Patent Assignment
Reel/Frame 038216/0193
Change of Name
Recorded: 2016-03-22
Pages: 32
Assignor
ALSTOM TECHNOLOGY LTD
Executed: 2015-11-02
Assignee
GENERAL ELECTRIC TECHNOLOGY GMBH
BROWN BOVERI STRASSE 7, 5400 BADEN, SWITZERLAND
Covered Properties
(957)
Burner
Patent:
5,738,508 →
Application:
08/597,029 →
Method of Operating a Sequentially Fired Gas-Turbine Group
Patent:
5,661,967 →
Application:
08/609,829 →
Combustion Chamber with Air Injector Systems Formed as a Continuation of the Combustor Cooling Passages
Patent:
5,832,732 →
Application:
08/662,798 →
Appatus for Cooling a Gas Turbine Combustion Chamber
Patent:
5,651,253 →
Application:
08/699,731 →
Process for the Production of a Body of Material Stable at High Temperatures from an Iron-Nickel Superalloy of the Type in 706
Patent:
5,846,353 →
Application:
08/707,603 →
Screw Retention Device
Patent:
5,711,644 →
Application:
08/707,605 →
Iron-Nickel Superalloy of the Type in 706
Patent:
5,863,494 →
Application:
08/707,610 →
Nickel-Base Superalloy
Patent:
5,888,451 →
Application:
08/738,106 →
Monocrystalline Nickel-Base Superalloy with Ti,Ta,and Hf Carbides
Patent:
5,759,301 →
Application:
08/738,107 →
Process for Applying a Metallic Adhesion Layer for Ceramic Thermal Barrier Coatings to Metallic Components
Patent:
5,894,053 →
Application:
08/743,936 →
Fluid Mixing Device with Vortex Generators
Patent:
5,803,602 →
Application:
08/744,270 →
Premix Burner
Patent:
5,833,451 →
Application:
08/746,139 →
Premix Burner
Patent:
5,791,894 →
Application:
08/747,569 →
Fuel Injector Arrangement; Method of Operating a Fuel Injector Arrangement
Patent:
6,095,791 →
Application:
08/755,978 →
Pressure Atomizer Nozzle
Patent:
5,934,555 →
Application:
08/811,006 →
Arrangement for the Thermal Protection of a Rotor of a High-Pressure Compressor
Patent:
5,842,831 →
Application:
08/822,920 →
Combustion Chamber
Patent:
5,885,068 →
Application:
08/828,540 →
Thermally Loaded Blade for a Turbomachine
Patent:
5,827,045 →
Application:
08/828,541 →
Burner
Patent:
5,857,846 →
Application:
08/839,645 →
Heat Treatment Process for Material Bodies Made of Nickel Base Superalloys
Patent:
5,882,446 →
Application:
08/843,642 →
Burner
Patent:
5,921,766 →
Application:
08/852,548 →
Device for Precontrolling the Feedwater of a Cooling-Air Temperature Controller for a Cooling-Air Cooler
Patent:
5,809,943 →
Application:
08/856,031 →
Temperature-Measuring Device
Patent:
6,142,665 →
Application:
08/865,054 →
Device for Separating Dust Particles
Patent:
5,837,019 →
Application:
08/891,786 →
Coolable Blade
Patent:
5,919,031 →
Application:
08/897,765 →
Premix Burner
Patent:
6,126,439 →
Application:
08/909,737 →
Coolable Blade
Patent:
5,934,874 →
Application:
08/916,789 →
Burner for Operating a Combustion Chamber
Patent:
5,954,496 →
Application:
08/919,476 →
Gas Turbine Having Sequential Combustion
Patent:
5,941,060 →
Application:
08/938,454 →
Process for Producing a Directionally Solidified Casting and Apparatus for Carrying Out This Process
Patent:
5,921,310 →
Application:
08/938,702 →
Heat Treatment Process for Material Bodies Made of a High-Temperature-Resistant Iron-Nickel Superalloy, and Heat-Treatment Material Body
Patent:
6,146,478 →
Application:
08/955,631 →
Gas Turbine Combustion Chamber with Two Stages and Enhanced Acoustic Properties
Patent:
6,050,078 →
Application:
08/965,865 →
Method for Controlling an Output of an Electrical Power Plant
Patent:
6,118,187 →
Application:
08/974,822 →
Burner Arrangement for a Gas Turbine for Preventing the Ingress of Fluids into a Fuel Passage
Patent:
6,038,863 →
Application:
08/984,688 →
Method of Cooling Thermally Highly Loaded Units of a Gas-Turbine Group
Patent:
6,085,514 →
Application:
08/999,256 →
Brush Seal and Method for the Manufacture of a Brush Seal
Patent:
6,079,714 →
Application:
09/024,705 →
Fuel Injector Arrangment for a Combustion Apparatus
Patent:
6,050,096 →
Application:
09/029,822 →
Method for Operating a Boiler Plant
Patent:
6,009,840 →
Application:
09/032,842 →
Cooled Gas-Turbine Blade
Patent:
5,993,155 →
Application:
09/034,231 →
Fully Martensitic Steel Alloy
Patent:
6,030,469 →
Application:
09/044,784 →
Method of Brazing Directionally Solidified or Monocrystalline Components
Patent:
6,050,477 →
Application:
09/050,901 →
Method for Operating a Gas Turbine Installation Combustion Chamber with Liquid Fuel
Patent:
6,067,789 →
Application:
09/074,312 →
Method for Protecting Against Vibrations in Rotary Machines
Patent:
6,330,515 →
Application:
09/079,179 →
Combustion Chamber
Patent:
6,106,278 →
Application:
09/079,396 →
Joint Between Two Joint Partners, and Its Use
Patent:
6,106,188 →
Application:
09/106,097 →
Control System for Controlling at Least One Variable of a Process as Well as a Use of Such a Control System
Patent:
6,167,690 →
Application:
09/110,898 →
Cooling System for the Leading-Edge Region of a Hollow Gas-Turbine Blade
Patent:
6,068,445 →
Application:
09/111,706 →
Cooling System for the Trailing Edge Region of a Hollow Gas Turbine Blade
Patent:
6,056,508 →
Application:
09/111,778 →
Cooling System for the Leading-Edge Region of a Hollow Gas-Turbine Blade
Patent:
6,168,380 →
Application:
09/111,874 →
Pressure Atomizer Nozzle
Patent:
6,045,058 →
Application:
09/114,883 →
Ceramic Liner
Patent:
5,957,067 →
Application:
09/119,585 →
Pipeline System for the Controlled Distribution of a Flowing Medium and Method for Operating Such a Pipeline System
Patent:
6,021,677 →
Application:
09/133,668 →
Pressure-Measuring Device
Patent:
6,053,048 →
Application:
09/133,669 →
Optic Pyrometer for Gas Turbines
Patent:
6,109,783 →
Application:
09/137,681 →
Combustor Plenum Having Flow Manipulators
Patent:
6,055,813 →
Application:
09/141,585 →
Turbine Blade of a Gas Turbine
Patent:
6,033,181 →
Application:
09/141,586 →
Cooling Arrangement for Gas-Turbine Components
Patent:
6,261,053 →
Application:
09/151,809 →
Combined Pressure Atomizing Nozzle
Patent:
6,378,787 →
Application:
09/152,515 →
Platform Cooling for Gas Turbines
Patent:
6,082,961 →
Application:
09/152,516 →
Method for Regulating the Power of Turbo Set, Device for Carrying Out the Method and Use of the Method
Patent:
6,216,437 →
Application:
09/153,020 →
Burner for Operating a Heat Generator
Patent:
5,944,511 →
Application:
09/153,269 →
Coatings for Turbine Components
Patent:
6,168,875 →
Application:
09/165,567 →
Burner for Operating a Heat Generator
Patent:
6,059,565 →
Application:
09/178,578 →
Method for Operating a Premix Burner
Patent:
6,270,338 →
Application:
09/179,460 →
Method and Device for Operating a Premix Burner
Patent:
6,132,202 →
Application:
09/179,462 →
Burner for Operating a Heat Generator
Patent:
6,027,331 →
Application:
09/187,343 →
Heat Shield
Patent:
6,492,034 →
Application:
09/190,364 →
Iron Aluminide Coating and Method of Applying an Iron Aluminide Coating
Patent:
6,245,447 →
Application:
09/201,780 →
Method of Operating a Gas-Turbine Group
Patent:
6,178,738 →
Application:
09/208,440 →
Method and Device for Injecting a Fuel/Liquid Mixture into the Combustion Chamber of a Burner
Patent:
6,491,236 →
Application:
09/208,441 →
Burner
Patent:
5,980,240 →
Application:
09/210,741 →
Blade and Method for Producing the Blade
Patent:
6,521,059 →
Application:
09/213,428 →
Burner for Operating a Heat Generator
Patent:
6,186,775 →
Application:
09/235,314 →
Method for Reliably Removing Liquid Fuel from the Fuel System of a Gas Turbine, and a Device for Carrying Out the Method
Patent:
6,256,975 →
Application:
09/255,710 →
Process for Producing a Casting Core, for Forming Within a Cavity Intended for Cooling Purposes
Patent:
6,374,898 →
Application:
09/268,722 →
Cooling-Air Bore
Patent:
6,183,199 →
Application:
09/271,267 →
Method of Producting a Noncircular Cooling Bore
Patent:
6,307,175 →
Application:
09/273,756 →
Gas Turbine Fuel Distributor Incorporating Separate Regulating Units
Patent:
6,189,321 →
Application:
09/289,492 →
Arrangement of Holes for Forming a Cooling Film
Patent:
6,267,552 →
Application:
09/312,061 →
Gas Turbine with a Plurality of Burners and a Fuel Distribution System, and a Method for Balancing a Fuel Distribution System
Patent:
6,293,105 →
Application:
09/339,945 →
Hollow-Cast Component
Patent:
6,193,468 →
Application:
09/345,509 →
Non-Contact Sealing of Gaps in Gas Turbines
Patent:
6,276,692 →
Application:
09/349,963 →
Method of Operating a Gas-Turbine Chamber with Gaseous Fuel
Burner Arrangement for a Gas Turbine Including an Inlet-Air Impingement Plate
Patent:
6,209,327 →
Application:
09/369,836 →
Burner Having a Frame for Operating an Internal Combustion Machine
Patent:
6,263,676 →
Application:
09/369,838 →
Turbomachine with Cooled Rotor Shaft
