| 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 | 191 hits | |
| NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES | ||
| F01K | 16 hits | |
| STEAM ENGINE PLANTS | ||
| F01L | 18 hits | |
| CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES | ||
| F01M | 25 hits | |
| LUBRICATING OF MACHINES OR ENGINES IN GENERAL | ||
| F01N | 60 hits | |
| GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL | ||
| F01P | 10 hits | |
| COOLING OF MACHINES OR ENGINES IN GENERAL | ||
| F02B | 39 hits | |
| INTERNAL-COMBUSTION PISTON ENGINES | ||
| F02C | 71 hits | |
| GAS-TURBINE PLANTS | ||
| F02D | 77 hits | |
| CONTROLLING COMBUSTION ENGINES | ||
| F02F | 10 hits | |
| CYLINDERS, PISTONS, OR CASINGS FOR COMBUSTION ENGINES | ||
| F02G | 6 hits | |
| HOT-GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS | ||
| F02K | 20 hits | |
| JET-PROPULSION PLANTS | ||
| F02M | 62 hits | |
| SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF | ||
| F02N | 13 hits | |
| STARTING OF COMBUSTION ENGINES | ||
| F02P | 10 hits | |
| IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES | ||
| F03B | 16 hits | |
| MACHINES OR ENGINES FOR LIQUIDS | ||
| F03C | 1 hits | |
| POSITIVE-DISPLACEMENT ENGINES DRIVEN BY LIQUIDS | ||
| F03D | 118 hits | |
| WIND MOTORS | ||
| F03G | 5 hits | |
| SPRING, WEIGHT, INERTIA, OR LIKE MOTORS | ||
| F04B | 34 hits | |
| POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS | ||
| F04C | 30 hits | |
| ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS | ||
| F04D | 56 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 | 39 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 | 73 hits | |
| DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS, WEDGES | ||
| F16C | 65 hits | |
| SHAFTS | ||
| F16D | 54 hits | |
| COUPLINGS FOR TRANSMITTING ROTATION | ||
| F16F | 38 hits | |
| SPRINGS | ||
| F16G | 12 hits | |
| BELTS, CABLES, OR ROPES, PREDOMINANTLY USED FOR DRIVING PURPOSES | ||
| F16H | 100 hits | |
| GEARING | ||
| F16J | 42 hits | |
| PISTONS | ||
| F16K | 48 hits | |
| VALVES | ||
| F16L | 68 hits | |
| PIPES | ||
| F16M | 11 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 | 3 hits | |
| SAFETY DEVICES 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 | 2 hits | |
| PIPE-LINE SYSTEMS | ||
| F21K | 26 hits | |
| LIGHT SOURCES NOT OTHERWISE PROVIDED FOR | ||
| F21L | 3 hits | |
| LIGHTING DEVICES OR SYSTEMS THEREOF, BEING PORTABLE OR SPECIALLY ADAPTED FOR TRANSPORTATION | ||
| F21S | 71 hits | |
| NON-PORTABLE LIGHTING DEVICES OR SYSTEMS THEREOF | ||
| F21V | 109 hits | |
| FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF | ||
| F21W | 14 hits | |
| FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF | ||
| F21Y | 68 hits | |
| FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF | ||
| F22B | 7 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 | 5 hits | |
| METHODS OR APPARATUS FOR COMBUSTION USING FLUENT FUEL | ||
| F23D | 12 hits | |
| BURNERS | ||
| F23G | 3 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 | 9 hits | |
| AIR SUPPLY | ||
| F23M | 3 hits | |
| CONSTRUCTIONAL DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR | ||
| F23N | 9 hits | |
| REGULATING OR CONTROLLING COMBUSTION | ||
| F23R | 47 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 | 50 hits | |
| OTHER DOMESTIC STOVES OR RANGES | ||
| F24D | 27 hits | |
| DOMESTIC- OR SPACE-HEATING SYSTEMS, e.g. CENTRAL HEATING SYSTEMS | ||
| F24F | 56 hits | |
| AIR-CONDITIONING | ||
| F24H | 19 hits | |
| FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, IN GENERAL | ||
| F24J | 36 hits | |
| PRODUCTION OR USE OF HEAT NOT OTHERWISE PROVIDED FOR | ||
| F25B | 61 hits | |
| REFRIGERATION MACHINES, PLANTS, OR SYSTEMS | ||
| F25C | 4 hits | |
| PRODUCTION, WORKING, STORING, OR DISTRIBUTION OF ICE | ||
| F25D | 24 hits | |
| REFRIGERATORS | ||
| F25J | 2 hits | |
| LIQUEFACTION, SOLIDIFICATION, OR SEPARATION OF GASES OR GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT | ||
| F26B | 10 hits | |
| DRYING SOLID MATERIALS OR OBJECTS BY REMOVING LIQUID THEREFROM | ||
| F27B | 9 hits | |
| FURNACES, KILNS, OVENS, OR RETORTS IN GENERAL | ||
| F27D | 12 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 | ||
| F28D | 33 hits | |
| HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT | ||
| F28F | 33 hits | |
| DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION | ||
| F41A | 13 hits | |
| FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS | ||
| F41B | 1 hits | |
| WEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE | ||
| F41C | 2 hits | |
| SMALLARMS, e.g. PISTOLS, RIFLES | ||
| F41F | 4 hits | |
| APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS | ||
| F41G | 9 hits | |
| WEAPON SIGHTS | ||
| F41H | 12 hits | |
| ARMOUR | ||
| F41J | 1 hits | |
| TARGETS | ||
| F42B | 7 hits | |
| EXPLOSIVE CHARGES, e.g. FOR BLASTING | ||
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| Vane assembly with improved vane roots | |
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| Method and device for coating path generation | |
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| Cooled aerofoil for a gas turbine engine | |
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| Mid turbine frame system for gas turbine engine | |
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| Turbine case impingement cooling for heavy duty gas turbines | |
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| Device to control the radial clearance of the rotor of a gas turbine | |
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| Method of making composite fan blade | |
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| Turbine blade | |
