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)
03/2012
03/15/2012WO2012032273A1 Propulsion system for a flying machine, particularly for a missile
03/15/2012WO2012031783A2 Method and apparatus for cooling a gaseous hydrocarbon stream
03/15/2012WO2012031782A1 Method and apparatus for cooling a gaseous hydrocarbon stream
03/15/2012US20120060511 Apparatus and method for cooling a combustor cap
03/15/2012US20120060510 Hot gas temperature measurement in gas turbine using tunable diode laser
03/15/2012US20120060508 Gas turbine engine breather exhaust oil collector
03/15/2012US20120060507 Gas turbine engine
03/15/2012US20120060463 Oil Varnish Mitigation Systems
03/15/2012DE102011110660A1 Von Heissgasen durchströmbarer Gehäusekörper mit innerem Hitzeschild Of hot gases flowed through the valve body with inner heat shield
03/15/2012DE102011053268A1 Vorrichtung und Verfahren zum Kühlen einer Brennkammer Apparatus and method for cooling a combustion chamber
03/14/2012EP2428663A1 Methods and devices for low speed low torque testing of a rotor in a turbomachinery
03/14/2012EP2428662A2 Gas turbine engine fuel control system
03/14/2012EP2428647A1 Transitional Region for a Combustion Chamber of a Gas Turbine
03/14/2012EP2427635A1 Supporting structure for a gas turbine engine
03/14/2012EP2427634A1 A strut and a gas turbine structure comprising the strut
03/14/2012EP2427370A2 Rotor-mounted electrical generator of a propfan engine
03/14/2012EP1635955B8 Water distribution and vaporization assembly
03/14/2012CN102378855A Rotating inlet cowl for a turbine engine, including an eccentric front end
03/14/2012CN102374031A Annular injector assembly and methods of assembling the same
03/14/2012CN102374030A Contoured axial-radial exhaust diffuser
03/14/2012CN102374026A Closed cycle brayton cycle system and method
03/14/2012CN102373972A Tip flowpath contour
03/14/2012CN102373970A Air turbine starter inlet housing assembly airflow path
03/14/2012CN102373964A Combustor transition piece with dilution sleeves and related method
03/14/2012CN102373963A Air turbine starter turbine nozzle airfoil
03/14/2012CN102373960A Hub flowpath contour
03/13/2012US8132417 Cooling of a gas turbine engine downstream of combustion chamber
03/13/2012US8132398 Apparatus and method of operating a gas turbine engine at start-up
03/09/2012CA2751970A1 Methods and devices for low speed low torque testing of a rotor in a turbomachinery
03/08/2012WO2012029540A1 Heat-masking coating film, process for production thereof, and heat-resistant alloy members using the same
03/08/2012WO2012007638A3 A solution for controlling a turbo compressor
03/08/2012WO2011082949A3 Combined cycle power plant and method of operating such power plant
03/08/2012US20120058013 Model based tempering air control and enhancement of exhaust for select catalytic reduction
03/08/2012US20120055167 Apparatus and method for mixing fuel in a gas turbine nozzle
03/08/2012US20120055164 Turbomachine combustion chamber comprising improved means of air supply
03/08/2012US20120055163 Fuel injection assembly for use in turbine engines and method of assembling same
03/08/2012US20120055162 Lance of a burner
03/08/2012DE102011052932A1 Brennstoffvorwärmsystem Brennstoffvorwärmsystem
03/08/2012DE102011051366A1 Vorrichtung und Verfahren zum Mischen von Brennstoff in einer Gasturbinendüse Device and method for mixing of fuel in a gas turbine nozzle
03/07/2012EP2426452A1 Method and apparatus for cooling a gaseous hydrocarbon stream
03/07/2012EP2426342A2 Turbofan engine with variable bypass nozzle exit area and method of operation
03/07/2012EP2426338A1 Plate-shaped bodies, manufacturing method therefor, gas turbine combustor, and gas turbine
03/07/2012EP2426337A1 Device for fuel preheating and method for fuel preheating
03/07/2012EP2426320A1 Lubrication driven gas turbine engine actuation system
03/07/2012EP2426314A2 System and method of cooling turbine airfoils with carbon dioxide
03/07/2012EP2425189A2 Transcritical thermally activated cooling, heating and refrigerating system
03/07/2012EP2425109A1 Method and device for feeding a turbine engine combustion chamber with a controlled fuel flow
03/07/2012EP2425099A1 Turbine for the expansion of gas/vapour provided with axial thrust compensation on the drive shaft
03/07/2012EP2260197B1 Contra-rotating propeller system with device for feathering propeller blades