Patent:
6,224,328 →
Application:
09/371,904 →
Method and Apparatus for Casting Directionally Solidified Article
Patent:
6,311,760 →
Application:
09/373,719 →
Cooled Vane for Gas Turbine
Patent:
6,305,903 →
Application:
09/379,465 →
Burner for a Heat Generator and Method for Operating the Same
Patent:
6,210,152 →
Application:
09/379,470 →
Method for Minimizing Thermoacoustic Oscillations in Gas Turbine Combustion Chambers
Patent:
6,460,341 →
Application:
09/382,627 →
Method for Manufacture of a Directionally Solidified Columnar Grained Article
Patent:
6,568,456 →
Application:
09/382,630 →
Coating Composition for High Temperature Protection
Patent:
6,221,181 →
Application:
09/388,275 →
Method for Generating a Shell Mold for a Casting
Patent:
6,714,900 →
Application:
09/390,674 →
Fluid-Flow Machine for Compressing or Expanding a Compressible Medium
Patent:
6,264,425 →
Application:
09/397,510 →
Ignition Appliance for a Heat Generator
Patent:
6,322,353 →
Application:
09/397,511 →
Cooling Passage of a Component Subjected to High Thermal Loading
Patent:
6,343,474 →
Application:
09/401,309 →
Method and Apparatus for Controlling Thermoacoustic Vibrations in a Combustion System
Patent:
6,464,489 →
Application:
09/404,820 →
Sealing Arrangement
Patent:
6,312,218 →
Application:
09/414,968 →
Burner for Operating a Heat Generator
Patent:
6,152,726 →
Application:
09/417,846 →
Turbine Blade
Patent:
6,241,469 →
Application:
09/419,789 →
Turbomachine and Method of Use
Patent:
6,161,385 →
Application:
09/420,414 →
Cooled Components with Conical Cooling Passages
Patent:
6,923,247 →
Application:
09/431,178 →
Flow Duct with Cross-Sectional Step
Patent:
6,216,644 →
Application:
09/431,179 →
Gas Turbine Component
Patent:
6,277,500 →
Application:
09/433,079 →
High Frequency Heating Cooking Apparatus Ans Manufacturing Method Thereof
Patent:
6,196,835 →
Application:
09/434,448 →
Burner
Patent:
6,183,240 →
Application:
09/438,588 →
Ceramic Lining
Patent:
6,223,538 →
Application:
09/442,480 →
Cooling in Gas Turbines
Patent:
6,276,897 →
Application:
09/449,521 →
Coolable casing of a gas turbine or the like
Patent:
6,322,320 →
Application:
09/450,728 →
Blade Cooling
Patent:
6,328,532 →
Application:
09/450,729 →
Platform Cooling in Turbomachines
Patent:
6,309,175 →
Application:
09/456,332 →
Burner with Acoustically Damped Fuel Supply System
Patent:
6,305,927 →
Application:
09/458,095 →
Turbine Blade with Actively Cooled Shroud-Band Element
Patent:
6,340,284 →
Application:
09/471,410 →
Method and Apparatus for the Rapid Startup and Rapid Increase in Output of a Gas Turbine Plant
Patent:
6,378,285 →
Application:
09/482,081 →
Method for coating and welding stator vanes of a gas turbine
Patent:
6,131,800 →
Application:
09/493,135 →
Cooled Gas Turbine Component with Adjustable Cooling
Patent:
6,416,279 →
Application:
09/499,398 →
Fluid-flow machine component
Patent:
6,343,914 →
Application:
09/499,399 →
Fuel lance for spraying liquid and/or gaseous fuels into a combustion chamber
Patent:
6,325,618 →
Application:
09/503,709 →
Fuel Lance for Spraying Liquid and/or Gaseous Fuels into a Combustion Chamber, and Method of Operating Such a Fuel Lance
Patent:
6,402,059 →
Application:
09/503,711 →
Burner for a Heat Generator
Patent:
6,461,151 →
Application:
09/531,184 →
Heat shield for a gas turbine
Patent:
6,361,273 →
Application:
09/540,526 →
Combustion chamber for a gas turbine
Patent:
6,351,947 →
Application:
09/543,079 →
Appliance for operating a gas turbine installation combustion chamber with liquid fuel
Patent:
6,230,482 →
Application:
09/550,283 →
Heat shield for a gas turbine
Patent:
6,302,642 →
Application:
09/551,565 →
Coolable blade for a gas turbine
Patent:
6,347,923 →
Application:
09/552,567 →
Casting Furnace with Centrally Located Heating Element for Producing Directionally Solidified Castings
Patent:
6,523,599 →
Application:
09/556,310 →
Coating Containing Nial-B Phase
Patent:
6,471,791 →
Application:
09/573,869 →
Process for Producing or Repairing Cooling Channels in Monocrystalline Components of Gas Turbines
Patent:
6,405,435 →
Application:
09/584,714 →
Cooling Arrangement for Blades of a Gas Turbine
Patent:
6,422,811 →
Application:
09/593,162 →
Premix burner
Patent:
6,331,109 →
Application:
09/624,258 →
Method for active suppression of hydrodynamic instabilities in a combustion system and a combustion system for carrying out the method
Patent:
6,343,927 →
Application:
09/625,041 →
Seal Between Static Turbine Parts
Patent:
6,431,825 →
Application:
09/628,328 →
Fastening devices for heat-protection shields
Patent:
6,361,274 →
Application:
09/632,795 →
Process for Strengthening the Grain Boundaries of a Component Made from a Ni Based Superalloy
Patent:
6,471,790 →
Application:
09/635,360 →
Friction-Susceptible Component of a Thermal Turbo Machine
Patent:
6,499,943 →
Application:
09/635,529 →
Method for Generating Hot Gases in a Combustion Device and Combustion Device for Carrying Out the Method
Patent:
6,449,951 →
Application:
09/637,866 →
Fastening and Fixing Device
Patent:
6,726,391 →
Application:
09/638,002 →
Method for Operating a Power Plant Having Turbine Cooling
Patent:
6,560,966 →
Application:
09/645,548 →
Hollow-Cast Component
Patent:
6,516,865 →
Application:
09/650,407 →
Turbo Machine
Patent:
6,499,944 →
Application:
09/657,304 →
Control of Primary Measures for Reducing the Formation of Thermal Nitrogen Oxides in Gas Turbines
Patent:
6,584,775 →
Application:
09/665,056 →
A Burner with Damper for Attenuating Thermo Acoustic Instabilities
Patent:
6,490,864 →
Application:
09/684,982 →
Three Degrees of Freedom Aft Mounting System for Gas Turbine Transition Duct
Patent:
6,442,946 →
Application:
09/712,735 →
Turbine Blade with Actively Cooled Shroud-Band Element
Arrangement for Cooling a Flow-Passage Wall Surrounding a Flow Passage, Having at Least One Rib Feature
Patent:
6,666,262 →
Application:
09/726,052 →
Cooled Heat Shield
Iron aluminide coating and method of applying an iron aluminide coating
Blade for Gas Turbines with Choke Cross Section at the Trailing Edge
Drilled Cooling Air Openings in Gas Turbine Components
Vmethod of and Appliance for Suppressing Flow Eddies Within a Turbomachine
Patent:
6,698,209 →
Application:
09/754,186 →
Nondestructive Method for Determining the Thickness of a Metallic Protective Layer on a Metallic Base Material via a Different Type of Layer Between the Metallic Protective Layer and Teh Metallic Base Material
Cooled Blade for a Gas Turbine
Method for Fixing a Ceramic Component in a Metallic Support
Platelike Projecting Component Portion of a Gas Turbine
Tip Material for a Turbine Blade and Method of Manfacturing or Repairing a Tip of a Turbine Blade
Method and Device for Demounting a Turbine Blade
Blade Arrangement with Damping Elements
Process for Producing a Thermally Loaded Casting
Apparatus for Damping Acoustic Vibrations in a Combustor
Method of Adjusting the Size of Cooling Holes of a Gas Turbine Component
Burner for Heat Generator
Patent:
6,702,574 →
Application:
09/869,062 →
Process for Repairing a Coated Component
Method for Cooling a Gas Turbine System and a Gas Turbine System for Performing This Method
Airfoil Trailing Edge Cooling Construction
Gas Turbine Airfoill
Turbine Blade with Rub Tolerant Cooling Construction
Airfoil Tip Squealer Cooling Construction
Labyrinth Seal for Rotating Shaft
Method for Producing a Cooled, Lost-Wax Cast Part
Premix Burner
Carrier for Guide Vane and Heat Shield Segment
Patent:
6,514,041 →
Application:
09/949,636 →
High-Temperature Alloy
Process for the Regeneration of a Catalyst Plant and Apparatus for Performing the Process
Method and Device for Producing Hot Working Gases
Method and Apparatus for the Rapid Startup and Rapid Increase in Output of a Gas Turbine Plant
Cooled Component, Casting Core for Manufacturing Such a Component, as Well as Method for Manufacturing Such a Component
Method for Injecting Fuel into a Burner
Method for Operating a Combustion Chamber
Burner System with Staged Fuel Injection and Method for Its Operation
Damper Arrangement for Reducing Combustion-Chamber Pulsations
Sealing Arrangement Between Components of a Rotating Assembly as Well as a Method for Producing a Sealing Joint
Gas Turbo-Group
Probe for Measuring Pressure Oscillations
Exhaust Gas System with Helmholtz Resonator
Premix Burner Arrangement for Operating a Combustion Chamber
Premix Burner Arrangement with Catalytic Combustion as Well as Method for Its Operation
Method for Producing a Cast Part, Model Mold, and Ceramic Insert for Use in This Method
Gas Turbine Set
Process for Controlling the Cooling Air Mass Flow of a Gas Turbine Set
Patent:
