| 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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| 09/18/2014 | WO2014143218A1 Gas turbine engine and electrical system comprising electrical buses |
| 09/18/2014 | WO2014143210A1 Gas turbine engine flow duct having two rows of integrated heat exchangers |
| 09/18/2014 | WO2014143190A1 Aerodynamic fairings secondarily attached to nosecone |
| 09/18/2014 | WO2014143187A1 Lifing and performance optimization limit management for turbine engine |
| 09/18/2014 | WO2014143097A1 Circumferential seal with ceramic runner |
| 09/18/2014 | WO2014143074A1 Geared architecture with inducer for gas turbine engine |
| 09/18/2014 | WO2014142184A1 Cooling promoting structure |
| 09/18/2014 | WO2014141937A1 Opening/closing device for high-temperature gas passage |
| 09/18/2014 | WO2014141936A1 Heat-retaining duct for high-temperature gas |
| 09/18/2014 | WO2014141825A1 Combustor and gas turbine |
| 09/18/2014 | WO2014141791A1 Gas turbine silencer, and gas turbine provided with same |
| 09/18/2014 | WO2014141521A1 Method for attaching/removing stationary blade ring and auxiliary support device for stationary blade segment used in said method |
| 09/18/2014 | WO2014141509A1 Exhaust flue |
| 09/18/2014 | WO2014140483A1 Turbine engine, such as an airplane turbofan or turboprop engine |
| 09/18/2014 | WO2014140441A1 V-shaped gearbox for driving turbomachine equipment |
| 09/18/2014 | WO2014139663A1 Employing applied fuels in the composition modified for energy recovery |
| 09/18/2014 | US20140272104 Coating methods and pressurized masking systems for controlling coating microstructures |
| 09/18/2014 | US20140271135 Turbofan Engine Bearing and Gearbox Arrangement |
| 09/18/2014 | US20140271118 Gas turbine engine lubrication system |
| 09/18/2014 | US20140271116 Heat exchanger integrated with a gas turbine engine and adaptive flow control |
| 09/18/2014 | US20140271112 Low noise turbine for geared gas turbine engine |
| 09/18/2014 | US20140265161 Seals for a gas turbine engine |
| 09/18/2014 | US20140265145 Seals for a gas turbine engine |
| 09/18/2014 | US20140262046 Impregnation mandrel with vacuum liner for making a gas turbine casing made of composite material |
| 09/18/2014 | US20140260324 Turbo-machinery rotors with rounded tip edge |
| 09/18/2014 | US20140260322 Support mechanism for heavy structure |
| 09/18/2014 | US20140260321 Gas turbine engine static structure joint with undercuts |
| 09/18/2014 | US20140260320 Bi-metal fastener for thermal growth compensation |
| 09/18/2014 | US20140260318 Side seal slot for a combustion liner |
| 09/18/2014 | US20140260317 Gas turbine combustor exit piece with hinged connections |
| 09/18/2014 | US20140260315 System having multi-tube fuel nozzle with floating arrangement of mixing tubes |
| 09/18/2014 | US20140260308 Rear mounted wash manifold retention system |
| 09/18/2014 | US20140260307 Rear mounted wash manifold and process |
| 09/18/2014 | US20140260306 Engine starting system using stored energy |
| 09/18/2014 | US20140260304 Algae-derived fuel/water emulsion |
| 09/18/2014 | US20140260301 Engine manifold drain system |
| 09/18/2014 | US20140260299 Fuel-air mixing system for gas turbine system |
| 09/18/2014 | US20140260296 Slinger combustor |
| 09/18/2014 | US20140260294 Apparatus and Method for Controlling a Pressure Gain Combustor |
| 09/18/2014 | US20140260287 Gas turbine firing temperature optimization based on sulfur content of fuel supply |
| 09/18/2014 | US20140260284 System and Method for Loading a Combined Cycle Power Plant |
| 09/18/2014 | US20140260276 End cover configuration and assembly |
| 09/18/2014 | US20140260274 Fuel distribution manifold for a combustor of a gas turbine |
| 09/18/2014 | US20140260272 System for providing fuel to a combustor |
| 09/18/2014 | US20140260264 System for controlling a flow rate of a compressed working fluid to a combustor fuel injector |
| 09/18/2014 | US20140260263 Fuel injection insert for a turbine nozzle segment |
| 09/18/2014 | US20140260261 Turbomachine with transition piece having dilution holes and fuel injection system coupled to transition piece |
| 09/18/2014 | US20140260183 Variable cycle intake for reverse core engine |
| 09/18/2014 | US20140260182 Free stream intake for reverse core engine |
| 09/18/2014 | US20140260178 Aerodynamically active stiffening feature for gas turbine recuperator |
| 09/18/2014 | US20140260176 Lube tube expansion and torque retaining device |
| 09/18/2014 | US20140260127 Interchangeable inlet protection systems for air intakes of aircraft engines and related method |
| 09/18/2014 | DE112012005537T5 Verfahren und Vorrichtung für eine eingedrückte Flüssigkeitsinjektordüse Method and apparatus for a depressed Flüssigkeitsinjektordüse |
| 09/18/2014 | DE102014103087A1 System zur Zuführung von Brennstoff zu einer Brennkammer System for supplying fuel to a combustion chamber |
