Patent Assignment
Reel/Frame 041731/0626
Assignment of Assignor's Interest
Recorded: 2017-02-16
Pages: 41
Assignor
GENERAL ELECTRIC TECHNOLOGY GMBH
Executed: 2017-01-09
Assignee
ANSALDO ENERGIA IP UK LIMITED
5TH FLOOR, NORTH SIDE, 7/10 CHANDOS STREET, CAVENDISH SQUARE, LONDON, W1G9DQ, GREAT BRITAIN
Covered Properties
(639)
Arrangement for the Thermal Protection of a Rotor of a High-Pressure Compressor
Patent:
5,842,831 →
Application:
08/822,920 →
Thermally Loaded Blade for a Turbomachine
Patent:
5,827,045 →
Application:
08/828,541 →
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 →
Coolable Blade
Patent:
5,919,031 →
Application:
08/897,765 →
Coolable Blade
Patent:
5,934,874 →
Application:
08/916,789 →
Gas Turbine Having Sequential Combustion
Patent:
5,941,060 →
Application:
08/938,454 →
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 →
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 →
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 Leading-Edge Region of a Hollow Gas-Turbine Blade
Patent:
6,168,380 →
Application:
09/111,874 →
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 →
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 →
Method for Operating a Premix Burner
Patent:
6,270,338 →
Application:
09/179,460 →
Burner for Operating a Heat Generator
Patent:
6,027,331 →
Application:
09/187,343 →
Method of Operating a Gas-Turbine Group
Patent:
6,178,738 →
Application:
09/208,440 →
Burner
Patent:
5,980,240 →
Application:
09/210,741 →
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 →
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 →
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 →
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 →
Method and Apparatus for Casting Directionally Solidified Article
Patent:
6,311,760 →
Application:
09/373,719 →
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 →
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 →
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 →
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 →
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 →
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 →
Process for Producing or Repairing Cooling Channels in Monocrystalline Components of Gas Turbines
Patent:
6,405,435 →
Application:
09/584,714 →
Fastening devices for heat-protection shields
Patent:
6,361,274 →
Application:
09/632,795 →
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 →
Effusion Cooled Transition Duct
A Burner with Damper for Attenuating Thermo Acoustic Instabilities
Patent:
6,490,864 →
Application:
09/684,982 →
Turbine Blade with Actively Cooled Shroud-Band Element
Cooled Heat Shield
Blade for Gas Turbines with Choke Cross Section at the Trailing Edge
Drilled Cooling Air Openings in Gas Turbine Components
Cooled Blade for a Gas Turbine
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
Process for Producing a Thermally Loaded Casting
Apparatus for Damping Acoustic Vibrations in a Combustor
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
Airfoil Tip Squealer Cooling Construction
Labyrinth Seal for Rotating Shaft
Means for Wear Reduction in a Gas Turbine Combustor
Patent:
6,467,272 →
Application:
09/891,003 →
Low Nox Combustion Liner with Cooling Air Plenum Recesses
Patent:
6,430,932 →
Application:
09/909,029 →
Method for Producing a Cooled, Lost-Wax Cast Part
High-Temperature Alloy
Process for the Regeneration of a Catalyst Plant and Apparatus for Performing the Process
Turbine Blade Pocket Shroud
Patent:
6,491,498 →
Application:
09/971,241 →
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
Burner System with Staged Fuel Injection and Method for Its Operation
Damper Arrangement for Reducing Combustion-Chamber Pulsations
Gas Turbo-Group
Probe for Measuring Pressure Oscillations
Exhaust Gas System with Helmholtz Resonator
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
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
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
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
Thermally Free Aft Frame for a Transition Duct
Patent:
6,619,915 →
Application:
10/064,675 →
Transition Duct Mounting System
Patent:
6,662,567 →
Application:
10/064,755 →
Coated Seal Article Used in Turbine Engines
Patent:
6,675,584 →
Application:
10/064,768 →
Gas Turbine Plant
Method for Igniting a Thermal Turbomachine
Method of Repairing a Ceramic Coating
Method for Isothermal Brazing of Single Crystal Components
Method for Running Up a Gas Turbine Plant
Fuel Supply System and an Associated Operating Method
Fully Premixed Secondary Fuel Nozzle with Improved Stability
