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)
09/2014
09/04/2014WO2014133778A1 Assembly with blind installation capability
09/04/2014WO2014133770A1 Gas turbine engine noise reducing nose cone
09/04/2014WO2014133713A1 Turbomachine fan clutch
09/04/2014WO2014133706A1 Edge treatment for gas turbine engine component
09/04/2014WO2014133659A1 High pressure compressor thermal management and method of assembly and cooling
09/04/2014WO2014133654A1 Multi stage air flow management
09/04/2014WO2014133639A1 Variable swirl fuel nozzle
09/04/2014WO2014133601A1 Gas turbine engine and method for operating a gas turbine engine
09/04/2014WO2014099937A8 Gas turbine engine vane embedded beam interrupt optical tip-timing probe system
09/04/2014WO2013123008A8 Gas turbine engine component with converging/diverging cooling passage
09/04/2014US20140248146 Attachment apparatus for ceramic matrix composite materials
09/04/2014US20140248136 Multifunction positioning lock washer
09/04/2014US20140248130 Seal Hook Mount Structure With Overlapped Coating
09/04/2014US20140248127 Turbine engine component with dual purpose rib
09/04/2014US20140248126 Inter-module finger seal
09/04/2014US20140248121 Aircraft power system
09/04/2014US20140248119 Bifurcated Inlet Scoop for Gas Turbine Engine
09/04/2014US20140248116 Acoustic treatment in an unducted area of a geared turbomachine
09/04/2014US20140246170 Ram air thermal management system
09/04/2014US20140245751 Passages to facilitate a secondary flow between components
09/04/2014US20140245750 Circumferentially retained fairing
09/04/2014US20140245749 Nacelle Anti-Ice Valve Utilized as Compressor Stability Bleed Valve During Starting
09/04/2014US20140245746 Combustion arrangement and method of reducing pressure fluctuations of a combustion arrangement
09/04/2014US20140245745 Fuel system of gas turbine engines
09/04/2014US20140245744 Control of gas turbine engine
09/04/2014US20140245739 Fuel system of gas turbine engines
09/04/2014US20140245738 System and method for reducing combustion dynamics
09/04/2014US20140245727 Turbine engine starting system
09/04/2014US20140245714 Turbine engine including a detonation chamber and aircraft provided with such a turbine engine
09/04/2014DE102014203498A1 Verstellbare Düseneinheit und Turbolader mit verstellbarer Geometrie Adjustable nozzle unit and a turbocharger with variable geometry
09/04/2014DE102013203521A1 Dichtungsanordnung eines Abgasturboladers, sowie Turboladerwelle für einen Abgasturbolader Seal assembly of a turbocharger and turbocharger shaft for an exhaust gas turbocharger
09/04/2014DE102006031551B4 Flammenrückschlag-Erfassungseinrichtung, Flammenrückschlag-Erfassungsverfahren und Gasturbine Flashback-detecting means, flashback detection method and gas turbine
09/04/2014DE102004056295B4 Ölversorgungsvorrichtung für ein Flugzeugtriebwerk Oil supply apparatus for an aircraft engine
09/04/2014CA2844552A1 Compressor shroud reverse bleed holes
09/03/2014EP2772619A1 Liquefied gas treatment system, control method therefor, liquefied gas carrier provided therewith, and liquefied gas storage facility provided therewith
09/03/2014EP2772616A1 Power plant
09/03/2014EP2771554A1 Gas turbine and method for guiding compressed fluid in a gas turbine
09/03/2014EP2771549A1 Gas turbine engine support strut assembly
09/03/2014EP2771174A1 Impregnation mandrel comprising a vacuum bag for the production of a gas turbine casing from composite material
09/02/2014US8821115 Seal assembly
09/02/2014US8820752 Intershaft seal with centrifugal compensation
09/02/2014US8820478 Lubricating and cooling epicyclic stepdown gearing
09/02/2014US8820344 Turbojet engine nacelle
09/02/2014US8820092 Gas turbine engine cooling system and method
09/02/2014US8820091 External cooling fluid injection system in a gas turbine engine
09/02/2014US8820088 Variable area fan nozzle with acoustic system for a gas turbine engine
09/02/2014US8820087 Method and system for controlling fuel to a dual stage nozzle
09/02/2014US8820085 Lean fuel intake gas turbine system
09/02/2014US8820047 Combustion burner
09/02/2014US8820046 Methods and systems for mitigating distortion of gas turbine shaft
