Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
06/2012
06/14/2012DE112010002048T5 Turbolader Turbocharger
06/14/2012DE112010001913T5 Federclipverfahren zur Verdrehsicherung und Schittbegrenzung einer Wälzelementlagerpatrone Spring clip method for preventing rotation and Schittbegrenzung a Wälzelementlagerpatrone
06/14/2012DE102011056181A1 Komponenten mit Kühlkanälen und Herstellungsverfahren Components with cooling channels and methods of manufacture
06/14/2012DE102010063071A1 Kühlvorrichtung für ein Strahltriebwerk A cooling apparatus for a jet engine
06/14/2012DE102010062968A1 Radial compressor for exhaust gas turbocharger for fuel cell system of combustion engine in motor car, has axial spacer attached to intake guide such that spacer measures distance between intake guide and bearing housing
06/14/2012CA2820150A1 Method of forming a composite structure comprising a flange
06/13/2012EP2463484A1 Tubular casing for a turbo engine
06/13/2012EP2462258A1 Electrolysis cell and electrical power unit incorporating same
06/13/2012EP1997922B1 High-temperature shape memory alloy, actuator and motor
06/13/2012CN202273714U 滚动轴承涡轮增压器 Rolling turbocharger
06/13/2012CN102498343A Apparatus and method for close coupling of heat recovery steam generators with gas turbines
06/13/2012CN102498266A Device for supporting a turbine ring, turbine having such a device, and turbine engine having such a turbine
06/13/2012CN102493865A Drainage turbine pressurization system
06/13/2012CN101514641B Protection system for turbo machine and power generating equipment
06/13/2012CN101429878B Turbocharger
06/13/2012CN101126330B Exhaust gas turbine supercharger for internal combustion engine
06/12/2012US8197197 Method of matching thermal response rates between a stator and a rotor and fluidic thermal switch for use therewith
06/12/2012US8197191 Inlet section of an aircraft engine nacelle
06/12/2012US8197190 Lever for rotating a turbomachine variable-pitch stator vane about its pivot
06/12/2012US8197187 Inspection hole plug with a ball swivel
06/12/2012US8197186 Flange with axially extending holes for gas turbine engine clearance control
06/12/2012US8197183 Spherical thrust bearing system for turbochargers
06/12/2012US8197180 Water flow energy extraction device
06/12/2012US8196934 Slider seal assembly for gas turbine engine
06/07/2012WO2012073542A1 Electric power generation plant
06/07/2012WO2012072069A1 Damping means for damping a blade movement of a turbomachine
06/07/2012US20120141294 Gas turbine rotor containment
06/07/2012US20120141277 Integrated Lightning Receptor System and Trailing Edge Noise Reducer for a Wind Turbine Rotor Blade
06/07/2012US20120141266 Pressure controlled wind turbine enhancement system
06/07/2012US20120141259 Blade segment and fluid flow machine
06/07/2012US20120141258 Air turbine starter
06/07/2012US20120141256 Annular gas turbine housing component and a gas turbine comprising the component
06/07/2012US20120141253 Turbomachine
06/07/2012US20120141248 Active fan flutter control
06/07/2012US20120137650 Fluid impingement arrangement
06/06/2012EP2461053A1 Hydrodynamic axial bearing
06/06/2012EP2460982A1 Turbine controls testing device
06/06/2012DE102010053497A1 Exhaust-gas turbocharger for internal combustion engine of motor vehicle, has rotor comprising shaft that is provided with ventilation channels with outlet opening for guiding air from retaining area into close area of sealing ring
06/06/2012CN202266328U Pulse supercharging turbine device with variable flow passage
06/06/2012CN202266306U Volute casing device of variable geometric pulse air inlet turbine
06/06/2012CN202266305U 一种可调式多喷嘴蒸汽压力匹配器 An adjustable multi-nozzle steam pressure match
06/06/2012CN202266304U 一种多喷嘴蒸汽压力匹配器 A multi-nozzle steam pressure match
06/06/2012CN102486098A Linear bearing seat device
06/05/2012US8192163 Wiper for wind turbine blades
06/05/2012US8192152 Repaired internal holding structures for gas turbine engine cases and method of repairing the same
06/05/2012US8192148 Fluid return in the splitter of turbomachines with bypass-flow configuration