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| Turbine vane | |
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| Turbine blade | |
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| Supersonic turbine moving blade and axial-flow turbine | |
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| Method of finishing a fan blade | |
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| Fan blade protection system | |
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| Method of improving fatigue strength in a fan blade and corresponding fan blade | |
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| 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 | |
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| Manufacturing method for a ceramic fiber reinforced ceramic composite component with internal three-dimensionally woven platform and corresponding component | |
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| Hybrid part made from monolithic ceramic skin and cmc core | |
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| Rotor assembly and reversible turbine blade retainer therefor | |
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| Impingement Cooled Nozzle Liner | |
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| Variable cycle turbine engine | |
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| Method for forming nozzle segments | |
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| Seal assembly for a rotational fluid metering valve | |
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| Fan blade with sheath | |
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| System and method for supporting a nozzle assembly | |
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| Plug assembly for blade outer air seal | |
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| Abrasive airfoil tip | |
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| Mechanism for turbine engine start from low spool | |
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| Radial spline arrangement for LPT vane clusters | |
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| Flowpath insert and assembly | |
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| Chordal mounting arrangement for low-ductility turbine shroud | |
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| Blade for a gas turbine and method for producing such a blade | |
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| Method for creating a platform cooling passage in a turbine rotor blade and corresponding platform cooling passage | |
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| TURBINE | |
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| AIRCRAFT GAS TURBINE | |
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| Liquid metal cooled blade | |
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| Seal system for a gas turbine | |
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| 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 | |
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| Rotor blade | |
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| Aeroengine fan assembly | |
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| Filtration system for gas turbines | |
| EP2072759A3 | 2012-12-26 |
| Turbine engine blade with multi-layer protective coating for the interior cooling passages | |
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| Engine bearing compartment | |
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| Cooling system for turbine airfoil including ice-cream-cone-shaped pedestals | |
| EP2538020A2 | 2012-12-26 |
| Gas Turbines | |
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| Methods and systems for cooling a transition nozzle | |
| EP2538027A2 | 2012-12-26 |
| Methods and systems for transferring heat from a transition nozzle | |
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| Combustor assembly for use in a turbine engine and methods of assembling same | |
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| Pressure and temperature actuation system | |
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| Composite article including silicon oxycarbide layer | |
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| Ventilated compressor rotor for a turbine engine and corresponding manufacturing method | |
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| 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 | |
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| 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 | |
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| Airfoil trailing edge cooling | |
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| Investment casting of cooled turbine airfoils | |
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| Component with cooling channels and method of manufacture | |
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| Component with cooling channels and method of manufacture | |
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| Hot gas path component and corresponding method of forming a component | |
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| Propulsion system with contrarotating open rotors and its balancing method | |
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| Propulsion system with contrarotating open rotors and its balancing method | |
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| Pressure housing | |
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| Ni-based alloy, and turbine rotor and stator blade for gas turbine | |
