Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
06/2008
06/05/2008US20080131285 RMC-defined tip blowing slots for turbine blades
06/05/2008US20080131277 Ball bearing with carbon-carbon cage for gas turbine engines
06/05/2008US20080131265 Downstream plasma shielded film cooling
06/05/2008US20080131264 Methods and system for cooling integral turbine shroud assemblies
06/05/2008US20080131262 Methods and system for cooling integral turbine nozzle and shroud assemblies
06/05/2008US20080131260 Method and system to facilitate cooling turbine engines
06/05/2008US20080131259 Methods and system for recuperated cooling of integral turbine nozzle and shroud assemblies
06/05/2008US20080127671 Fan for Air Conditioner
06/05/2008US20080127627 Compact recirculating lubrication system for a miniature gas turbine engine
06/05/2008DE202008002380U1 Gehäuse eines Verdichter-/Turbinengehäuses eines Abgasturboladers Housing of a compressor / turbine housing of an exhaust turbocharger
06/04/2008EP1927732A2 Articles comprising composite structures having mounting flanges
06/04/2008EP1927728A2 Methods for reducing stress on composite structures
06/04/2008EP1927675A1 Ceramic corrosion resistant coating for oxidation resistance
06/04/2008EP1927408A2 Automated detection and control system and method for high pressure water wash application and collection applied to aero compressor washing
06/04/2008EP1926888A1 Turbocharger cleaning arrangement
06/04/2008EP1926564A1 Method of cleaning cavities on gas turbine components
06/04/2008CN201068808Y Drainage recoverer
06/04/2008CN101191426A Washing system and method for cleaning aviation compressor
05/2008
05/30/2008CA2612043A1 Upstream plasma shielded film cooling
05/30/2008CA2612042A1 Downstream plasma shielded film cooling
05/30/2008CA2603636A1 Methods and system for recuperated cooling of integral turbine nozzle and shroud assemblies
05/30/2008CA2603312A1 Method and system to facilitate cooling turbine engines
05/30/2008CA2603174A1 Methods and system for cooling integral turbine nozzle and shroud assemblies
05/30/2008CA2602311A1 Method and system to facilitate enhanced local cooling of turbine engines
05/30/2008CA2601686A1 Methods and system for cooling integral turbine shroud assemblies
05/30/2008CA2601612A1 Method and system to facilitate preferentially distributed recuperated film cooling of turbine shroud assembly
05/29/2008WO2008062678A1 Intake air heating control apparatus for gas turbine
05/29/2008WO2008062051A1 Non wetable surface coating of steam turbine parts which work in wet steam
05/29/2008WO2008061959A2 Thermoelastic joint connector
05/29/2008WO2008061944A1 Radial plain bearing
05/29/2008US20080124215 Gas turbine engine with concave pocket with knife edge seal
05/29/2008US20080122226 Compact assemblies for high efficiency performance of cryogenic liquefied gas expanders and pumps
05/29/2008DE102006055415A1 Bearing device for turbocharger of motor vehicle engine, has radial pin providing safety for bearing bush against rotation, where pin is engaged by hub in bearing bush and is designed as oil supply channel communicating with ring channel
05/28/2008EP1925835A1 Radial sliding bearing
05/28/2008EP1925833A1 Damper element of bearing, method of manufacturing damper element, bearing, and gas turbine engine
05/28/2008EP1925785A1 Water drainage apparatus for a turbine
05/28/2008EP1925782A1 Non wetable surface coating of steam turbine parts which work in wet steam
05/28/2008EP1924761A1 System and method for augmenting power output from a gas turbine engine
05/28/2008EP1924760A1 Arrangement and method in connection with a piston engine having a turbocompressor
05/28/2008EP1649145B1 Turbofan casing, turbofan engine and corresponding method
05/28/2008CN201065773Y Turbine jigger force-increasing device
05/28/2008CN100390387C Diffuser located between a compressor and a combustion chamber of a gasturbine
05/28/2008CA2611629A1 Turbine exhaust strut airfoil profile
05/27/2008US7377749 Device for balancing a rotating part, in particular a turbojet rotor
05/27/2008US7377745 Water pump
05/27/2008US7377742 Turbine shroud assembly and method for assembling a gas turbine engine
05/27/2008US7377417 Repair process
05/27/2008US7377305 Method and apparatus for production of a cast component
05/27/2008US7377115 Approach to extending life of gas turbine engine