| 09/18/2014 | DE102014103086A1 Systeme und Verfahren zur stromabwärtigen Brennstoff- und Luftinjektion bei Gasturbinen Systems and methods for the downstream injection, fuel and air in gas turbines |
| 09/18/2014 | DE102014103083A1 System und Verfahren zur Luftkonditionierung auf Rohrniveau System and method for air conditioning to pipe level |
| 09/18/2014 | DE102014103082A1 Strömungshülse für ein Brennkammermodul für eine Gasturbine Flow sleeve on a combustor module for a gas turbine |
| 09/18/2014 | DE102014103081A1 Strömungshülsenanordnung für ein Verbrennungsmodul eines Gasturbinenbrenners Flow tube arrangement for a combustion module of a gas turbine burner |
| 09/18/2014 | DE102014103079A1 System mit einer Vielrohr-Brennstoffdüse System with a multi-tube fuel nozzle |
| 09/18/2014 | DE102014103020A1 Systeme und Vorrichtungen zur stromabwärtigen Brennstoff- und Luftinjektion bei Gasturbinen Systems and devices for the downstream fuel and air injection in gas turbines |
| 09/18/2014 | DE102014103007A1 Kühlkanäle für Turbinenschaufeln einer Gasturbine Cooling channels for turbine blades of a gas turbine |
| 09/18/2014 | DE102014103005A1 Verfahren und Vorrichtung zur Verbesserung der Wärmeübertragung in Turbinenabschnitten von Gasturbinen A method and apparatus for improving the heat transfer in the turbine sections of gas turbines |
| 09/18/2014 | DE102014102787A1 Luftdiffusor für eine Brennkammer Air diffuser for a combustion chamber |
| 09/18/2014 | DE102014102784A1 Turbomaschine mit Übergangsstück mit Verdünnungslöchern und mit Brennstoffeinspritzsystem, das mit dem Übergangsstück verbunden ist Turbo engine with transition piece with holes and dilution with fuel injection system which is connected to the transition piece |
| 09/18/2014 | DE102014102783A1 Mikromischkappenanordnung Micromixing cap assembly |
| 09/18/2014 | DE102014102782A1 Multiinjektor-Mikromischsystem Multiinjector micro-mixing system |
| 09/18/2014 | DE102014102781A1 Brennstoff-Luft-Mischsystem für ein Gasturbinensystem Fuel and air mixing system for a gas turbine system |
| 09/18/2014 | DE102014102779A1 Brennkammerendabdeckung mit Brennstoffkammern Brennkammerendabdeckung with fuel chambers |
| 09/18/2014 | DE102014102777A1 System und Verfahren mit Vielrohr-Brennstoffdüse mit mehreren Brennstoffinjektoren System and method with multi-tube fuel nozzle with multiple fuel injectors |
| 09/18/2014 | DE102013204307A1 Strahlbrenner mit Kühlkanal in der Grundplatte Ray burner with cooling channel in the base plate |
| 09/17/2014 | EP2779422A1 Series battery start controller |
| 09/17/2014 | EP2779367A2 Gas turbine engine actuation systems including high temperature actuators and methods for the manufacture thereof |
| 09/17/2014 | EP2778532A1 Combustor liner |
| 09/17/2014 | EP2778373A1 Seal assembly and gas turbine provided therewith |
| 09/17/2014 | EP2778372A2 Gas turbine engine fuel system with ecology valve |
| 09/17/2014 | EP2778371A2 Engine manifold drain system |
| 09/17/2014 | EP2778370A1 Combustor for gas turbine engine |
| 09/17/2014 | EP2778369A1 Impingement cooling mechanism, turbine blade, and combustor |
| 09/17/2014 | EP2778368A1 Combined-cycle power plant with control of the inlet air temperature and method for controlling a combined-cycle power plant |
| 09/17/2014 | EP2778344A1 Film cooling structure and turbine wing |
| 09/17/2014 | EP2778241A1 Heat-resistant nickel-based superalloy |
| 09/17/2014 | EP2778069A1 Apparatus and method for detecting obstructions in pipes or channels |
| 09/17/2014 | EP2776692A1 Power generating system and corresponding method |
| 09/16/2014 | US8838359 Starter control valve prediction system to predict and trend starter control valve failures in gas turbine engines using a starter control valve health prognostic, computer readable medium and related methods |
| 09/16/2014 | US8834649 System for reducing deposits on a compressor |
| 09/16/2014 | US8834154 Transition piece of combustor, and gas turbine having the same |
| 09/16/2014 | US8834134 Flow sensing dual pump switching system and method |
| 09/16/2014 | US8833515 Method for the production of a sound absorber, especially for a gas turbine exhaust cone |
| 09/16/2014 | US8833323 Ignition laser |
| 09/16/2014 | US8833312 External combustion engine |
| 09/16/2014 | US8833087 Flow splitter for gas turbine engine |
| 09/16/2014 | US8833086 Lubrication arrangement for a gas turbine engine gear assembly |
| 09/16/2014 | US8833085 System and method for gas turbine startup control |
| 09/16/2014 | US8833079 Method and apparatus for generating electricity |
| 09/16/2014 | US8833053 Cooling system for an aero gas turbine engine |
| 09/16/2014 | CA2623999C Two-shackle aircraft engine rear attachment |
| 09/16/2014 | CA2594139C Ventilation for a downstream cavity in a centrifugal compressor impeller |
| 09/14/2014 | CA2846520A1 Aerodynamically active stiffening feature for gas turbine recuperator |
| 09/14/2014 | CA2845185A1 Engine starting system using stored energy |
| 09/14/2014 | CA2844186A1 Gas turbine engine with transmission and method of adjusting rotational speed |