6,523,346 →
Application:
09/993,673 →
Fixation Device for Blading of a Turbo-Machine
Device for Cooling a Shroud of a Gas Turbine Blade
Process for the Rapid Production of Hollow Components of Flow Machines for Manufacturing Development
Method for Operating a Premix Burner
Flow Machine and Process of Operation
Burner with High Flame Stability
Process for the Operation of a Gas Turbine Plant and Related Gas Turbine Plant
Device and Method for Cooling a Platform of a Turbine Blade
Arrangement for Using a Plate Shaped Element with Through-Openings for Cooling a Component
Burner for the Production of a Hot Gas
Platform Arrangement in an Axial-Throughflow Gas Turbine with Improved Cooling of the Wall Segments and a Method for Reducing the Gap Losses
Cooling System and Method for Cooling a Turbo-Machine Housing
Apparatus and Process for Impingement Cooling of a Component Exposed to Heat in a Flow Power Machine
Component of a Flow Machine
Device for Reducing the Sealing Gap Between a Rotating Component and a Stationary Component Inside a Rotary Turbo-Engine Through Which a Flow Passes Axially
Catalyzer
Process for the Operation of an Annular Combustion Chamber, and Annular Combustion Chamber
Gas Turbine Plant
Re-Fired Gas Turbine Engine
Method for Igniting a Thermal Turbomachine
Method of Repairing a Ceramic Coating
Gas Turbine
Gas Turbine Seal
Catalytic Burner
Catalyzer
Catalyzer
Method for Isothermal Brazing of Single Crystal Components
Burner System
Method for Running Up a Gas Turbine Plant
Fuel Supply System and an Associated Operating Method
Device and Process for Producing a Soldered Joint Between Two Joining Partners Which Can Be Joined by Means of a Common Contact Surface
Method of Fitting an Impingement Plate
Computerized Electronic Runout
Rotor for a Gas Turbine
Patent:
6,808,362 →
Application:
10/204,479 →
Process for Treating a Coated Gas Turbine Part, and Coated Gas Turbine Part
Turbogroup of a Power Generating Plant
Process for Producing a Groove-Like Recess, and a Groove-Like Recess of This Type
Combustion Device for Generating Hot Gases
Method and Device for Fixing a Ceramic Component in a Metallic Support
Deformable Brush Seal Support
Nickel-Base Superalloy
Patent:
6,706,241 →
Application:
10/291,392 →
Device for Separating Dirt and Debris in Flowing Media
Method for Operating a Burner and Burner with Stepped Premix Gas Injection
Membrane Seals
Fluidic Control of Fuel Flow
Directionally Solidified Columnar Grained Article and Apparatus for Manufacture Thereof--
Exhaust Gas Housing of a Thermal Engine
Method for the Reduction of Combustion-Driven Oscillations in Combustion Systems and Premixing Burner for Carrying Out the Method
Thermal Turbomachine, Axial Flow Gas Turbine in Particular
Method for Introducing Fuel into a Premix Burner
Method and Appliance for Supplying Fuel to a Premixiing Burner
Sealing Arrangement
Nickel-Base Superalloy
Quasicrystalline Alloys and Their Use as Coatings
Catalytic Burner
Tip Material for a Turbine Blade and Method of Manufacturing or Repairing a Tip of a Turbine Blade
Reheat Combustion System for a Gas Turbine
Burner Unit and Method for Operation Thereof
Method for the Production of a Burner Unit
Damping Arrangement for Reducing Combustion-Chamber Pulsation in a Gas Turbine System
Mcraly-Coating
Method of Growing a Mcraly-Coating and an Article Coated with the Mcraly-Coating
Device for Separating Dust and Dirt Out of Flowing Media
Intermetallic Material and Use of This Material
Premixing Burner Arrangement for Operating a Combustion Chamber in Addition to a Method for Operating a Combustion Chamber
Gap Seal for Sealing a Gap Between Two Adjacent Components
Atomizer Device and Method for the Production of a Liquid-Gas Mixture
Burner and Pilot Burner
Annular Combustor for a Gas Turbine
Premix Burner and Method of Operation
Method of Protecting a Local Area of a Component
Gas Turbine Set
Bellows Seal
Process for Operation of a Burner with Controlled Axial Central Air Mass Flow
Method for Operating a Combined-Cycle Power Station
Seal Assembly
Method for Operating a Premix Burner
Fogging Device for Gas Turbines
Method for Fabricating, Modifying or Repairing of Single Crystal or Directionally Solidified Articles
Turbine Blade
Method and Device for Affecting Thermoacoustic Oscillations in Combustion Systems
Sealing Arrangements
Combustion Method and Burner for Carrying Out the Method
Combustion Chamber
Method of Installing Spiral Threaded Inserts and Installation Tool
Hybrid Blade for Thermal Turbomachines
Extraction Tool for Extracting Spiral Threaded Inserts and Use of the Extraction Tool
Process for Strengthen Grain Boundaries of an Article Made from a Ni Based Superalloy
Process for the Regeneration of a Catalyst Plant and Apparatus for Performing the Process
Rotor End Piece
Device for Efficient Usage of Cooling Air for Acoustic Damping of Combustion Chamber Pulsations
Seal System
Methods and Apparatus for Starting Up Emission-Free Gas-Turbine Power Stations
Axial-Flow Thermal Turbomachine
Axial-Flow Thermal Turbomachine
Method and Arrangement for Adapting a Parameter of a Hot Gas of a Hot-Gas Generator Having a Downstream Technological Process
Gas Turbine Having Exhaust Recirculation
Device for Filtering Particles Out of a Coolant Flow in a Turbo Machine
Process for Controlling the Cooling Air Mass Flow of a Gas Turbine Set
Turbomachine
Turbomachine
Fuel Supply System and an Associated Operating Method
Gas Turbo Set
Method and Apparatus for Achieving Power Augmentation in Gas Turbines Using Wet Compression
Method and Apparatus for Achieving Power Augmentation in Gas Turbines Using Wet Compression
Thermally Loaded Component
Hot Gas Path Assembly
Gas Turbine Arrangement
Method for Injecting a Fuel-Air Mixture into a Combustion Chamber
Burner with Stepped Fuel Injection
Support for a Reflective Target
Catalytic Reactor and Associated Operating Method
Method for Operating a Gas Turbine Group
Combustion Chamber for a Gas Turbine
Burner Arrangement for the Annular Combustion Chamber of a Gas Turbine
Method of Reconditioning a Turbine Blade
High-Temperature Protection Layer
Method for Operating a Turbine Group
Gas Turbine and Associated Cooling Method
Method of Controlled Remelting of or Laser Metal Forming on the Surface of an Article
Method of Removing Casting Defects
Apparatus for Manufacture of Directionally Solidified Columnar Grained Article Thereof
Burner Having a Burner Lance and Staged Fuel Injection
Method of Determining the Elastoplastic Behavior of Components Consisting of Anisotropic Material and Use of the Method
Rotor Blade for a Flow Machine, and an Associated Pulling-Off Tool
Cooled Turbine Blade or Vane
Process of Masking Cooling Holes of a Gas Turbine Component
Method for Operating a Gas Turbine and Gas Turbine System for Carrying Out the Method
Gas Turbine Airfoil Leading Edge Cooling Construction
Turbine Rotor Blade for Gas Turbine Engine
Method for Casting a Directionally Solidified Article
Compressor Rotor Blade
Process of Masking Cooling Holes of a Gas Turbine Component
Flange for Flame Observation
Method for Operating a Compressor
Burner with Staged Fuel Injection
Method of Producing a Composite Component
Method for Influencing and Monitoring the Oxide Layer on Metallic Components of Hot CO2/H20 Cycle Systems
Method for Operating a Gas Turbine Combustion Chamber Including a Plurality of Burners Arranged in Groups
Rotor with Core Surrounded by Shielding Rings
Adaptive Sensor Model
Hybrid Burner and Associated Operating Method
Method and Device for Mixing Fluid Flows
Method for the Combustion of a Fuel-Oxidizer Mix
Profiled Sealing Body with Spring Section
Method for Controlling the Microstructure of a Laser Metal Formed Hard Layer
Property Recovering Method
Method of Controlling the Injection of Liquid into an Inflow Duct of a Prime Mover or Driven Machine
Method for Combustion of a Fuel
Connecting Stator Elements
Patent:
43,611 →
Application:
11/181,003 →
Method and an Apparatus for Determining the Clearance Between a Turbine Casing and the Tip of a Moving Turbine Blade
Method for Operating a Furnace
Process and Apparatus for Producing Service Blades
Method of Operating a Gas Turbine Group
Rope Seal for Gas Turbine Engines
Method for Operating a Gas Turbine
Device and Method for Cooling a Housing of a Gas Turbine or a Combustion Chamber
Gas Supply Arrangement and Associated Method, Particularly for a Gas Turbine
Method for Measuring a Thickness of a Coating
Power Plant and Operating Method
Premix Burner
Turbomachine
Guide Vane Ring of a Turbomachine and Associated Modification Method
Apparatus for the Rapid Measurement of Temperatures in a Hot Gas Flow