Computerized Electronic Runout
Process for Producing a Groove-Like Recess, and a Groove-Like Recess of This Type
Combustion Chamber/Venturi Configuration and Assembly Method
Transition Duct with Enhanced Profile Optimization
Patent:
6,644,032 →
Application:
10/277,659 →
Effusion Cooled Transition Duct with Shaped Cooling Holes
Device for Separating Dirt and Debris in Flowing Media
Coated Seal Article with Multiple Coatings
Membrane Seals
Method of Fuel Nozzle Sizing and Sequencing for a Gas Turbine Combustor
Patent:
6,883,329 →
Application:
10/350,756 →
Convoluted Seal with Enhanced Wear Capability
Directionally Solidified Columnar Grained Article and Apparatus for Manufacture Thereof--
Turbine Blade Platform Trailing Edge Undercut
Patent:
6,761,536 →
Application:
10/355,883 →
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
Nickel-Base Superalloy
Flamesheet Combustor
Method of Operating a Flamesheet Combustor
Tip Material for a Turbine Blade and Method of Manufacturing or Repairing a Tip of a Turbine Blade
Gas Only Fin Mixer Secondary Fuel Nozzle
Reheat Combustion System for a Gas Turbine
Device for Separating Dust and Dirt Out of Flowing Media
Apparatus and Method for Improving Combustion Stability
Atomizer Device and Method for the Production of a Liquid-Gas Mixture
Method of Protecting a Local Area of a Component
Bellows Seal
Gas Turbine Fuel Pilot Nozzle
Transition Duct Honeycomb Seal
Method for Operating a Combined-Cycle Power Station
Vane Enhanced Trailing Edge Cooling Design
Patent:
6,824,352 →
Application:
10/673,311 →
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
Cooling and Sealing Design for a Gas Turbine Combustion System
Flow Sleeve for a Law Nox Combustor
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 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
Methods and Apparatus for Starting Up Emission-Free Gas-Turbine Power Stations
Method and Arrangement for Adapting a Parameter of a Hot Gas of a Hot-Gas Generator Having a Downstream Technological Process
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
Fuel Supply System and an Associated Operating Method
Fastened Vane Assembly
Combustion Liner Seal with Heat Transfer Augmentation
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
Gas Turbine Arrangement
Method for Injecting a Fuel-Air Mixture into a Combustion Chamber
Burner with Stepped Fuel Injection
Support for a Reflective Target
Tornado Torch Igniter
Method for Operating a Gas Turbine Group
Combustion Chamber for a Gas Turbine
Method of Reconditioning a Turbine Blade
High-Temperature Protection Layer
Method for Operating a Turbine Group
Apparatus and Method for Providing an Off-Gas to a Combustion System
Apparatus and Method for Reducing Carbon Monoxide Emissions
Counter Swirl Shear Mixer
Self-Purging Pilot Fuel Injection System
Combustion Liner with Enhanced Heat Transfer
Shroud Block with Enhanced Cooling
Seal for a Gas Turbine Engine Having Improved Flexibility
Flashback Suppression System for a Gas Turbine Combustor
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
Rotor Blade for a Flow Machine, and an Associated Pulling-Off Tool
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
Process of Masking Cooling Holes of a Gas Turbine Component
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
Adaptive Sensor Model
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
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
Air Cooler for Power Plants and Use of Such an Air Cooler
Process and Apparatus for Producing Service Blades
Method of Operating a Gas Turbine Group
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 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
Cooled Blade or Vane for a Gas Turbine
Method for Reducing the Nox Emissions from a Burner Arrangement Comprising a Plurality of Burners, and Burner Arrangement for Carrying Out the 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
Gas Turbine Transition Duct
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
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
Nickel-Base Alloy for Gas Turbine Applications
Conveyor Device
Masking Material for Holes of a Component
Multiple Burner Arrangement for Operating a Combustion Chamber, and Method for Operating the Multiple Burner Arrangement
Method of Operating a Thermal Power Plant
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
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
Turbine Static Structure for Reduced Leakage Air
Method of Modifying a Turbocompressor
Method for Operating a Gas Turbine Group
Hybrid Burner Lance
