Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
04/2008
04/02/2008EP1905948A1 Power recovery machine
04/02/2008EP1904718A1 Combined steam turbine, steam- or gas- and steam-turbine power plant, method of operating a combined steam turbine
04/02/2008EP1904717A2 Hot gas-conducting housing element, protective shaft jacket, and gas turbine system
04/02/2008CN201043478Y Special thermal insulation layer structure of turbine
04/02/2008CN201043477Y Heater for turbine fuel tank
04/02/2008CN101155973A Component of a steam turbine installation, steam turbine installation, use thereof and method for producing the same
04/02/2008CN100378296C High-pressure inner cylinder cooling method for steam turbine
04/02/2008CA2603503A1 Annular gas turbine engine case and method of manufacturing
04/02/2008CA2602994A1 Annular gas turbine engine case and method of manufacturing
04/02/2008CA2602981A1 Annular gas turbine engine case and method of manufacturing
04/02/2008CA2601659A1 Annular gas turbine engine case and method of manufacturing
04/01/2008US7351030 Connection device for making a connection between a turbomachine nozzle and a feed enclosure for feeding cooling fluid to injectors
03/2008
03/28/2008CA2604455A1 Self-contained electrostatic air/oil separator for aircraft engine
03/28/2008CA2604453A1 Oil scavenge system for gas turbine engine bearing cavity
03/28/2008CA2600171A1 Labyrinth seal repair
03/27/2008WO2008034215A1 Electrostatic air/oil separator for aircraft engine
03/27/2008US20080075879 metal substrate, metal bonding layer, ceramics thermal barrier; columnar structure of stabilized zirconia, or ZrO2-HfO2 solid solution; simultaneously melting two ZrO2 deposition and Lanthanum oxide deposition materials by electron beam physical vapor deposition; low thermal conductivity; durability
03/27/2008US20080075589 Assembling member
03/27/2008US20080075587 Ice strike sheathing ring for the fan casing of an aircraft gas turbine
03/27/2008US20080075584 Set of insulating sheets on a casing to improve blade tip clearance
03/27/2008US20080075581 Fan cover
03/27/2008DE19821889B4 Verfahren und Vorrichtung zur Durchführung von Reparatur- und/oder Wartungsarbeiten im Innengehäuse einer mehrschaligen Turbomaschine Method and apparatus for performing repair and / or maintenance in the inner casing of a multi-layered turbomachine
03/27/2008DE102007045138A1 Laufschaufel-Rückhaltesystem für ein Gasturbinentriebwerk A blade retention system for a gas turbine engine
03/27/2008CA2604367A1 Bleed holes oriented with gaspath and flared for noise reduction
03/27/2008CA2604365A1 Oil feed assembly
03/26/2008EP1903188A2 System and method for augmenting turbine power output
03/26/2008EP1903185A2 Thermal and external load isolating impeller shroud
03/26/2008EP1902952A1 Fan conduit for a turbomachine
03/26/2008EP1753938B1 A support structure in a turbine or compressor device and a method for assembling the structure
03/26/2008CN101148997A System and method for aligning and sealing a turbine shell assembly
03/26/2008CN100376862C Method for measuring piping forces acting on a turbine casing
03/25/2008US7347672 Rotor disk balancing device, disk fitted with such a device and rotor with such a disk
03/25/2008US7347664 High-temperature component for a turbomachine, and a turbomachine
03/25/2008US7347661 Casing arrangement
03/25/2008CA2604106A1 Tower shaft (uts) shielding
03/25/2008CA2602319A1 Blade containment system for a gas turbine engine
03/22/2008CA2603595A1 Heat shield with stress relieving feature
03/22/2008CA2602940A1 Insulating plate device on crankcase to improve backlash at the top of the blade
03/20/2008WO2008032430A1 Motor-integrated magnetic bearing device
03/20/2008WO2008031195A1 Access housing for gas turbine engine
03/20/2008US20080069690 Thermal and external load isolating impeller shroud
03/20/2008US20080069688 Gas turbine engine casing
03/20/2008US20080069293 Liquid Flow Sensor Fox X-Ray Tubes
03/20/2008CA2663247A1 Power recovery machine
03/19/2008EP1900910A2 Thrust bearing housing for a gas turbine engine
