| 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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| 01/25/2005 | US6846575 Article having turbulation and method of providing turbulation on an article |
| 01/25/2005 | US6846258 Gas turbine power generation facility |
| 01/25/2005 | US6846158 Method and apparatus for varying the critical speed of a shaft |
| 01/25/2005 | US6845745 Modification of lubricant properties in a recirculating lubricant system |
| 01/25/2005 | US6845738 Method for operating an internal combustion engine |
| 01/25/2005 | US6845606 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation |
| 01/21/2005 | CA2473279A1 Hybrid fuel cell-pulse detonation power system |
| 01/20/2005 | WO2005005888A1 Cooling structure of gas turbine tail pipe |
| 01/20/2005 | WO2005005810A1 Aircraft turbine engine arrangement |
| 01/20/2005 | WO2004069749A3 Improved configuration and process for carbonyl removal |
| 01/20/2005 | US20050011863 Method for inspecting a titanium-based component |
| 01/20/2005 | US20050011198 Electrostatic evaporative cooling system |
| 01/20/2005 | US20050011197 Fuel delivery system having an ecology valve |
| 01/20/2005 | US20050011180 Gas turbine installation |
| 01/20/2005 | US20050011179 Gas turbine system comprising closed system of fuel and combustion gas using underground coal layer |
| 01/20/2005 | DE4402941B4 Kombinierter Motor mit integrierten Arbeitsweisen als Ejektor für turbokomprimierte, gekühlte oder verflüssigte Luft, als Staustrahltriebwerk und als Überschall-Staustrahltriebwerk Combined motor with integrated ways of working as an ejector for turbo-compressed, cooled or liquefied air as ramjet and a supersonic ramjet |
| 01/20/2005 | DE102004029833A1 Nickelbasis-Superlegierung und Einkristall-Gussstücke Nickel-base superalloy and single crystal castings |
| 01/20/2005 | DE102004004911A1 Gas turbine assembly has non-catalytic preliminary combustion stage upstream of catalytic first burner stage; burner of preliminary combustion stage is configured as diffusion burner |
| 01/20/2005 | DE102004004424A1 Aktive Kühltafel aus Thermostruktur-Kompositwerkstoff und Verfahren zur Herstellung selbiger Active cooling panel of thermostructural composite material and method for producing Selbiger |
| 01/19/2005 | EP1498731A2 Method for inspecting a titanium-base component |
| 01/19/2005 | EP1497476A1 Process of masking cooling holes of a gas turbine component |
| 01/19/2005 | CN1568397A Methods and apparatus for cooling gas turbine engine blade tips |
| 01/19/2005 | CN1566619A Heat regenerator for small combustion turbine |
| 01/18/2005 | US6844518 Hole-drilling guide and method |
| 01/18/2005 | US6844075 Silicon bonding layer, tantalum or niobium aluminate inter-mediate layer resistant to solid state subsurface reactions and topcoat inert to reactions with silica at high tempera-tures; gas turbine engines, heat exchangers |
| 01/18/2005 | US6843928 Removing titanium cladding that is adhered to a turbine (fan) blade via etching with hydrofluoric acid |
| 01/18/2005 | US6843449 Fail-safe aircraft engine mounting system |
| 01/18/2005 | US6843060 Fault management system for gas turbine engines |
| 01/18/2005 | US6842980 Method for increasing heat transfer from combustors |
| 01/13/2005 | WO2005003521A1 Electrical power generation system and method |
| 01/13/2005 | WO2005003520A1 Turbine shroud segment |
| 01/13/2005 | US20050008487 Integrated bridge turbine blade |
| 01/13/2005 | US20050008482 Inlet guide vane |
| 01/13/2005 | US20050008477 Method of guiding a blade having a variable pitch angle |
| 01/13/2005 | US20050007722 Partitioned exciter system |
| 01/13/2005 | US20050005733 Mixing and heating two alloy powders with different melting points; high temperature parts in gas turbines and jet engines |
| 01/13/2005 | US20050005608 Long life nozzle flap for aircraft turbojets |
| 01/13/2005 | US20050005607 System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber |
| 01/13/2005 | US20050005445 Method of manufacturing a hollow blade for a turbine engine |
| 01/13/2005 | US20050005444 Process and apparatus for producing a turbine component, turbine component and use of the apparatus |
| 01/13/2005 | DE10336978B3 Carrier housing for exhaust gas turbo-supercharger |
| 01/12/2005 | EP1496302A2 Failure tolerant passive lubrication system |
| 01/12/2005 | EP1496220A2 High efficiency low pollution hybrid brayton cycle combustor |
| 01/12/2005 | EP1496205A1 Cooled blade for a gas turbine engine |
