Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › 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)
06/2014
06/03/2014US8739513 Gas turbine engine exhaust mixer
06/03/2014US8739512 Combined cycle power plant
06/03/2014CA2533956C Trip manifold
05/2014
05/30/2014WO2014081794A1 Method of extending life of rotating parts
05/30/2014WO2014081790A1 Gas turbine engine compressor rotor assembly and balancing system
05/30/2014WO2014081723A1 Hardened silver coated journal bearing surfaces and method
05/30/2014WO2014081509A1 Composite articles and methods
05/30/2014WO2014081500A2 Auxiliary component mounts
05/30/2014WO2014081493A2 Low profile compressor bleed air-oil coolers
05/30/2014WO2014081492A2 Cooling for combustor liners with accelerating channels
05/30/2014WO2014080758A1 Power generation system, method for powering power generation system, and combustor
05/30/2014WO2014042723A3 Vane support assembly
05/30/2014WO2014042720A3 Gas turbine engine turbine blade airfoil profile
05/30/2014WO2014040672A8 Air inlet system for a stationary internal combustion engine, in particular for a stationary gas turbine
05/30/2014WO2014035522A3 Blade outer air seal hybrid casting core
05/30/2014WO2013122713A3 Geared turbofan engine low noise compressor rotor
05/30/2014WO2013025818A9 Fuel system using dual pressure hi-speed centrifugal pump arrangement
05/30/2014CA2834870A1 Air cooling shaft at bearing interface
05/30/2014CA2831658A1 Operations support systems and methods with acoustics evaluation and control
05/29/2014US20140147269 Aircraft nacelle incorporating an improved connection between an air intake and a powerplant
05/29/2014US20140147268 Aircraft nacelle comprising a deformable connection between an air intake and a power plant
05/29/2014US20140147266 Ceramic Matrix Composite Liner Attachment
05/29/2014US20140147258 Hydraulic bearing for a stationary gas turbine
05/29/2014US20140147251 Insert element for closing an opening inside a wall of a hot gas path component of a gas turbine and method for enhancing operational behaviour of a gas turbine
05/29/2014US20140144519 Aircraft nacelle comprising a reinforced connection between an air intake and a powerplant
05/29/2014US20140144158 Turbomachine component including a seal member
05/29/2014US20140144155 Gas turbine comprising a heat shield and method of operation
05/29/2014US20140144154 Gas turbine engine with bearing buffer air flow and method
05/29/2014US20140144152 Premixer With Fuel Tubes Having Chevron Outlets
05/29/2014US20140144148 Cooled Combustor Seal
05/29/2014US20140144140 Fuel boost module
05/29/2014US20140144139 Air cooled air cooler for gas turbine engine air system
05/29/2014US20140144124 Gas Turbine Anti-Icing System
05/29/2014US20140144123 Inlet particle separator system with air injection
05/29/2014US20140144121 Gas turbine engine with bearing oil leak recuperation system
05/29/2014US20140144120 Lubrication Cut-Off at High Speed
05/28/2014DE10325599B4 Brennkammerdichtungsring und Brennkammer, die einen solchen Ring aufweist Combustion chamber sealing ring and the combustion chamber, having such a ring
05/28/2014DE102013112411A1 Modulares Turbinengehäuse Modular turbine housing
05/28/2014DE102012022938A1 Electrical propelled supercharger for energy converter, has transmission unit that is coupled with shaft in axial direction, for transferring axial forces resulting gas forces on air bearing unit from compressor side and turbine side
05/28/2014DE102012022260A1 Verfahren zur Herstellung einer Welle eines Gasturbinentriebwerks, insbesondere einer Radialwelle oder einer zur Maschinenachse in einem Winkel angeordneten Welle A method of manufacturing a shaft of a gas turbine engine, in particular a rotary shaft or arranged at an angle to the machine axis shaft
05/28/2014DE102012022259A1 Brennkammerschindel einer Gasturbine sowie Verfahren zu deren Herstellung Combustion chamber tile of a gas turbine and processes for their preparation
05/28/2014DE102012022198A1 Welle eines Gasturbinentriebwerks, insbesondere einer Radialwelle oder einer zur Maschinenachse in einem Winkel angeordneten Welle Shaft of a gas turbine engine, particularly a radial shaft or arranged to the machine axis at an angle shaft
05/28/2014DE102012015454A1 Verfahren zur Regelung der Kraftstofftemperatur einer Gasturbine Method for controlling the fuel temperature of a gas turbine
05/28/2014CN203614234U 燃机电厂余热锅炉利用余热加热天然气系统 Gas turbine power plant waste heat boilers and gas heating system utilizing waste heat
05/28/2014CN203614233U 支承式角位移传感器安装结构 Bearing angular displacement sensor mounting structure
05/28/2014CN203614232U 一种圆周密封冷却结构及航空发动机 One kind of circumferential seal cooling structure and aero-engine
05/28/2014CN203614231U 涡喷发动机轴承室用供滑油结构 Turbojet engine compartment for oil bearing structure