Device for Sound Attenuation in a Flow Duct
Method for Determination of the Temperature, Mass-Averaged Over a Flow Cross-Section, of a Gas Flow in a Gas Turbine
Method and Apparatus for the Cooling of the Outer Shrouds of the Rotor Blades of a Gas Turbine
Optical Sensor Device for Local Analysis of a Combustion Process in a Combustor of a Thermal Power Plant
Method for Operating a Gas Turbine and a Gas Turbine for Implementing the Method
Method for Operating a Gas Turbine and a Gas Turbine for Implementing the Method
Method for Operating a Gas Turbine as Well as a Gas Turbine for Implementing the Method
Method for Operating a Gas Turbine and a Gas Turbine for Implementing the Method
Protection Process and Control System for a Gas Turbine
Automated Adaptive Machining of Obstructed Passages
Rotating Machine
Gas Turbine Installation
High Temperature Seal and Methods of Use
Apparatus and Method for Testing Combustion
Tile and Exo-Skeleton Tile Structure
Cooled Blade or Vane for a Gas Turbine
Method for Operating an Air-Breathing Engine
Method for Reducing the Nox Emissions from a Burner Arrangement Comprising a Plurality of Burners, and Burner Arrangement for Carrying Out the Method
Parametric Production of Drilled Cooling Holes
Fuel Injection System and Purging Method
Method for Injecting a Liquid Mist into an Intake Duct
Rotor Shaft, in Particular for a Gas Turbine
Sealing Arrangement, in Particular for the Blade Segments of Gas Turbines
Method for Operating a Power Plant
Power Plant
Method of Operating an Atomizing Arrangement
Method for Operating a Turbo Engine and Turbo Engine
Rotor for a Compressor
Apparatus for Injecting a Fuel-Air Mixture into a Combustion Chamber
Method of Using a Combustion Chamber for a Gas Turbine
Method to determine the internal structure of a heat conducting body
Burner for Premix-Type Combustion
Thermal Power Plant with Sequential Combustion and Reduced-CO2 Emission, and a Method for Operating a Plant of This Type
Method for the Introduction of Fuel into a Premixing Burner
Method and Apparatus for Achieving Power Augmentation in Gas Turbines Using Wet Compression
Method and Apparatus for Achieving Power Augmentation in Gas Turbines Using Wet Compression
Cooled Blade for a Gas Turbine
Conveyor Device
Masking Material for Holes of a Component
Premix Burner with a Swirl Generator Delimiting a Conical Swirl Space and Having Sensor Monitoring
Multiple Burner Arrangement for Operating a Combustion Chamber, and Method for Operating the Multiple Burner Arrangement
Method of Operating a Thermal Power Plant
Method of Operating a Thermal Power Plant
Turbomachine
Rotor End Piece
Combustor for a Gas Turbine
Leaf Seal, in Particular for a Gas Turbine, and Method of Producing It
Method of Processing Seals Like Leaf Seals
Process for Producing Leaves for Leaf Seal
Leaf Seal and Method of Producing a Leaf Seal
Burner
Method and Apparatus for Delivering a Liquid
Method for the Application of a Protective Coating to a Thermally Stressed Component
Method for the Operation of a Compressor of a Gas Turbine with Evaporative Cooling of the Compressor Induction Air
Gas Turbine Blade Shroud
Turbomachine Blade
Method of Modifying a Turbocompressor
Method of Dismantling a Portion of a Turbomachine
Mixer Assembly
Premix Burner with Staged Liquid Fuel Supply and Also Method for Operating a Premix Burner
Catalyzer
Combustor Liners
Method for Operating a Gas Turbine Group
Combustion Chamber
Hybrid Burner Lance
Combustion Chamber for a Gas Turbine
Blade with Shroud
Measuring Device for Measuring the Temperature of a Thermally Loaded Metallic Base Element, Provided with a Protective Surface Coating, and Method for Producing Such a Measuring Device
Gas Turbine Plant and Method of Operation
Burner for a Gas Turbine
Device for Fastening a Sequentially Operated Burner in a Gas Turbine Arrangement
Burner System with Staged Fuel Injection
Method of Processing Turbine Components
Premix Burner
Method and Device for Burning Hydrogen in a Premix Burner
Leaf Seal, in Particular for a Gas Turbine
Premix Burner with Mixing Section
Method of Producing a Hot Gas Component of a Turbomachine Including an Embedded Channel
Turbomachine Blade with Erosion and Corrosion Protective Coating and Method of Manufacturing
Method for Modifying a Multistage Compressor
Method for Operating a Turbocompressor
Method for the Operation of a Gas Turbo Group
Cross Flange Seal for a Pressure Vessel, Especially for a Turbomachine Casing
Sealing Element for Use in a Fluid-Flow Machine
Gas Turbine Airfoil with Leading Edge Cooling
Premixing Burner for Generating an Ignitable Fuel/Air Mixture
Turbo Machine
Premix Burner for Operating a Combustion Chamber
Method for the Heat Treatment of Nickel-Based Superalloys
Method and Device for the Combustion of Hydrogen in a Premix Burner
Heat Shield for Sealing a Flow Channel of a Turbine Engine
Heat Accumulation Segment
Premix Burner for a Gas Turbine Combustion Chamber
Method for Operating a Gas Turbine Plant
Ceramic Thermal Barrier Coating
Process for Extending the Cylic Service Life of Thermal Barrier Coatings, in Particular on Gas Turbine Components
Guide Vane Arrangement of a Turbomachine
Operating Method for a Turbogroup
Gap Seal in Blades of a Turbomachine
Vane Arrangement of a Turbo Machine
Method for Automatic Closed-Loop Control of One or More Combustion Temperatures in a Gas Turbine Installation and Method for Determination of the Water Content in the Working Fluid of a Gas Turbine Instalation
Sound Absorber for Gas Turbine Installations
Gas Turbogroup
Method for Protecting the Hot Gas Parts of a Gas Turbine Installation from Overheating and for Detecting Flame Extinction in the Combustion Chamber
Gas Turbine System for Injecting a Mixture of High Value Hydrocarbons Plural Distinct Fuels into the Gas Turbine Combustion Chamber
Combustion Chamber with Burner and Associated Operating Method
Apparatus for the Combustion of a Fuel-Oxidizer Mix
Gas Turbine with Axial Thrust Balance
Measuring Apparatus
Method for Designating a Component Having a Heat Insulation Layer and for Determining Its Operating Time
High-Temperature Alloy
Device and Method for Mounting a Turbine Engine
Method of Operating a Gas Turbine Power Plant
Burner for the Operation of a Heat Generator and Method of Use
Fuel Lance for a Gas Turbine Installation and a Method for Operating a Fuel Lance
Burner Arrangement
Combustor for a Gas Turbine Engine with Effusion Cooled Baffle
Methods of Reducing Emissions for a Sequential Combustion Gas Turbine and Combustor for a Gas Turbine
Fuel Lance for a Gas Turbine Engine Including Outer Helical Grooves
Method for Operating a Burner
Method of Depositing a Wear Resistant Seal Coating and Seal System
Method for Operating a Gas Turbine, Method of Operation of a Combined Cycle Power Plant, and Combined Cycle Power Plant
Fuel Distribution System for a Gas Turbine with Multistage Burner Arrangement
Method for Controlling a Gas Turbine in a Power Plant and Power Plant for Carrying Out the Method
Method for Operating a Gas Turbine and Also Gas Turbine for Carrying Out the Method
Device for Cleaning Oxidized or Corroded Components in the Presence of a Halogenous Gas Mixture
Combustion Chamber of a Combustion System
Combustion Chamber of a Combustion System
Gas Turbine Engine Fuel Supply Arrangement Using Plural Distinct Fuels
Wall Structure for Limiting a Hot Gas Path
Gas Turbine Airfoil
Operation of a Gas Turbine
Methods for the Protection of a Thermal Barrier Coating System and Methods for the Renewal of Such a Protection
Gas Turbine Hot Gas Component Repair Method
Burner and Fuel Lance for a Gas Turbine Installation
Comprehensive Method for Local Application and Local Repair of Thermal Barrier Coatings
Continuous-Flow Machine, Turbine, or Compressor
System for Controlling a Combustion Process for a Gas Turbine
Method for Reducing Emissions from a Combustor
Combustor with Reduced Carbon Monoxide Emissions
Burner with Lance
Burner for a Second Chamber of a Gas Turbine Plant
Multilayer Thermal Barrier Coating
Method for Operating a Gas Turbine
Method for Oxidising a Thermocouple Sheath
Alignment of Machine Components Within Casings
High-Temperature Alloy
Apparatus for Broaching Repair of Turbine Rotor Steeples
Plug Assembly with Moveable Mounting Members
High-Temperature-Resistant Cobalt-Base Superalloy
Creep-Resistant Steel
Hydraulic Trip Unit for a Valve Unit in a Prime Mover Plant, Especially for a Fast-Acting Shut-Off Valve of a Turbine Plant
Shiplap Arrangement
Stator Heat Shield
Fluid Flow Machine
Method of Operating a Gas Turbine, and Gas Turbine with Water Injection
