| F01B | 2 hits |  |
| MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES | ||
| F01C | 9 hits | |
| ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES | ||
| F01D | 218 hits | |
| NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES | ||
| F01K | 19 hits | |
| STEAM ENGINE PLANTS | ||
| F01L | 21 hits | |
| CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES | ||
| F01M | 26 hits | |
| LUBRICATING OF MACHINES OR ENGINES IN GENERAL | ||
| F01N | 66 hits | |
| GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL | ||
| F01P | 13 hits | |
| COOLING OF MACHINES OR ENGINES IN GENERAL | ||
| F02B | 41 hits | |
| INTERNAL-COMBUSTION PISTON ENGINES | ||
| F02C | 80 hits | |
| GAS-TURBINE PLANTS | ||
| F02D | 85 hits | |
| CONTROLLING COMBUSTION ENGINES | ||
| F02F | 12 hits | |
| CYLINDERS, PISTONS, OR CASINGS FOR COMBUSTION ENGINES | ||
| F02G | 9 hits | |
| HOT-GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS | ||
| F02K | 25 hits | |
| JET-PROPULSION PLANTS | ||
| F02M | 71 hits | |
| SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF | ||
| F02N | 18 hits | |
| STARTING OF COMBUSTION ENGINES | ||
| F02P | 11 hits | |
| IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES | ||
| F03B | 17 hits | |
| MACHINES OR ENGINES FOR LIQUIDS | ||
| F03C | 1 hits | |
| POSITIVE-DISPLACEMENT ENGINES DRIVEN BY LIQUIDS | ||
| F03D | 146 hits | |
| WIND MOTORS | ||
| F03G | 7 hits | |
| SPRING, WEIGHT, INERTIA, OR LIKE MOTORS | ||
| F04B | 38 hits | |
| POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS | ||
| F04C | 31 hits | |
| ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS | ||
| F04D | 67 hits | |
| NON-POSITIVE-DISPLACEMENT PUMPS | ||
| F04F | 1 hits | |
| PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED | ||
| F15B | 44 hits | |
| SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL | ||
| F15D | 3 hits | |
| FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS | ||
| F16B | 80 hits | |
| DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS, WEDGES | ||
| F16C | 78 hits | |
| SHAFTS | ||
| F16D | 57 hits | |
| COUPLINGS FOR TRANSMITTING ROTATION | ||
| F16F | 44 hits | |
| SPRINGS | ||
| F16G | 16 hits | |
| BELTS, CABLES, OR ROPES, PREDOMINANTLY USED FOR DRIVING PURPOSES | ||
| F16H | 105 hits | |
| GEARING | ||
| F16J | 42 hits | |
| PISTONS | ||
| F16K | 53 hits | |
| VALVES | ||
| F16L | 80 hits | |
| PIPES | ||
| F16M | 12 hits | |
| FRAMES, CASINGS, OR BEDS, OF ENGINES OR OTHER MACHINES OR APPARATUS, NOT SPECIFIC TO AN ENGINE, MACHINE, OR APPARATUS PROVIDED FOR ELSEWHERE | ||
| F16N | 10 hits | |
| LUBRICATING | ||
| F16P | 4 hits | |
| SAFETY DEVICES IN GENERAL | ||
| F16S | 1 hits | |
| CONSTRUCTIONAL ELEMENTS IN GENERAL | ||
| F16T | 2 hits | |
| STEAM TRAPS OR LIKE APPARATUS FOR DRAINING-OFF LIQUIDS FROM ENCLOSURES PREDOMINANTLY CONTAINING GASES OR VAPOURS | ||
| F17C | 17 hits | |
| VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES | ||
| F17D | 3 hits | |
| PIPE-LINE SYSTEMS | ||
| F21K | 29 hits | |
| LIGHT SOURCES NOT OTHERWISE PROVIDED FOR | ||
| F21L | 3 hits | |
| LIGHTING DEVICES OR SYSTEMS THEREOF, BEING PORTABLE OR SPECIALLY ADAPTED FOR TRANSPORTATION | ||
| F21S | 89 hits | |
| NON-PORTABLE LIGHTING DEVICES OR SYSTEMS THEREOF | ||
| F21V | 126 hits | |
| FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF | ||
| F21W | 17 hits | |
| FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF | ||
| F21Y | 81 hits | |
| FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF | ||
| F22B | 10 hits | |
| METHODS OF STEAM GENERATION | ||
| F22D | 1 hits | |
| PREHEATING, OR ACCUMULATING PREHEATED, FEED-WATER | ||
| F22G | 1 hits | |
| SUPERHEATING OF STEAM | ||
| F23B | 4 hits | |
| METHODS OR APPARATUS FOR COMBUSTION USING ONLY SOLID FUEL | ||
| F23C | 6 hits | |
| METHODS OR APPARATUS FOR COMBUSTION USING FLUENT FUEL | ||
| F23D | 20 hits | |
| BURNERS | ||
| F23G | 4 hits | |
| CREMATION FURNACES | ||
| F23H | 1 hits | |
| GRATES | ||
| F23J | 11 hits | |
| REMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES | ||
| F23K | 5 hits | |
| FEEDING FUEL TO COMBUSTION APPARATUS | ||
| F23L | 11 hits | |
| AIR SUPPLY | ||
| F23M | 3 hits | |
| CONSTRUCTIONAL DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR | ||
| F23N | 12 hits | |
| REGULATING OR CONTROLLING COMBUSTION | ||
| F23Q | 1 hits | |
| IGNITION | ||
| F23R | 56 hits | |
| GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS | ||
| F24B | 1 hits | |
| DOMESTIC STOVES OR RANGES FOR SOLID FUELS | ||
| F24C | 56 hits | |
| OTHER DOMESTIC STOVES OR RANGES | ||
| F24D | 36 hits | |
| DOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATING SYSTEMS | ||
| F24F | 62 hits | |
| AIR-CONDITIONING | ||
| F24H | 19 hits | |
| FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, IN GENERAL | ||
| F24J | 45 hits | |
| PRODUCTION OR USE OF HEAT NOT OTHERWISE PROVIDED FOR | ||
| F25B | 67 hits | |
| REFRIGERATION MACHINES, PLANTS, OR SYSTEMS | ||
| F25C | 5 hits | |
| PRODUCTION, WORKING, STORING, OR DISTRIBUTION OF ICE | ||
| F25D | 32 hits | |
| REFRIGERATORS | ||
| F25J | 2 hits | |
| LIQUEFACTION, SOLIDIFICATION, OR SEPARATION OF GASES OR GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT | ||
| F26B | 12 hits | |
| DRYING SOLID MATERIALS OR OBJECTS BY REMOVING LIQUID THEREFROM | ||
| F27B | 12 hits | |
| FURNACES, KILNS, OVENS, OR RETORTS IN GENERAL | ||
| F27D | 13 hits | |
| DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE | ||
| F28B | 1 hits | |
| STEAM OR VAPOUR CONDENSERS | ||
| F28C | 1 hits | |
| HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA COME INTO DIRECT CONTACT WITHOUT CHEMICAL INTERACTION | ||
| F28D | 38 hits | |
| HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT | ||
| F28F | 40 hits | |
| DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION | ||
| F28G | 1 hits | |
| CLEANING OF INTERNAL OR EXTERNAL SURFACES OF HEAT-EXCHANGE OR HEAT-TRANSFER CONDUITS, e.g. WATER TUBES OF BOILERS | ||
| F41A | 16 hits | |
| FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS | ||
| F41B | 2 hits | |
| WEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE | ||
| F41C | 4 hits | |
| SMALLARMS, e.g. PISTOLS, RIFLES | ||
| F41F | 5 hits | |
| APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS | ||
| F41G | 11 hits | |
| WEAPON SIGHTS | ||
| F41H | 14 hits | |
| ARMOUR | ||
| F41J | 1 hits | |
| TARGETS | ||
| F42B | 9 hits | |
| EXPLOSIVE CHARGES, e.g. FOR BLASTING | ||
| EP2535521A3 | 2013-01-02 |
| Vane assembly with improved vane roots | |
| EP2468463A3 | 2013-01-02 |
| Method and device for coating path generation | |
| EP2236752A3 | 2013-01-02 |
| Cooled aerofoil for a gas turbine engine | |
| EP2192275A3 | 2013-01-02 |
| Mid turbine frame system for gas turbine engine | |
| EP1914392A3 | 2013-01-02 |
| Turbine case impingement cooling for heavy duty gas turbines | |
| EP1600607A3 | 2013-01-02 |
