| 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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| 07/29/2008 | CA2419018C High-temperature member for use in gas turbine |
| 07/29/2008 | CA2412160C Method and apparatus for cooling the inlet air of combustion turbines |
| 07/29/2008 | CA2394669C Brush seals |
| 07/29/2008 | CA2351322C Method and apparatus for production of a cast component |
| 07/29/2008 | CA2334933C Ambient air compression machine and related process, and corresponding air distillation and gas turbine plants |
| 07/26/2008 | CA2619416A1 Device for the assembly of two sets, for example for turbomachine stator |
| 07/25/2008 | CA2619315A1 Acoustic splitter for turbojet fan case |
| 07/24/2008 | WO2008032215A3 Power recovery machine |
| 07/24/2008 | US20080173270 Fuel injection device including plasma-inducing electrode arrays |
| 07/24/2008 | US20080173021 Method for improved efficiency for IGCC |
| 07/24/2008 | US20080173006 Gas turbine apparatus |
| 07/24/2008 | US20080173005 Gas turbogroup |
| 07/24/2008 | US20080173002 Method for treating oil waste in a gas turbine engine |
| 07/23/2008 | EP1947311A2 Turbine engine transient power extraction system and method |
| 07/23/2008 | EP1947310A1 Two-stage fuel injector |
| 07/23/2008 | EP1947309A2 Flame stability enhancement |
| 07/23/2008 | EP1947298A2 Slider seal assembly for gas turbine engine |
| 07/23/2008 | EP1946868A1 Directional solidification method and apparatus |
| 07/23/2008 | EP1945931A2 Device and method for axially displacing a turbine rotor |
| 07/23/2008 | EP1945930A2 Gas turbine engine mixing duct and method to start the engine |
| 07/23/2008 | CN101228069A Propulsion unit for aircraft and aircraft comprising at least one such propulsion unit |
| 07/23/2008 | CN101225770A Dust internal-combustion engine |
| 07/23/2008 | CN101225769A Power augmentation of combustion turbines by injection of cold air upstream of compressor |
| 07/23/2008 | CN100404820C Gas turbine plant |
| 07/23/2008 | CN100404819C Apparatus to facilitate sealing between rotating turbine shafts |
| 07/23/2008 | CN100404818C Apparatus to reduce seal rubbing within gas turbine engines |
| 07/23/2008 | CN100404817C Radial turbine and method of cooling nozzle of the same |
| 07/23/2008 | CN100404816C Methods and apparatus for cooling gas turbine engine rotor assemblies |
| 07/23/2008 | CN100404815C Methods and apparatus for cooling turbine engine combustor exit temperatures |
| 07/23/2008 | CN100404793C Gas turbine bucket tip cap |
| 07/22/2008 | US7401461 Reduced-weight fuel system for gas turbine engine, gas turbine engine having a reduced-weight fuel system, and method of providing fuel to a gas turbine engine using a reduced-weight fuel system |
| 07/17/2008 | US20080172267 Rotation Planning Apparatus and Rotation Planning System |
| 07/17/2008 | US20080168761 Method for increasing the aerodynamic stability of a working fluid flow of a compressor |
| 07/16/2008 | EP1944486A2 Aircraft fuel system |
| 07/16/2008 | EP1944485A2 Fuel system for a gas turbine engine and operation method therefore |
| 07/16/2008 | EP1944475A2 Heat exchange system |
| 07/16/2008 | EP1943419A2 Infrared suppression system |
| 07/16/2008 | CN101222172A Variable magnetic coupling of rotating machinery |
| 07/16/2008 | CN100402931C Double circular burning chamber prefabricated machine cover of gas turbine engine and its producing method |
| 07/16/2008 | CN100402930C Splashboard and method for producing the same |
| 07/16/2008 | CN100402816C Multi-core brush type sealing assembly for rotary machinery |
| 07/16/2008 | CN100402815C Process for processing ring-shape original surface heat regenerator for minisize gas turbine |
| 07/16/2008 | CN100402804C Axes difference measure device and method |
| 07/16/2008 | CN100402800C Synthetic high-temp assembly and manufacturing method therefor |
| 07/16/2008 | CA2618781A1 Combustion systems with rotary fuel slingers |
| 07/15/2008 | US7398641 Aeroengine intake having a heat exchanger within an annular closed chamber |
| 07/15/2008 | CA2307186C Fuel nozzle for gas turbine engine |
| 07/10/2008 | WO2008082336A1 A power transmission device for a gas turbine engine, an aeroplane and a method for operating a gas turbine engine |
| 07/10/2008 | WO2008082335A1 A power transmission device for a gas turbine engine |
| 07/10/2008 | WO2008082334A1 A gas turbine engine, an aircraft provided therewith, and a method of controlling the operation of such an engine |
| 07/10/2008 | US20080166548 Coating material for thermal barrier coating having excellent corrosion resistance and heat resistance and method of producing the same |
| 07/10/2008 | US20080163627 Fuel-flexible triple-counter-rotating swirler and method of use |
| 07/10/2008 | US20080163604 Turbine blade with reverse cooling air film hole direction |