Multi-Vane Segment Design and Casting Method
Power Plant and Operating Method
Rotor Blade Arrangement and Gas Turbine
Cool Flame Combustion
Application:
12/618,136 →
Publication:
US 2010/0089066
High Temperature and Oxidation Resistant Material
Combustion Chamber Arrangement for Operating a Gas Turbine
Hot Gas Component of a Turbomachine Including an Embedded Channel
Rotor Blade for a Gas Turbine
Turbine Blades
Burner of a Gas Turbine
Gas Turbine Installation with Flue Gas Recirculation Dependent on Oxygen Content of a Gas Flow
Heat Shield Segment for a Stator of a Gas Turbine
Conical Gas Turbine Burner Having a Fuel Lance with Inclined Side Nozzles
Burner for a Gas Turbine and Method for Feeding a Gaseous Fuel in a Burner
Burner Fuel Lance Configuration and Method of Use
Strip Seal and Method for Designing a Strip Seal
Cooling of a Gas Turbine Engine Downstream of Combustion Chamber
Method for Improving the Sealing on Rotor Arrangements
Injection Nozzle Having Constant Diameter Pin and Method for Operating the Injection Nozzle
Welding Additive Material
Method for Joining Two Rotationally Symmetrical Metal Parts by Tungsten Inert Gas (Tig) Welding, and a Device for Carrying Out the Method
Support for a Turbine
Burner of a gas turbine
Burner Including Non-Uniformly Cooled Tetrahedron Vortex Generators and Method for Cooling
Multilayer Thermal Protection System and Method for Making Same
Application:
12/723,559 →
Publication:
US 2010/0247953
Lamellar Seal for a Turbomachine
Process for Producing a Body Provided with a Slot as a Test Crack
Blade for an Axial Compressor and Manufacturing Method Thereof
Gas Turbine Stator/Rotor Expansion Stage Having Bumps Arranged to Locally Increase Static Pressure
Method for Reconditioning a Turbine Blade
Method for Operating a Gas Turbine Plant with a Compressor Station for Gaseous Fuel
Gas Turbine Vane with Improved Cooling
Method and Device for Combusting Hydrogen in a Premix Burner
Premix Burner for a Gas Turbine
Method for Operating a Gas Turbine Installation and Equipment for Carrying Out the Method
Fuel Injection Method
Turbine Stator Nozzle Cooling Structure
Slurry Formulation for the Production of Thermal Barrier Coatings
Guide Vane of a Gas Turbine and Method for Replacing a Cover Plate of a Guide Vane of a Gas Turbine
Method for Synchronizing an Electric Machine with an Electric Grid and Arrangement of an Electric Machine and an Electric Grid
Burner of a Gas Turbine
Method for Early Detection and Anticipatory Control of Consumer-End Load Shedding in an Electrical Grid, and Apparatus for Carrying Out the Method
Method for Operating a Gas Turbine Plant
Combustion Device of a Gas Turbine Including a Plurality of Passages and Chambers Defining Helmholtz Resonators
Gas Turbine
Method for Controlling a Gas Turbine in a Power Station, and a Power Station for Carrying Out the Method
Burner Arrangement, and Use of Such a Burner Arrangement
Method for Switching Over a Gas Turbine Plant from Gaseous Fuel to Liquid Fuel and Vice-Versa
Method and Burner Arrangement for the Production of Hot Gas, and Use of Said Method
Blade for a Gas Turbine
Turbine Blade
Hollow-Cast Casting with a Closure Device
Gas Turbine
Guide Vane for a Gas Turbine
Guide Vane Having Hooked Fastener for a Gas Turbine
Varying Cross-Sectional Area Guide Blade
Stator Blade for a Gas Turbine and Gas Turbine Having Same
Cooling Duct Arrangement Within a Hollow-Cast Casting
Method of Applying Multiple Materials with Selective Laser Melting on a 3D Article
Methods for Repairing a Gas Turbine Component
Abradable Coating System
Abrasive Single-Crystal Turbine Blade
Wear-Resistant and Oxidation-Resistant Turbine Blade
Leaf Seals
Application:
12/940,497 →
Publication:
US 2011/0182729
Rotor for an Axial-Throughflow Turbomachine and Moving Blade for Such a Rotor
Gas Turbine with a Stator Blade
Turbine Blade
Method of Estimating the Maximum Power Generation Capacity and for Controlling a Specified Power Reserve of a Single Cycle or Combined Cycle Gas Turbine Power Plant, and a Power Generating System for Use with Said Method
Seal and Seal Arrangement for Confining Leakage Flows Between Adjacent Components of Turbo-Machines and Gas Turbines
Sequential Combustor Gas Turbine Including a Plurality of Gaseous Fuel Injection Nozzles and Method for Operating the Smae
Process for Producing a 3-Dimensional Component by Selective Laser Melting (Slm)
Leaf Seal
Shroud Seal Segments Arrangement in a Gas Turbine
Turbine Guide Vane
Application:
13/012,317 →
Publication:
US 2011/0189002
Nickel-Base Superalloy with Improved Degradation Behavior
Method for Adjusting a Helmholtz Resonator and an Adjustable Helmholtz Resonator
Blade Arrangement of a Gas Turbine
Application:
13/024,545 →
Publication:
US 2011/0171039
Accelerated Cooling of a Gas Turbine
Application:
13/030,288 →
Publication:
US 2011/0214430
Combustion Device with a Layered Wall Structure for a Gas Turbine
Gas Turbine and Method for Its Operation
Valve Assembly
Blade for a Gas Turbine
Sealing Structure on a Shroud of a Turbine Blade
Gas Turbine Model and a Method for the Modeling of a Gas Turbine
Blade for a Gas Turbine
Gas Turbine Plant with Exhaust Gas Recirculation and Also Method for Operating Such a Plant
Cooled Blade for a Gas Turbine, Method for Producing Such a Blade, and Gas Turbine Having Such a Blade
Combustion Device for a Gas Turbine Configured to Suppress Thermo-Acoustical Pulsations
Lance of a Gas Turbine Burner
Method for Producing a Blade by Casting and Blade for a Gas Turbine
Cooled Blade for a Gas Turbine
Combined Cycle Power Plant with Flue Gas Recirculation
Combined Cycle Power Plant with Flue Gas Recirculation
Gas Turbine
Method for Optimizing the Contact Surfaces of Shroud Segments, Which Abut Against One Another, of Adjacent Blades of a Gas Turbine
Application:
13/117,166 →
Publication:
US 2011/0293428
Damper Arrangement and Method for Designing Same
Exhaust Gas Housing for a Gas Turbine and Method for Producing Same
Helmholtz Damper and Method for Regulating the Resonance Frequency of a Helmholtz Damper
Thermal Barrier Coating System, Components Coated Therewith and Method for Applying a Thermal Barrier Coating System to Components
Method for Checking the Bearing Alignment in a Gas Turbine
Lance of a Burner
Thermally Loaded, Cooled Component
Process for Producing a Single-Crystal Component Made of a Nickel-Based Superalloy
Gas Turbine Arrangement with Oval Flanged Secondary Air Openings and Method for Retrofitting Same
Application:
13/178,788 →
Publication:
US 2012/0017604
Method and Device for Adjusting the Rotor Position in a Gas Turbine or Steam Turbine
Gas Turbine with Flow Separation and Recirculation
Cooled Constructional Element for a Gas Turbine
Cooled Blade for a Gas Turbine
Reheat Burner
Gas Turbine Engine and Method for Cooling the Compressor of a Gas Turbine Engine
Reheat Burner
Process for Extending the Cyclic Service Life of Thermal Barrier Coatings, in Particular on Gas Turbine Components
Casing Body Through Which Hot Gases Can Flow and Comprising an Inner Heat Shield
Method for Operating a Combustion Chamber and Combustion Chamber
Application:
13/217,030 →
Publication:
US 2012/0047907
Method and Device for Ascertaining the Approach of the Lean Blow Off of a Gas Turbine Engine
Combustion Device
Premix Burner for a Gas Turbine
Burner Arrangement with Deflection Elements for Deflecting Cooling Air Flow
Braze Foil for High-Temperature Brazing and Methods for Repairing or Producing Components Using a Braze Foil
Patent:
8,235,275 →
Application:
13/232,109 →
Braze Alloy for High-Temperature Brazing and Methods for Repairing or Producing Components Using a Braze Alloy
Combustion Chamber and Method for Operating a Combustion Chamber
Gas Turbine
Gas Turbine with Improved Part Load Emissions Behavior
Blade for a Gas Turbine
Cooled Component for a Gas Turbine
Application:
13/247,429 →
Publication:
US 2012/0063891
Dual Brazing Alloy Element, Process for Producing It and Uses Thereof
Combined Cycle with Recirculation Plant Inlet Oxygen Concentration System
Power Plant and Method for Its Operation
Combined Cycle Plant Including Chilled Ammonia Based CO2 Capture Unit and Utilizing System Produced Nitric Acid
Blade Arrangement, Especially Stator Blade Arrangement
Method for Ascertaining Process Values for a Process Control
Method for Controlling a Gas Turbine and Gas Turbine for Implementing the Method
Gas Turbine Arrangement and Method for Operating a Gas Turbine Arrangement
Combustion Chamber and Method for Damping Pulsations
Rotating Machine