06/05/2012US8192144 Compressor and heat pump system
05/2012
05/31/2012WO2012071254A2 Exhaust-gas turbocharger
05/31/2012WO2012071166A2 Integrated variable geometry flow restrictor and heat exchanger
05/31/2012WO2012070647A1 Tool for assembly and disassembly of turbine device, and method of assembly and disassembly of turbine device
05/31/2012WO2012069773A1 Device for uncoupling a bearing carrier
05/31/2012WO2012069772A1 Oil discharge device and turbomachine comprising such a device
05/31/2012WO2012069306A1 METALLIC BONDCOAT OR ALLOY WITH A HIGH γ/γ' TRANSITION TEMPERATURE AND A COMPONENT
05/31/2012WO2012069305A1 METALLIC BONDCOAT OR ALLOY WITH A HIGH γ/γ' TRANSITION TEMPERATURE AND A COMPONENT
05/31/2012US20120134844 Nose cone assembly
05/31/2012US20120134843 Nose cone assembly
05/31/2012US20120134798 Fan module with multiple cooling fans
05/31/2012US20120134791 Gas turbine nozzle attachment scheme and removal/installation method
05/31/2012US20120134785 Axial flow gas turbine
05/31/2012US20120134781 Axial flow gas turbine
05/31/2012US20120134780 Axial flow gas turbine
05/31/2012US20120134778 Axial flow gas turbine
05/31/2012US20120134777 Engine case with wash system
05/31/2012US20120134774 Gas turbine engine blade containment arrangement
05/31/2012CA2818705A1 Oil discharge device and turbomachine comprising such a device
05/31/2012CA2817526A1 Integrated variable geometry flow restrictor and heat exchanger
05/30/2012EP2458164A1 Pump for conveying a medium and lubricant system
05/30/2012EP2458163A2 Gas turbine of the axial flow type
05/30/2012EP2458161A1 Method for monitoring the oil system of a turbomachine
05/30/2012EP2458158A1 Lubrication system for a turbomachine
05/30/2012EP2458152A2 Gas turbine of the axial flow type
05/30/2012EP2458150A1 Method for damping mechanical vibrations occurring during operation in a turbomachine blade, turbomachine blade for carrying out the method and piezoelectric damping element to be installed in such a turbomachine blade
05/30/2012EP2458147A2 Gas turbine of the axial flow type
05/30/2012EP2456958A1 Method for manufacturing a micro gas turbine
05/30/2012EP2137382B1 Stator heat shield
05/30/2012CN202250307U Silencer of air outlet of pressure shell
05/30/2012CN202250269U Medium-low pressure communicating tube structure in steam turbine
05/30/2012CN202250268U Supporting ring
05/30/2012CN202250267U Lubricating oil tank provided with water drainage device
05/30/2012CN202250266U Lubricant control valve of turbocharger
05/30/2012CN202250265U Improved intermediate internal sleeve structure of ball-bearing turbocharger
05/30/2012CN202250264U Intermediate body inner casing structure of ball bearing turbocharger
05/30/2012CN202250263U Improved intermediate structure of ball bearing turbocharger
05/30/2012CN202250262U Intermediate structure of ball bearing turbocharger
05/30/2012CN202250261U Rotor shaft supporting structure of turbocharger
05/30/2012CN202250260U Rotor supporting mechanism for rolling bearing turbocharger
05/30/2012CN202250259U Water-cooling volute of automotive turbosuperchager
05/30/2012CN202250258U Vehicle turbo supercharger water-cooled volute
05/30/2012CN202250257U Squeeze film damper for rolling bearing turbocharger
05/30/2012CN202250251U Laminated medium-pressure steam inlet insertion tube of steam turbine
05/30/2012CN1978870B Improved bladed stator for a turbo-engine
05/30/2012CN102482991A Method for determining bearing play of exhaust-gas-turbocharger friction bearings
05/30/2012CN102482947A Clearance control at the blade tips of a turbomachine
05/30/2012CN102482945A A mounting apparatus
05/30/2012CN102482786A 电解槽以及包括有该电解槽的电源单元 The electrolytic cell and the electrolytic cell comprising a power supply unit
05/30/2012CN102477873A Gas turbine of the axial flow type
05/30/2012CN102477872A Axial flow gas turbine
05/30/2012CN102477871A Axial flow gas turbine
05/30/2012CN101828039B Pressure vessel having a lid
05/30/2012CN101213354B Turbocharger bearing and associated components
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