| 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) |
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| 06/26/2014 | WO2014100087A1 Gas turbine engine including a pre-diffuser heat exchanger |
| 06/26/2014 | WO2014100081A1 Low pressure ratio fan engine having a dimensional relationship between inlet and fan size |
| 06/26/2014 | WO2014099937A1 Gas turbine engine vane embedded beam interrupt optical tip-timing probe system |
| 06/26/2014 | WO2014099932A1 Coating process for gas turbine engine component with cooling holes |
| 06/26/2014 | WO2014099890A1 Gas turbine engine with accessory gear box |
| 06/26/2014 | WO2014099713A1 Lightweight shrouded fan |
| 06/26/2014 | WO2014099712A1 Fan drive gear system assembly guide |
| 06/26/2014 | WO2014099520A1 Compressor blade for gas turbine engine |
| 06/26/2014 | WO2014099482A1 Oscillating heat pipe for thermal management of gas turbine engines |
| 06/26/2014 | WO2014099409A1 Cross-flow turbine engine |
| 06/26/2014 | WO2014099366A1 Hollow airfoil with composite cover and foam filler |
| 06/26/2014 | WO2014099259A1 Variable outer air seal fluid control |
| 06/26/2014 | WO2014099160A1 Closure of cooling holes with a filling agent |
| 06/26/2014 | WO2014099156A1 Composite ducts and methods |
| 06/26/2014 | WO2014099102A1 Airfoil member and composite platform having contoured endwall |
| 06/26/2014 | WO2014099088A2 Environmental defense shield |
| 06/26/2014 | WO2014098962A1 Two spool gas generator to create family of gas turbine engines |
| 06/26/2014 | WO2014098961A1 Two spool gas generator with improved pressure split |
| 06/26/2014 | WO2014098936A1 Gas turbine engine inner case including non-symmetrical bleed slots |
| 06/26/2014 | WO2014098005A1 Foil bearing |
| 06/26/2014 | WO2014096647A1 Intermediate casing extension of improved design |
| 06/26/2014 | WO2014096634A1 Removable acoustic panels for turbojet engine casing |
| 06/26/2014 | WO2014096620A1 Turbomachine fuel circuit |
| 06/26/2014 | WO2014096361A1 Method for operating a gas turbine in frequency-support mode |
| 06/26/2014 | WO2014095787A1 Sealing arrangement for axially split turbomachines |
| 06/26/2014 | WO2014095237A1 Method for operating a gas turbine |
| 06/26/2014 | WO2014071136A3 System and method for a turbine combustor |
| 06/26/2014 | WO2014051799A3 Fairing assembly |
| 06/26/2014 | WO2013170915A3 Apparatus for pre-heating natural gas and method for operating a power station |
| 06/26/2014 | US20140178187 Staggered double row, slotted airfoil design for gas turbine exhaust frame |
| 06/26/2014 | US20140174858 Combined sump service |
| 06/26/2014 | US20140174094 APU Exhaust Housing Perforated Ring |
| 06/26/2014 | US20140174093 Gas turbine engine lube oil system |
| 06/26/2014 | US20140174089 System for reducing flame holding within a combustor |
| 06/26/2014 | US20140174088 Alignment system and methodology to account for variation in a gas turbine engine |
| 06/26/2014 | US20140174055 Turbine section of high bypass turbofan |
| 06/26/2014 | US20140173897 Anti-Torsion Assembly |
| 06/26/2014 | DE102012224196A1 Ultraschallvorrichtung und Haltegerät zum Reinigen von Bauteiloberflächen An ultrasonic system and supporting tool for cleaning component surfaces |
| 06/26/2014 | DE102012224068A1 Turbocharger for internal combustion engine in motor vehicle, has shaft that is concentric and is adapted to be plunged towards open annular duct in lid and is communicated with oil sump arranged in housing |
| 06/26/2014 | DE102012224013A1 Verfahren zum Betreiben einer Gasturbine im Frequenzstützungsmodus A method of operating a gas turbine in the frequency support mode |
| 06/26/2014 | DE102012224009A1 Verfahren zum Betreiben einer Gasturbine A method of operating a gas turbine |
| 06/26/2014 | DE102012024845A1 Storage arrangement for rotor on housing of exhaust gas turbocharger for internal combustion engine of vehicle, has storage unit that has support element which is formed from wire mesh for damping vibrations of rotor |
| 06/26/2014 | DE102011056826B4 Schallschutzvorrichtung und damit versehenes Triebwerk und Verfahren zur Bereitstellung The sound insulation device and thus provided the engine and method for providing |
| 06/25/2014 | EP2746555A2 Fuel routing system of a gas turbine engine and method of routing fuel |
| 06/25/2014 | EP2745051A1 Staged cooling flow nozzle valve |
| 06/25/2014 | EP2744996A1 Split control unit |
| 06/25/2014 | EP2744995A1 Air inlet arrangement and method of making the same |
| 06/25/2014 | CN203670008U 航空发动机的压气机的引气装置及航空发动机的压气机 Aircraft engine compressor bleed air system and air compressor engine |