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| Ni-based alloy for casting used for steam turbine and casting component of steam turbine | |
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| Blade of a turbomaschine | |
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| Radially movable seal system for a gas turbine | |
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| Rotor with sealing element for a stationary gas turbine | |
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| Labyrinth seal system for a gas turbine | |
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| Method for starting a stationary gas turbine | |
| EP2538054A1 | 2012-12-26 |
| STRUCTURE FOR GAS TURBINE CASING | |
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| Portable boroscope for inspecting turbomachine blades | |
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| Interturbine duct strut and vane ring for gas turbine engine | |
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| Vane with integral inner air seal | |
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| Turbine blade and fixation structure thereof | |
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| Method for repairing composite containment casings | |
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| System for supplying air to a vehicle having a turbofan engine | |
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| Vane assembly with improved vane roots | |
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| Turbofan engine bearing support | |
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| Turbofan engine comprising a fan rotor support | |
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| Method of repairing a turbine nozzle segment in a turbine engine | |
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| Method and apparatus to repair a turbomachine rotor wheel | |
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| 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 | |
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| Turbine seal system and method of assembly thereof | |
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| Surge margin control for a gas turbine engine | |
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| W-shaped seal | |
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| Turbocharger variable-nozzle assembly with vane sealing ring | |
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| A retention device for a rotating blade | |
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| Blade mounting system | |
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| A bearing chamber apparatus | |
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| Rotor device for a jet engine with a disc and multiple rotor blades | |
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| Turbocharger, notably for a combustion engine | |
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| Turbocharger, notably for a combustion engine. | |
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| Turbocharger, notably for a combustion engine | |
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| Method for friction soldering blades to an axial compressor drum, and corresponding device | |
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| Rotor blade root section with cooling passage and method for supplying cooling fluid to a rotor blade | |
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| 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 | |
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| Bimaterial turbine blade damper | |
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| 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 | |
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| 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 | |
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| 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 | |
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| Interstage seal for a gas turbine and corresponding gas turbine | |
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| A seal in a gas turbine and a method of manufacturing a seal | |
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| Gas turbine engine case | |
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| A blade mounting | |
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| Sheath for use on airfoil components | |
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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 | |
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| 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 | |
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| 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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| An apparatus and a method of shaping an edge of an aerofoil | |
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| An apparatus and a method of shaping an edge of an aerofoil | |
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| Fuel air heat exchanger | |
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| Bearing assembly | |
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| Water separator and method for separating water from a saturated steam flow | |
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| Linear transition duct for a gas turbine | |
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| 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 | |
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| 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 | |
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| 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 | |
