Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
03/2005
03/23/2005CN1598271A Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions
03/23/2005CN1598249A Composite condensing equipment of turbine
03/17/2005WO2005024206A1 Power plant and method for operating said plant
03/17/2005WO2005024095A1 Aqueous compositions and method for cleaning gas turbine compressor blades
03/17/2005WO2005023405A1 Aerodynamic noise abatement device and method for air-cooled condensing systems
03/17/2005US20050060120 Method for measuring piping forces acting on a turbine casing
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
03/17/2005US20050058534 Network cooled coated wall
03/17/2005US20050057003 Seal device
03/17/2005US20050056726 Closure panel arrangement
03/17/2005US20050056015 Exhaust-gas turbocharger for an internal combustion engine
03/17/2005DE10353620B3 Sensor monitoring method for rotating machine e.g. for axial turbocompressor for jet propulsion drive or gas turbine, using ultrasonic pulses for detecting rotor parameters and air temperature between stator and rotor
03/17/2005DE10337491A1 Exhaust gas turbocharger for IC engines esp. for motor vehicles has flow channel component fastened by bolts, with one bolt passing through turbine guide blade to form pivot axis
03/17/2005CA2480983A1 Network cooled coated wall
03/16/2005EP1515006A1 A closure panel arrangement
03/16/2005EP1515002A1 Anti-rotation means for turbine stator vanes in the split plane of the casing
03/16/2005EP1514018A1 A turbine and a component
03/16/2005EP1514017A2 Miniature gas turbine engine with unitary rotor shaft for power generation
03/16/2005EP1144808B1 Method of cooling a combustion turbine
03/16/2005CN1193184C Secured coupling assembling and method of preventing loosening
03/15/2005US6868366 Method for measuring piping forces acting on a turbine casing
03/15/2005US6866479 Exhaust diffuser for axial-flow turbine
03/15/2005US6866478 Miniature gas turbine engine with unitary rotor shaft for power generation
03/10/2005WO2005021936A2 Energy recovery system
03/10/2005WO2005021806A1 High temperature bolt material
03/10/2005US20050053466 Reinforced fan blade and method of making
03/10/2005US20050053464 Methods and apparatus for cooling gas turbine engine rotor assemblies
03/10/2005US20050053463 Exhaust-gas-turbine casing
03/10/2005US20050053462 Sealing of nozzles in a steam turbine
03/10/2005US20050053457 Turbine blade ring assembly and clocking method
03/10/2005US20050050898 Gas turbine installation, cooling air supplying method and method of modifying a gas turbine installation
03/10/2005CA2536962A1 Energy recovery system
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
03/09/2005CN1590735A Methods and apparatus to facilitate sealing between rotating turbine shafts
03/09/2005CN1590733A Methods and apparatus for cooling gas turbine engine rotor assemblies
03/09/2005CN1590709A Turbine airfoil cooling flow particle separator
03/08/2005US6863497 Stator vane span attachment for a gas turbine
03/03/2005WO2005019732A2 Diffuser for a gas turbine and gas turbine for energy generation
03/03/2005WO2005019621A1 Diffuser arranged between the compressor and the combustion chamber of a gas turbine
03/03/2005WO2005019604A1 Flow guide device contained in the diffuser of turbomachinery and flow diversion method
03/03/2005WO2005019603A1 Method for braking a rotor of a turbine engine and a turning gear for driving the rotor of a turbine engine
03/03/2005US20050049168 Aqueous compositions for cleaning gas turbine compressor blades
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
03/03/2005US20050047907 Transition duct cooling system
03/03/2005US20050047902 Turbine airfoil cooling flow particle separator
03/03/2005US20050047694 Rolling bearing
03/03/2005US20050047690 Bearing assembly with fluid circuit for delivery of lubricating fluid between bearing surfaces
03/03/2005US20050045767 Locking the cowl doors of a turbojet
03/03/2005US20050045416 Aerodynamic noise abatement device and method for air-cooled condensing systems
03/03/2005US20050045306 Transpiration cooling system
03/03/2005US20050044685 Tooling provision for split cases
03/02/2005EP1510659A2 Turbine airfoil cooling flow particle separator
03/02/2005EP1510658A2 Emergency lubrication system
03/02/2005EP1510296A1 Apparatus and method for separating flanges
03/02/2005EP1509683A1 Gas turbine engine with active tip clearance control
03/02/2005EP1509447A2 Bifurcated turbofan nozzle
03/02/2005EP1169585B1 Self-centering brush seal
03/02/2005CN1589361A Gas turbo group
03/02/2005CN1587651A High and low pressure by-path system
03/01/2005US6860719 Method and apparatus for sealing turbine casing
03/01/2005US6860716 Turbomachine frame structure
03/01/2005US6860110 Gas turbine shaft and heat shield cooling arrangement
02/2005
02/28/2005CA2476471A1 Tooling provision for split cases
02/28/2005CA2476470A1 Turbine airfoil cooling flow particle separator
02/24/2005WO2005017375A2 Fluidics-balanced fluid bearing
02/24/2005WO2005017333A2 Wide-angle concentric diffuser
02/24/2005WO2005016500A1 Noise level reduction of sparger assemblies
02/24/2005US20050043870 Method and apparatus for recording and retrieving maintenance, operating and repair data for turbine engine components
02/24/2005US20050042090 Methods and apparatus for fabricating gas turbine engines
02/24/2005US20050042087 Method and apparatus for reducing total pressure loss in a turbine engine
02/24/2005US20050042085 Arrangement for mounting a non-rotating component
02/24/2005US20050042081 Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle
02/24/2005US20050040579 Method and apparatus to decrease combustor emissions
02/24/2005US20050039459 High temperature splash plate for temperature reduction by optical reflection and process for manufacturing
02/24/2005US20050039435 Ice protection system for an aircraft engine
02/24/2005US20050039333 Method for manufacturing steam turbines
02/24/2005DE10334448A1 Wind power unit has a rotor to drive a generator and an additional drive to turn the drive element to a given angle
02/24/2005DE10311996B4 Anordnung eines Abgasturboladers mit einem Trägergehäuse Arrangement of an exhaust gas turbocharger with a carrier housing
02/23/2005EP1508881A1 Method and apparatus for recording and retrieving maintenance, operating and repair data for turbine engine components
02/23/2005EP1508747A1 Gas turbine diffusor and gas turbine for the production of energy
02/23/2005EP1508680A1 Diffuser located between a compressor and a combustion chamber of a gasturbine
02/23/2005EP1508673A2 Methods for fabricating gas turbine engines
02/23/2005EP1507959A1 Arrangement for axially and radially fixing the guide vanes of a vane ring of a gas turbine
02/23/2005EP1507882A2 Method for removing at least one partial area of a component made of metal or a metallic compound
02/23/2005CN2680862Y Steam discharge cooling apparatus for assisting miniature steam turbine
02/23/2005CN1585852A Air cooling system for electric assisted turbocharger
02/23/2005CN1584298A Seal device
02/23/2005CN1584118A Upgrading of aluminide coating on used turbine engine component
02/23/2005CN1584104A Turbine element repair
02/23/2005CN1584103A Turbine element repair
02/22/2005US6857849 Membrane seals
02/22/2005US6857847 Simplified support device for nozzles of a gas turbine stage
02/22/2005US6857669 Device for connecting two tubular pieces of an aircraft turbine engine
02/22/2005US6857330 Apparatus and methods for automatically inspecting dovetails on turbine rotors