| 01/12/2005 | EP1496204A1 Turbine blade |
| 01/12/2005 | EP1496201A1 Gas turbine |
| 01/12/2005 | EP1496200A1 Gas turbine |
| 01/12/2005 | EP1495166A1 Method for producing for producing mono-crystalline structures |
| 01/12/2005 | EP1397584B1 Gas turbine arrangement |
| 01/12/2005 | EP1284903B1 Compact millimeter wave technical system for de-icing and/or preventing the formation of ice on the outer surface of hollow or shell structures exposed to meteorological influences |
| 01/12/2005 | EP1208295B1 Integrated bleed air and engine starting system (ibaness) |
| 01/12/2005 | EP1185765B1 Apparatus for reducing combustor exit duct cooling |
| 01/12/2005 | CN1563689A Water saving method applied to turboset |
| 01/12/2005 | CN1184413C Gas turbie exhaust passage and damper system for same |
| 01/11/2005 | US6841195 Process for corrosion protection of turbine internal components |
| 01/11/2005 | US6841011 Iron base high temperature alloy and method of making |
| 01/11/2005 | US6840309 Heat exchanger |
| 01/11/2005 | US6840049 Gas turbine and method for operating a gas turbine |
| 01/11/2005 | CA2284494C Combined cycle power plant |
| 01/06/2005 | WO2005002025A1 Electric starter motor with integral clutch |
| 01/06/2005 | WO2005001974A1 Fuel cell/constant pressure turbine/hybrid system |
| 01/06/2005 | WO2005001260A2 Blade cooling in a gas turbine engine |
| 01/06/2005 | WO2004104392A3 Air turbine starter with angular contact thrust bearing |
| 01/06/2005 | US20050004810 Turbine shroud segment |
| 01/06/2005 | US20050002781 Compressor for a gas turbine engine |
| 01/06/2005 | US20050002780 Turbine shroud segment |
| 01/06/2005 | US20050002779 Turbine shroud segment |
| 01/06/2005 | US20050001598 Electrical power generation system and method |
| 01/06/2005 | US20050000753 Failure tolerant passive lubrication system |
| 01/06/2005 | US20050000603 Nickel base superalloy and single crystal castings |
| 01/06/2005 | US20050000547 Liquid crystalline polymer containing intake, discharging aperture in substrate; plug; froming stacks |
| 01/06/2005 | US20050000228 Combustion chamber having a flexible connexion between a chamber end wall and a chamber side wall |
| 01/06/2005 | US20050000225 Transition duct support bracket wear cover |
| 01/06/2005 | US20050000224 Gas turbine arrangement |
| 01/06/2005 | US20050000223 Methods for regulating gas turbine engine fluid flow |
| 01/06/2005 | US20050000091 Method for manufacturing a stator or rotor component |
| 01/05/2005 | EP1493664A1 Latch for turbine nacelle cowls |
| 01/05/2005 | EP1492941A1 Steam and gas turbine installation |
| 01/05/2005 | EP1492900A1 Component comprising a masking layer |
| 01/05/2005 | EP0911487B1 Gas turbine cooling moving blades |
| 01/05/2005 | DE10326532A1 Gasturbine und Anbaugerät für eine Gasturbine Gas turbine and attachment for a gas turbine |
| 01/05/2005 | DE10325111A1 Verfahren zur Erzeugung von Energie in einer eine Gasturbine umfassende Energieerzeugungsanlage sowie Energieerzeugungsanlage zur Durchführung des Verfahrens Process for the production of energy in a gas turbine power generation plant as well as comprehensive energy generation system for implementing the method |
| 01/05/2005 | CN1560452A Apparatus of controlling gasoline of mini-turbine jet engine |
| 01/05/2005 | CN1560437A Heat regenerator of original surface for gas turbine |
| 01/05/2005 | CN1183318C Gas-turbine installation |
| 01/04/2005 | US6838779 Aircraft starter generator for variable frequency (vf) electrical system |
| 01/04/2005 | US6838778 Integrated starter generator drive having selective torque converter and constant speed transmission for aircraft having a constant frequency electrical system |
| 01/04/2005 | US6837676 Gas turbine |
| 01/04/2005 | US6837419 Recuperator for use with turbine/turbo-alternator |
| 01/04/2005 | US6837056 Turbine inlet air-cooling system and method |
| 01/04/2005 | US6837051 Gas turbine combustor |
| 01/04/2005 | US6837050 Gas turbine combustor |
| 01/04/2005 | US6837038 Variable cycle boost propulsor |
| 01/04/2005 | CA2099710C Exhaust system for a turbomachine |
| 12/30/2004 | US20040266274 Device for maintaining and positioning harnesses on a turbo-jet engine |
| 12/30/2004 | US20040265129 Cooled gas turbine blades |
| 12/30/2004 | US20040265054 Link between two mechanical members |
| 12/30/2004 | US20040262366 Repair process |
| 12/30/2004 | US20040261923 Clean atmosphere heat treat for coated turbine components |
| 12/30/2004 | US20040261418 Arrangement at gas turbine |