Method for Influencing, Damping, or Suppressing Mechanical Vibrations Occurring During Operation in a Turbomachine Blade, a Turbomachine Blade Useful for Carrying Out the Method, and a Piezoelectric Damping Element
Method of Analyzing and Controlling a Combustion Process in a Gas Turbine and Apparatus for Performing the Method
Combustion Chamber and Method for Supplying Fuel to a Combustion Chamber
Application:
13/312,116 →
Publication:
US 2012/0148962
Blade Arrangement for a Gas Turbine and Method for Operating Such a Blade Arrangement
Turbine Blade
Nickel-Based Superalloy
Industrial Plant with Noise Attenuation Hood
Filler Material for Welding
Application:
13/346,830 →
Publication:
US 2012/0187093
Method for Operating a Gas Turbine
Method for Operating a Power Plant and Gas Turbine Unit for Implementing the Method
Control of the Gas Composition in a Gas Turbine Power Plant with Exhaust Gas Recirculation
Application:
13/355,491 →
Publication:
US 2012/0186268
Sealing Arrangement for a Thermal Machine
Method for Repairing or Reconditioning a Badly Damaged Component, in Particular from the Hot Gas Region of a Gas Turbine
Turbomachine Component
Method for Combusting Hydrogen-Rich, Gaseous Fuels in a Burner, and Burner for Performing Said Method
Using Return Water of an Evaporative Intake Air Cooling System for Cooling a Component of a Gas Turbine
Gas Turbine Generator Set
Method for Switching Over a Gas Turbine Burner Operation from Liquid to Gas Fuel and Vice-Versa
Methods of Using Laser Optical Devices
Gas Turbine Combustor Including an Acoustic Damper Device
Component for a Turbomachine and Method for Manufacturing Such a Component
Application:
13/425,658 →
Publication:
US 2012/0251777
Gas Turbine Power Plant with Flue Gas Recirculation and Oxygen-Depleted Cooling Gas
Gas Turbine Air Intake Manifold Controllably Changing a Mechnical Rigidity of the Walls of Said Intake Manifold
Method for Operating a Gas Turbine Power Plant with Exhaust Gas Recirculation
Method for Protecting a Gas Turbine Engine Against High Dynamical Process Values and Gas Turbine Engine for Conducting the Method
Welded Rotor of a Gas Turbine Engine Compressor
Reheat Burner Injection System with Fuel Lances
Reheat Burner Injection System
Cooling Scheme for an Increased Gas Turbine Efficiency
Reheat Burner Injection System
Premixed Burner for a Gas Turbine Combustor
Flow Straightener and Mixer
Swirler Having Vanes Provided With At Least Two Lobes In Opposite Transverse Directions With Reference To A Vane Central Plane
An Emergency Shut-Off Signal Generator for a Valve Assembly
Gas Turbine Reheat Combustor Including a Fuel Injector for Delivering Fuel into a Gas Mixture Together with Cooling Air Previously Used for Convectively Cooling the Reheat Combustor
Turbomachine Clearance Control Configuration Using a Shape Memory Alloy or a Bimetal
Pressurized Casing
Method for Operating a Fuel Supply for a Heat Engine
Method for Cooling a Gas Turbine Plant and Gas Turbine Plant for Implementing the Method
Gas Turbine Blade and Method for Producing a Blade
Blade of a Turbomachine
Device for the Mutual Fixation of Two Components
Application:
13/552,771 →
Publication:
US 2013/0081404
Method for Operating a Gas Turbine and Gas Turbine Unit Useful for Carrying Out the Method
Compressor Rotor
Axial Compressor with an Injection Device for Injecting a Fluid
Method for Injecting Water into a Multistage Axial Compressor of a Gas Turbine
Method for Operating a Gas Turbine Power Plant with Flue Gas Recirculation
Control of Load Rejection
Method for Operating a Gas Turbine Plant and Gas Turbine Plant for Implementing the Method
method for operating a combustion device including injecting a fluid together with diluent fuel to address combustion pulsations
Vibration Damper for Rotating Parts
Method for Switching Over a Combustion Device Between a First Fuel and a Second Fuel
Gas Duct for a Gas Turbine and Gas Turbine Having Such a Gas Duct
Wall Structure with Noise Damping Insulation Properties and Gas Turbine with Such a Wall Structure
Gas Turbine
Gas Turbine Controller and a Method for Controlling a Gas Turbine
Method for Operating a Firing Plant
Self-Adjusting Device for Controlling the Clearance Between Rotating and Stationary Components of a Thermally Loaded Turbo Machine
Gas Turbine Airfoil with Shaped Trailing Edge Coolant Ejection Holes
Method for Operating a Gas Turbine Power Plant with Flue Gas Recirculation
Method and Apparatus for Detecting Combustion Conditions in Combustors of a Sequential Combustion Gas Turbine Engine
Operating Method for Hydrogen/Natural Gas Blends Within a Reheat Gas Turbine
Application:
13/649,502 →
Publication:
US 2013/0091852
Method for Manufacturing Components or Coupons Made of a High Temperature Superalloy
Application:
13/664,604 →
Publication:
US 2013/0263977
Process for the Production of Articles Made of a Gamma-Prime Precipitation-Strengthened Nickel-Base Superalloy by Selective Laser Melting (Slm)
Light Weight Shroud Fin for a Rotor Blade
Transitional Region for a Secondary Combustion Chamber of a Gas Turbine
Axial Compressor for Fluid-Flow Machines
Diffuser, in Particular for an Axial Flow Machine
Application:
13/678,676 →
Publication:
US 2013/0129498
Method of Estimating the Maximum Power Generation Capacity and for Controlling a Specified Power Reserve of a Single Cycle or Combined Cycle Gas Turbine Power Plant, and a Power Generating System for Use with Said Method
Damping System for Combustor
Apparatus and Method for the Forming of Turbine Vane Cover Plates
Exhaust Gas Housing for a Gas Turbine and Gas Turbine Having an Exhaust Gas Housing
High Pressure Compressor
Method for Operating a Gas Turbine
Application:
13/736,980 →
Publication:
US 2013/0174565
Method for Reconditioning a Blade of a Gas Turbine and Also a Reconditioned Blade
Control System
Flushing the Exhaust Gas Recirculation Lines of a Gas Turbine
Method for Operating a Combined Cycle Power Plant and Plant to Carry Out Such a Method
Methods of Operation of A Gas Turbine With Improved Part Load Emissions Behavior
Method for Early Detection and Anticipatory Control of Consumer-End Load Shedding in an Electrical Grid, and Apparatus for Carrying Out the Method
Axial Compressor
Method and Apparatus for Determining Geometry Deformation in Rotating Components
Application:
13/926,733 →
Publication:
US 2014/0000380
Stand-By Operation of a Gas Turbine
Application:
13/928,996 →
Publication:
US 2014/0000270
Compressor for a Gas Turbine and Method for Repairing and/or Changing the Geometry of and/or Servicing Said Compressor
Application:
13/929,366 →
Publication:
US 2014/0003926
Diffuser for the Exhaust Section of a Gas Turbine and Gas Turbine with Such a Diffuser
Cooled Blade for a Gas Turbine
Gas Turbine Combustion System
Burner Arrangement Including an Air Supply with Two Flow Passages
Axial Swirler for a Gas Turbine Burner
Premix Burner of the Multi-Cone Type for a Gas Turbine
Premix Burner of the Multi-Cone Type for a Gas Turbine
Combustor Arrangement with Slidable Multi-Cone Premix Burner
Method and Arrangement for Gas Turbine Engine Surge Control
Application:
13/939,748 →
Publication:
US 2014/0013765
Mixing Element for Gas Turbine Units with Flue Gas Recirculation
Method for Monitoring Machines with Rotating Shafts
Application:
13/948,748 →
Publication:
US 2014/0026650
Stationary Gas Turbine Arrangement and Method for Performing Maintenance Work
Near-Wall Roughness for Damping Devices Reducing Pressure Oscillations in Combustion Systems
Reheat Burner and Method of Mixing Fuel/Carrier Air Flow Within a Reheat Burner
Oxidation Resistant Nickel Alloy
Method for Manufacturing a Three-Dimensional Article
Application:
13/972,127 →
Publication:
US 2014/0053956
Method for Mixing a Dilution Air in a Sequential Combustion System of a Gas Turbine
Application:
13/974,523 →
Publication:
US 2014/0053569
Method for Mixing a Dilution Air in a Sequential Combustion System of a Gas Turbine
Modular Blade or Vane for a Gas Turbine and Gas Turbine with Such a Blade or Vane
Application:
14/012,101 →
Publication:
US 2014/0234088
Premix Burner
Method and Guide for Removing an Inner Casing from a Turbomachine
Method for Removing an Inner Casing from a Machine
Method and Cooling System for Cooling Blades of at Least One Blade Row in a Rotary Flow Machine
Gas Turbine Assembly and Corresponding Operating Method
Burner Including a Swirl Chamber with Slots Having Different Widths
Method for Operating a Gas Turbine with Sequential Combustion and Gas Turbine for Conducting Said Method
Burner for a Combustion Chamber of a Gas Turbine Having a Mixing and Injection Device
Gas Turbine and Turbine Blade for Such a Gas Turbine
Damper Arrangement for Reducing Combustion-Chamber Pulsation