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
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
Stator Damper Shim
Leaf Seal, in Particular for a Gas Turbine
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
Gas Turbine Airfoil with Leading Edge Cooling
Turbo Machine
Method for Operating a Gas Turbine Plant
Process for Extending the Cylic Service Life of Thermal Barrier Coatings, in Particular on Gas Turbine Components
Utilizing Inlet Bleed Heat to Improve Mixing and Engine Turndown
Gap Seal in Blades of a Turbomachine
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
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
Measuring Apparatus
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
Burner Arrangement
Axial Retention of a Platform Seal
Shaped Cooling Holes for Reduced Stress
Cooled Gas Turbine Vane Assembly
Method for Operating a Gas Turbine, Method of Operation of a Combined Cycle Power Plant, and Combined Cycle Power Plant
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
Gas Turbine Hot Gas Component Repair Method
Comprehensive Method for Local Application and Local Repair of Thermal Barrier Coatings
System for Controlling a Combustion Process for a Gas Turbine
Method for Reducing Emissions from a Combustor
Burner for a Second Chamber of a Gas Turbine Plant
Multilayer Thermal Barrier Coating
Method for Oxidising a Thermocouple Sheath
Apparatus for Broaching Repair of Turbine Rotor Steeples
Application of Dense Vertically Cracked and Porous Thermal Barrier Coating to a Gas Turbine Component
Plug Assembly with Moveable Mounting Members
High-Temperature-Resistant Cobalt-Base Superalloy
Gas Turbine Transition Duct Profile
Hydraulic Trip Unit for a Valve Unit in a Prime Mover Plant, Especially for a Fast-Acting Shut-Off Valve of a Turbine Plant
Fluid Flow Machine
Multi-Vane Segment Design and Casting Method
Power Plant and Operating Method
Rotor Blade Arrangement and Gas Turbine
Compressor Vane Diaphragm
Combustion Chamber Arrangement for Operating a Gas Turbine
Rotor Blade for a Gas Turbine
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
Burner Fuel Lance Configuration and Method of Use
Strip Seal and Method for Designing a Strip Seal
Method for Improving the Sealing on Rotor Arrangements
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 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
Process for Producing a Body Provided with a Slot as a Test Crack
Blade for an Axial Compressor and Manufacturing Method Thereof
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
Stabilizing a Gas Turbine Engine via Incremental Tuning
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
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
Method for Switching Over a Gas Turbine Plant from Gaseous Fuel to Liquid Fuel and Vice-Versa
Blade for a Gas Turbine
Turbine Blade
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
Extending Useful Life of a Cobalt-Based Gas Turbine Component
Method of Applying Multiple Materials with Selective Laser Melting on a 3D Article
Methods for Repairing a Gas Turbine Component
Abrasive Single-Crystal Turbine Blade
Wear-Resistant and Oxidation-Resistant Turbine Blade
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
Process for Producing a 3-Dimensional Component by Selective Laser Melting (Slm)
Shroud Seal Segments Arrangement in a Gas Turbine
Turbine Guide Vane
Application:
13/012,317 →
Publication:
US 2011/0189002
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
Valve Assembly
Dynamically Auto-Tuning a Gas Turbine Engine
Sealing Structure on a Shroud of a Turbine Blade
Turbine Blade Platform Undercut
Employing Fuel Properties to Auto-Tune a Gas Turbine Engine
Selecting and Applying to Fuel-Flow Splits Bias Values to Correct for Elevated Inlet Air Humidity
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
Cooled Blade for a Gas Turbine
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
Method for Checking the Bearing Alignment in a Gas Turbine
Lance of a Burner
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
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
Premix Burner for a Gas Turbine
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
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
Gas Turbine Arrangement and Method for Operating a Gas Turbine Arrangement
Combustion Chamber and Method for Damping Pulsations
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
Industrial Plant with Noise Attenuation Hood
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