| Device to control the radial clearance of the rotor of a gas turbine | |
| EP2540486A2 | 2013-01-02 |
| Method of making composite fan blade | |
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| Turbine blade | |
| EP2540981A2 | 2013-01-02 |
| Turbine vane | |
| EP2540986A2 | 2013-01-02 |
| Turbine blade | |
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| Supersonic turbine moving blade and axial-flow turbine | |
| EP2540966A2 | 2013-01-02 |
| Method of finishing a fan blade | |
| EP2540978A2 | 2013-01-02 |
| Fan blade protection system | |
| EP2540977A2 | 2013-01-02 |
| Method of improving fatigue strength in a fan blade and corresponding fan blade | |
| EP2540980A2 | 2013-01-02 |
| Damper for an integrally bladed rotor | |
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| Turbine disk preform, welded turbine rotor made therewith and methods of making the same | |
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| Grit blast free thermal barrier coating rework | |
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| Repairable double sided brush seal | |
| EP2540965A2 | 2013-01-02 |
| Manufacturing method for a ceramic fiber reinforced ceramic composite component with internal three-dimensionally woven platform and corresponding component | |
| EP2540975A2 | 2013-01-02 |
| Hybrid part made from monolithic ceramic skin and cmc core | |
| EP2540979A2 | 2013-01-02 |
| Rotor assembly and reversible turbine blade retainer therefor | |
| EP2540984A2 | 2013-01-02 |
| Impingement Cooled Nozzle Liner | |
| EP2540989A2 | 2013-01-02 |
| Variable cycle turbine engine | |
| EP2540962A2 | 2013-01-02 |
| Method for forming nozzle segments | |
| EP2540990A2 | 2013-01-02 |
| Seal assembly for a rotational fluid metering valve | |
| EP2540974A2 | 2013-01-02 |
| Fan blade with sheath | |
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| System and method for supporting a nozzle assembly | |
| EP2540988A2 | 2013-01-02 |
| Plug assembly for blade outer air seal | |
| EP2540961A2 | 2013-01-02 |
| Abrasive airfoil tip | |
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| Mechanism for turbine engine start from low spool | |
| EP2540983A2 | 2013-01-02 |
| Radial spline arrangement for LPT vane clusters | |
| EP2540982A2 | 2013-01-02 |
| Flowpath insert and assembly | |
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| Chordal mounting arrangement for low-ductility turbine shroud | |
| EP2540972A1 | 2013-01-02 |
| Blade for a gas turbine and method for producing such a blade | |
| EP2540971A1 | 2013-01-02 |
| Method for creating a platform cooling passage in a turbine rotor blade and corresponding platform cooling passage | |
| EP2540987A1 | 2013-01-02 |
| TURBINE | |
| EP2540993A1 | 2013-01-02 |
| AIRCRAFT GAS TURBINE | |
| EP2540970A1 | 2013-01-02 |
| Liquid metal cooled blade | |
| EP2540973A1 | 2013-01-02 |
| Seal system for a gas turbine | |
| EP2540969A1 | 2013-01-02 |
| Impingement cooling of turbine blades or vanes | |
| EP2192271A3 | 2012-12-26 |
| Mid turbine frame for gas turbine engine | |
| EP2192270A3 | 2012-12-26 |
| Mid turbine frame system for gas turbine engine | |
| EP2192274A3 | 2012-12-26 |
| Mid turbine frame for gas turbine engine | |
| EP2192273A3 | 2012-12-26 |
| Mid turbine frame for gas turbine engine | |
| EP2159378A3 | 2012-12-26 |
| Rotor blade | |
| EP2108786A3 | 2012-12-26 |
| Aeroengine fan assembly | |
| EP2159396A3 | 2012-12-26 |
| Filtration system for gas turbines | |