| 06/25/2014 | CN203670007U 具有翼型件的过渡管以及用于涡轮机的热气体路径组件 Having a hot gas path component of the transition tube and the airfoil for turbine |
| 06/25/2014 | CN103890350A 密封组装体及具备该密封组装体的燃气涡轮 The seal assembly and the seal assembly comprising a gas turbine |
| 06/25/2014 | CN103890349A 空气入口装置及其制造方法 The air inlet device and manufacturing method |
| 06/25/2014 | CN103890348A 陶瓷基复合构件及其制造方法 Ceramic-based composite member and its manufacturing method |
| 06/25/2014 | CN103889693A 包括用于制造由复合材料制成的燃气涡轮外壳的真空内衬的浸渍心轴 Including dipping mandrel made of composite material for the manufacture of a gas turbine casing lined vacuum |
| 06/25/2014 | CN103883401A 组合油底壳装置 Combination sump unit |
| 06/25/2014 | CN103883399A 一种原动机的半闭式正时定容热力循环方法及系统 A primal motivation of semi-closed thermodynamic cycle timing volumetric method and system |
| 06/24/2014 | US8756939 Method and system for testing an overspeed protection system of a powerplant machine |
| 06/24/2014 | US8756938 Gas compressor operating method and gas turbine equipped with gas compressor |
| 06/24/2014 | US8756934 Combustor cap assembly |
| 06/24/2014 | US8756909 Aircraft engine protection device |
| 06/24/2014 | US8756908 Fundamental gear system architecture |
| 06/21/2014 | CA2836689A1 Combined sump service |
| 06/19/2014 | WO2014093659A1 Overmolded vane platform |
| 06/19/2014 | WO2014093290A1 Fan containment case with thermally conforming liner |
| 06/19/2014 | WO2014093054A1 Turbine hub retainer |
| 06/19/2014 | WO2014092925A1 Gas turbine engine fan blade platform seal |
| 06/19/2014 | WO2014092922A1 Gas turbine engine turbine blade leading edge tip trench cooling |
| 06/19/2014 | WO2014092909A1 Multi-piece blade for gas turbine engine |
| 06/19/2014 | WO2014092778A1 Dual filtration particle separator |
| 06/19/2014 | WO2014092777A1 Gas turbine engine with plural accessory air paths |
| 06/19/2014 | WO2014092750A1 Gas turbine engine with cooling scheme for drive gear system and pitch control |
| 06/19/2014 | WO2014092185A1 Multi-fuel-capable gas turbine combustor |
| 06/19/2014 | WO2014091599A1 Rotary fluid machine |
| 06/19/2014 | WO2014058493A3 Suction side turbine blade tip cooling |
| 06/19/2014 | WO2013162672A8 Gas turbine engine sump pressurization system |
| 06/19/2014 | WO2013122713A8 Geared turbofan engine low noise compressor rotor |
| 06/19/2014 | US20140169959 Sealing system for flanged joint |
| 06/19/2014 | US20140169943 Components with porous metal cooling and methods of manufacture |
| 06/19/2014 | US20140166255 Closure of Cooling Holes with a Filing Agent |
| 06/19/2014 | US20140165590 Turbine hub retainer |
| 06/19/2014 | US20140165589 Gas Turbine Engine With Accessory Gear Box |
| 06/19/2014 | US20140165587 System for converting gaseous fuel into liquid fuel |
| 06/19/2014 | US20140165586 Turbine start method |
| 06/19/2014 | US20140165585 Oblong Swirler Assembly for Combustors |
| 06/19/2014 | US20140165584 Cryogenic pump system for converting fuel |
| 06/19/2014 | US20140165582 Cross-flow turbine engine |
| 06/19/2014 | US20140165575 Nozzle section for a gas turbine engine |
| 06/19/2014 | US20140165572 Fuel gas heating with thermal energy storage |
| 06/19/2014 | US20140165571 Fuel circuit of a turbine engine |
| 06/19/2014 | US20140165570 Oscillating heat pipe for thermal management of gas turbine engines |
| 06/19/2014 | US20140165531 Heated rigid electrical system |
| 06/18/2014 | EP2743477A1 Heated rigid electrical system |
| 06/18/2014 | EP2743178A1 An air inlet combining a filter and a bypass device for use with a turbine engine |
| 06/18/2014 | DE102012112410A1 Industrial truck for use in explosion-proof design with internal combustion engine, which is provided with exhaust gas turbocharger that is partially closed from liquid-cooled covering having surface contact at flow-through of exhaust gases |
| 06/18/2014 | DE102012024314A1 Turbocharger for energy converter, has shaft mounted at housing by air suspension which is supplied with air for bearing shaft due to pressure difference between compressor room and turbine room and due to pressure drop over labyrinth seal |
| 06/18/2014 | DE102009046940B4 Mehrstufige Aufladegruppe, Aufladesystem und Brennkraftmaschine, jeweils mit der mehrstufigen Aufladegruppe Multi-stage supercharger, turbocharger system and the internal combustion engine, each with the multi-stage turbocharger |
| 06/18/2014 | CN203655442U 余热为动力的燃气轮机进气冷却装置 Heat-powered gas turbine inlet air cooling device |
| 06/18/2014 | CN203655441U 一种能源综合利用装置 An energy utilization device |
| 06/18/2014 | CN203655440U 涡喷发动机 Turbojet |
| 06/18/2014 | CN103867301A Remote-control internal combustion rotor engine |
| 06/18/2014 | CN102089499B One-stage stator vane cooling structure and gas turbine |