Method for Repairing or Reconditioning a Badly Damaged Component, in Particular from the Hot Gas Region of a Gas Turbine
Turbine Blade Having Improved Flutter Capability and Increased Turbine Stage Output
Turbomachine Component
Using Return Water of an Evaporative Intake Air Cooling System for Cooling a Component of a Gas Turbine
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
An Emergency Shut-Off Signal Generator for a Valve Assembly
Pressurized Casing
Compressor Blade
Method for Operating a Fuel Supply for a Heat Engine
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
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
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
Gas Turbine Airfoil with Shaped Trailing Edge Coolant Ejection Holes
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)
Transitional Region for a Secondary Combustion Chamber of a Gas Turbine
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
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
Detecting Flashback by Monitoring Engine-Dynamic Spikes
Method for Reconditioning a Blade of a Gas Turbine and Also a Reconditioned Blade
Control System
Transition Duct Mounting System
Application:
13/778,674 →
Publication:
US 2013/0255276
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
Method and Arrangement for Gas Turbine Engine Surge Control
Application:
13/939,748 →
Publication:
US 2014/0013765
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
Oxidation Resistant Nickel Alloy
Method for Manufacturing a Three-Dimensional Article
Application:
13/972,127 →
Publication:
US 2014/0053956
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
Variable Length Combustor Dome Extension for Improved Operability
Combustor with Radially Staged Premixed Pilot for Improved
Application:
14/038,029 →
Publication:
US 2014/0090396
Thermally Free Liner Retention Mechanism
Variable Flow Divider Mechanism for a Multi-Stage Combustor
Application:
14/038,056 →
Publication:
US 2014/0090400
Flamesheet Combustor Dome
Method of Operating a Multi-Stage Flamesheet Combustor
Application:
14/038,070 →
Publication:
US 2015/0184858
Axial Retention of a Platform Seal
Burner Including a Swirl Chamber with Slots Having Different Widths
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 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
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
Method of Repairing a Transition Duct Side Seal
Anti-Rotation Lug and Splitline Jumper
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
Method for Manufacturing a Hybrid Component
Compressor Airfoil
Labyrinth Seal
Grain Size Inspection of a Gas Turbine Component by X-Ray Refraction
Application:
14/203,815 →
Publication:
US 2014/0270072
Turbine Blade Tip Repair Using Dual Fusion Welding
Stabilizing a Gas Turbine Engine via Incremental Tuning During Transients
Dynamic and Automatic Tuning of a Gas Turbine Engine Using Exhaust Temperature and Inlet Guide Vane Angle
Dynamic Tuning of a Gas Turbine Engine to Detect and Prevent Lean Blowout
Ensuring Non-Excessive Variation of Gradients in Auto-Tuning a Gas Turbine Engine
Method for Coating a Component of a Turbomachine and Coated Component for a Turbomachine
Method for Welding Rotors for Power Generation
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
Removable Swirler Assembly for a Combustion Liner
Application:
14/256,022 →
Publication:
US 2014/0318150
Premixer Assembly for Gas Turbine Combustor
Application:
14/256,023 →
Publication:
US 2014/0318139
Premixer Assembly and Mechanism for Altering Natural Frequency of a Gas Turbine Combustor
Application:
14/256,025 →
Publication:
US 2014/0318140
Combustion Liner with Bias Effusion Cooling
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 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
Axially Staged Gas Turbine Combustor with Interstage Premixer
Stator Component with Segmented Inner Ring for a Turbomachine
Turbine Blade and Turbine with Improved Sealing
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
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
Intake Arrangement in Gas Turbine Power Plant
Gas Turbine Plant Having Exhaust Gas Recirculation
Application:
14/467,591 →
Publication:
US 2014/0360154
Combustor Dome Damper System
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
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
Method for Operating a Gas Turbine and Gas Turbine for Performing the Method
Turbine Blade
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 and Method to Operate the Gas Turbine
Application:
14/492,664 →
Publication:
US 2015/0082801
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