| EP2072759A3 | 2012-12-26 |
| Turbine engine blade with multi-layer protective coating for the interior cooling passages | |
| EP2538037A2 | 2012-12-26 |
| Engine bearing compartment | |
| EP2538026A2 | 2012-12-26 |
| Cooling system for turbine airfoil including ice-cream-cone-shaped pedestals | |
| EP2538020A2 | 2012-12-26 |
| Gas Turbines | |
| EP2538028A2 | 2012-12-26 |
| Methods and systems for cooling a transition nozzle | |
| EP2538027A2 | 2012-12-26 |
| Methods and systems for transferring heat from a transition nozzle | |
| EP2538138A2 | 2012-12-26 |
| Combustor assembly for use in a turbine engine and methods of assembling same | |
| EP2538023A2 | 2012-12-26 |
| Pressure and temperature actuation system | |
| EP2537822A2 | 2012-12-26 |
| Composite article including silicon oxycarbide layer | |
| EP2538021A2 | 2012-12-26 |
| Ventilated compressor rotor for a turbine engine and corresponding manufacturing method | |
| EP2538055A2 | 2012-12-26 |
| Oil bypass channel deaerator for a geared turbofan engine | |
| EP2538035A2 | 2012-12-26 |
| Joint assembly | |
| EP2538036A2 | 2012-12-26 |
| Integral bearing support and centering spring assembly for a gas turbine engine | |
| EP2538039A2 | 2012-12-26 |
| Gas turbine support structure forming method | |
| EP2538022A2 | 2012-12-26 |
| Non-mechanically fastened TOBI heat shield | |
| EP2538034A2 | 2012-12-26 |
| MFCC and CELP to detect turbine engine faults | |
| EP2538070A2 | 2012-12-26 |
| TURBINE WITH RADIAL INLET AND OUTLET ROTOR FOR USE IN BIDIRECTIONAL FLOWS | |
| EP2538029A1 | 2012-12-26 |
| Airfoil trailing edge cooling | |
| EP2537606A1 | 2012-12-26 |
| Investment casting of cooled turbine airfoils | |
| EP2537636A1 | 2012-12-26 |
| Component with cooling channels and method of manufacture | |
| EP2537635A1 | 2012-12-26 |
| Component with cooling channels and method of manufacture | |
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| Hot gas path component and corresponding method of forming a component | |
| EP2537747A1 | 2012-12-26 |
| Propulsion system with contrarotating open rotors and its balancing method | |
| EP2537746A1 | 2012-12-26 |
| Propulsion system with contrarotating open rotors and its balancing method | |
| EP2538038A1 | 2012-12-26 |
| Pressure housing | |
| EP2537951A1 | 2012-12-26 |
| Ni-based alloy, and turbine rotor and stator blade for gas turbine | |
| EP2537608A1 | 2012-12-26 |
| Ni-based alloy for casting used for steam turbine and casting component of steam turbine | |
| EP2538024A1 | 2012-12-26 |
| Blade of a turbomaschine | |
| EP2538032A1 | 2012-12-26 |
| Radially movable seal system for a gas turbine | |
| EP2538031A1 | 2012-12-26 |
| Rotor with sealing element for a stationary gas turbine | |
| EP2538030A1 | 2012-12-26 |
| Labyrinth seal system for a gas turbine | |
| EP2538033A1 | 2012-12-26 |
| Method for starting a stationary gas turbine | |
| EP2538054A1 | 2012-12-26 |
| STRUCTURE FOR GAS TURBINE CASING | |
| EP2495553A3 | 2012-12-19 |
| Portable boroscope for inspecting turbomachine blades | |
| EP2192269A3 | 2012-12-19 |
| Interturbine duct strut and vane ring for gas turbine engine | |
| EP2105581A3 | 2012-12-19 |
| Vane with integral inner air seal | |
| EP2151545A3 | 2012-12-19 |
| Turbine blade and fixation structure thereof | |
| EP2071137A3 | 2012-12-19 |
| Method for repairing composite containment casings | |
| EP1939426A3 | 2012-12-19 |
| System for supplying air to a vehicle having a turbofan engine | |
