| 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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| 03/31/2009 | US7509794 Waste heat steam generator |
| 03/31/2009 | US7509793 Fluid system |
| 03/31/2009 | US7509734 Repairing turbine element |
| 03/28/2009 | CA2636340A1 Reduced pressure load finger seal assembly |
| 03/26/2009 | WO2009036970A2 Hydraulic drive, hydraulic supply device, airplane with a hydraulic supply device and method for configuring a hydraulic supply device |
| 03/26/2009 | WO2008139096A3 Helicopter turboshaft engine comprising a gas generator and a free turbine |
| 03/26/2009 | WO2007120185A3 Gas turbine engine mixing duct and method to start the engine |
| 03/26/2009 | US20090081027 Seal in gas turbine |
| 03/26/2009 | US20090081025 Segmented cooling air cavity for turbine component |
| 03/26/2009 | US20090081024 Turbine blade |
| 03/26/2009 | US20090077979 Residual steam removal mechanism and residual steam removal method for steam cooling piping of gas turbine |
| 03/26/2009 | US20090077977 Combustion chamber of a turbomachine |
| 03/26/2009 | US20090077973 Gas Turbine Fuel System for High Altitude Starting and Operation |
| 03/26/2009 | US20090077943 Gas turbine power plant |
| 03/26/2009 | DE102007043585A1 Turbocharger arrangement for internal-combustion engine, has turbochargers with turbine housings arranged in turbines, where pressure side of one turbocharger is connected gas-prominently with annular gap of other turbocharger |
| 03/26/2009 | CA2699693A1 A hydraulic drive, a hydraulic supply device, an aircraft comprising a hydraulic supply device, as well as a method for configuring a hydraulic supply device |
| 03/25/2009 | EP2038875A2 Sliding element in the form of an acoustic cushion for soundproofing power turbines |
| 03/25/2009 | EP2038534A1 Turbine engine for aircraft |
| 03/25/2009 | EP2038533A2 Turbine engine for aircraft |
| 03/25/2009 | EP2038532A1 Air intake for an aircraft turbine engine |
| 03/25/2009 | EP2038518A2 Arrangement for fixing a turbocompressor to a combustion engine of a motor vehicle |
| 03/25/2009 | EP2038517A2 Method for operating a gas turbine and gas turbine for carrying out said method |
| 03/25/2009 | EP1340071B1 A method for chromatographic fingerprinting and standardization of single medicines and formulations |
| 03/25/2009 | CN101392687A Cooling circuit for enhancing turbine performance |
| 03/25/2009 | CN101392686A Internal waverider hypersonic inlet and design method for giving attention to internal and external flow performance |
| 03/25/2009 | CN101392685A Internal waverider hypersonic inlet and design method based on random shock form |
| 03/25/2009 | CN101392662A Oil pipe filter for steam turbine and gas turbine |
| 03/25/2009 | CN100472055C Methods and apparatus for assembling gas turbine engines |
| 03/25/2009 | CN100472047C Methods for tuning fuel injection assemblies for a gas turbine fuel nozzle |
| 03/25/2009 | CN100472046C Link device between an enclosure for passing cooling air and a stator nozzle in a turbomachine |
| 03/25/2009 | CN100472045C Link device between an enclosure for passing cooling air and a stator nozzle in a turbomachine |
| 03/25/2009 | CN100472044C Method and device of heat exchanging |
| 03/25/2009 | CA2640040A1 Gear assembly system |
| 03/24/2009 | US7507306 An Fe Ni Cr alloy formulated to contain a strengthening phase that is able to maintain a fine grain structure during forging and high temperature processing of the alloy. The alloy contains a sufficient amount of titanium, zirconium, carbon and nitrogen so that fine titanium and zirconium carbonitride |
| 03/24/2009 | US7506838 Air intake structure for aircraft engine |
| 03/24/2009 | US7506517 System and method for turbine engine startup profile characterization |
| 03/24/2009 | US7506516 Concentric catalytic combustor |
| 03/24/2009 | US7506515 Method for regulating fuel flow into a turbine |
| 03/24/2009 | US7506510 System and method for cooling a staged airblast fuel injector |
| 03/24/2009 | US7506499 Turbofan jet engine with ancillaries distribution support |
| 03/24/2009 | CA2639975A1 Injection system arrangement in the base of a combustion chamber of an aircraft engine |
| 03/24/2009 | CA2639627A1 Seal in gas turbine |
| 03/24/2009 | CA2635565A1 Flexible fitting for rigid tubing assembly |
| 03/24/2009 | CA2331748C A device for the supply of a liquid fuel to a burner member |
| 03/21/2009 | CA2767297A1 Generator for gas turbine engine having main dc bus accessory ac bus |
| 03/19/2009 | WO2009035487A1 Wavy cmc wall hybrid ceramic apparatus |
| 03/19/2009 | WO2009034629A1 Intake silencer for gas turbine |
| 03/19/2009 | WO2009033579A2 Device for transporting air in a drive system of a vehicle and fuel cell system comprising a device of this type |