09/02/2014CA2799712C Device and control method for a drive installation including at least one turbine engine, and aircraft
09/02/2014CA2643374C Calibration of optical patternator spray parameter measurements
09/02/2014CA2602141C Integrated propellant system that includes a by-pass engine
09/02/2014CA2573076C Cooling arrangement for an accessory gearbox and method of cooling
09/02/2014CA2552214C Blades for a gas turbine engine with integrated sealing plate and method
08/2014
08/28/2014WO2014130980A1 Modular instrumentation egress seal for a gas turbine engine
08/28/2014WO2014130978A1 Finned ignitor grommet for a gas turbine engine
08/28/2014WO2014130817A1 Removing non-homogeneous ice from a fuel system
08/28/2014WO2014130712A1 Air monitoring system and method
08/28/2014WO2014130662A1 Rolling element bearing configured with a gutter and one or more fluid passages
08/28/2014WO2014130650A1 Self-purging fuel injector system for a gas turbine engine
08/28/2014WO2014130528A1 Aerating fuel injector system for a gas turbine engine
08/28/2014WO2014130494A1 Gas turbine engine core utilized in both commercial and military engines
08/28/2014WO2014130332A1 Gas turbine engine having a mistuned stage
08/28/2014WO2014130244A1 Gas turbine engine airfoil platform cooling passage and core
08/28/2014WO2014130217A1 Gas turbine engine attachment structure and method therefor
08/28/2014WO2014130214A1 Stator vane assembly and method therefore
08/28/2014WO2014130148A1 Combined cycle power plant
08/28/2014WO2014130121A1 Shaft displacement control
08/28/2014WO2014130117A2 Turbine engine assembly and dual fuel aircraft system
08/28/2014WO2014130102A1 Distributed spark ignition system for a combustor
08/28/2014WO2014130101A2 Gas turbine engine combustor heat exchanger
08/28/2014WO2014128124A1 Gas turbine with fuel composition control
08/28/2014WO2014128112A1 Gas turbine with fuel composition control
08/28/2014WO2014099082A3 Turbine blade root profile
08/28/2014WO2014092834A3 High pressure rotor disk
08/28/2014WO2014084951A3 Bleed port ribs for turbomachine case
08/28/2014WO2014074199A3 Root bow geometry for airfoil shaped vane
08/28/2014WO2014074196A3 Singlet vane cluster assembly
08/28/2014WO2014055887A3 Gas turbine engine combustor liner
08/28/2014WO2014007881A3 Gas turbine engine geared architecture axial retention arrangement
08/28/2014US20140241877 Shaft sealing device and rotating machine comprising same
08/28/2014US20140241852 Methods and apparatus for measuring axial shaft displacement within gas turbine engines
08/28/2014US20140241850 Air particle separator
08/28/2014US20140238041 Combustor can temperature control system
08/28/2014US20140238040 Combined cycle power plant
08/28/2014US20140238039 System and method for operating a power plant
08/28/2014US20140238038 Gas turbine variable focus laser ignition
08/28/2014US20140238036 Fuel/air mixing system for fuel nozzle
08/28/2014US20140238033 Systems and Methods to Control Combustion Dynamic Frequencies
08/28/2014US20140238027 Thermally compliant dual wall liner for a gas turbine engine
08/28/2014US20140238026 Fuel nozzle for reducing modal coupling of combustion dynamics
08/28/2014US20140237989 Laser-ignition combustor for gas turbine engine
08/28/2014US20140237954 Particle separator
08/28/2014DE102014201732A1 Brennkraftmaschine mit flüssigkeitsgekühlter Turbine Internal combustion engine with liquid-cooled turbine
08/28/2014DE102014102584A1 Brennstoffdüse zur Reduktion der modalen Kopplung der Verbrennungsdynamik Fuel nozzle to reduce the modal coupling of the combustion dynamics
08/28/2014DE102014102213A1 Systeme und Verfahren zur Beeinflussung der Verbrennungsdynamikfrequenzen Systems and methods for influencing the combustion dynamics frequencies
08/28/2014DE102014101990A1 Regelsystem für die Brennkammerbrennstofftemperatur A control system for the combustor fuel temperature
08/28/2014DE102014101976A1 Verfahren zur Erzeugung einer mikrokanalgekühlten Komponente Method for producing a micro-channel-cooled component
08/28/2014DE102013203376A1 Brennkraftmaschine mit flüssigkeitsgekühlter Turbine Internal combustion engine with liquid-cooled turbine
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