F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants

Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889)
12/2011
12/29/2011	US20110314827 Fuel nozzle assembly
12/29/2011	US20110314825 Gas turbine system having premixed injector vanes
12/29/2011	US20110314823 Gas turbine combustor liner cap assembly
12/29/2011	US20110314822 Switchable Solar Heating Device For A Gas Turbine
12/29/2011	DE102011051415A1 System mit einer Speisewasserheizvorrichtung zum Abführen von Wärme von einer Niederdruckdampfturbine System with a Speisewasserheizvorrichtung for removing heat from a low pressure steam turbine,
12/29/2011	DE102011051369A1 Additiv-Einspritzsystem zur Verwendung mit einer Turbine und Verfahren zum Einbau desselben Of the same additive injection system for use with a turbine and method of installing
12/29/2011	DE102010030516A1 Exhaust gas turbocharger for internal combustion engine, has turbine wheel rotatably arranged in bearing housing, compressor housing and turbine housing via drive shaft, where shaft is driven by compressor wheel
12/29/2011	DE102010025588A1 Profile heat exchanger for gas turbine, has heat exchanger packages including supply passage, exhausting passage and hollow profiles that are extended and bent against each other on two sides of supply and exhausting passages
12/29/2011	DE102010025587A1 Gas turbine i.e. propeller gas turbine, has hollow sections with profile axles bent against series axles around profile angle, and exhausting passage bent against gas turbine around passage angle along longitudinal axis
12/29/2011	DE102010025286A1 Light metal cast part for multi-cylinder internal combustion engine, has channels with surfaces coated with coating, where temperature of coating is greater than maximum temperature of gas and equal to melting temperature of metal melt
12/29/2011	DE102010025014A1 Vorrichtung zur Reduzierung von Strahllärm Device for reducing jet noise
12/29/2011	CA2803855A1 Secondary water injection for diffusion combustion systems
12/29/2011	CA2743281A1 Lubrication system for aircraft engine
12/28/2011	EP2399828A1 Method for preventing the clogging of a grating, grating and air intake implementing such a method
12/28/2011	EP2399030A1 Device for restricting the throughflow quantity at a pump, and pump arrangement having a device of this type
12/28/2011	EP2399018A1 Air vehicle propulsion system with counter rotating fan design and method for noise reduction
12/28/2011	EP2398706A2 Engine mounting with an adapted load/deformation curve
12/28/2011	CN202087142U Zigzag-flow passage air dehumidifying and filtering device with hooks
12/28/2011	CN1826431B 机械零件的修理和制造方法及修复机械零件的制造方法 Repair and manufacturing methods of mechanical parts and manufacturing methods to repair the mechanical parts
12/28/2011	CN1609427B 膜式冷却燃气轮机燃烧器的方法和装置 Film cooling method and a gas turbine combustor apparatus
12/28/2011	CN102301122A 用于飞行器发动机机舱的声衰减板 Sound attenuation for aircraft engine nacelle board
12/28/2011	CN102301107A 燃烧器结构部件的制造方法、燃烧器结构部件、燃气轮机用燃烧器及燃气轮机 The method of manufacturing the structural component burner, the burner structural components, the gas turbine and a gas turbine burner
12/28/2011	CN102301097A 包括agb和储油器的组件 Including agb and reservoir assembly
12/28/2011	CN102297027A 燃气涡轮起动控制 Gas turbine starting control
12/28/2011	CN102297026A 除尘装置及地面燃气轮机 Dust collector and ground gas turbine
12/28/2011	CN102297025A 微型混合富氧燃烧的燃气轮发电机 Micro hybrid oxyfuel gas turbine generator
12/28/2011	CN102297024A 一种微型纯氧燃烧的燃气轮发电机 A miniature oxygen combustion gas turbine generator
12/27/2011	US8083030 Gearbox lubrication supply system for a tip engine
