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)
05/2012
05/10/2012US20120111023 Supporting structure for a gas turbine engine
05/10/2012US20120111022 Combined air turbine starter, air-oil cooler, and fan
05/10/2012US20120111019 System and method for combustion dynamics control by acoustic control/cancellation of fuel flow fluctuation at fuel injection location
05/10/2012US20120111016 End-fed liquid fuel gallery for a gas turbine fuel injector
05/10/2012US20120111015 Self-oscillating fuel injection jets
05/10/2012US20120111014 Low calorific fuel combustor for gas turbine
05/10/2012US20120111013 System for directing air flow in a fuel nozzle assembly
05/10/2012US20120110975 Igniter with integral pressure sensing line
05/10/2012DE102011055109A1 Anlage zum Lenken des Luftstroms in einer Kraftstoffdüsenanordnung System for directing the air flow in a fuel nozzle assembly
05/10/2012DE102011055024A1 System und Verfahren zur Verbrennungsdynamiksteuerung durch akustische Steuerung/Unterdrückung von Brennstoffdurchflussschwankungen an einer Brennstoffeinspritzstelle System and method for controlling combustion dynamics by acoustic control / suppression of fuel flow fluctuations to a fuel injection point
05/10/2012CA2815962A1 Ammonia injection device
05/09/2012EP2450550A2 Air turbine starter assembly
05/09/2012EP2450531A1 Cooling of an axial compressor
05/09/2012EP2449231A2 Method of operating a heated guide vane assembly
05/09/2012EP2449228A2 Method for operating a power plant using a gas turbine system
05/09/2012EP2449217A1 Heated guide vane
05/09/2012CN202215437U Integrated system with wind power generation and compressed air energy storage functions
05/09/2012CN102449288A Intake air temperature control device and a method for operating an intake air temperature control device
05/09/2012CN102449268A Turbine
05/09/2012CN102444479A Axial retention device for turbine system
05/09/2012CN102444478A System and method for turbine compartment ventilation
05/09/2012CN102444477A Inducer for gas turbine system
05/09/2012CN102444476A Wave-shaped diffuser of gas turbine
05/09/2012CN102444475A Gas turbine tail nozzle residual oil recovery device
05/09/2012CN102441303A Filtration system and method of design
05/09/2012CN101705871B Gas fuel regulating valve of combustion gas turbine
05/08/2012US8171739 Internally mounted fuel manifold with support pins
05/08/2012US8171719 Igniter assembly for a gas turbine
05/08/2012US8171718 Methods and systems involving carbon sequestration and engines
05/08/2012CA2554956C Movement system for the inspection of a turbine
05/03/2012WO2012058282A1 Engine-load connection strategy
05/03/2012WO2012058277A1 Utilizing heat discarded from a gas turbine engine
05/03/2012WO2012057994A2 Gas turbine combustor with mounting for helmholtz resonators
05/03/2012WO2012057282A1 Gas turbine and gas turbine plant provided with same
05/03/2012WO2012057204A1 Shaft seal mechanism and rotary machine provided with same
05/03/2012WO2011089169A3 Method for using energy temporarily present in a power grid and exceeding the instantaneous power load
05/03/2012WO2009148682A3 Fuel distributor and method of manufacturing
05/03/2012WO2009148680A3 Unitary conduit for transporting fluids and method of manufacturing
05/03/2012WO2009126403A3 Swirlers and method of manufacturing
05/03/2012US20120102971 Tapered bearings
05/03/2012US20120102964 Turbomachine including a carbon dioxide (co2) concentration control system and method
05/03/2012US20120102963 Gas turbine combustor with mounting for helmholtz resonators
05/03/2012US20120102958 Late lean injection manifold
05/03/2012US20120102957 Premixing nozzle
05/03/2012US20120102912 Low cost containment ring
05/03/2012US20120102910 High Flow Eductor
05/03/2012DE102011054745A1 Verteiler zur späten Magergemischeinspritzung Distributors for late lean injection
05/03/2012DE102010049885A1 Turbo jet engine for aircraft, has static support tube concentrically supported within low pressure shaft, where front end of tube is guided into front area of engine and motor-generator-unit is arranged at front end of tube
05/02/2012EP2447508A2 Fireproof systems in aircraft engines
05/02/2012EP2447507A2 Turbomachine cooling arrangement
05/02/2012EP2447157A2 Fan case and mount ring snap fit assembly
05/02/2012EP2446131A2 Filter element support assembly, quick installation system, and methods
05/02/2012EP2134604B9 Device for de-icing the air intake of a gas turbine
05/02/2012EP1896157B1 Particle separator for a gas turbine engine
05/02/2012EP1458967B1 Gas turbine engine with offset drive
05/02/2012CN202209812U Combined cooling heating and power tri-generation system assisted by photo-thermal solar energy
