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)
05/2014
05/20/2014US8727709 Casing component
05/20/2014US8727707 Intake duct liner for a turbofan gas turbine engine
05/20/2014US8727703 Gas turbine engine
05/20/2014US8727699 Rotating machinery with damping system
05/20/2014US8727695 Chamfer-fillet gap for thermal management
05/20/2014US8727632 Bearing support apparatus for a gas turbine engine
05/20/2014US8727629 Series bearing support apparatus for a gas turbine engine
05/20/2014US8727628 Dual mode scavenge scoop
05/20/2014DE202013005524U1 Vorrichtung zum Reinigen der Core Engine eines Strahltriebwerks Device for cleaning the core engine of a jet engine
05/20/2014CA2557104C Process for assembling a turbine engine
05/20/2014CA2504173C Methods and apparatus for assembling a bearing assembly
05/15/2014WO2014074792A1 Split intermediate case
05/15/2014WO2014074603A1 Pressurized reserve lubrication system for a gas turbine engine
05/15/2014WO2014074437A1 Method for joining bearing housing segments of a turbocharger incorporating an electric motor
05/15/2014WO2014074436A1 Swirl inducing bearing housing spacer and core
05/15/2014WO2014074433A1 Supplemental air cooling system and air pressure oil sealing system for electrical turbocompound machine
05/15/2014WO2014074432A1 Centrifugal compressor with inlet swirl slots
05/15/2014WO2014074396A1 External cooling fluid injection system in a gas turbine engine
05/15/2014WO2014074368A1 Air injection system for cooling a rotor in a gas turbine engine and method of cooling such rotor
05/15/2014WO2014074306A1 Modular drop-in transition assembly for industrial gas turbine and method for installation
05/15/2014WO2014074305A1 Modular drop-in combustor assembly for industrial gas turbine and method for installation
05/15/2014WO2014074195A2 Turbine engine support assembly including self anti-rotating bushing
05/15/2014WO2014073227A1 Seal structure for vapor turbine
05/15/2014WO2014072643A2 Air exhaust tube holder in a turbomachine
05/15/2014WO2014072626A2 Air exhaust tube holder in a turbomachine
05/15/2014WO2014072575A1 Cooling arrangement for a gas turbine
05/15/2014US20140134399 Components with environmental barrier coatings having improved surface roughness
05/15/2014US20140133984 Electrical power transfer system for propeller system
05/15/2014US20140133978 Turbomachine bearing assembly preloading arrangement
05/15/2014US20140133976 Radial Fixing and Positioning Flanges for Shells of Axial Turbine Compressor Housings
05/15/2014US20140133973 Power cable and connector arrangement for a gas turbine engine
05/15/2014US20140133966 Clutched turbine wheels
05/15/2014US20140133962 Interturbine vane with multiple air chambers
05/15/2014US20140133956 Process for cooling the turbine stage and gas turbine having a cooled turbine stage
05/15/2014US20140130514 Turbine nozzle having non-linear cooling conduit
05/15/2014US20140130510 Systems and methods for directing cooling flow into the surge plenum of an exhaust eductor cooling system
05/15/2014US20140130422 Modular turbine enclosure
05/15/2014US20140130351 Variable geometry turbomachine
05/15/2014DE112004001587B4 Kraftwerksanlage und Verfahren zum Betrieb Power plant and method of operation
05/15/2014CA2832771A1 Radial fixing and positioning flanges for shells of axial turbine compressor housings
05/14/2014EP2730754A2 Turbomachine bearing assembly preloading arrangement
05/14/2014EP2730753A1 A system for assembling and disassembling a turbine section of a gas turbine
05/14/2014EP2730748A2 A system for cooling a hot gas path component, corresponding gas turbine combustor and cooling method
05/14/2014EP2730371A1 Device for setting a predetermined radial gap size of the blades of a turbomachine
05/14/2014EP2730370A1 Method and device to adjust a predetermined radial tip clearance of a turbomachine blade
05/14/2014EP2729686A1 Cooling for a fluid flow machine
05/14/2014EP2729668A1 Turbine engine drive shaft device
05/14/2014CN103797219A 用于将流体机械的转子从第一位置枢转到第二位置中的设备 The fluid machine for rotor pivot from a first position to a second position of the device
05/14/2014CN103797218A 朗肯循环系统 Rankine cycle system
05/14/2014CN103797217A 用于在燃气涡轮中喷射蒸汽的方法和设备 Method and apparatus for steam injection in a gas turbine
05/14/2014CN103790757A 海底管道自发电装置 Subsea pipelines self-generating device
05/14/2014CN103790656A 涡轮机排气罩和相关安装方法 Turbine exhaust hood and related installation method
05/14/2014CN103790655A 蒸汽轮机机罩系统 Steam turbine hood system