03/06/2012US8131383 Method and system for rapid modeling and verification of excitation systems for synchronous generators
03/06/2012US8127828 Air-oil heat exchanger
03/06/2012US8127546 Turbine engine fuel injector with helmholtz resonators
03/06/2012US8127526 Recoatable exhaust liner cooling arrangement
03/06/2012CA2662030C External rigid fuel manifold
03/06/2012CA2657254C Nacelle inlet lip
03/06/2012CA2570777C Internally mounted device for a gas turbine engine
03/06/2012CA2528124C Improved bearing chamber pressurization system
03/06/2012CA2481588C Process for manufacturing or repairing a monobloc bladed disc
03/06/2012CA2471665C Arrangement of bearing supports for the rotating shaft of an aircraft engine and an aircraft engine fitted with such an arrangement
03/06/2012CA2359924C Noise reduction sandwich panel, notably for aircraft turbojet engine
03/01/2012WO2012027154A2 Integral plus proportional dual pump switching system
03/01/2012WO2012026354A1 Co-based alloy
03/01/2012WO2012025967A1 Solar gas turbine system
03/01/2012WO2012025690A2 Method for mounting shielding on a turbine casing, and mounting assembly for implementing same
03/01/2012WO2012025689A1 Method for optimizing the control of a free turbine power package for an aircraft, and control for implementing same
03/01/2012WO2012025687A2 Method for optimizing the overall energy efficiency of an aircraft, and main power package for implementing same
03/01/2012US20120048390 Wrought and cast aluminum alloy with improved resistance to mechanical property degradation
03/01/2012US20120047910 Stepped inlet ring for a transition downstream from a combustor basket in a combustion turbine engine
03/01/2012US20120047909 Combustor liner concentric support and method
03/01/2012US20120047906 Combustion turbine cooling media supply method
03/01/2012US20120047905 Casing body through which hot gases can flow and comprising an inner heat shield
03/01/2012US20120047903 Staged pilots in pure airblast injectors for gas turbine engines
03/01/2012US20120047902 Fuel delivery system for a turbine engine
03/01/2012US20120047898 Premix burner for a gas turbine
03/01/2012US20120047896 Combustion device
03/01/2012CA2808588A1 Integral plus proportional dual pump switching system
03/01/2012CA2808180A1 Method for optimizing the overall energy efficiency of an aircraft, and main power package for implementing same
03/01/2012CA2807913A1 Method for mounting shielding on a turbine casing, and mounting assembly for implementing same
03/01/2012CA2807912A1 Method for optimizing the control of a free turbine power package for an aircraft, and control for implementing same
02/2012
02/29/2012EP2423489A2 Methods for controlling fuel splits to a gas turbine combustor
02/29/2012EP2423461A2 Systems Involving Hybrid Power Plants
02/29/2012EP2422126A1 Elbow support for aeronautical equipment
02/29/2012EP2422063A1 One-piece mounting for aeronautical apparatuses
02/29/2012EP2422054A1 An annular gas turbine housing component and a gas turbine comprising the component
02/29/2012EP2422050A1 Improvement of a turbine for the expansion of gas/vapour
02/29/2012CN202152703U System used for operating compressed gas fuel
02/29/2012CN202152702U 新型高压油顶升装置 The new high-pressure oil lifting device
02/29/2012CN102365487A Elbow support for aeronautical equipment
02/29/2012CN102365441A Variable actuation pressure system for independent pressure control
02/29/2012CN102365120A Filter cassette, filter arrangement, and gas turbine with such filter cassette
02/29/2012CN101772586B Ni-base alloy-high chromium steel structure and process for producing the ni-base alloy-high chromium steel structure
02/28/2012US8123821 Regulating vanadium inhibitor in a gas turbine
02/28/2012US8122727 Compliant metal support for ceramic combustor liner in a gas turbine engine
02/28/2012US8122726 Combustion chamber of a combustion system
02/28/2012US8122725 Methods and systems for operating gas turbine engines
02/28/2012US8122698 Vent for the lubricating oil system of a jet engine
02/28/2012US8122600 Fan and compressor blade dovetail restoration process
02/28/2012CA2660938C Combustor nozzle
02/28/2012CA2546881C Gas turbine engine combustor with improved cooling
02/28/2012CA2466756C Differential geared turbine engine with torque modulation capability
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