| 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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| 01/19/2011 | CN101952574A Thermal insulation structure for structural member, and scroll structure |
| 01/19/2011 | CN101952573A Air intake structure for an aircraft nacelle |
| 01/19/2011 | CN101952558A Fastening device for an exhaust-gas turbocharger |
| 01/19/2011 | CN101952555A Gas turbin and disc and method for forming radial passage of disc |
| 01/19/2011 | CN101952171A Aircraft propulsion assembly comprising hot air bleed systems |
| 01/18/2011 | US7871248 Airframe mounted electric motor driven lubrication pump control deoil system |
| 01/18/2011 | US7871247 aircraft engine turbine blade formed from base metal that has a high modulus crystallographic orientation that is aligned with the primary, i.e. radial, direction of the turbine blade; base metal is Ni, Fe, Ti, Co, Al, Nb, or Mo based alloy; provides enhanced high cycle fatigue life |
| 01/18/2011 | US7870717 Advanced hydrogen auxiliary power unit |
| 01/18/2011 | CA2374753C Apparatus for reducing combustor exit duct cooling |
| 01/17/2011 | CA2711175A1 Substrate features for mitigating stress |
| 01/17/2011 | CA2710053A1 Substrate features for mitigating stress |
| 01/13/2011 | WO2011005858A2 Compressor cooling for turbine engines |
| 01/13/2011 | WO2011005438A2 Filter element support assembly, quick installation system, and methods |
| 01/13/2011 | WO2011004565A1 Bearing device, bearing unit, and rotary machine |
| 01/13/2011 | WO2011004069A1 A gas filtering device and a method of manufaturing a gas filtering device |
| 01/13/2011 | WO2010111357A3 High-flow-capacity centrifugal hydrogen gas compression systems, methods and components therefor |
| 01/13/2011 | US20110005234 Connection structure of exhaust chamber, support structure of turbine, and gas turbine |
| 01/13/2011 | US20110005232 Aerodynamic swept vanes for fuel injectors |
| 01/13/2011 | US20110005231 Fuel nozzle guide plate mistake proofing |
| 01/13/2011 | US20110005230 Fuel nozzle assembly for a gas turbine engine |
| 01/13/2011 | US20110005229 Lean direct injection for premixed pilot application |
| 01/13/2011 | DE10217399B4 Flugzeugturbine mit einer Vorrichtung zum sicheren Abschalten trotz Einwirken einer großen Unwucht des Laufrades Aircraft turbine with a device for safe disconnection, despite the action of a large unbalance of the impeller |
| 01/13/2011 | DE102010017643A1 Brennstoffdüsenanordnung für einen Gasturbinenmotor Fuel nozzle assembly for a gas turbine engine |
| 01/13/2011 | DE102010017627A1 Abstimmbares Fluiddurchflusssteuersystem A tunable fluid flow control system |
| 01/13/2011 | DE102010017434A1 Einrichtung und Verfahren zum Testen eines Verdichters Apparatus and method for testing a compressor |
| 01/13/2011 | DE102010016547A1 Injektor mit integriertem Resonator Injector with integrated resonator |
| 01/13/2011 | DE102009038736B3 Turbine und Turboverdichter, insbesondere für ein Turbo-Compound-System Turbine and turbo compressor, particularly for a turbo-compound system |
| 01/13/2011 | DE102009032685A1 Vormontierte Ventilbaugruppe zur Verwendung in einem Turbolader Preassembled valve assembly for use in a turbocharger |
| 01/13/2011 | DE102009032306A1 Bearing house for turbo-machine, has insert piece i.e. circular disk, arranged at house in region of contact areas of blades, and consisting of material with higher abrasion resistance than material of house |
| 01/13/2011 | DE102009031787A1 Turbocharger for internal-combustion engine of motor vehicle, has cover band arranged at turbine wheel such that band is fixedly connected with free ends of turbine blades, and turbine and band integrally designed |
| 01/12/2011 | EP2273088A1 Adaptive heat sink for thermal management systems |
| 01/12/2011 | EP2273075A2 Method and apparatus for monitoring debris in a gas turbine engine |
| 01/12/2011 | EP2271843A1 Fluid intake assembly |
| 01/12/2011 | EP1428001B1 Method and apparatus for model based estimation of natural frequency responses of tube sub-systems including shrouded bellows |
| 01/12/2011 | CN101946073A Gas turbine |
| 01/12/2011 | CN101946072A Gas turbine, and interior opening method for the gas turbine |
| 01/12/2011 | CN101945808A Aircraft engine assembly comprising downwardly offset engine mounts on the fan casing |
| 01/12/2011 | CN101338702B Pulse knock rotor spindle engine |
| 01/11/2011 | US7866939 Liner for a gas turbine engine casing |
| 01/11/2011 | US7866162 Exhaust cone for channeling a stream of gas downstream from a turbine |
| 01/11/2011 | US7866161 Method of operating a gas engine plant and fuel feeding system for a gas engine |
| 01/11/2011 | CA2512973C Intake housing for axial fluid flow engines |
| 01/11/2011 | CA2442460C Method for selective surface protection of a gas turbine blade which has previously been in service |
| 01/11/2011 | CA2430153C Process and system for detecting aircraft engine rotor damage |
| 01/11/2011 | CA2416150C Diffuser for terrestrial or aeronautic gas turbine engines |