05/02/2012CN202209212U Dedusting system for gas inlet screen of gas turbine
05/02/2012CN102439274A Method and device for feeding a turbine engine combustion chamber with a controlled fuel flow
05/02/2012CN102439273A System and method for operating power generation systems
05/02/2012CN102438894A Electric generator disposed on a rotating turboprop part
05/02/2012CN102434760A Enclosure for power generation system
05/02/2012CN102434289A Gas turbine engine fuel control thrust control override system
05/02/2012CN102434288A Fuel heating system
05/02/2012CN102434287A Components with conformal curved film holes and methods of manufacture
05/02/2012CN102434286A Efficient compact primary surface heat regenerator with low pressure loss
05/02/2012CN102434285A Special air bag-based axially-symmetrical deformable air inlet channel
05/02/2012CN102434282A Gas turbine circulating device with middle water spray cooling and steam reinjection
05/02/2012CN102434281A Dual-mode gas generating device and generating method
05/02/2012CN102434217A Integrated cantilever rotor structure
05/02/2012CN102431653A Plate applied to front end and air inlet part of aircraft turbine engine
05/01/2012US8168261 Process for applying a heat shielding coating system on a metallic substrate
05/01/2012US8166767 Gas turbine combustor exit duct and hp vane interface
05/01/2012CA2495979C Turbojet with fan connected to a drive shaft supported by a first and second level
05/01/2012CA2492171C Double flow turbojet engine comprising an ancillaries distribution support and the ancillaries distribution support
05/01/2012CA2486496C Device for attaching an engine under an aircraft wing
05/01/2012CA2478954C Cooled blade for gas turbine engine
05/01/2012CA2472323C Device to install and maintain electrical harnesses on a turbojet
04/2012
04/26/2012WO2012054310A2 System and method for liquid air production, power storage and power release
04/26/2012WO2012053517A1 Ni-based superalloy member having heat-resistant bond coat layer formed therein
04/26/2012WO2012052658A2 Lubricating device having a bypass valve
04/26/2012US20120098276 Dry 3-way catalytic reduction of gas turbine nox
04/26/2012US20120096869 Utilizing heat discarded from a gas turbine engine
04/26/2012US20120096867 Semi-Tubular Vane Air Swirler
04/26/2012US20120096866 Fuel nozzle for combustor
04/26/2012DE19902437B4 Verfahren und Vorrichtung zum schnellen Anfahren und zur schnellen Leistungssteigerung einer Gasturbinenanlage Method and apparatus for fast start-up and rapid increase in performance of a gas turbine plant
04/26/2012DE102011054712A1 System und Verfahren zur Kühlung einer Düse System and method for cooling a nozzle
04/26/2012DE102011054669A1 System und Verfahren zur Kühlung einer Düse System and method for cooling a nozzle
04/26/2012DE102011054667A1 System und Verfahren zur Kühlung einer Düse System and method for cooling a nozzle
04/26/2012DE102011054666A1 Kombikraftwerkssystem mit integrierter Brennstoffvergasung, das eine stickstoffgekühlte Gasturbine aufweist Combined cycle power plant system with integrated gasification fuel having a nitrogen-cooled gas turbine
04/26/2012DE102010060152A1 Verschleißschutzbeschichtung Wear-resistant coating
04/26/2012DE102010049541A1 Moving blade for turbomachine, particularly for gas turbine, comprises cooling hole which is provided for guiding cooling air to moving blade, where valve device is partially arranged in cooling hole
04/26/2012DE102010042707A1 Turbine component for, e.g. gas turbine used in gas-fired power plant, comprises end hole formed perpendicular to guide bore which is formed vertical to edge portion to form breaking point between inner wall of guide bore and flat side
04/26/2012DE102010042104A1 Supercharger for combustion engine, has compressor housing comprising coolant channel that is integrated into coolant circuit and extended tangentially and radially around compressor screw arranged radially around compressor wheel
04/26/2012CA2815003A1 System and method for liquid air production, power storage and power release
04/26/2012CA2813923A1 Lubricating device having a bypass valve
04/25/2012EP2444701A1 Shaft seal device
04/25/2012EP2444699A1 Shaft seal and rotary machine with same
04/25/2012EP2444633A2 Drive shaft, in particular radial shaft for a gas turbine engine, with fibre compound layers
04/25/2012EP2444630A1 Solar thermal gas turbine power plant
04/25/2012EP2444508A1 FERRITIC Cr-STEEL FOR HEAT-RESISTANT PRECISION COMPONENT AND METHOD FOR PRODUCING SAME, AND HEAT-RESISTANT PRECISION COMPONENT AND METHOD FOR PRODUCING SAME
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