12/27/2011	US8082739 Combustor exit temperature profile control via fuel staging and related method
12/24/2011	CA2743279A1 Cooler in nacelle with radial coolant
12/22/2011	WO2011157962A1 Airflow-straightening structure for the nacelle of an aircraft engine
12/22/2011	WO2011157943A1 Architecture for a non-lubricated turboshaft engine
12/22/2011	WO2011157937A1 Guiding and sealing device for a turbine engine, having a carbon seal and built-in journal bearing
12/22/2011	WO2011157548A1 Damping device for damping pressure oscillations within a combustion chamber of a turbine
12/22/2011	US20110309187 Nested core gas turbine engine
12/22/2011	US20110308257 Attachment structure for a turbojet engine
12/22/2011	US20110308254 Turbine Engine Fuel Injector
12/22/2011	US20110308145 Method of inhibiting deposit formation in a jet fuel at high temperatures
12/22/2011	DE102011050838A1 Verfahren und Vorrichtung zur Rotordrehmomentübertragung Method and device for rotor torque transmission
12/22/2011	DE102010048304A1 Turbo supercharger for use with combustion engine, has drive wheels arranged opposite to each other in driving connection, and seal provided between bearing and drive wheels and comprising piston rings and expansion chambers
12/22/2011	CA2802590A1 Airflow-straightening structure for the nacelle of an aircraft engine
12/22/2011	CA2801680A1 Architecture for a non-lubricated turboshaft engine
12/22/2011	CA2801678A1 Guiding and sealing device for a turbine engine, having a carbon seal and built-in journal bearing
12/21/2011	EP2397762A1 Damping device for damping pressure oscillations within a combustion chamber of a turbine
12/21/2011	EP2397672A2 Regenerator, regeneration process, and liquid polymer mixture for a regenerator
12/21/2011	EP2397671A1 Gas and steam turbine plant and corresponding process
12/21/2011	EP2397670A1 Method for controlling emissions in a heat engine, in particular a gas turbine, and a heat engine
12/21/2011	EP2397657A1 Method and device for checking bearing alignment in a gas turbine and gas turbine
12/21/2011	EP2396526A1 Aircraft engine with cooling for an electric starting device
12/21/2011	EP2396525A1 System of compact contra-rotating propellers
12/21/2011	CN102288070A 气体延迟反冲方法 Gas delayed recoil method
12/21/2011	CN102287853A 用于燃气轮机NOx排放物控制的稀释剂喷射的备选方法 Alternative gas turbine NOx emission control for diluent injection
12/21/2011	CN102287514A 齿轮装置 Gearing
12/21/2011	CN102287454A 带有用于准确对准的安装构造的界面 For accurate alignment with the mounting structure of the interface
12/21/2011	CN102287269A 用于小型涡轮发动机的电起动装置 Electric starter for small turbine engines
12/21/2011	CN102287268A 状态转换活门及系统 Gates and system state transitions
12/21/2011	CN102287267A 使用多个再生器来进行周期性冷却、存储和加热的方法和系统 Using a plurality of cooling the regenerator to periodically, storing and heating method and system
12/21/2011	CN102287266A 一种微型全风富氧燃烧的燃气轮发电机 A miniature of the whole wind oxyfuel gas turbine generator
12/21/2011	CN102287243A 燃气和蒸汽轮机设备 Gas and steam turbine equipment
12/21/2011	CN102287238A 用于热气路径构件的密封部件 Hot gas path components for sealing member
12/21/2011	CN101688542B 用于涡轮机转子的前罩 Front cover for the turbine rotor
12/21/2011	CN101571055B 气体涡轮发电设备的运转方法 The method of operating a gas turbine power plant
12/20/2011	CA2528098C Internally cooled gas turbine airfoil and method
12/20/2011	CA2456563C Anti-icing apparatus and method for aero-engine nose cone
12/15/2011	WO2011156130A1 Cooling system for controlling cooling of rotor cooling air and heating of fuel gas
12/15/2011	WO2011154641A1 Device for supplying fuel to a gas turbine airplane engine
12/15/2011	WO2011154281A1 Emission reduction of a turboshaft engine
