Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
04/2012
04/04/2012CN102405336A 内燃发动机 Internal combustion engine
04/04/2012CN102405331A A gas turbine engine
04/04/2012CN102400723A Turbine of submerged furnace
04/04/2012CN102400722A Exhaust plenum flow splitter
04/04/2012CN102400721A 一种涡轮支承支点隔热屏的更换方法 Replacement of a turbine bearing fulcrum heat shield
04/04/2012CN102400720A Turbine housing assembly with wastegate
04/04/2012CN102400716A 一种压缩气体发动机 A compressed gas engine
04/03/2012US8147199 Pump and balancing cover thereof
04/03/2012US8147194 Turbine engine components
04/03/2012US8147181 Device for inhibiting the flow of oil along a rotating shaft
04/03/2012US8147179 Hot-gas-ducting housing element, protective shaft jacket and gas turbine system
04/03/2012US8146711 Reduced gulp fluid reservoir
04/03/2012US8146358 Bearing health monitor
04/03/2012CA2520464C Turbojet with a one-piece servicing connector arm and one-piece servicing connector arm
03/2012
03/30/2012CA2754240A1 Gas turbine engine casing
03/29/2012WO2012040573A1 Hydraulic shaft coupling apparatus
03/29/2012WO2012040214A1 High efficiency power production methods, assemblies, and systems
03/29/2012WO2012040039A2 Vtg cartridge of an exhaust-gas turbocharger
03/29/2012WO2012039385A1 Weld bead cutting device and method for extracting radial pin from steam turbine
03/29/2012WO2012038667A1 System for pressurising the bearing chambers of turbine engines machines using air taken from the intake duct
03/29/2012WO2012038638A1 Sealing device having a sleeve for the passage of a connecting rod of a system for controlling the orientation of the blower blades of a turboprop engine through a partition
03/29/2012WO2012038165A1 Gas turbine and method for operating a gas turbine
03/29/2012US20120076650 Shroud Structure for Gas Turbine
03/29/2012US20120076635 Nacelle with porous surfaces
03/29/2012DE102011053764A1 Befestigungsbolzen für eine verstellbare Leitschaufelanordnung eines Turbinenverdichters Mounting bolts for a variable vane of a turbine compressor
03/29/2012DE102011052675A1 Komponenten mit konform gekrümmten Filmlöchern und Verfahren für deren Herstellung Components compliant with curved film holes and methods for their preparation
03/29/2012DE102011052672A1 Spitzenströmungspfadprofil Peak flow path profile
03/29/2012DE102010053078A1 Exhaust gas supercharger, has connecting element formed between exhaust gas guide section and bearing portion, and bearing section and exhaust system portion comprising connector that is formed in region of connection joint
03/29/2012DE102010046598A1 Exhaust gas turbocharger has housing provided with air guiding section, exhaust gas guiding section and bearing section, where friction condition is adjusted in bearing
03/29/2012CA2812554A1 Hydraulic shaft coupling apparatus
03/29/2012CA2811945A1 High efficiency power production methods, assemblies, and systems
03/29/2012CA2811409A1 System for pressurising the bearing chambers of turbine engines machines using air taken from the intake duct
03/29/2012CA2811269A1 Sealing device having a sleeve for the passage of a connecting rod of a system for controlling the orientation of the blower blades of a turboprop engine through a partition
03/28/2012EP2434125A1 Method for producing impeller applied to supercharger
03/28/2012EP2434108A1 Support screw element
03/28/2012EP2434107A2 Anti-fret liner assembly for a turbine engine
03/28/2012EP2434106A2 Shroud structure for gas turbine
03/28/2012EP2434105A2 Metallic backing for composite flange of a fan containment case
03/28/2012EP2434101A2 A damped assembly
03/28/2012EP2434100A1 Turbine engine apparatus with protective coating
03/28/2012EP2136050B1 Gas turbine plant
03/28/2012CN102395772A Double-body gas turbine engine provided with an inter-shaft bearing
03/28/2012CN102395770A Anti-rotation method for a rolling element bearing cartridge
03/28/2012CN102395769A Insulating spacer for ball bearing cartridge
03/28/2012CN102392703A Double reheat steam turbine
03/28/2012CN102392699A Steam turbine operation method
03/28/2012CN102392698A Intermediate structure of ball-bearing turbocharger
03/28/2012CN102392697A Thrust structure for turbocharger
