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)
12/2007
12/18/2007US7309208 Turning gear drive system
12/18/2007US7309207 Fan shroud structure reinforcement to reduce or eliminate warping and distortion
12/18/2007CA2355181C Secured coupling assembly and method of preventing loosening
12/13/2007WO2007140748A1 Method of producing or repairing turbine or engine components, and a component, namely a turbine or engine component
12/13/2007WO2007140730A1 Gas turbine and method of operating a gas turbine
12/13/2007US20070286725 Structure for assembling and disasembling a fan
12/13/2007DE102007021340A1 Control device for axially blown turbine of turbocharger of stroke piston-internal combustion engine, has control arrangement supported with support directly in tension ring, and comprising connector and cooling fluid line
12/12/2007EP1865155A1 Turbine casing for a steam turbine and/or a gas turbine
12/12/2007CN200989221Y Compressed air vortex shell
12/12/2007CN101087929A Turbocharger with balancing features
12/12/2007CN101087928A Static gas turbine component and method for repairing such a component
12/12/2007CN100354503C Diffusion coupler cap of axial-connected turbine
12/11/2007US7306024 Refractory metal core wall thickness control
12/11/2007US7305998 Mobile flushing unit and process
12/11/2007CA2354261C Soft bearing support
12/06/2007US20070280820 Methods and apparatus for assembling turbine engines
12/06/2007US20070280819 Gas turbine engine case and method of making
12/06/2007DE102007023916A1 Turbocharger for a vehicle comprises a bearing housing with a bearing arrangement having a bushing arranged around a rotor shaft forming an annular chamber between the shaft and bushing
12/05/2007EP1862639A1 Device for optimizing cooling in gas turbines
12/05/2007EP1862605A2 Thermal-acoustic enclosure
12/05/2007EP1861585A1 Heat accumulation segment
12/05/2007EP1861584A1 Heat accumulation segment for sealing a flow channel of a turbine engine
12/05/2007EP1861583A1 Heat accumulation segment
12/05/2007CN200985806Y Dehumidifier for nuclear power steam turbine through flow portion
12/05/2007CN200985805Y Water supplying deoxygenize device of air cooling steam turbine steam releasing device
12/05/2007CN100353035C System for reducing fuel consumption in gas turbine engine
12/05/2007CN100353032C Open-cooled component for a gas turbine, combustion chamber, and gas turbine
12/04/2007US7304844 Cooling fan assembly
12/04/2007CA2185854C Damper disposition mounted between rotor vanes
12/01/2007CA2590113A1 Device for optimizing cooling in gas turbines
12/01/2007CA2590081A1 Thermal-acoustic enclosure
11/2007
11/29/2007WO2007135449A1 A turbine for a turbocharger
11/28/2007EP1860367A2 Loss reduction apparatus
11/28/2007EP1860299A1 Sealing means for a lubrication system in a turbocharger
11/28/2007EP1860284A1 Casings assembling
11/28/2007EP1859896A1 Method of removing deposits
11/28/2007EP1502008B1 Device for fixing a rotor on a shaft
11/28/2007CN200982204Y Water-driven check valve position indicator
11/28/2007CN100351507C Fuel metering device with compensation regulator valve in turbine engine
11/27/2007US7300708 shape memory alloy to decrease the rate of wear/erosion of the blade due to contact of the blade with its surrounding shroud
11/27/2007US7300242 Turbine airfoil with integral cooling system
11/27/2007US7299618 Gas turbine combustion apparatus
11/23/2007CA2588950A1 Central body for a turbojet engine exhaust channel
11/22/2007WO2007133984A1 Compressor stage assembly lock
11/22/2007US20070269608 Rotor repair method and rotor repair apparatus
11/22/2007DE102006022683A1 Flugtriebwerk-Baugruppe, nämlich Verdichter oder Turbine eines Flugtriebwerks, Flugtriebwerk-Bauteil sowie Verfahren zur Herstellung oder Instandsetzung eines Flugtriebwerk-Bauteils Aircraft engine assembly, namely the compressor or turbine aircraft engine, aircraft engine component and methods for making or repairing an aircraft engine-component
11/21/2007EP1857639A2 Fan frame
11/21/2007EP1857638A2 Thermal management system for turbofan engines
11/21/2007EP1856420A1 Compact resilient anisotropic support for bearing
11/21/2007CN200978685Y Energy-saving discharge device with built-in heat exchanger
