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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10/07/2014 | US8850825 Generating power using an ion transport membrane |
10/07/2014 | US8850820 Burner |
10/07/2014 | US8850818 Systems and methods for gas fuel delivery with hydrocarbon removal utilizing active pressure control and dew point analysis |
10/07/2014 | US8850793 Turbine section of high bypass turbofan |
10/07/2014 | US8850790 Gas turbine engine speed control system and method during maximum fuel flow |
10/07/2014 | US8850789 Systems and methods for power generation with exhaust gas recirculation |
10/07/2014 | US8850787 Hybrid thermal power generation system and method of constructing same |
10/02/2014 | WO2014160953A1 Movable air seal for gas turbine engine |
10/02/2014 | WO2014160851A1 Rear bearing sleeve for gas turbine auxiliary power unit |
10/02/2014 | WO2014160695A1 Gas turbine component manufacturing |
10/02/2014 | WO2014160641A1 Rotor blade with l-shaped feather seal |
10/02/2014 | WO2014160565A1 Turbine engine and turbine engine component with improved cooling pedestals |
10/02/2014 | WO2014160299A1 Combustor panel with increased durability |
10/02/2014 | WO2014160215A1 Rotor blade with a conic spline fillet at an intersection between a platform and a neck |
10/02/2014 | WO2014159800A1 Obtuse angle chevron trip strip |
10/02/2014 | WO2014159641A1 Rear mounted wash manifold retention system |
10/02/2014 | WO2014159635A1 Turbine blade with a pin seal slot |
10/02/2014 | WO2014159589A1 Gas turbine engine component cooling with interleaved facing trip strips |
10/02/2014 | WO2014159575A1 Gas turbine engine multi-vaned stator cooling configuration |
10/02/2014 | WO2014159525A1 Caes plant using steam injection and bottoming cycle expander |
10/02/2014 | WO2014159505A1 Gas turbine engine heat exchanger manifold |
10/02/2014 | WO2014159212A1 Gas turbine engine stator vane platform cooling |
10/02/2014 | WO2014159200A1 Gas turbine engine turbine impeller pressurization |
10/02/2014 | WO2014159152A1 Turbine blade and damper retention |
10/02/2014 | WO2014158589A1 Multi-axial brush seal |
10/02/2014 | WO2014158447A1 Fan blade dovetail and spacer |
10/02/2014 | WO2014158439A1 Flexible coupling for geared turbine engine |
10/02/2014 | WO2014158294A2 Seal assembly including a notched seal element for arranging between a stator and a rotor |
10/02/2014 | WO2014158293A2 Stator anti-rotation device |
10/02/2014 | WO2014158292A2 Wear liner spring seal |
10/02/2014 | WO2014158283A1 A subsonic shock strut |
10/02/2014 | WO2014158254A1 Fan blade damping device |
10/02/2014 | WO2014158247A1 Generator for flight vehicle |
10/02/2014 | WO2014158238A1 Intelligent integrated propulsion control system and method |
10/02/2014 | WO2014157277A1 Engine fault detection method, engine control device implementing this method, and power generation plant equipped with this device |
10/02/2014 | WO2014156961A1 Axial flow rotating machine and diffuser |
10/02/2014 | WO2014156645A1 Preheating device for gas-turbine fuel, gas-turbine plant provided therewith, and preheating method for gas-turbine fuel |
10/02/2014 | WO2014156277A1 Intake air cooling device |
10/02/2014 | WO2014155009A1 Cooling device for a turbo engine of an aircraft nacelle |
10/02/2014 | US20140291987 Engine architecture using electric machine |
10/02/2014 | US20140291418 Multi-circuit airblast fuel nozzle |
10/02/2014 | US20140291066 Air intake structure for turbojet engine nacelle |
10/02/2014 | US20140290911 Intake air cooling system |
10/02/2014 | US20140290910 Intake air cooling system |
10/02/2014 | US20140290271 Mounting arrangement |
10/02/2014 | US20140290270 Attachment pylon for a turbine engine |
10/02/2014 | US20140290269 Duct blocker seal assembly for a gas turbine engine |
10/02/2014 | US20140290268 Gas turbine engine geared architecture axial retention arrangement |
10/02/2014 | US20140290267 Power plant and method for generating electrical power |
10/02/2014 | US20140290266 Fuel and actuation system for gas turbine engine |