03/28/2012CN102392696A Turbocharger heat insulation structure
03/28/2012CN102392695A Squeeze film damper for rolling bearing turbochargers
03/28/2012CN101680306B Blade structure for turbine
03/27/2012US8142159 Fan and motor thereof
03/27/2012US8142151 Intermediate housing floor for a fluid kinetic machine
03/27/2012US8142150 Alignment device for gas turbine casings
03/27/2012US8142149 Fan device and fan device assembly
03/27/2012US8142138 Turbine engine having cooling pin
03/27/2012US8142136 Oil-sealing arrangement for cooling fan
03/27/2012US8141879 Seals for a turbine engine, and methods of assembling a turbine engine
03/27/2012CA2618116C Coated variable area fan nozzle
03/27/2012CA2504165C Chevron film cooled wall
03/27/2012CA2472939C Device to passively control thermal expansion of the extension casing of a turbojet
03/24/2012CA2751867A1 Method and system for synthetic jet cooling
03/22/2012WO2012035658A1 Wing arrangement method
03/22/2012WO2012034906A1 Assembly of a blade and a composite carrier, obtained by sealing
03/22/2012US20120070278 Gas turbine engine bearing arrangement
03/22/2012US20120070276 Turbine shroud thermal distortion control
03/22/2012US20120070275 Airfoil for energy extracting shrouded fluid turbines
03/22/2012US20120070274 Turbocharger Unit with Associated Auxiliary Component, for an Internal Combustion Engine
03/22/2012US20120070270 Damped assembly
03/22/2012US20120068003 Wireless sensor for an aircraft propulsion system
03/22/2012US20120067054 High efficiency power production methods, assemblies, and systems
03/22/2012DE102010041144A1 Schnellstartvorrichtung für eine Turbine, sowie Verfahren zum Betreiben einer Schnellstartvorrichtung Quick start-up device for a turbine and method for operating a quick start device
03/22/2012DE102010041066A1 Trägergehäuse und Brennkraftmaschine Support housing and internal combustion engine
03/22/2012CA2811069A1 Assembly of a blade and a composite carrier, obtained by sealing
03/21/2012EP2431588A1 Turbocharger unit with associated auxiliary component for an internal combustion engine
03/21/2012EP2431578A2 Gas turbine engine bearing arrangement
03/21/2012EP2431577A2 Axial flow compressor, gas turbine system having the axial flow compressor and method of modifying the axial flow compressor
03/21/2012EP2431576A1 Method and apparatus for simulation test of centrifugal stress of turbine blade
03/21/2012EP2431574A1 Gas turbine and method for operating a gas turbine
03/21/2012EP2431571A1 Assembly of a blade and a composite support by secure fixing
03/21/2012CN202170817U 一种双缸式蒸汽动力装置的内汽缸悬挂装置 A twin cylinder steam power plant suspension
03/21/2012CN102388209A Insulating and damping sleeve for a rolling element bearing cartridge
03/21/2012CN102383919A Supercharging device for compressing charge air for an internal combustion engine
03/21/2012CN102383918A Turbocharger
03/21/2012CN102383879A Steam turbine structure
03/21/2012CN102383877A Volute device of variable geometry pulse gas inlet turbine
03/21/2012CN102383876A Lubricating oil control valve for turbocharger and operating method thereof
03/21/2012CN102383875A Connecting method for lubricating oil pipeline of steam turbine
03/21/2012CN102383874A Turbine housing assembly
03/21/2012CN102383870A Natural gas pressure difference generating system self-adaptive to back-end load change
03/21/2012CN101575991B Engine having a turbocharger coupler
03/21/2012CN101542092B Intake air heating control apparatus for gas turbine
03/21/2012CN101526032B Compressed air heat-linkage energy-storage system based on reversible air engine
03/20/2012US8137058 Method and apparatus for determining clearance between moving and static members in a machine
03/20/2012US8136999 Turbomachine shaft guidance
03/20/2012CA2506174C System and devices for collecting and treating waste water from engine washing
03/20/2012CA2470069C Ignition plug waterproofing device, not soldered to the chamber wall
03/15/2012WO2012033564A1 Screw shaft turbine compressor and system
03/15/2012WO2012032270A1 Hyperstatic truss comprising connecting rods
03/15/2012WO2012032016A1 Turbojet engine blade, in particular a guide blade, and turbojet engine receiving such blades
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