11/21/2007CN200978684Y Turbine main oil pump layout structure independent of turbine
11/21/2007CN200978683Y Oil-filtering machine dedicated for full-automatic steam turbine oil
11/20/2007US7299279 System and method for real-time viewing of monitoring system data
11/20/2007US7297367 Inorganic solid lubricant for high temperature foil bearing
11/20/2007US7297260 System and devices for collecting and treating waste water from engine washing
11/20/2007US7296964 Apparatus and methods for minimizing solid particle erosion in steam turbines
11/20/2007US7296398 Counter-rotating turbine engine and method of assembling same
11/20/2007CA2301151C Turbocharger integrated bearing system
11/15/2007WO2007128098A1 Gas turbine engine oil system operation
11/15/2007US20070264126 Method of Protecting a Component Against Hot Corrosion
11/15/2007US20070264119 Fan cover
11/14/2007EP1854962A2 Turbine engine mid-turbine frames
11/14/2007EP1854960A1 Method and system for rotating a turbine stator ring
11/14/2007CN101072933A Axial flow supercharger and fluid compression machine
11/13/2007US7294361 Method and device for gas phase diffusion coating of metal components
11/08/2007WO2007124586A1 Machine prognostics and health monitoring using speech recognition techniques
11/08/2007US20070258808 Combustor spring clip seal system
11/08/2007DE102007007090A1 Gas turbine has cooling air transfer system with several tubular nozzles which are independently arranged in a circle inside a chamber, encompass the rotor and can discharge cooling air
11/08/2007DE102006020597A1 Housing for a waste gas turbine supercharger of an internal combustion engine comprises a gas inlet channel designed so that part of the incoming gas flows toward a separating wall onto a turbine blade
11/07/2007EP1852574A2 Method of operating a gas turbine engine oil system
11/07/2007EP1852573A2 Sealing assembly for gas turbine engines
11/07/2007EP0919701B2 Sealing structure for joint surfaces of flanges of gas turbine
11/07/2007CN200971792Y On-line monitoring device for change of through-flow gap of steam turbine
11/07/2007CN101069023A Multi-thickness film layer bearing cartridge and housing
11/07/2007CN100347415C Casing of a turbocharger
11/07/2007CN100347414C Method of manufacturing steam turbine
11/07/2007CN100347413C Bearing for axially mounting a rotor of a gas turbine, and gas turbine
11/07/2007CN100347411C Gas-turbine engine turbon-nozzle arc section with single-branch open cavity hollow blade
11/06/2007US7290982 Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle
11/06/2007US7290806 Assembly fixture
11/06/2007US7290769 Sealing device with a brush gasket and flexible washer for a high-pressure turbine of a turbomachine
11/06/2007US7290385 Approach to extending life of gas turbine engine
11/06/2007CA2243333C Apparatus for ventilating a turbine stator ring
11/01/2007WO2007121551A1 Pre-heating of a liquid in an aircraft reservoir and associated apparatus
11/01/2007US20070251210 Liquid Injection in a Gas Turbine During a Cooling Down Phase
11/01/2007CA2643465A1 Pre-heating of a liquid in an aircraft reservoir
10/2007
10/31/2007EP1849986A1 Jet engine comprising an afterburner cooled by a ventilation flow with variable flow
10/31/2007EP1849974A2 Turbine engine tailcone resonator
10/31/2007EP1849965A2 Vane platform cooling
10/31/2007EP1849881A2 Steam turbine
10/31/2007EP1848883A1 System for providing continuous lubrication to engine turbocharger shaft and bearing arrangement
10/31/2007EP1848877A1 Bearing arrangement in a gas turbine aircraft engine
10/30/2007US7287379 Turbo compressor system for internal combustion engine comprising two serially placed turbo units with their rotation axes essentially concentric
10/30/2007US7287368 Fluid system
10/25/2007US20070248460 Magnetic-attaching structure for a fan
10/25/2007US20070246302 Pre-heating an aircraft oil reservoir
10/25/2007US20070246183 Refractory metal core wall thickness control
10/25/2007US20070245706 Pre-heating of a liquid in an aircraft reservoir
10/24/2007EP1847689A2 Apparatus and method of diaphragm assembly
10/24/2007EP1847687A1 Device for cooling a turbine casing of a turbomachine and a distributor therefore
1 ... 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 ... 222