05/28/2014CN203614230U 燃气轮机转子的封油装置 Turbine rotor seal oil installations
05/28/2014CN203614229U 发动机融合外涵出口导叶支板结构以及航空发动机 Engine fusion outer culvert outlet guide vane structure and aero-engine support plate
05/28/2014CN203614228U 气门结构涡轴发动机 Turboshaft engine valve structure
05/28/2014CN103827466A 用于废气涡轮增压机的隔热屏以及隔热屏的在废气涡轮增压机的两个壳体部件之间的布置结构 Arrangement for exhaust gas turbocharger heat shield and a heat shield between the two housing parts of the exhaust gas turbocharger
05/28/2014CN103821615A 一种发动机进气防护装置 An engine air intake guards
05/28/2014CN102317608B 最优化低环境影响背景信息的对旋风扇设计和可变叶片列间隔 Optimization of low environmental impact of background information on the design and variable fan blades spin column spacing
05/28/2014CA2833759A1 Gas turbine engine with bearing buffer air flow and method
05/28/2014CA2833451A1 Gas turbine engine with bearing oil leak recuperation system
05/27/2014US8733693 Aircraft engine assembly comprising an annular load-transfer structure surrounding the central casing of a turbojet engine
05/27/2014US8733111 Cooling hole with asymmetric diffuser
05/27/2014US8733108 Combustor and combustor screech mitigation methods
05/27/2014US8733078 Igniter with integral pressure sensing line
05/27/2014CA2747614C Fan embedded power generator
05/22/2014WO2014078157A1 Gas turbine engine with mount for low pressure turbine section
05/22/2014WO2014078042A1 Hybrid gas turbine bearing support
05/22/2014WO2014078003A2 Gas turbine engine with inlet particle separator and thermal management
05/22/2014WO2014077922A2 Nacelle scoop inlet
05/22/2014WO2014077909A2 Multi-lobed cooling holes in gas turbine engine components having thermal barrier coatings
05/22/2014WO2014077156A1 Power generation system and method for operating power generation system
05/22/2014WO2014077058A1 Rotary machine
05/22/2014WO2014076829A1 Gas turbine member having thermal barrier coating
05/22/2014WO2014042735A3 Gas turbine engine component with discharge slot having oval geometry
05/22/2014WO2014035516A3 Gas turbine engine turbine vane airfoil profile
05/22/2014WO2014008117A9 Method for turbine wheel balance stock removal
05/22/2014WO2013154650A3 Anti-icing stator assembly for a gas turbine
05/22/2014US20140140830 Inner structure for an aircraft nacelle
05/22/2014US20140140817 Micro gas turbine having compact structure
05/22/2014US20140140809 Heat protection assembly
05/22/2014US20140137568 Device for mounting a spark plug in a combustion engine of a gas turbine engine
05/22/2014US20140137567 Micro gas turbine having ignitor-coupling structurer and method of assembling the same
05/22/2014US20140137565 Combination air assist and pilot gaseous fuel circuit
05/22/2014US20140137562 Hydrogen Generator Having a Thermal Actuator
05/22/2014US20140137558 Fuel supply system for supplying fuel to a combustion section of a gas turbine
05/22/2014US20140137557 Gas turbine combustor
05/22/2014US20140137535 Clocked combustor can array
05/22/2014DE102013112879A1 Superteleleskopisches Querzündrohr und Verfahren zur Montage einer Brennkammeranordnung Superteleleskopisches crossfire tube and method of assembling a combustor assembly
05/22/2014DE102013112790A1 Umkehrbarer V-Zellen- oder Minifaltenfilter mit mechanisch abgedichtetem Faltenpack Reversible V-cell or mini pleated filter with mechanically sealed fold pack
05/22/2014DE102012221303A1 Drive device for motor car, has bearing portions that are cooled convectively by coolant flow such that exhaust gas is removed from bearing portions by supplying coolant between fuel cell and turbine of supercharger
05/22/2014DE102006058343B4 Gasturbinenölabscheider Gasturbinenölabscheider
05/22/2014CA2845618A1 Geared architecture for high speed and small volume fan drive turbine
05/21/2014EP2733330A2 A heat protection assembly
05/21/2014EP2733312A2 Gas turbine engine optimization by electric power transfer
05/21/2014EP2732145A2 Gas turbine engine sump pressurization system
05/21/2014EP2732138A1 Improved diverter damper
05/21/2014EP2732137A1 Method for starting a turbomachine that reduces the thermal imbalance
05/21/2014CN203604054U 涡桨发动机用点火装置 Turboprop engine ignition device
05/21/2014CN203604053U 地面用燃气轮机 Ground gas turbine
05/21/2014CN103814199A 使用涡轮机的压缩气体能量储存系统 Using a compressed air turbine energy storage system
05/21/2014CN103811932A 缆线组件及密封电缆和柔性管道的方法 The method of sealing cables and cable assemblies and flexible pipe
05/21/2014CN103807025A 燃料计量阀系统 Fuel metering valve system
05/21/2014CN103807024A 包括燃料预热系统的燃气涡轮机 Fuel warm-up system including a gas turbine
05/21/2014CN103807023A 用于冷却燃气涡轮机燃烧器的高温气体部件的系统 System for cooling the high temperature gas are the gas turbine combustor
05/21/2014CN103807021A 叶轮机构发动机 Impeller institutions engine
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