| 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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| 04/19/2005 | US6881024 System for decoupling a fan from a turbojet by means of an explosive charge |
| 04/19/2005 | US6880829 Compliant brush shroud assembly for gas turbine engine compressors |
| 04/19/2005 | US6880343 Supercharged gas turbine with improved control |
| 04/19/2005 | US6880342 Structure and method for controlling inlet shock position of a hypersonic vehicle |
| 04/19/2005 | US6880339 Combination of a premixing chamber and a combustion chamber, with low emission of pollutants, for gas turbines running on liquid and/or gas fuel |
| 04/19/2005 | US6880325 Gas turbine combustor apparatus |
| 04/19/2005 | US6880324 1-axis type combined cycle plant |
| 04/19/2005 | CA2363136C Gas turbine steam passage seal structure between blade ring and stationary blade |
| 04/19/2005 | CA2357555C Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system, and fuel nozzle wash system |
| 04/16/2005 | CA2485152A1 Refractory metal core wall thickness control |
| 04/14/2005 | US20050079464 Premix burner and method for operation thereof |
| 04/14/2005 | US20050079089 Alloy coating, method for forming the same, and member for high temperature apparatuses |
| 04/14/2005 | US20050079046 Perfected device for setting synchronizing rings of a turbojet compressor |
| 04/14/2005 | US20050076646 Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 04/14/2005 | US20050076645 Method for operating a power plant by means of a CO2 process |
| 04/14/2005 | US20050076644 Quiet combustor for a gas turbine engine |
| 04/14/2005 | US20050076642 Seal element for sealing a gap and combustion turbine having a seal element |
| 04/14/2005 | US20050076523 Methods and apparatus for securing components for inspection |
| 04/14/2005 | US20050076503 Blade for a turbine engine and method for production of said blade |
| 04/13/2005 | EP1522772A1 Turbine containing two components connected by a sealing |
| 04/13/2005 | EP1522731A2 Pump health monitoring |
| 04/13/2005 | EP1522696A2 Gas turbine axial compressor with water injection |
| 04/13/2005 | EP1522607A1 Method for fabricating a coated superalloy stabilized against the formation of secondary reaction zone |
| 04/13/2005 | EP1522535A2 Environmental barrier coating |
| 04/13/2005 | EP1522533A1 Target destined for electron beam evaporation, its process of manufacture, a thermal barrier layer obtained using the target and a workpiece comprising such a layer. |
| 04/13/2005 | EP1522062A1 Device and method for active soundproofing, and power unit for aeroplanes |
| 04/13/2005 | CN1605730A High temperature gas seal structure with heat insulating and cooling action |
| 04/12/2005 | US6877324 Gas turbine, gas turbine apparatus, and refrigerant collection method for gas turbine moving blades |
| 04/12/2005 | US6877321 Method and system for reducing turbine exhaust turbulence |
| 04/12/2005 | US6877320 Turbine arrangement and a method of operating a turbine arrangement |
| 04/12/2005 | US6877306 Nozzle assembly with flow divider and ecology valve |
| 04/12/2005 | CA2213792C Aircraft labyrinth fire seal |
| 04/07/2005 | US20050074356 Containing at least iron, silicon, manganese, chromium, nickel, molybdenum, tungsten, cobalt, vanadium, nitrogen and niobium and/or tantalum; controlled ratio of nickel to colbalt and molybdenum to tungsten; fuel efficiency |
| 04/07/2005 | US20050074325 Cooling jets |
| 04/07/2005 | US20050074049 Shaft-misalignment-measuring device, a shaft-misalignment-measuring method, a single-shaft combined plant using the shaft-misalignment-measuring device and a start-up method of the single-shaft combined plant |
| 04/07/2005 | US20050073152 Method and apparatus for controlling output voltages and frequencies of turbine/alternator on common shaft |
| 04/07/2005 | US20050072164 Combined heat and power system |
| 04/07/2005 | US20050072163 Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner |
| 04/07/2005 | US20050072162 Ejector for cooling air supply pressure optimization |
| 04/07/2005 | DE19814588B4 Hochtemperaturfeste oxidische Faserverbundwerkstoffe, ihre Herstellung und Verwendung High-temperature oxide fiber composites, their preparation and use |
| 04/07/2005 | DE10342097A1 Axialkompressor Axial Compressor |
| 04/07/2005 | DE102004040428A1 Power unit with gas turbine and compressed air store has stored fluid heat supply unit upstream from the pressure release device |
| 04/07/2005 | CA2540583A1 Power generation |
| 04/06/2005 | EP1520961A2 Methods for controlling lubrication oil draining in gas turbine engines |
| 04/06/2005 | EP1520960A2 Cooling air supply |
| 04/06/2005 | EP1520102A1 Methods for starting a combustion turbine and combustion turbine generator configured to implement same methods |