Combustor Transition
Combustor Transition
Reheat Burner Arrangement Having an Increasing Flow Path Cross-Section
Axial Swirler
Method for Operating a Gas Turbine Burner with a Swirl Generator
Blade for a Gas Turbine and Casting Technique Method for Producing Same
Application:
14/075,555 →
Publication:
US 2014/0060766
Insert Element for Closing an Opening Inside a Wall of a Hot Gas Path Component of a Gas Turbine and Method for Enhancing Operational Behaviour of a Gas Turbine
Gas Turbine Temperature Measurement
Damping Device for a Gas Turbine Combustor
Gas Turbine Part Comprising a Near Wall Cooling Arrangement
Method for Manufacturing a Metallic Component by Additive Laser Manufacturing
Application:
14/091,780 →
Publication:
US 2014/0154088
Method and Gas Turbine Combustion System for Safely Mixing H2-Rich Fuels with Air
Apparatus for Broaching Repair of Turbine Rotor Steeples
Turbo-Machine with Active Electrical Clearance Control
Application:
14/152,108 →
Publication:
US 2014/0193237
Arrangement for Sealing an Open Cavity Against Hot Gas Entrainment
Method for Barring a Rotor of a Turbomachine and Barring Apparatus for Conducting Such Method
Gas Turbine Plant with Exhaust Gas Recirculation and Also Method for Operating Such a Plant
Application:
14/157,982 →
Publication:
US 2014/0130507
Gas Turbine Power Generation System Comprising an Emergency Power Supply System
Power Generating Unit and Method for Operating Such a Power Generating Unit
Application:
14/175,150 →
Publication:
US 2014/0225372
Turbomachine Component with an Erosion and Corrosion Resistant Coating System and Method for Manufacturing Such a Component
Method for Adjusting a Natural Gas Temperature for a Fuel Supply Line of a Gas Turbine Engine
Method for Manufacturing a Metal-Ceramic Composite Structure and Metal-Ceramic Composite Structure
Rotary Flow Machine and Method for Disassembling the Same
Method for Manufacturing a Hybrid Component
Labyrinth Seal
Method for Coating a Component of a Turbomachine and Coated Component for a Turbomachine
Method for Welding Rotors for Power Generation
Method for Welding Rotors for Power Generation
Rotor
Application:
14/245,320 →
Publication:
US 2014/0301851
Combustion Chamber for Adjusting a Mixture of Air and Fuel Flowing into the Combustion Chamber and a Method Thereof
Gas Turbine Thermal Shroud with Improved Durability
Method for Obtaining a Configuration for Joining a Ceramic Material to a Metallic Structure
Method for Automatic Positioning of a Gas Turbine Rotor
Gas Turbine Rotor Positioning Device
Can Combustor for a Can-Annular Combustor Arrangement in a Gas Turbine
Sensor Mounting Attachment
Gas Turbine Damper with Inner Neck Extending into Separate Cavities
Damper for Gas Turbines
Method for Closing an Aperture on a Blade of a Gas Turbine
Application:
14/280,786 →
Publication:
US 2014/0353289
Airfoil for Gas Turbine, Blade and Vane
Method for Additively Manufacturing an Article Made of a Difficult-to-Weld Material
Application:
14/303,880 →
Publication:
US 2014/0295087
Method and Device for Suppressing the Formation of Ice on Structures at the Air Intake of a Turbomachine
Method for Post-Weld Heat Treatment of Welded Components Made of Gamma Prime Strengthened Superalloys
Control of the Gas Composition in a Gas Turbine Power Plant with Flue Gas Recirculation
Application:
14/306,571 →
Publication:
US 2014/0290264
Pressure Casing of a Turbomachine
Application:
14/317,643 →
Publication:
US 2015/0010389
Gas Turbine Engine and Operations
Application:
14/317,758 →
Publication:
US 2015/0016964
Maintenance Assembly Adaptable Within Gas Turbine Engine
Stator Component with Segmented Inner Ring for a Turbomachine
Turbine Blade and Turbine with Improved Sealing
Gas Turbine with Improved Part Load Emissions Behavior
Rotor Shaft for a Turbomachine
Fluid Seal Arrangement and Method for Constricting a Leakage Flow Through a Leakage Gap
Application:
14/341,264 →
Publication:
US 2015/0050125
Intake Arrangement in Gas Turbine Power Plant
Damper for Combustion Oscillation Damping in a Gas Turbine
Operation of Gas Turbine Power Plant with Carbon Dioxide Separation
Shaft Coupling Assembly and Method for Coupling Shafts
Fixation Device for Turbine and Method for Applying Fixation
Sequential Combustion with Dilution Gas Mixer
Method for Producing a Near-Surface Cooling Passage in a Thermally Highly Stressed Component, and Component Having Such a Passage
Component for a Thermal Machine, in Particular a Gas Turbine
Combustor of a Gas Turbine with Pressure Drop Optimized Liner Cooling
Application:
14/445,413 →
Publication:
US 2015/0047313
Burner Arrangement and Method for Operating a Burner Arrangement
Method for Controlling a Gas Turbine Group
Intake Arrangement in Gas Turbine Power Plant
Method of Operating a Gas Turbine Power Plant with Exhaust Gas Recirculation and Corresponding Gas Turbine Power Plant
Gas Turbine Plant Having Exhaust Gas Recirculation
Application:
14/467,591 →
Publication:
US 2014/0360154
Gas Turbine Power Plant with Exhaust Gas Recirculation
Blade of a Rotary Flow Machine with a Radial Strip Seal
Method for Applying a High-Temperature Stable Coating Layer on the Surface of a Component and Component with Such a Coating Layer
Application:
14/474,564 →
Publication:
US 2015/0284834
Method for Fixing Heat Resistant Component on a Surface of a Heat Exposed Component
Application:
14/488,410 →
Publication:
US 2015/0083787
Method for Applying Heat Resistant Protection Components Onto a Surface of a Heat Exposed Component
Annular Helmholtz Damper
Gas Turbine Having Fuel Monitoring
Method for Producing Means with Thermal Resistance for Applying at a Surface of a Heat Exposed Component
Ultrasonic Ndt Sensor Arrangement and Method for Inspecting Surfaces of Variable Geometry of Metal Bodies
Simultaneous Broadband Damping at Multiple Locations in a Combustion Chamber
Method for Operating a Gas Turbine and Gas Turbine for Performing the Method
Strip Seal and Method for Designing a Strip Seal
Turbine Blade
Cooled Wall
Combustion Device Having a Distribution Plenum
Method for Determining at Least One Firing Temperature for Controlling a Gas Turbine and Gas Turbine for Performing the Method
Application:
14/491,172 →
Publication:
US 2015/0000297
Gas Turbine Power Plant with Non-Homogeneous Input Gas
Gas Turbine and Method to Operate the Gas Turbine
Application:
14/492,664 →
Publication:
US 2015/0082801
Carrier Ring
Mixing Arrangement for Mixing a Fuel with a Stream of Oxygen Containing Gas
Method for Manufacturing Components Made of Single Crystal (Sx) or Directionally Solidified (Ds) Nickelbase Superalloys
Method of Exhaust Gas Treatment for a Gas Turbine System and Exhaust Gas Treatment Assembly
Method for Separating a Metal Part from a Ceramic Part
Application:
14/494,893 →
Publication:
US 2015/0041434
Gas Turbine Combustor
Application:
14/494,984 →
Publication:
US 2015/0007571
Method for Manufacturing a Metallic Component by Additive Laser Manufacturing
Application:
14/496,316 →
Publication:
US 2015/0090074
Method for Determining the Temperature Inside a Combustor
Method for Processing a Modular Hybrid Component
Application:
14/496,485 →
Publication:
US 2015/0028021
Method of Operating a Turbine Engine After Flame Off
Method for Operating a Combined Cycle Power Plant and Combined Cycle Power Plant for Using Such Method
Application:
14/496,985 →
Publication:
US 2015/0007579
Combustion Chamber Seal Segments Equipped with Damping Devices
Application:
14/498,136 →
Publication:
US 2015/0075168
Exhaust Diffuser for a Gas Turbine
Gas Turbine with Adjustable Cooling Air System
Application:
14/498,297 →
Publication:
US 2015/0027129
Turbine Blade or Vane
Method and Device for Safely Operating a Gas Turbine Plant
Gas Turbine with Cooling Air Cooling System and Method for Operation of a Gas Turbine at Low Part Load
Application:
14/501,465 →
Publication:
US 2015/0089955
Gas Turbine with Sequential Combustion Arrangement
Acoustic Damping Device
Arrangement for Cooling a Component in the Hot Gas Path of a Gas Turbine
Helmholtz Damper for Gas Turbine with Cooling Air Flow
Impingement Cooling Arrangement
Combustor Cooling Structure
Gas Turbine with Flexible Air Cooling System and Method for Operating a Gas Turbine
Application:
14/514,772 →
Publication:
US 2015/0107258
Damping Device for a Combustor of a Gas Turbine
Application:
14/522,994 →
Publication:
US 2015/0113991
Damper with Bent Neck for Gas Turbine
Device for Emergency Operation of Actuators
Application:
14/557,840 →
Publication:
US 2015/0152898
Rotor Blade Arrangement and Gas Turbine
Seal Between Static Turbine Parts
