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)
03/2005
03/23/2005EP1516690A1 Method of manufacturing or repairing a bladed rotor disc
03/23/2005EP1516110A1 Flow divider and ecology valve
03/23/2005EP1183444B1 Turbomachine and sealing element for a rotor thereof
03/23/2005CN1598272A Gas turbine brush seal arrangement for cabin air supply
03/23/2005CN1598271A Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions
03/23/2005CN1194165C Efficient electric power generation method
03/22/2005US6869703 Thermal barrier coatings with improved impact and erosion resistance
03/22/2005US6868893 Method and apparatus for directionally solidified casting
03/22/2005US6868664 Main propulsion engine system integrated with secondary power unit
03/17/2005WO2005024206A1 Power plant and method for operating said plant
03/17/2005US20050058541 Casing, a compressor, a turbine, and a combustion turbine engine including such a casing
03/17/2005US20050058537 Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion
03/17/2005US20050058535 Formed disk plate heat exchanger
03/17/2005US20050058534 Network cooled coated wall
03/17/2005US20050058533 Sealing arrangement in a compressor
03/17/2005US20050056724 Stress releiving; computer for data storage; input temperature profile; measuring starup temperature; calibration; injecting water, alcohol in response to signal
03/17/2005US20050056029 Evaporative duplex counterheat exchanger
03/17/2005US20050056025 Provision of sealing for the cabin-air bleed cavity using a segment seal
03/17/2005US20050056023 Method of chilling inlet air for gas turbines
03/17/2005US20050056022 Method and apparatus to decrease combustor acoustics
03/17/2005US20050056021 Multi-spool turbogenerator system and control method
03/17/2005US20050056019 Integral compressor housing of gas turbine engines
03/17/2005US20050056000 Combustor drain valve
03/17/2005DE10337372A1 Vorrichtung zur Stabilisierung der Triebwerks-Einlaufströmung bei Triebwerks-Standläufen Device to stabilize the engine inlet flow in engine static tests
03/17/2005CA2480983A1 Network cooled coated wall
03/16/2005EP1515090A1 Thick coated combustor liner
03/16/2005EP1515004A1 Piston ring type seal for the compressor of a gas turbine
03/16/2005EP1514018A1 A turbine and a component
03/16/2005EP1144808B1 Method of cooling a combustion turbine
03/16/2005CN1594845A Provision of sealing for the cabin-air bleed cavity using a segment seal
03/15/2005US6865891 Gas turbine engine
03/15/2005US6865877 Compression feed for high humidity fuel gas
03/15/2005CA2341844C Gas turbine combustor
03/11/2005CA2479275A1 Helicopter turbine engine protection system
03/10/2005WO2005021976A1 Control device for compressor
03/10/2005WO2005021950A2 Atomization and injection system, and method for operating the same
03/10/2005US20050053876 Method for igniting the combustion chamber of a gas turbine unit and an ignition device for carrying out the method
03/10/2005US20050053799 Thermal barrier coating utilizing a dispersion strengthened metallic bond coat
03/10/2005US20050053466 Reinforced fan blade and method of making
03/10/2005US20050053464 Methods and apparatus for cooling gas turbine engine rotor assemblies
03/10/2005US20050053459 Microcircuit cooling for a turbine airfoil
03/10/2005US20050050901 Part load blade tip clearance control
03/10/2005US20050050899 Turbine engine sequenced combustion
03/10/2005US20050050898 Gas turbine installation, cooling air supplying method and method of modifying a gas turbine installation
03/10/2005US20050050896 Thick coated combustor liner
03/10/2005US20050050877 Methods and apparatus for operating gas turbine engines
03/10/2005CA2480136A1 Axial compressor
03/09/2005EP1512855A1 Power plant and method for operation
