Patents
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)
03/2014
03/27/2014US20140083113 Flow control tab for turbine section flow cavity
03/27/2014US20140083112 Cooled Combustor Liner Grommet
03/27/2014US20140083111 Gas turbine asymmetric fuel nozzle combustor
03/27/2014US20140083109 Systems and Methods For Carbon Dioxide Capture In Low Emission Combined Turbine Systems
03/27/2014US20140083107 Method for Setting a Gear Ratio of a Fan Drive Gear System of a Gas Turbine Engine
03/27/2014US20140083101 Gas turbine engine preswirler with angled holes
03/27/2014US20140083100 Gas turbine engine combustor
03/27/2014DE102013109116A1 Bauteil mit Kühlkanälen und Verfahren zur Herstellung Component with cooling channels and methods for preparing
03/27/2014DE102012217535A1 Gasturbine mit einem Wärmeflusssensor Gas turbine with a heat flux sensor
03/27/2014DE102007048527B4 Schubtriebwerk Thruster
03/27/2014DE102005057995B4 Steuerungsanlage für Brennstoffgaserwärmung und damit ausgerüstete Gasturbinen-Kraftwerkseinrichtung Control system for fuel gas heating and thus equipped gas turbine power generation facility
03/27/2014DE102004052433B4 Gasturbinen-Regelungsvorrichtung, Gasturbinensystem und Gasturbinen-Regelungsverfahren Gas turbine control device, gas turbine and gas turbine system control method
03/26/2014EP2711506A1 Infrared suppressing exhaust system
03/26/2014EP2711505A1 Auxiliary transmission device
03/26/2014EP2711502A1 Turbine stator vane
03/26/2014EP2710245A1 Method for rationalising a chain of electric components of an aircraft, implementation architecture and corresponding aircraft
03/26/2014EP2710227A1 A gas turbine system and corresponding method for assembling this system
03/26/2014CN203499854U Engine fuel supply system
03/26/2014CN203499823U Brush type sealing device
03/26/2014CN203499822U Thermal insulation device of gas turbine supporting system
03/26/2014CN203499821U Air blocking prevention structure of hollow pump shaft
03/26/2014CN103688037A Apparatus and method for controlling a pressure gain combustor
03/26/2014CN103687932A Carbon dioxide membrane separation system in coal gasification process, and coal gasification combined cycle power generation facility using same
03/26/2014CN103670719A Turbine observation hole sealing device
03/26/2014CN103670718A Electric starting control method and device for gas turbine
03/26/2014CN103670717A Antirotated piston rack
03/26/2014CN103670716A Minimum pressure shut-off valve
03/26/2014CN103670715A By-pass valve of filter
03/26/2014CN103670712A Power generation system of combustion gas turbine
03/26/2014CN103662087A Hypersonic aerocraft and air inlet internal and external waverider integrated design method
03/25/2014USRE44815 System and method for chilling inlet air for gas turbines
03/25/2014US8678814 Control system of an internal combustion engine
03/25/2014US8678772 Intake cone for a gas-turbine engine
03/25/2014US8677766 Radial pre-swirl assembly and cooling fluid metering structure for a gas turbine engine
03/25/2014US8677765 Gas-turbine combustion chamber with a holding mechanism for a seal for an attachment
03/25/2014US8677763 Method and apparatus for gas turbine engine temperature management
03/25/2014US8677760 Fuel nozzle with integrated passages and method of operation
03/25/2014US8677757 Combustion chamber head of a gas turbine
03/25/2014US8677755 Method for controlling thermal effluents generated by an aircraft and cooling device for an aircraft implementing said method
03/25/2014US8677754 Fuel supply system for a gas-turbine engine
03/25/2014US8677729 System for heating a fuel
03/25/2014CA2828414A1 Gearbox positioning device
03/20/2014WO2014043567A1 Interwoven channels for internal cooling of airfoil
03/20/2014WO2014043537A1 Light weight swirler for gas turbine engine combustor and a method of manufacturing
03/20/2014WO2014043493A1 Improved fan case drainage system
03/20/2014WO2014042996A1 Hard lead egress adapter for an instrumentation component
03/20/2014WO2014042975A1 Hollow fan blade with honeycomb filler
03/20/2014WO2014042956A1 Turbine airfoil platform rail with gusset
03/20/2014WO2014042955A1 Gas turbine engine serpentine cooling passage
03/20/2014WO2014042699A1 Axial non-contact seal
03/20/2014WO2014041855A1 Collector and gas turbine plant provided with same
03/20/2014WO2014041297A1 Method for mounting an acoustic panel in a housing of a turbomachine and turbomachine comprising an acoustic panel