05/14/2014CN103790654A 一种涡轮外环的冷却组件 A turbine cooling component of the outer ring
05/14/2014CN103790653A 基于气磁复合支撑的龙门式航空发动机转子装配方法与装置 Gantry aero-engine rotor assembly method and apparatus for gas-based magnetic composite support
05/14/2014CN103790652A 基于光电编码器测角的航空发动机转子气浮装配方法与装置 Based on aero-engine rotor flotation optical encoder assembly methods and apparatus for measuring angles
05/14/2014CN103790651A 基于气/磁混合导向的航空发动机转子装配方法与装置 Aero-engine rotor assembly method and apparatus based on gas / magnetic hybrid-oriented
05/14/2014CN103790650A 基于同心度优化的磁悬浮式航空发动机转子装配方法与装置 Maglev aero engine rotor assembly method and apparatus for optimization based concentricity
05/14/2014CN103790649A 可移动式双立柱结构的航空发动机转子装配方法与装置 Aero-engine rotor assembly method can be mobile and apparatus for dual-column structure
05/14/2014CN103790648A 基于多部件同心度优化的航空发动机转子装配方法与装置 Aero-engine rotor assembly method and apparatus for multi-component-based optimization of concentricity
05/14/2014CN103790647A 基于电感传感的液压抓卡式航空发动机转子装配方法与装置 Cassette aero-engine rotor assembly method and apparatus for sensing inductor-based hydraulic grab
05/14/2014CN103790646A 基于光电编码器测角的航空发动机转子电驱动磁浮装配方法与装置 Based on the measured angle optical encoder electrically driven air engine rotor assembly method and apparatus for magnetic levitation
05/14/2014CN103790645A 基于同心度与垂直度评定与优化的航空发动机转子装配方法与装置 Concentricity and squareness based evaluation and optimization of aero-engine rotor assembly method and apparatus
05/14/2014CN103790644A 基于空间矢量投影的航空发动机转子装配方法与装置 Based on space vector projection aviation engine rotor assembly method and apparatus
05/14/2014CN103790643A 一种提高汽轮机排汽参数的方法 A steam turbine exhaust parameters of methods to improve
05/14/2014CN102575581B 燃气轮机静叶片的插入件去除装置及燃气轮机静叶片的插入件去除方法 A gas turbine stationary blade removal insert device and the gas turbine stationary blade insert removal method
05/14/2014CN102395772B 设置有轴间轴承的双主体气体涡轮引擎 Is provided between the main shaft bearing twin gas turbine engine
05/14/2014CN101903665B 具有射流排水阀的涡轮增压器 Jet drain valve having a turbocharger
05/13/2014US8721278 Exhaust manifold flange connection
05/13/2014US8721277 Unit for locking ring sectors on a turbomachine casing, comprising radial passages for gripping it
05/13/2014US8721256 Turbomachine optimized for fastening a rotary shaft bearing, A method of mounting said bearing on said turbomachine
05/13/2014US8720059 Apparatus and method for aircraft engine core exchange
05/13/2014CA2697741C Combined acoustic absorber and heat exchanging outlet guide vanes
05/08/2014WO2014071136A2 System and method for a turbine combustor
05/08/2014WO2014071121A1 System and method for a turbine combustor
05/08/2014WO2014071088A1 System and method for protecting components in a gas turbine engine with exhaust gas recirculation
05/08/2014WO2014070691A1 Gas turbine engine with bearing compartment wall cooling
05/08/2014WO2014070630A1 Gas turbine engine synchronization ring
05/08/2014WO2014070436A2 Temperature control within a cavity of a turbine engine
05/08/2014WO2014069109A1 Bearing structure for turbocharger
05/08/2014WO2014068355A1 Gas turbine engine exhaust system and corresponding method for accessing turbine buckets
05/08/2014WO2014068261A1 Turbomachine casing
05/08/2014WO2014068220A1 Exhaust housing hub for a turbomachine
05/08/2014WO2014067736A1 Aid device
05/08/2014WO2014035512A3 Non-interrupted turbomachine fluid supply
05/08/2014WO2014031205A3 Seal land for static structure of a gas turbine engine
05/08/2014WO2014031198A3 Variable blade outer air seal
05/08/2014WO2014031194A3 Direct feed auxiliary oil system for geared turbofan engine
05/08/2014WO2014028095A3 Blade outer air seal with cored passages
05/08/2014US20140127051 Turbocharger
05/08/2014US20140127012 Oil deflector
05/08/2014US20140127011 Mounting apparatus for fans
05/08/2014US20140126998 Compressor Bellmouth with a Wash Door
05/08/2014US20140126991 Systems and methods for active component life management for gas turbine engines
05/08/2014US20140123674 Inlet Bleed Heat System with Integrated Air Knife/Silencer Panels
05/08/2014DE102013222067A1 Ölablenker Ölablenker
05/08/2014DE102013111810A1 Schalldämpfendes Schornsteinelement für ein Turbomaschinensystem The acoustic damping element chimney for a turbo machine system
05/08/2014DE102012211950A1 Abgasturbine Exhaust gas turbine
05/08/2014DE102010051562B4 Abgasführungsvorrichtung für eine Verbrennungskraftmaschine Exhaust routing device for an internal combustion engine
05/07/2014EP2728132A1 Storage tank
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