03/09/2005EP1512844A2 Gas turbine installation, cooling air supplying method and method of modifying a gas turbine installation
03/09/2005EP1512843A2 Methods and apparatus for cooling gas turbine engine rotor assemblies
03/09/2005EP1512841A2 Methods and apparatus to reduce seal rubbing within gas turbine engines
03/09/2005EP1512840A2 Methods and apparatus to facilitate sealing between rotating turbine shafts
03/09/2005EP1512835A2 Rotor blade and gas turbine engine comprising a corresponding rotor assembly
03/09/2005EP1511883A1 Heat insulating layer
03/09/2005EP1511700A1 Heat resistant product
03/09/2005CN1590815A Sealer
03/09/2005CN1590735A Methods and apparatus to facilitate sealing between rotating turbine shafts
03/09/2005CN1590734A Gas turbine combustor
03/09/2005CN1590733A Methods and apparatus for cooling gas turbine engine rotor assemblies
03/09/2005CN1590712A Abradable device on fan case for gas turbine engine
03/09/2005CN1590710A Methods and apparatus for cooling gas turbine engine rotor assemblies
03/09/2005CN1590709A Turbine airfoil cooling flow particle separator
03/08/2005US6863937 Method of operating an electron beam physical vapor deposition apparatus
03/08/2005US6863927 Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure
03/08/2005US6862877 Gas turbines
03/03/2005WO2005019622A1 Cogeneration system
03/03/2005US20050047912 Fluid-cooled mechanical face seal rotor
03/03/2005US20050047911 Methods and apparatus to facilitate sealing between rotating turbine shafts
03/03/2005US20050047910 Methods and apparatus to reduce seal rubbing within gas turbine engines
03/03/2005US20050047906 Methods and apparatus for cooling gas turbine engine rotor assemblies
03/03/2005US20050047902 Turbine airfoil cooling flow particle separator
03/03/2005US20050046398 Control apparatus for a starter/generator system
03/03/2005US20050045767 Locking the cowl doors of a turbojet
03/03/2005US20050044708 Method for manufacturing a hollow blade for a stator or rotor component
03/03/2005US20050044685 Tooling provision for split cases
03/03/2005DE10392247T5 Brennkammer für Gasturbine Combustion chamber for gas turbine
03/03/2005DE102004028314A1 Fluidmaschine zum Umwandeln von Wärmeenergie in Drehkraft Fluid machine for converting heat energy into rotational force
03/02/2005EP1510795A2 Device for estimating fuel mass flow rate
03/02/2005EP1510757A2 Gas turbine combustor
03/02/2005EP1510691A2 Control apparatus for a starter/generator system
03/02/2005EP1510676A1 Gas turbine plant
03/02/2005EP1510659A2 Turbine airfoil cooling flow particle separator
03/02/2005EP1510657A1 Device adradable for the fan casing of a gas turbine
03/02/2005EP1510296A1 Apparatus and method for separating flanges
03/02/2005EP1509702A1 Method for operating a compressor
03/02/2005EP1509631A2 Thermal spray compositions for abradable seals
03/02/2005EP1169585B1 Self-centering brush seal
03/02/2005CN1589367A Drying machine system utilizing gas turbine, and method of use
03/02/2005CN1589361A Gas turbo group
03/02/2005CN1587666A Once surface heat regenerator
03/02/2005CN1191431C 涡轮燃油泵 Turbo fuel pump
03/02/2005CN1191427C Silencer for compressor of exhaust gas turbocharger
03/02/2005CN1191426C Turbomachine
03/02/2005CN1191425C Gas turbine engine power plant and its working method
03/01/2005US6860726 Dual drive for hydraulic pump and air boost compressor
03/01/2005US6860110 Gas turbine shaft and heat shield cooling arrangement
03/01/2005US6860109 Turbine equipment
03/01/2005US6860108 Gas turbine tail tube seal and gas turbine using the same
03/01/2005US6860098 Gas turbine combustor having bypass and annular gas passage for reducing uneven temperature distribution in combustor tail cross section
02/2005
02/28/2005CA2476471A1 Tooling provision for split cases
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