03/19/2008EP1900906A2 Method and apparatus for robotically inspecting gas turbine combustor components
03/19/2008EP1899583A1 Lubrication system
03/19/2008EP1784557B1 Fluid injection in a gas turbine during a cooling down period
03/19/2008CN101146652A Jig
03/19/2008CN101144510A Automatic synchronizing clutch and water supply pump steam turbine high speed jigger device with the same
03/18/2008US7343676 Method of restoring dimensions of an airfoil and preform for performing same
03/18/2008CA2353694C System for the precision machining of rotationally symmetrical components
03/18/2008CA2351281C Link component for aircraft engine mounting systems
03/18/2008CA2292821C Acoustically adjusted multi-channel turbine engine exhaust device
03/13/2008WO2008029211A1 Electric supercharger
03/13/2008WO2008028792A1 Turbine engine and method of operating the same
03/13/2008WO2008028702A1 Cooled turbine rotor blade
03/13/2008WO2008028274A1 Thrust bearing housing for a gas turbine engine
03/13/2008WO2008012294A3 A gas turbine arrangement
03/13/2008US20080063514 Seal system for an interturbine duct within a gas turbine engine
03/13/2008US20080063513 Turbine blade tip gap reduction system for a turbine engine
03/12/2008EP1898055A2 Variable geometry guide vane for a gas turbine engine
03/12/2008EP1898048A1 Rotor for steam turbine and process for producing the same
03/12/2008EP1897806A2 System for washing an aero gas turbine engine
03/12/2008EP1896696A1 Turbocharger bearing and associated components
03/12/2008EP1896695A1 Secondary air charger
03/12/2008EP1815210A4 Illumination system for measurement system
03/12/2008CN201034029Y Novel low-pressure saturated steam engine
03/12/2008CN100374706C Process for replacing an abradable on the fan case of a turbojet
03/12/2008CN100374687C Apparatus, method and software for use with an air conditioning cycle
03/12/2008CA2599786A1 Combustor with enhanced cooling access
03/11/2008US7341428 Turbine blade for monitoring torsional blade vibration
03/11/2008US7341380 Installation layout for two coaxial shaft lines
03/11/2008US7340882 Turbomachine with means for axial retention of the rotor
03/11/2008US7340881 Gas turbine combustor
03/11/2008CA2600818A1 Exhaust duct and tail cone attachment of aircraft engines
03/11/2008CA2312949C Support for a turbine stator assembly
03/08/2008CA2600823A1 Integral tandem bearing for high speed flexible shafts
03/08/2008CA2600170A1 Fan case abradable
03/07/2008CA2599799A1 Fan case abradable drainage trench and slot
03/06/2008WO2008025136A1 Turbofan bypass duct air cooled fluid cooler installation
03/06/2008WO2008006960A3 Turbine engine for aircraft
03/06/2008US20080057254 Turbine element repair
03/06/2008US20080056888 Guide vane for a gas turbine engine
03/06/2008US20080053107 Slidable spring-loaded transition-to-turbine seal apparatus and heat-shielding system, comprising the seal, at transition/turbine junction of a gas turbine engine
03/06/2008DE102006041321A1 Housing section, particularly fan housings, for gas-turbine engine, has endangered section seperated by shovel or rotor parts in which flexible protective cover arranged is arranged at periphery of matrixes
03/05/2008EP1895141A2 Splitter for a turbo-fan engine
03/05/2008EP1895124A2 Oil cooling apparatus in fan cowling and method therefor
03/05/2008EP1895122A1 Modular turbine engine
03/05/2008EP1895109A2 Guide vane for a gas turbine engine
03/05/2008EP1895107A1 Exhaust gas turbine with segmented shroud ring
03/05/2008EP1895096A1 Cooled turbine rotor blade
03/05/2008EP1895095A1 Turbine engine and method of operating the same
03/05/2008CN101135251A Systems for moisture removal in steam turbine engines
03/05/2008CN101135250A Heat pipe-based cooling apparatus and method for turbine engine
03/05/2008CA2599095A1 Turbine exhaust strut airfoil and gas path profile
03/04/2008US7340319 Method and system for maintaining an aircraft engine
03/04/2008US7338259 High modulus metallic component for high vibratory operation
03/04/2008US7338254 Turbocharger with sliding piston assembly
03/04/2008US7337605 Thermal management for aircraft auxiliary power unit compartment