05/27/2008US7377110 Deoiler for a lubrication system
05/27/2008CA2282010C Film-cooling hole and method of producing it
05/22/2008WO2008059620A1 Film cooling structure
05/22/2008WO2008058821A1 Diffuser and exhaust system for turbine
05/22/2008WO2008058368A1 Nacelle drag reduction device for a turbofan gas turbine engine
05/22/2008US20080118377 Exhaust Gas Turbo Charger
05/22/2008US20080118347 Turbine engine diffusing exhaust muffler
05/22/2008US20080118346 Air seal unit adapted to be positioned adjacent blade structure in a gas turbine
05/22/2008US20080115477 Localized arc filament plasma actuators for noise mitigation and mixing enhancement
05/22/2008CA2666190A1 Nacelle drag reduction device for a turbofan gas turbine engine
05/22/2008CA2610676A1 Turbine exhaust strut airfoil profile
05/21/2008EP1923544A2 Fuel system and ecology valve for use therein
05/21/2008EP1923543A1 Device for fixing a free turbine stator by double centring
05/21/2008EP1923542A2 Interdependant lubrication systems
05/21/2008EP1923541A2 Lubrication scavenge system
05/21/2008EP1923540A2 Oil Sump Housing
05/21/2008EP1922489A1 Turbocharger with bearing housing having an aerodynamically enhanced compressor wheel pocket geometry
05/21/2008DE102006054853A1 Insulating segment for e.g. exhaust gas turbo charger, of supercharged internal combustion engine, has protection unit for protecting insulating core in edge area, where unit has insulating protective band for surrounding core in edge area
05/21/2008CN101184911A System for providing continuous lubrication to engine turbocharger shaft and bearing arrangement
05/21/2008CN101182787A Steam turbine exhaust steam moisture on-line measurement device
05/21/2008CA2610117A1 Methods for fabricating composite structures having mounting flanges
05/21/2008CA2610097A1 Apparatus for use with structures having mounting flanges
05/21/2008CA2610096A1 Articles comprising composite structures having mounting flanges
05/21/2008CA2610094A1 Methods for reducing stress on composite structures
05/21/2008CA2610032A1 Methods for making structures having mounting flanges
05/20/2008US7374404 Methods and apparatus for gas turbine engines
05/20/2008US7374403 Low solidity turbofan
05/20/2008US7374402 Fastening arrangement for an impeller on a shaft
05/20/2008US7373781 Methods and apparatus for injecting cleaning fluids into combustors
05/20/2008US7373780 Method of scavenging oil within a gas turbine engine
05/20/2008US7373773 Gas turbine installation, cooling air supplying method and method of modifying a gas turbine installation
05/15/2008WO2008056790A1 Gas turbine power generation system and method of detecting its calorie abnormality
05/15/2008WO2008055999A1 Compressor
05/15/2008WO2008055717A1 Housing connection of an exhaust gas turbocharger
05/15/2008WO2008055471A2 Vane for a compressor or a turbine of an aircraft engine, aircraft engine comprising such a vane, and method for coating a vane of an aircraft engine
05/15/2008DE102006052990A1 Assembly has turbo machine, cooler and support frame, where cooler has horizontal cooling element and frame segments are arranged at distance from each other in longitudinal direction of horizontal cooling element
05/15/2008CA2668298A1 Vane for a compressor or a turbine of an aircraft engine, aircraft engine comprising such a vane and a method for coating a vane of an aircraft engine
05/15/2008CA2609290A1 Transpiration clearance control turbine
05/14/2008EP1921383A2 Combustor dome and methods of assembling such
05/14/2008EP1921292A2 Compound tubine cooled engine
05/14/2008EP1921279A2 Method for utilising waste heat when operating a turbine with a gaseous medium
05/14/2008EP1921278A1 Diffuser and exhaust system for turbine
05/14/2008EP1921277A2 Mechanical support of a ceramic gas turbine vane ring
05/14/2008EP1921276A2 Radially energised oil capture device for a geared turbofan
05/14/2008EP1921275A2 Cooling arrangement for aircraft electronics
05/14/2008EP1921271A2 Titanium foil as a structural heater element
05/14/2008EP1921270A2 Compound nozzle cooled engine
05/14/2008EP1921007A2 A turbine engine mounting arrangement
05/14/2008EP1756406B1 Gas turbine compression system and compressor structure
05/14/2008EP1550792B1 Elastically coupled barring apparatus
05/14/2008CN101180215A Mobile on-wing engine washing and water reclamation system