10/02/2014 | US20140290265 Gas turbine engine with transmission |
10/02/2014 | US20140290260 System and method for generating nitrogen from a gas turbine |
10/02/2014 | US20140290259 Combustion systems and combustion system components for rotary ramjet engines |
10/02/2014 | US20140290255 Hollow curved plate, manufacturing method of the same and combustor of gas turbine |
10/02/2014 | US20140290253 Intake air cooling system |
10/02/2014 | DE102014103622A1 System und Verfahren zur Erzeugung von Stickstoff mit einer Gasturbine System and method for the production of nitrogen at a gas turbine |
10/02/2014 | DE102014100482A1 Heißgaspfadbauteil für Turbinensystem Hot gas path components for turbine system |
10/02/2014 | DE102013005431A1 Axialströmungsmaschine Axial flow |
10/01/2014 | EP2784394A1 Combustor and gas turbine |
10/01/2014 | EP2784290A2 Mounting arrangement |
10/01/2014 | EP2784270A2 Fuel and actuation system for gas turbine engine |
10/01/2014 | EP2784267A2 A gas turbine engine cooling arrangement |
10/01/2014 | EP2783986A2 Hydraulic pump start system and method |
10/01/2014 | EP2783777A1 Drilling device and drilling method using such a drilling device |
10/01/2014 | EP2783092A1 System and method for anomaly detection |
10/01/2014 | EP2783075A1 Airfoil with cooling passages |
09/30/2014 | US8849541 Fuel delivery system |
09/30/2014 | US8845898 APU fuel filter housing scupper |
09/30/2014 | US8845819 System for reducing deposits on a compressor |
09/30/2014 | US8845489 Powerplant and a method of driving a mechanical system via said powerplant |
09/30/2014 | US8845275 Cranking pad interlock |
09/30/2014 | US8844863 Device for mechanically decoupled fastening of an aircraft component perfused by hot gas |
09/30/2014 | US8844553 Passive boundary layer bleed system for nacelle inlet airflow control |
09/30/2014 | US8844491 Laser spark plug |
09/30/2014 | US8844297 Gas turbine and method for maintaining and inspecting the same |
09/30/2014 | US8844296 Main engine start by means of an aircraft air conditioning system |
09/30/2014 | US8844295 Method for meeting a purge flow requirement for a power plant and a power plant having a purge control system |
09/30/2014 | US8844293 Fuel system for gas turbine engine |
09/30/2014 | US8844292 Fuel system of gas turbine engines |
09/30/2014 | US8844289 System and method of cooling turbines |
09/30/2014 | US8844265 Turbine section of high bypass turbofan |
09/30/2014 | US8844263 Aircraft turbine engine and use of such a turbine engine |
09/30/2014 | US8844258 Systems and methods for de-icing a gas turbine engine inlet screen and dehumidifying inlet air filters |
09/30/2014 | US8844257 Bypass arrangement of a lubrication valve for a gas turbine engine gear assembly |
09/30/2014 | CA2752426C Cmc turbine stator blade |
09/30/2014 | CA2621837C Aircraft engine oil removal system |
09/30/2014 | CA2618007C A method for operating a gas turbine and a gas turbine for implementing the method |
09/30/2014 | CA2533040C Heat shield for a fuel manifold and method |
09/25/2014 | WO2014152875A1 Gas turbine engine architecture with nested concentric combustor |
09/25/2014 | WO2014152870A1 Turbine cap for turbo-molecular pump |
09/25/2014 | WO2014152636A1 Selective coating removal or masking for ground path |
09/25/2014 | WO2014152619A1 Brass alloys for use in turbocharger bearing applications |
09/25/2014 | WO2014152414A1 Gas turbine engine rotor disk-seal arrangement |
09/25/2014 | WO2014152390A1 Bearing assembly with lubricant/coolant passages |
09/25/2014 | WO2014152300A1 Shield for arranging between a bearing and a rotating seal element |
09/25/2014 | WO2014152244A1 Eccentrically bored sleeve for locating a bearing |
09/25/2014 | WO2014152209A1 Assembly for sealing a gap between components of a turbine engine |
09/25/2014 | WO2014152167A1 Rolling element bearing configured with a channel and one or more fluid passages |
09/25/2014 | WO2014152123A1 Heatshield discourager seal for a gas turbine engine |
09/25/2014 | WO2014152111A1 Triple flange arrangement for a gas turbine engine |