| 01/11/2011 | CA2412898C Connecting system for a transition duct in a gas turbine |
| 01/11/2011 | CA2405335C Gas turbine engine compressor blade restoration |
| 01/06/2011 | WO2011000548A2 Method for operating a power plant using a gas turbine system |
| 01/06/2011 | WO2010124698A8 The silenced aspirator anergy amplified/driven air compressor/turbine |
| 01/06/2011 | WO2010099535A3 Liquid-gas heat exchanger |
| 01/06/2011 | WO2010099193A3 Improved air riding seal |
| 01/06/2011 | WO2009150069A3 Combustion chamber device, and method for the operation of a combustion chamber device |
| 01/06/2011 | US20110004390 Gas turbine control method and device |
| 01/06/2011 | US20110001324 System and Method for Gas Turbine Chilled Water Storage Discharge Control and/or Gas Turbine Output Control |
| 01/06/2011 | US20110001003 Filtering device with integrated bypass for an air inlet |
| 01/06/2011 | US20110000666 Vitiated Steam Generator |
| 01/06/2011 | US20110000223 gas turbine component and a method for producing a gas turbine component |
| 01/06/2011 | US20110000222 Gas turbine rotor-stator support system |
| 01/06/2011 | US20110000221 Low Emission Power Generation and Hydrocarbon Recovery Systems and Methods |
| 01/06/2011 | US20110000220 Power generation system having an exhaust attemperating device and method for controlling a temperature of exhaust gases |
| 01/06/2011 | US20110000219 Method and apparatus for actively controlling fuel flow to a mixer assembly of a gas turbine engine combustor |
| 01/06/2011 | US20110000218 Gas turbine and method of opening chamber of gas turbine |
| 01/06/2011 | US20110000216 Gas turbine combustor |
| 01/06/2011 | US20110000215 Combustor Can Flow Conditioner |
| 01/06/2011 | US20110000214 Methods and systems to thermally protect fuel nozzles in combustion systems |
| 01/06/2011 | US20110000183 Assembly providing contaminant removal |
| 01/05/2011 | EP2270323A2 Clutched steam turbine low pressure sections and methods therefore |
| 01/05/2011 | EP2270322A1 Cooling circuit for removing waste heat from an electromechanical convertor and power plant assembly with such a cooling circuit |
| 01/05/2011 | EP2270315A2 Aircraft gas turbine engine counter-rotatable generator |
| 01/05/2011 | EP2102060B1 Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
| 01/05/2011 | DE19926949B4 Kühlungsanordnung für Schaufeln einer Gasturbine Cooling arrangement for a gas turbine blades |
| 01/05/2011 | DE102009031843A1 Verfahren zum Betrieb eines Kraftwerks mit einer Gasturbinenanlage Method for operating a power plant with a gas turbine plant |
| 01/05/2011 | CN101939539A Engine-driven hydraulic pump |
| 01/05/2011 | CN101936220A System and method of cooling turbine airfoils with sequestered carbon dioxide |
| 01/05/2011 | CN101936219A Power augmentation system for engine and method of humidifying air |
| 01/04/2011 | US7861536 Ejector controlled twin air source gas turbine pressurizing air system |
| 01/04/2011 | US7861535 Self-aligning liner support hanger |
| 01/04/2011 | US7861534 Method of starting turbine engine from low engine speed |
| 01/04/2011 | US7861533 Relighting a turbofan engine |
| 01/04/2011 | US7861529 Device for injecting a mixture of air and fuel, and combustion chamber and turbomachine both equipped with such a device |
| 01/04/2011 | US7861510 Ceramic regenerator for a gas turbine engine |
| 01/04/2011 | CA2481111C Process of masking cooling holes of a gas turbine component |
| 12/30/2010 | US20100332103 NOX Compliant Peak for Gas Turbine |
| 12/30/2010 | US20100329843 Panel for supporting abradable material in a turbomachine |
| 12/30/2010 | US20100329835 Airfoil with hybrid drilled and cutback trailing edge |
| 12/30/2010 | US20100327588 Gas turbine with magnetic shaft forming part of a generator/motor assembly |
| 12/30/2010 | US20100326089 Method and systems for bleed air supply |
| 12/30/2010 | US20100326086 Method and system for enhancing start of a turbine engine, and ignition module |
| 12/30/2010 | US20100326085 Lightweight start system for a gas turbine engine |
| 12/30/2010 | US20100326083 Spray system, power augmentation system for engine containing spray system and method of humidifying air |
| 12/30/2010 | US20100326082 Methods and apparatus for combustor fuel circuit for ultra low calorific fuels |
| 12/30/2010 | US20100326080 Acoustically Tuned Combustion for a Gas Turbine Engine |
| 12/30/2010 | US20100326079 Method and system to reduce vane swirl angle in a gas turbine engine |
| 12/30/2010 | US20100326078 Turbomachine combustion chamber |
| 12/30/2010 | US20100326077 System for mitigating a fuel system transient |
| 12/30/2010 | US20100326041 Heated guide vane |
| 12/30/2010 | DE102010017284A1 System und Verfahren zur Erwärmung von Turbinenbrennstoff in einem Einfachzyklus-Kraftwerk System and method for heating turbine fuel in a simple cycle power plant, |
| 12/30/2010 | CA2707943A1 Aircraft gas turbine engine counter-rotatable generator |
| 12/29/2010 | EP2267369A1 Cooling structure for gas turbine combustor |
| 12/29/2010 | EP2267290A2 A clamping assembly |