| 03/19/2009 | US20090074638 Feed injector cooling apparatus and method of assembly |
| 03/19/2009 | US20090074565 Turbine engine with differential gear driven fan and compressor |
| 03/19/2009 | US20090074563 Seal for gas turbine engine component |
| 03/19/2009 | US20090074562 Nozzle guide vanes |
| 03/19/2009 | US20090072497 Seal structure for gas turbine combustor |
| 03/19/2009 | US20090072047 Aircraft defense system and method |
| 03/19/2009 | US20090071167 Turbomachine, especially gas turbine |
| 03/19/2009 | US20090071161 Combustors and combustion systems for gas turbine engines |
| 03/19/2009 | US20090071160 Wavy CMC Wall Hybrid Ceramic Apparatus |
| 03/19/2009 | US20090071159 Secondary Fuel Delivery System |
| 03/19/2009 | US20090071158 Fuel injector for injecting fuel into a turbomachine combustion chamber |
| 03/19/2009 | US20090071121 Counter-rotating gearbox for tip turbine engine |
| 03/19/2009 | US20090071119 Method and system for protecting gas turbine fuel injectors |
| 03/19/2009 | DE102008044495A1 Kühlkreis zur Verbesserung der Turbinenleistung Cooling circuit to improve turbine performance |
| 03/19/2009 | DE102007043626A1 Gasturbinenmagerbrenner mit Kraftstoffdüse mit kontrollierter Kraftstoffinhomogenität Gas turbine lean burner with fuel nozzle with controlled fuel |
| 03/18/2009 | EP2037081A1 Platform cooling structure of gas turbine rotor blade |
| 03/18/2009 | EP1825170B1 Gearbox lubrication supply system for a tip turbine engine |
| 03/18/2009 | CN101389841A Integration of a starter/generator module in a gas turbine transmission housing |
| 03/18/2009 | CN100470041C Turbojet engine structure with two fans at the front |
| 03/17/2009 | US7503748 Mounting arrangement for turbine blades |
| 03/17/2009 | US7503178 Thermal power plant with sequential combustion and reduced-CO2 emission, and a method for operating a plant of this type |
| 03/17/2009 | US7503164 Ducted fan with containment structure |
| 03/17/2009 | CA2422963C Methods and apparatus for cooling gas turbine engine nozzle assemblies |
| 03/12/2009 | WO2009031945A2 Gas turbine plant |
| 03/12/2009 | WO2009031552A1 Intake air heating control device for gas turbine |
| 03/12/2009 | WO2009030987A2 Cooling arrangement of a gas turbine air inlet |
| 03/12/2009 | WO2008128322A3 Diffuser with improved erosion resistance |
| 03/12/2009 | US20090069998 Event-driven starter controller |
| 03/12/2009 | US20090068052 Heat resisting steel, gas turbine using the steel, and components thereof |
| 03/12/2009 | US20090067999 Extended impingement cooling device and method |
| 03/12/2009 | US20090065297 Dual action inlet door and method for use thereof |
| 03/12/2009 | US20090064685 Device and method for mounting a turbine engine |
| 03/12/2009 | US20090064684 Systems Involving Inlet-Mounted Engine Controls |
| 03/12/2009 | US20090064683 Power take-off system and gas turbine engine assembly including same |
| 03/12/2009 | US20090064682 Method and system to determine composition of fuel entering combustor |
| 03/12/2009 | US20090064657 Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters |
| 03/12/2009 | US20090064644 Single/multiple guard(s)/cap(s) and/or screen(s) with engine attached apparatus and/or pole with rotational system(s) - centrifuge chamber/manifold particle collector |
| 03/12/2009 | US20090064500 Method of repairing a turbine engine component |
| 03/12/2009 | DE202008015934U1 Triebwerk Frontschutzabdeckung Engine Front cover |
| 03/12/2009 | DE102008039048A1 Vorrichtung und Verfahren zur druckbeaufschlagten Eingangsverdampfungskühlung von Gasturbinen Apparatus and method for evaporative cooling of the pressurized input gas turbines |
| 03/11/2009 | EP2034159A2 Active flow control for nacelle air intake |
| 03/11/2009 | EP2032829A1 Engine exhaust system with directional nozzle |
| 03/11/2009 | EP2032828A2 Engine exhaust system |
| 03/11/2009 | EP2032822A1 Turboreactor for aircraft |
| 03/11/2009 | EP1697687B1 Method for determining fluctuating fuel properties during the operation of a power plant |
| 03/11/2009 | EP1643575B1 Fuel cell/constant pressure turbine/hybrid system |
| 03/11/2009 | EP1546527B1 Nested channel ducts for nozzle construction and the like |
| 03/11/2009 | CN101382088A Apparatus and method for pressurized inlet evaporative cooling of gas turbine engines |
| 03/11/2009 | CN101382087A Apparatus and method for reducing eccentricity and out-of-roundness in turbines |
| 03/11/2009 | CN100467200C Method for repairing curved section of nozzle guide device |
| 03/10/2009 | USRE40658 Methods and apparatus for cooling gas turbine nozzles |
| 03/10/2009 | US7500644 Device for maintaining and positioning harnesses on a turbo-jet engine |