03/20/2014WO2014041291A1 Device and method for supplying non-propulsive power for an aircraft
03/20/2014WO2014040672A1 Air inlet system for a stationary internal combustion engine, in particular for a stationary gas turbine
03/20/2014WO2014022046A3 Heat exchanger for an intercooler and water extraction apparatus
03/20/2014WO2014011265A3 Gas turbine fuel nozzle end cover using au-ni braze and method producing same
03/20/2014WO2014011245A3 Planetary gear system arrangement with auxiliary oil system
03/20/2014WO2014011244A3 Non-combustion energy source and configuration for brayton cycle heat engines
03/20/2014WO2014007902A3 Tie shaft arrangement for turbomachine
03/20/2014WO2014007880A3 Reverse core gear turbofan
03/20/2014WO2013038085A3 Method for monitoring the volumetric efficiency of an hp pump of a turbomachine hydraulic regulation system
03/20/2014WO2012003471A3 Improved multi-spool intercooled recuperated gas turbine
03/20/2014US20140079546 Gas turbine engine front center body architecture
03/20/2014US20140077039 Heated Screen For Air Intake Of Aircraft Engines
03/20/2014US20140075957 Formed gussets for brackets on gas turbine engines
03/20/2014US20140075954 Methods And Systems For Substance Profile Measurements In Gas Turbine Exhaust
03/20/2014US20140075952 Method for the elimination of rotational stall in a turbine engine
03/20/2014US20140075951 Mid-turbine frame buffer system
03/20/2014US20140075950 Minimum pressure shut-off valve
03/20/2014US20140075948 Fire Seal
03/20/2014US20140075916 Method and device for supplying a lubricant
03/20/2014DE112012002595T5 Phasen- und Amplitudenangepasster Treibstoffinjektor Phase and amplitude Adjusted fuel injector
03/20/2014DE102013108984A1 Kühlung einer Turbinenlaufschaufelplattform Cooling a turbine bucket platform
03/20/2014DE102012018603A1 Hilfsgerätegetriebevorrichtung Accessory gearbox device
03/20/2014DE102006031330B4 Für Eis empfänglicher Abschnitt eines Flugzeugs, insbesondere Flugtriebwerk- Zelleneinlasslippe, umfassend ein Eisschutzsystem, Flugtriebwerk mit einer solchen Einlasslippe sowie ein Verfahren zum Schutz einer solchen Einlasslippe vor Vereisung For ice receptive portion of an aircraft, in particular Flugtriebwerk- cells inlet lip comprising an ice protection, aircraft engine with such inlet lip and a method for protection of such intake lip before icing
03/19/2014EP2708720A2 Gas turbine and operating method thereof
03/19/2014EP2708703A2 Mounting device and method of assembling the same
03/19/2014EP2708702A2 Pressurization of Generator
03/19/2014EP2708701A2 Air cooling design for tail-cone generator installation
03/19/2014EP2708272A1 Inlet particle separator systems
03/19/2014CN103649478A Hydraulic bearing for a stationary gas turbine
03/19/2014CN103649472A Improved housing for the accessory relay of a gas turbine
03/19/2014CN103649471A Method for starting a turbomachine that reduces the thermal imbalance
03/19/2014CN103644032A System for heating natural gas through gradient utilization of water supplied at medium pressure from waste heat boiler of gas turbine power plant
03/19/2014CN102472168B Structure for gas turbine casing
03/19/2014CN102287269B Electric starter for small turbine engine
03/19/2014CN102159795B Method and system for lubricating turbine engine
03/19/2014CN102016235B Gas turbine blade and gas turbine equipped with the same
03/19/2014CN101463765B Turbine control system
03/18/2014US8672095 Method and system for lubricating a turbine engine
03/18/2014US8671696 Method and apparatus for increasing thrust or other useful energy output of a device with a rotating element
03/18/2014US8671690 Combustor of gas turbine
03/18/2014CA2707267C Spray system, power augmentation system for engine containing spray system and method of humidifying air
03/18/2014CA2367612C Acoustic board with an improved composite structure
03/14/2014CA2826301A1 Pressurization of generator
03/14/2014CA2809356A1 Air cooling design for tail-cone generator installation
03/13/2014WO2014039934A1 Sensor and tooth arrangement for shaft speed detection
03/13/2014WO2014039826A1 Gas turbine engine compressor undercut spacer
03/13/2014WO2014039315A1 Method for operating a gas turbine engine including a combustor shell air recirculation system
03/13/2014WO2014039288A1 Combustor shell air recirculation system in a gas turbine engine
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