Method for Manufacturing a Metallic Component by Additive Laser Manufacturing
Application:
14/496,316 →
Publication:
US 2015/0090074
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
Arrangement for Cooling a Component in the Hot Gas Path of a Gas Turbine
Helmholtz Damper for Gas Turbine with Cooling Air Flow
Sealing Device for a Gas Turbine Combustor
Gas Turbine with Flexible Air Cooling System and Method for Operating a Gas Turbine
Application:
14/514,772 →
Publication:
US 2015/0107258
Flamesheet Combustor Contoured Liner
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
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
Composite Turbine Blade for High-Temperature Applications
Automated Extended Turndown of a Gas Turbine Engine Combined with Incremental Tuning to Maintain Emissions and Dynamics
Combustion Device for a Gas Turbine
Internally Cooled Airfoil for a Rotary Machine
Process for Welding Pipe Connections for High Temperature Applications
Application:
14/657,177 →
Publication:
US 2015/0258629
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
Vane Carrier for a Compressor or a Turbine Section of an Axial Turbo Machine
Method for Post-Built Heat Treatment of Additively Manufactured Components Made of Gamma-Prime Strengthened Superalloys
Gamma Prime Precipitation Strengthened Nickel-Base Superalloy for Use in Powder Based Additive Manufacturing Process
Application:
14/715,882 →
Publication:
US 2015/0344994
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
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
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
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
Mounting and Sealing Arrangement for a Guide Vane of a Gas Turbine
Application:
14/837,078 →
Publication:
US 2016/0076390
Flow Control Device for Rotating Flow Supply System
Method for Reconditioning a Hot Gas Path Part of a Gas Turbine
Method for Manufacturing a Component Using an Additive Manufacturing Process
Application:
14/868,734 →
Publication:
US 2016/0151860
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
Engine Casing Element
Application:
14/948,582 →
Publication:
US 2016/0146036
Leading Edge Cooling Channel for Airfoil
Tapered Cooling Channel for Airfoil
Cooling Channel for Airfoil with Tapered Pocket
Application:
14/951,163 →
Publication:
US 2016/0146019
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 Producing Contoured Holes
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
Device for Hvof Spraying Process Having a Hot Gas Section Insert
Application:
15/033,369 →
Publication:
US 2016/0251745
Guide Vane Assembly on the Basis of a Modular Structure
Application:
15/038,873 →
Publication:
US 2016/0376899
Blade Assembly on Basis of a Modular Structure for a Turbomachine
Application:
15/039,277 →
Publication:
US 2017/0175534
Blade Assembly for a Turbomachine on the Basis of a Modular Structure
Application:
15/039,296 →
Publication:
US 2017/0022821
Method of Controlling the Fuel Distribution Among Different Stages of a Gas Turbine Combustion Chamber
Application:
15/042,008 →
Publication:
US 2016/0237916
Method for Manufacturing a Braze Joint Gap and Method for Brazing or Soldering
Application:
15/101,187 →
Publication:
US 2016/0303674
Rotor Blade or Guide Vane Assembly
Application:
15/106,660 →
Publication:
US 2017/0002661
Gamma Prime Precipitation Strengthened Nickel-Base Superalloy for Use in Powder Based Additive Manufacturing Process
Application:
15/107,001 →
Publication:
US 2017/0021453
Method for Operating a Gas Turbine at Part Load
Application:
15/112,902 →
Publication:
US 2016/0333731
Gas Turbine Component
Omnidirectional Moving Device and Omnidirectional Treading System Incorporated in Such Device
Application:
15/168,687 →
Publication:
US 2016/0362134
Structure Adaptable Moving Device
Application:
15/176,787 →
Publication:
US 2016/0368548
Calibration Block for Inspection of Gas Turbine Component and Manufacturing Method
Application:
15/211,613 →
Publication:
US 2017/0016804
Related Assignments
(4)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest
Sep 10, 2012
From: ALSTOM
To: ALSTOM TECHNOLOGY LTD
Reel/Frame 028930/0507 →
Assignment of Assignor's Interest
Sep 19, 2012
From: ALSTOM (SWITZERLAND) LTD
To: ALSTOM TECHNOLOGY LTD
Reel/Frame 028991/0521 →
Assignment of Assignor's Interest
Mar 25, 2014
From: BRICAUD, CYRILLE; STEIGER, ULRICH ROBERT; HEIDECKE, AXEL; SIMON-DELGADO, CARLOS
To: ALSTOM TECHNOLOGY LTD
Reel/Frame 032515/0616 →
Change of Name
Mar 22, 2016
From: ALSTOM TECHNOLOGY LTD
To: GENERAL ELECTRIC TECHNOLOGY GMBH
Reel/Frame 038216/0193 →