| EP2535521A2 | 2012-12-19 |
| Vane assembly with improved vane roots | |
| EP2535528A2 | 2012-12-19 |
| Turbofan engine bearing support | |
| EP2535527A2 | 2012-12-19 |
| Turbofan engine comprising a fan rotor support | |
| EP2535512A2 | 2012-12-19 |
| Method of repairing a turbine nozzle segment in a turbine engine | |
| EP2535520A2 | 2012-12-19 |
| Method and apparatus to repair a turbomachine rotor wheel | |
| EP2535530A2 | 2012-12-19 |
| System and method for adjusting a shroud block in a casing | |
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| Rotor structure including an internal hydraulic tension device | |
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| Apparatus and method for servicing dynamolectric machine components in-situ | |
| EP2535523A2 | 2012-12-19 |
| Turbine seal system and method of assembly thereof | |
| EP2535525A2 | 2012-12-19 |
| Surge margin control for a gas turbine engine | |
| EP2535522A2 | 2012-12-19 |
| W-shaped seal | |
| EP2535524A2 | 2012-12-19 |
| Turbocharger variable-nozzle assembly with vane sealing ring | |
| EP2535519A2 | 2012-12-19 |
| A retention device for a rotating blade | |
| EP2535518A2 | 2012-12-19 |
| Blade mounting system | |
| EP2535529A2 | 2012-12-19 |
| A bearing chamber apparatus | |
| EP2535517A2 | 2012-12-19 |
| Rotor device for a jet engine with a disc and multiple rotor blades | |
| EP2535609A1 | 2012-12-19 |
| Turbocharger, notably for a combustion engine | |
| EP2535526A1 | 2012-12-19 |
| Turbocharger, notably for a combustion engine. | |
| EP2535607A1 | 2012-12-19 |
| Turbocharger, notably for a combustion engine | |
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| Method for friction soldering blades to an axial compressor drum, and corresponding device | |
| EP2535515A1 | 2012-12-19 |
| Rotor blade root section with cooling passage and method for supplying cooling fluid to a rotor blade | |
| EP2151543A3 | 2012-12-12 |
| Repair methods for turbines involving conductive heat resistance welding | |
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| De-icing system for engine inlet and method of preventing ice formation | |
| EP2009240A3 | 2012-12-12 |
| Bimaterial turbine blade damper | |
| EP1978208A3 | 2012-12-12 |
| Multi-alloy turbine rotors and methods of manufacturing the rotors | |
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| Thermally compliant c-clip | |
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| Gas turbine blade | |
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| Low solidity turbofan | |
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| Bifurcated outlet guide vanes | |
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| Flexible support structure for a geared architecture gas turbine engine | |
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| Flexible support structure for a geared architecture gas turbine engine | |
| EP2532834A2 | 2012-12-12 |
| Cooling flow control elements for turbomachine buckets and control method thereof | |
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| Turbomachine blade locking system | |
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| Seal assemly for gas turbine | |
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| System and method for packing and transporting a gas turbine | |
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| Combustion liner and transistion piece | |
