051787A9 Piloted airblast lean direct fuel injector
10/31/2002US20020161483 Automated system for repairing components
10/31/2002US20020159888 Methods and systems for cooling gas turbine engine airfoils
10/31/2002US20020159886 Axial-flow turbine having stepped portion formed in axial-flow turbine passage
10/31/2002US20020158165 Air intake and flying device, particularly a missile, equipped with such an air intake
10/31/2002US20020157738 A high-temperature component made of a nickel super-alloy consists of in wt %: 11-13% of Chromium, 3-5% of tungsten, 0.5- 2.5% of molybdenum, 3-5% aluminum, 3-5% of titanium , 3-7% of tantalum, 1-5% Re, reminder Nickel
10/31/2002US20020157401 Diffuser combustor
10/31/2002US20020157251 Method of producing a turbine blade
10/31/2002DE10117231A1 Rotorspalt-Steuermodul Rotor gap control module
10/30/2002EP1253379A2 Methods and apparatus for cooling gas turbine engine combustors
10/30/2002EP1253378A2 Gas turbine combustor having bypass passage
10/30/2002EP1253307A2 Turbocharger rotor with ball bearings
10/30/2002EP1253295A2 Axial-flow turbine having a stepped portion in a flow passage
10/30/2002EP1253292A2 Methods and systems for cooling gas turbine engine airfoils
10/30/2002EP1253289A2 Integrally bladed rotor airfoil fabrication and repair techniques
10/30/2002EP1252370A1 Chemical cleaning solution for gas turbine blades
10/30/2002CN1376855A Charged air cooler of gas turbine
10/30/2002CN1093594C Fuel supply device for gas-turbine and controller thereof
10/29/2002US6473705 System and method for direct non-intrusive measurement of corrected airflow
10/29/2002US6471478 Axial seal system for a gas turbine steam-cooled rotor
10/29/2002US6471469 Methods and apparatus for sealing gas turbine engine variable nozzles
10/29/2002US6470688 Apparatus for the rapid startup and rapid increase in output of a gas turbine plant
10/29/2002US6470686 System for chilling inlet air for gas turbines
10/29/2002US6470668 Methods and apparatus for water injection in a turbine engine
10/29/2002US6470667 Methods and apparatus for water injection in a turbine engine
10/29/2002US6470666 Methods and systems for preventing gas turbine engine lube oil leakage
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