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| Variable geometry vane assembly for a turbocharger | |
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| Turbine power generation system and corresponding operating method | |
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| Aeroengine bleed valve | |
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| Bearing mounting system in a low pressure turbine | |
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| Turbine rotor apparatus and system | |
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| Shrouded single crystal dual alloy turbine disk | |
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| Gas turbine blade | |
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| Aero engine bleed valve | |
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| Aeroengine bleed valve | |
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| Double feeding for the serpentine of a cooled blade | |
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| Retention ring for gas turbine | |
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| Non-uniform stator vane spacing in a compressor and methods of installation | |
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| Cantilevered stator stage | |
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| Flade Duct Turbine Cooling And Power And Thermal Management | |
| EP2527602A2 | 2012-11-28 |
| Turbomachine comprising a thermocouple well and method of mounting a thermocouple well in a turbomachine | |
| EP2527592A2 | 2012-11-28 |
| Tool for removing pins from a gas turbine casing | |
| EP2527598A2 | 2012-11-28 |
| Gas turbine compressor last stage rotor blades with axial retention | |
| EP2527597A2 | 2012-11-28 |
| Turbine blade with curved film cooling passages | |
| EP2527601A2 | 2012-11-28 |
| Heating system for use in a turbine engine and method of operating same | |
| EP2527595A2 | 2012-11-28 |
| Balancing of rotatable components for a gas turbine engine | |
| EP2527599A2 | 2012-11-28 |
| Apparatus to seal with a turbine blade stage in a gas turbine | |
| EP2527073A1 | 2012-11-28 |
| Dissimilar metal weld and its manufacturing method of large welded structures such as the turbine rotor | |
| EP2527600A1 | 2012-11-28 |
| Turbo machine | |
| EP2527605A1 | 2012-11-28 |
| Gas turbine engine module adapter to a carrier | |
| EP2527253A1 | 2012-11-28 |
| De-icing device for an aviation gas turbine engine | |
| EP2527596A1 | 2012-11-28 |
| TURBINE ROTOR BLADE AND TURBO MACHINE | |
| EP2527077A1 | 2012-11-28 |
| METHOD FOR REPAIRING WALL MEMBER WITH PASSAGE | |
| EP2527619A1 | 2012-11-28 |
| INSERT REMOVAL DEVICE FOR GAS TURBINE STATIONARY BLADE AND INSERT REMOVAL METHOD FOR GAS TURBINE STATIONARY BLADE | |
| EP2527594A1 | 2012-11-28 |
| Random propylene copolymer with high stiffness and low haze | |
| EP2527604A1 | 2012-11-28 |
| An arrangement in which an inner cylindrical casing is connected to a concentric outer cylindrical casing | |
| EP2527593A1 | 2012-11-28 |
| Random propylene copolymer with high stiffness and low haze | |
close
| Title: | Porous ceramic coating system |
| Applicants: | SIEMENS AG |
| Inventors: | Stamm, Werner, Dr. |
| Main IPC Subclass: | C23C 28/00; C23C 28/04; F01D 5/28 |
| Application: | 2010-07-14 as 10007240.4 |
| Publication: | 2012-01-18 as EP2407579A1 |
| Patent FamilyFull Text | Register & FilePDF |
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| 1. | 57 | GENERAL ELECTRIC CO. |
| 2. | 43 | UNITED TECHNOLOGIES CORP. |
| 3. | 24 | ROLLS-ROYCE PLC |
| 4. | 13 | SIEMENS AG |
| 5. | 10 | PRATT & WHITNEY CANADA CORP. |
| 6. | 7 | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 7. | 7 | ALSTOM TECHNOLOGY LTD |
| 8. | 6 | HONEYWELL INTERNATIONAL INC. |
| 9. | 4 | HITACHI LTD. |
| 10. | 3 | AIRBUS OPERATIONS SAS |
| 11. | 3 | AKTIEBOLAGET SKF |
| 12. | 2 | TECHSPACE AERO S.A. |
| 13. | 2 | HAMILTON SUNDSTRAND CORP. |
| 14. | 2 | BOREALIS AG |
| 15. | 2 | ROLLS-ROYCE DEUTSCHLAND LTD & CO KG |
| 16. | 1 | K.K. TOSHIBA |
| 17. | 1 | INSTITUTO SUPERIOR TECNICO |
| 18. | 1 | NERCESSIAN, KEVORK |
| 19. | 1 | SIEMENS ENERGY, INC. |
| 20. | 1 | OERLIKON TRADING AG, TRUBBACH |
| 1. | 187 | GENERAL ELECTRIC CO. |
| 2. | 103 | UNITED TECHNOLOGIES CORP. |
| 3. | 66 | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 4. | 59 | ROLLS-ROYCE PLC |
| 5. | 52 | SIEMENS AG |
| 6. | 45 | TOYOTA JIDOSHA K.K. |
| 7. | 32 | PANASONIC CORP. |
| 8. | 25 | ROBERT BOSCH GMBH |
| 9. | 23 | PRATT & WHITNEY CANADA CORP. |
| 10. | 20 | ALSTOM TECHNOLOGY LTD |
| 11. | 20 | MITSUBISHI ELECTRIC CORP. |
| 12. | 19 | BSH BOSCH UND SIEMENS HAUSGERATE GMBH |
| 13. | 18 | HONEYWELL INTERNATIONAL INC. |
| 14. | 15 | YAMAHA HATSUDOKI K.K. |
| 15. | 15 | SHARP K.K. |
| 16. | 15 | HAMILTON SUNDSTRAND CORP. |
| 17. | 13 | JTEKT CORP. |
| 18. | 13 | LG ELECTRONICS INC. |
| 19. | 13 | AKTIEBOLAGET SKF |
| 20. | 12 | HONDA MOTOR CO., LTD. |
| 1. | 423 | GENERAL ELECTRIC CO. |
| 2. | 218 | SAMSUNG ELECTRONICS CO., LTD. |
| 3. | 185 | UNITED TECHNOLOGIES CORP. |
| 4. | 182 | SIEMENS AG |
| 5. | 177 | LG ELECTRONICS INC. |
| 6. | 176 | PANASONIC CORP. |
| 7. | 157 | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 8. | 141 | ZTE CORP. |
| 9. | 134 | TOYOTA JIDOSHA K.K. |
| 10. | 123 | SONY CORP. |
| 11. | 112 | SHARP K.K. |
| 12. | 109 | ROLLS-ROYCE PLC |
| 13. | 90 | CANON K.K. |
| 14. | 88 | K.K. TOSHIBA |
| 15. | 83 | ROBERT BOSCH GMBH |
| 16. | 80 | RESEARCH IN MOTION LTD. |
| 17. | 80 | HUAWEI TECHNOLOGIES CO., LTD. |
| 18. | 78 | MITSUBISHI ELECTRIC CORP. |
| 19. | 76 | HONEYWELL INTERNATIONAL INC. |
| 20. | 74 | ALCATEL LUCENT |