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| Rotating blade analysis | |
| EP2532838A1 | 2012-12-12 |
| A compliant plate seal assembly for a turbo machine | |
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| Method and device for assisted monitoring of an aircraft turbine engine. | |
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| Arc source | |
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| Rotor assembly with interstage seal | |
| EP2208860A3 | 2012-12-05 |
| Interstage seal for a gas turbine and corresponding gas turbine | |
| EP2196632A3 | 2012-12-05 |
| A seal in a gas turbine and a method of manufacturing a seal | |
| EP2078826A3 | 2012-12-05 |
| Gas turbine engine case | |
| EP2009246A3 | 2012-12-05 |
| A blade mounting | |
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| Sheath for use on airfoil components | |
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| Apparatur and method for assemblying a gas turbine stator | |
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| Shrouded turbofan bleed duct | |
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| Sensor diagnostics using a quality parameter model | |
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| Method and system for active tip clearance control in turbines | |
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| Mount Device For Transition Duct In Turbine System | |
| EP2530252A2 | 2012-12-05 |
| Flexible seal | |
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| Hinge seal | |
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| A turbine blade or vane segment and a method of cooling a gap between these segments | |
| EP2530246A2 | 2012-12-05 |
| System for mounting combustor transition piece to frame of gas turbine engine | |
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| Composite article having silicate barrier layer and method therefor | |
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| Injector | |
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| Article having vitreous monocoating | |
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| An apparatus and a method of shaping an edge of an aerofoil | |
| EP2530242A2 | 2012-12-05 |
| An apparatus and a method of shaping an edge of an aerofoil | |
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| Fuel air heat exchanger | |
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| Flap seal spring and sealing apparatus | |
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| Valve seat and gasket for exhaust bypass valve | |
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| Bearing assembly | |
| EP2530255A2 | 2012-12-05 |
| Water separator and method for separating water from a saturated steam flow | |
| EP2530248A1 | 2012-12-05 |
| Linear transition duct for a gas turbine | |
| EP2529877A1 | 2012-12-05 |
| Method and apparatus for repairing an engine component | |
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| Seal assembly for a gas turbine engine, corresponding gas turbine engine and assembly method | |
| EP2530328A1 | 2012-12-05 |
| Easily adaptable compressor bleed system downstream of a vane platform | |
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| Piston seal ring | |
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| SPLIT RING COOLING STRUCTURE AND GAS TURBINE | |
| EP2256300A3 | 2012-11-28 |
| Knife edge seal assembly and corresponding rotor stage | |