| 07/10/2008 | DE102006058343A1 Gas turbine oil separator for aircraft engine, has filter unit displaceable in rotation and arranged in housing, where filter unit includes air outlet downstream to filter unit, and force applying unit arranged upstream of filter unit |
| 07/09/2008 | EP1942258A2 Particle separator using boundary layer control |
| 07/09/2008 | EP1942249A2 Heat transfer system for turbine engine using heat pipes |
| 07/09/2008 | CN101218426A Gas and steam turbine installation and method for operating the same |
| 07/09/2008 | CN100400967C Sector staging combustor |
| 07/09/2008 | CN100400797C Combustion turbine with axial relative movel guide unit |
| 07/09/2008 | CN100400222C Manufacture of hollow blades for turbine |
| 07/08/2008 | US7396592 Composite target of a bar made of ceramic powders, zirconia and a zirconia stabilizer, after sintering of the target, zirconia contains a monoclinic phase; barrier is deposited on a superalloy substrate; low thermal conductivity, high thermomechanical strength |
| 07/08/2008 | US7395657 Flade gas turbine engine with fixed geometry inlet |
| 07/08/2008 | US7395655 Regulator feeding control with two flow rate laws |
| 07/08/2008 | CA2332353C Exciter controlled by full authority digital electronic control (fadec) system |
| 07/08/2008 | CA2329721C Turbine engine with cooled p3 air to impeller rear cavity |
| 07/03/2008 | US20080159857 Turbine or compressor device and method for assembling the device |
| 07/03/2008 | US20080156930 Engine Mount For an Aircraft, to be Placed Between an Engine and an Engin Mounting Structure |
| 07/03/2008 | US20080155987 Methods and apparatus for low emission gas turbine energy generation |
| 07/03/2008 | US20080155959 Detonation combustor to turbine transition piece for hybrid engine |
| 07/03/2008 | DE102007001026A1 Technical system e.g. gas turbine, controlling and/or regulating method, involves executing learning and/or optimizing procedure based on concealed states in state space to control and/or regulate system |
| 07/03/2008 | DE102007001024A1 Technical system i.e. gas turbine, controlling and/or regulating method, involves selecting learning and/or optimization procedure suitable for technical system, and regulating and/or controlling system by selected procedure |
| 07/02/2008 | EP1939988A2 Electrical connection for titanium metal heater in jet turbine applications |
| 07/02/2008 | EP1939460A2 Intertial particle separator for compressor shroud bleed |
| 07/02/2008 | EP1939431A2 Methods and apparatus to facilitate gas turbine fuel control |
| 07/02/2008 | EP1939430A2 Turbofan engine assembly and method of assembling same |
| 07/02/2008 | EP1939429A2 Power take-off system and gas turbine engine assembly including same |
| 07/02/2008 | EP1939428A2 Flame prevention device |
| 07/02/2008 | EP1939408A2 Vapor cooling of detonation engines |
| 07/02/2008 | EP1937949A2 Rotation coupling employing torque converter and synchronization motor |
| 07/02/2008 | EP1747054B1 A fluid separation device |
| 07/02/2008 | EP1546526B1 Particle separator for a turbine engine |
| 07/02/2008 | CN101210518A Heat transfer system for turbine engine using heat pipes |
| 07/01/2008 | US7392927 Combinatorial production of material compositions from a single sample |
| 06/27/2008 | CA2615936A1 Integrated overboost protection gear |
| 06/27/2008 | CA2614160A1 Heat transfer system for turbine engine using heat pipes |
| 06/26/2008 | WO2008076471A2 Aircraft engine inlet pivotable barrier filter |
| 06/26/2008 | WO2008075747A1 Compressor |
| 06/26/2008 | WO2008075671A1 Jet flow discharge nozzle and jet engine |
| 06/26/2008 | WO2008075400A1 Gas turbine |
| 06/26/2008 | WO2008075022A1 Processing biomass |
| 06/26/2008 | US20080149771 System for Deicing the Leading Edge of a Nose Inlet Cowl Turbine Engine |
| 06/26/2008 | US20080148737 Turbine Static Structure for Reduced Leakage Air |
| 06/26/2008 | DE102007062496A1 Lageranordnung und Verfahren zum Zusammenbau derselben Bearing assembly and method of assembling same |
| 06/26/2008 | DE102007061568A1 Verfahren und System zum Einsetzen von Brenngas geringen Heizwertes in einer Gasturbine A method and system for insertion of low calorific value fuel gas in a gas turbine |
| 06/26/2008 | DE102007059676A1 Gewölbte Schienen zur Halterung bogenförmiger Elemente Curved rails for mounting arcuate elements |
| 06/26/2008 | DE102006060857A1 Combustion chamber lining of gas turbine, has gas-permeable heat protective layer that faces hot gas side and carrier layer that is separated from heat protective layer by displacement element |
| 06/25/2008 | EP1936312A2 Vapor cooled heat exchanger |
| 06/25/2008 | EP1936239A1 Gear with built-in overtorque protection |
| 06/25/2008 | EP1936238A2 Variable magnetic coupling of rotating machinery |
| 06/25/2008 | EP1936150A2 High-speed high-pole count generators |