Seal System for a Gas Turbine
Rotor Blade and Guide Vane Airfoil for a Gas Turbine Engine
Combustor for a Sequential Gas Turbine Having a Deflection Unit Between First and Second Combustion Chambers
Method for a Part Load Co Reduction Operation for a Sequential Gas Turbine
Flushing the Exhaust Gas Recirculation Lines of a Gas Turbine
Application:
14/589,243 →
Publication:
US 2015/0107257
Method for Repairing a Single Crystal Turbine Blade
Gas Turbine Power Plant with Flue Gas Recirculation and Catalytic Converter
Gas Turbine Power Plant with Flue Gas Recirculation
Application:
14/591,997 →
Publication:
US 2015/0128608
Cooled Stator Heat Shield
Application:
14/592,127 →
Publication:
US 2015/0198063
Method for Manufacturing a Metallic or Ceramic Component by Selective Laser Melting Additive Manufacturing
Sequential Combustion Arrangement with Dilution Gas
Method of Operating a Gas Turbine Assembly and the Gas Turbine Assembly
Composite Turbine Blade for High-Temperature Applications
Combustion Device for a Gas Turbine
Internally Cooled Airfoil for a Rotary Machine
Sequential Combustion with Dilution Gas Mixer
Acoustic Damping Device for Chambers with Grazing Flow
Process for Welding Pipe Connections for High Temperature Applications
Application:
14/657,177 →
Publication:
US 2015/0258629
Combustion Chamber with Cooling Sleeve
Application:
14/660,269 →
Publication:
US 2015/0267918
Rotor Shaft with Cooling Bore Inlets
Probe for Measuring Pressure Oscillations in the Combustor of a Gas Turbine
Airfoil Portion of a Rotor Blade or Guide Vane of a Turbo-Machine
Application:
14/661,318 →
Publication:
US 2015/0267557
Pullable Drawer for a Turbine and Turbine with Such a Drawer
Gas Turbine Blade
Tool for Removing an Inner Casing from a Turbomachine
Application:
14/662,268 →
Publication:
US 2015/0267563
Turbine Vane with Cooled Fillet
Turbomachine and Method for Disassembling Such a Turbomachine
Vane Carrier for a Compressor or a Turbine Section of an Axial Turbo Machine
Method for Premixing Air with a Gaseous Fuel and Burner Arrangement for Conducting Said Method
Sequential Combustion with Dilution Gas Mixer
Method for Post-Built Heat Treatment of Additively Manufactured Components Made of Gamma-Prime Strengthened Superalloys
Airfoil with Improved Cooling
Gamma Prime Precipitation Strengthened Nickel-Base Superalloy for Use in Powder Based Additive Manufacturing Process
Application:
14/715,882 →
Publication:
US 2015/0344994
Method and Device for Mounting and Removing of a Turbine Component
Application:
14/715,994 →
Publication:
US 2015/0336222
Method and Device for Mounting and Removing a Turbine Component
Application:
14/716,062 →
Publication:
US 2015/0337685
Rotor Assembly for Gas Turbine
Impingement Cooled Wall Arrangement
Method for Recirculation of Exhaust Gas from a Combustion Chamber of a Combustor of a Gas Turbine and Gas Turbine for Conducting Said Method
Application:
14/741,838 →
Publication:
US 2015/0369126
Method for Increasing the Power of a Combined-Cycle Power Plant, and Combined-Cycle Power Plant for Conducting Said Method
Application:
14/741,893 →
Publication:
US 2015/0369125
Exhaust Gas Liner for a Gas Turbine and Gas Turbine with Such an Exhaust Gas Liner
Combustor Cooling Structure
Damper for Gas Turbine
Apparatus for Broaching Repair of Turbine Rotor Steeples
Apparatus and Method for the Forming of Turbine Vane Cover Plates
Application:
14/754,047 →
Publication:
US 2015/0300184
Axial Swirler
Sequential Combustor Arrangement with a Mixer
Method for Measuring the Mass Flow of a Stream of a Gaseous Medium and Fuel Supply System for Conducting the Method
Application:
14/795,190 →
Publication:
US 2016/0011030
Method for the Control and Protection of a Gas Turbine and Gas Turbine Using Such Method
Compressor Assembly for Gas Turbine
Gas Turbine with Fuel Composition Control
Application:
14/813,743 →
Publication:
US 2015/0337741
Gas Turbine with Fuel Composition Control
Application:
14/814,731 →
Publication:
US 2015/0337742
Method of Operating a Gas Turbine with Staged and/or Sequential Combustion
Application:
14/814,864 →
Publication:
US 2016/0018111
Method for Controlling a Gas Turbine
Application:
14/835,839 →
Publication:
US 2016/0061114
Device and Method for Mounting or Dismantling, Replacement and Maintenance of a Can-Combustor
Apparatus for an Assembly Tool for Mounting or Dismantling, Replacement and Maintenance of a Component of an Engine
Application:
14/836,082 →
Publication:
US 2016/0076773
Dilution Gas or Air Mixer for a Combustor of a Gas Turbine
Mounting and Sealing Arrangement for a Guide Vane of a Gas Turbine
Application:
14/837,078 →
Publication:
US 2016/0076390
Tool for Measuring Geometrical Parameters of a Blade or Vane in a Turbomachine
Sealing Arrangement at the Interface Between a Combustor and a Turbine of a Gas Turbine and Gas Turbine with Such a Sealing Arrangement
Method for Reconditioning a Hot Gas Path Part of a Gas Turbine
Cooling Scheme for a Turbine Blade of a Gas Turbine
Application:
14/858,285 →
Publication:
US 2016/0090847
Method for Manufacturing a Component Using an Additive Manufacturing Process
Application:
14/868,734 →
Publication:
US 2016/0151860
Combustor Arrangement with Fastening System for Combustor Parts
Combustor Front Panel
Diverting System
Diffuser for a Gas Turbine
Turbo Machine and Method for Operating Such Turbo Machine
Sequential Combustion with Dilution Gas
Combined Cycle Power Plant
Application:
14/924,231 →
Publication:
US 2016/0115826
Combustor Arrangement for a Gas Turbine
Combustor Arrangement for a Gas Turbine
Can Combustion Chamber
Damping Inlay for Turbine Blades
Helmholtz Damper and Gas Turbine with Such a Helmholtz Damper
Application:
14/934,277 →
Publication:
US 2016/0153661
Cooling for Turbine Blade Platform-Aerofoil Joints
Application:
14/934,932 →
Publication:
US 2016/0130951
Lobe Lance for a Gas Turbine Combustor
Fuel Lance Cooling for a Gas Turbine with Sequential Combustion
Component or Coupon for Being Used Under High Thermal and Stress Load and Method for Manufacturing Such Component or Coupon
Application:
14/959,004 →
Publication:
US 2016/0082547
Method for Producing a Three-Dimensional Article and Article Produced with Such a Method
Application:
14/963,688 →
Publication:
US 2016/0090848
Blading Member for a Fluid Flow Machine
Method for Producing a Metallic Component
Application:
14/963,838 →
Publication:
US 2016/0175986
Blading Member for a Fluid Flow Machine
Application:
14/965,244 →
Publication:
US 2016/0177749
Method for Processing Materials
Application:
15/004,028 →
Publication:
US 2018/0185961
Method for Manufacturing an Element and Element
Application:
15/006,400 →
Publication:
US 2016/0221115
Method for Manufacturing a Part by Means of an Additive Manufacturing Technique
Application:
15/006,413 →
Publication:
US 2016/0243644
Component and Method for Manufacturing Said Component
Application:
15/006,440 →
Publication:
US 2018/0149039
Method for Controlling the Operation of a Gas Turbine with Sequential Combustion
Application:
15/006,480 →
Publication:
US 2016/0252017
Related Assignments
(12)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest
Sep 10, 2012
From: ALSTOM (SWITZERLAND) LTD
To: ALSTOM TECHNOLOGY LTD
Reel/Frame 028929/0381 →
Assignment of Assignor's Interest
Sep 10, 2012
From: ALSTOM
To: ALSTOM TECHNOLOGY LTD
Reel/Frame 028930/0507 →
Change of Address of Assignee (Assignment Previously Recorded October 16, 2001, Reel 012232, Frame 0072)
Sep 11, 2013
From: ALSTOM
To: ALSTOM
Reel/Frame 031207/0032 →
Assignment of Assignor's Interest
Sep 11, 2013
From: ALSTOM
To: ALSTOM TECHNOLOGY LTD
Reel/Frame 031186/0561 →
Change of Name
Nov 5, 2013
From: ALSTOM POWER UK LTD
To: ALSTOM POWER UK HOLDINGS
Reel/Frame 031582/0994 →
Change of Name
Nov 5, 2013
From: ALSTOM POWER UK HOLDINGS
To: NEWBOLD POWER UK HOLDINGS
Reel/Frame 031583/0083 →
Change of Name
Nov 5, 2013
From: ALSTOM GAS TURBINES LTD
To: ABB ALSTOM POWER UK LTD
Reel/Frame 031582/0790 →
Assignment of Assignor's Interest
Nov 5, 2013
From: NEWBOLD POWER UK HOLDINGS (IN LIQUIDATION-COMPANY NUMBER 00476835)
To: ALSTOM TECHNOLOGY LTD
Reel/Frame 031549/0178 →
Change of Name
Nov 5, 2013
From: EUROPEAN GAS TURBINES LIMITED
To: ALSTOM GAS TURBINES LTD
Reel/Frame 031581/0965 →
Change of Name
Nov 5, 2013
From: ABB ALSTOM POWER UK LTD
To: ALSTOM POWER UK LTD
Reel/Frame 031582/0936 →
Assignment of Assignor's Interest
Feb 11, 2017
From: GENERAL ELECTRIC TECHNOLOGY GMBH
To: ANSALDO ENERGIA SWITZERLAND AG
Reel/Frame 041686/0884 →
Assignment of Assignor's Interest
Feb 16, 2017
From: GENERAL ELECTRIC TECHNOLOGY GMBH
To: ANSALDO ENERGIA IP UK LIMITED
Reel/Frame 041731/0626 →