| 04/06/2005 | EP1520062A1 Highly oxidation resistant component |
| 04/06/2005 | CN1603596A Gas turbine plant |
| 04/06/2005 | CN1603578A Jp2005106738 |
| 04/05/2005 | US6875464 Using ceramic paste containing zirconia particles in binder; heating |
| 04/05/2005 | US6875292 Oxidation, corrosion resistant protective coatings; surface treatment; controlling temperature |
| 04/05/2005 | US6875256 Methods for filtering air for a gas turbine system |
| 04/05/2005 | US6874324 Gas turbine and gas turbine power generator |
| 04/05/2005 | CA2202952C Gas turbine subassembly having a brush seal |
| 03/31/2005 | WO2005028843A2 Rotary injector |
| 03/31/2005 | WO2005028832A1 Multi-spool turbogenerator system and control method |
| 03/31/2005 | WO2005028815A2 Device for the generation of mechanical or electrical energy using any thermal potential |
| 03/31/2005 | WO2005028813A1 Sealing arrangement in a compressor |
| 03/31/2005 | US20050067061 containing nickel, palladium, and restricted amounts of boron and silicon; for repairing nickel-based superalloy articles, or for joining different sections of superalloy components |
| 03/31/2005 | US20050066664 Gas turbine installation |
| 03/31/2005 | US20050066648 Multi-mode shutdown system for a fuel metering unit |
| 03/31/2005 | DE10340177A1 Zerstäubungs- und Eindüsensystem, und Verfahren zum Betrieb Atomizing and Eindüsensystem, and method for operating |
| 03/31/2005 | DE10333208A1 Verfahren zum Betrieb einer luftatmenden Kraftmaschine Method for operating an air-breathing combustion engine |
| 03/31/2005 | DE102004040890A1 Power station installation, has heat supply device arranged in waste gas path of gas turbo-group, upstream of heat transmission equipment |
| 03/31/2005 | DE102004040577A1 Method for starting power station installation in deactivated electricity network, involves forming connection between generator of pressure store-relaxation turbine and start device of gas turbine group |
| 03/31/2005 | CA2538749A1 Sealing arrangement in a compressor |
| 03/31/2005 | CA2538223A1 Multi-spool turbogenerator system and control method |
| 03/31/2005 | CA2526029A1 Rotary injector |
| 03/30/2005 | EP1519115A2 Method to operate a gas turbine with different fuels |
| 03/30/2005 | EP1519018A1 Power transmission arrangement |
| 03/30/2005 | EP1519007A1 Gas turbine |
| 03/30/2005 | EP1518636A2 Nickel-based braze alloy compositions, and related processes and articles |
| 03/30/2005 | EP1518039A1 Method for operating a gas turbine installation, and gas turbine installation |
| 03/30/2005 | EP1517762A2 Diffusion bond mixture for healing single crystal alloys |
| 03/30/2005 | CN1602236A Method for removing coating material from a cooling hole of a gas turbine engine component |
| 03/30/2005 | CN1601181A Method and apparatus for reducing gas turbine engine emissions |
| 03/29/2005 | US6872232 Engine with upstream and rotationally attached guard |
| 03/29/2005 | US6872047 Steam-cooling-type turbine |
| 03/29/2005 | US6872003 Oil-damped rolling bearing |
| 03/29/2005 | US6871820 Aircraft engine mounting |
| 03/29/2005 | US6871819 Protection device for a jet engine air intake structure |
| 03/29/2005 | US6871725 For use in a sound attenuation panel in the high velocity air flow region of an engine nacelle |
| 03/29/2005 | US6871504 Turbine power plant, installation process and removal process of the turbine power plant |
| 03/29/2005 | CA2330751C Gas turbine |
| 03/29/2005 | CA2284474C Combined cycle electric power plant |
| 03/24/2005 | WO2005025718A1 System and method for thermal management |
| 03/24/2005 | US20050064225 Thermal barrier composition, a superalloy machine part provided with a coating having such a composition, a ceramic coating, and a method of fabricating the coating |
| 03/24/2005 | US20050063819 Axial compressor |
| 03/24/2005 | US20050061005 Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions |
| 03/24/2005 | US20050061004 Method and apparatus for reducing gas turbine engine emissions |
| 03/24/2005 | US20050060984 Convergent-divergent turbojet nozzle |
| 03/24/2005 | US20050060982 Method and system for reduction of jet engine noise |
| 03/23/2005 | EP1517088A2 Method and apparatus for reducing gas turbine engine emissions |
| 03/23/2005 | EP1517087A1 Method and apparatus to decrease combustor acoustics |
| 03/23/2005 | EP1517022A2 Method and system for reduction of jet engine noise |
| 03/23/2005 | EP1517021A1 Power fluctuation suppressing method and power generation facility using same |
| 03/23/2005 | EP1517008A2 Cooling of a coated wall by a network of cooling channels |
| 03/23/2005 | EP1517006A1 Gas turbine brush seal arrangement for cabin air supply |
| 03/23/2005 | EP1517005A1 Gas turbine sealing joint having lamellar structure |
| 03/23/2005 | EP1516942A1 Method for coating a substrate |