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| Bleed assembly for a gas turbine engine, corresponding diffuser screen and gas turbine engine | |
| EP2239425A3 | 2012-11-28 |
| Variable geometry vane assembly for a turbocharger | |
| EP2206888A3 | 2012-11-28 |
| Turbine power generation system and corresponding operating method | |
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| Aeroengine bleed valve | |
| EP2071139A3 | 2012-11-28 |
| Bearing mounting system in a low pressure turbine | |
| EP2031182A3 | 2012-11-28 |
| Turbine rotor apparatus and system | |
| EP1983159A3 | 2012-11-28 |
| Shrouded single crystal dual alloy turbine disk | |
| EP1944465A3 | 2012-11-28 |
| Gas turbine blade | |
| EP1892399A3 | 2012-11-28 |
| Aero engine bleed valve | |
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close
| Title: | Compressor blade of a gas turbine engine with self-sharpening leading edge structure |
| Applicants: | ROLLS-ROYCE DEUTSCHLAND LTD & CO KG; FORMTECH GMBH |
| Inventors: | Schreiber, Karl; Beck, Werner |
| Main IPC Subclass: | F01D 5/28 |
| Agent: | Weber, Joachim |
| Application: | 2011-07-20 as 11005950.8 |
| Publication: | 2012-01-25 as EP2410132A2 |
| Patent FamilyFull Text | Register & FilePDF |
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| 1. | 68 | GENERAL ELECTRIC CO. |
| 2. | 48 | UNITED TECHNOLOGIES CORP. |
| 3. | 26 | ROLLS-ROYCE PLC |
| 4. | 16 | SIEMENS AG |
| 5. | 10 | PRATT & WHITNEY CANADA CORP. |
| 6. | 8 | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 7. | 7 | ALSTOM TECHNOLOGY LTD |
| 8. | 6 | HONEYWELL INTERNATIONAL INC. |
| 9. | 4 | AKTIEBOLAGET SKF |
| 10. | 4 | HITACHI LTD. |
| 11. | 3 | AIRBUS OPERATIONS SAS |
| 12. | 2 | BOREALIS AG |
| 13. | 2 | TECHSPACE AERO S.A. |
| 14. | 2 | K.K. TOSHIBA |
| 15. | 2 | HAMILTON SUNDSTRAND CORP. |
| 16. | 2 | ROLLS-ROYCE DEUTSCHLAND LTD & CO KG |
| 17. | 1 | THERMODYN |
| 18. | 1 | INSTITUTO SUPERIOR TECNICO |
| 19. | 1 | NERCESSIAN, KEVORK |
| 20. | 1 | AIRBUS SAS |
| 1. | 224 | GENERAL ELECTRIC CO. |
| 2. | 113 | UNITED TECHNOLOGIES CORP. |
| 3. | 75 | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 4. | 67 | ROLLS-ROYCE PLC |
| 5. | 61 | SIEMENS AG |
| 6. | 48 | TOYOTA JIDOSHA K.K. |
| 7. | 38 | PANASONIC CORP. |
| 8. | 29 | ROBERT BOSCH GMBH |
| 9. | 23 | PRATT & WHITNEY CANADA CORP. |
| 10. | 22 | ALSTOM TECHNOLOGY LTD |
| 11. | 21 | MITSUBISHI ELECTRIC CORP. |
| 12. | 21 | BSH BOSCH UND SIEMENS HAUSGERATE GMBH |
| 13. | 20 | HONEYWELL INTERNATIONAL INC. |
| 14. | 16 | HAMILTON SUNDSTRAND CORP. |
| 15. | 16 | SHARP K.K. |
| 16. | 15 | YAMAHA HATSUDOKI K.K. |
| 17. | 15 | AKTIEBOLAGET SKF |
| 18. | 14 | GAMESA INNOVATION & TECHNOLOGY, S.L. |
| 19. | 14 | LG ELECTRONICS INC. |
| 20. | 14 | JTEKT CORP. |
| 1. | 511 | GENERAL ELECTRIC CO. |
| 2. | 248 | SAMSUNG ELECTRONICS CO., LTD. |
| 3. | 208 | SIEMENS AG |
| 4. | 204 | LG ELECTRONICS INC. |
| 5. | 202 | PANASONIC CORP. |
| 6. | 202 | UNITED TECHNOLOGIES CORP. |
| 7. | 177 | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 8. | 158 | ZTE CORP. |
| 9. | 146 | TOYOTA JIDOSHA K.K. |
| 10. | 144 | SONY CORP. |
| 11. | 128 | SHARP K.K. |
| 12. | 125 | ROLLS-ROYCE PLC |
| 13. | 102 | CANON K.K. |
| 14. | 100 | ROBERT BOSCH GMBH |
| 15. | 99 | K.K. TOSHIBA |
| 16. | 97 | RESEARCH IN MOTION LTD. |
| 17. | 87 | HUAWEI TECHNOLOGIES CO., LTD. |
| 18. | 86 | ALCATEL LUCENT |
| 19. | 85 | MITSUBISHI ELECTRIC CORP. |
| 20. | 84 | HONEYWELL INTERNATIONAL INC. |