12/15/2011	WO2011124985A3 Turbine inlet nozzle guide vane mounting structure for radial gas turbine engine
12/15/2011	US20110305572 Mechanical arrangement
12/15/2011	US20110304104 Spring loaded seal assembly for turbines
12/15/2011	US20110304103 Pre-compressed seal including removable pre-compression member
12/15/2011	US20110304101 Film riding pressure actuated leaf seal assembly
12/15/2011	US20110302929 Exhaust gas housing for a gas turbine and method for producing same
12/15/2011	US20110302927 Fuel control method for starting a gas turbine engine
12/15/2011	US20110302924 Cooled conduit for conveying combustion gases
12/15/2011	US20110302903 Lubrication driven gas turbine engine actuation system
12/15/2011	DE202008018190U1 Motor Motor
12/15/2011	DE102011002060A1 Turbineneinlasswärmeübertragungssystem Turbine inlet heat transfer system
12/15/2011	DE102011001293A1 Inlet air filtration system for gas turbine apparatus of gas turbine engine assembly, has power source that applies voltage sufficient to establish electrostatic field between electrodes and filter elements, to electrodes
12/15/2011	DE102011000347A1 Heiß- und Warmwasserquellen enthaltendes Brennstoffheizsystem Hot and warm water sources containing fuel heating system
12/15/2011	DE102010060279A1 Tragender Rotationsring aus Verbundstoff und Herstellungsverfahren dafür Broadcaster rotation ring of composite and manufacturing method thereof
12/15/2011	DE102010056297B3 Abwärmenutzungsanlage Waste heat utilization system
12/15/2011	DE102010023702A1 Aircraft gas turbine, has bleed air aperture that is opened into air conduit tube which is arranged within silencer element parallel to core thruster, where air conduit tube opens at end region of silencer element
12/15/2011	DE102010023475A1 Thrust bearing for supercharger of commercial vehicle, has surface profile formed between lubricant grooves, detent surface arranged adjacent to wedge surface, and connecting edge formed on wedge surface and detent surface
12/15/2011	DE102010023474A1 Axiallager, Abgasturbolader mit einem Axiallager und Verfahren zur Herstellung eines Axiallagers Thrust bearings, turbocharger with a thrust bearing and methods of making a thrust bearing
12/15/2011	CA2743411A1 Bearing support
12/14/2011	EP2395214A1 Exhaust housing for a gas turbine and method for producing the same
12/14/2011	EP2395202A2 A mounting assembly for a gearbox of gas turbine engine
12/14/2011	EP2394039A1 Method for flushing a section of a fuel system of a gas turbine
12/14/2011	EP2393713A2 Turbojet engine nacelle
12/14/2011	EP2393711A1 Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelle
12/14/2011	EP2393648A1 Method for making a network of drainage pipes and acoustic processing panel including such a network of drainage pipes
12/14/2011	CN202073642U 涡旋复合式热机 Vortex composite heat engine
12/14/2011	CN102282349A 使涡轮机壳体与支承壳体相连接的连接组件以及排气涡轮增压器 The turbine housing and the bearing housing is connected to the connection assembly and the exhaust turbocharger
12/14/2011	CN102282276A Ni基单晶超合金 Ni-base single crystal superalloy
12/14/2011	CN102278207A 基于溶液除湿的燃气轮机进气冷却方法 Liquid desiccant-based gas turbine inlet air cooling method
12/14/2011	CN102278206A 一种大推重比发动机 One kind of big thrust to weight ratio of the engine
12/14/2011	CN102278205A 可用于分布式的空气及燃料湿化燃气轮机联合循环方法 Air and fuel can be used in a distributed method of wet gas turbine combined cycle
12/14/2011	CN102278204A 固体燃料粉末燃烧、作功的方法及装置 Solid fuel burning powder, method and apparatus for power
12/14/2011	CN102278155A 燃气和蒸汽轮机系统 Gas and steam turbine system

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