Patent Assignment
Reel/Frame 041686/0884
Assignment of Assignor's Interest
Recorded: 2017-02-11
Pages: 30
Assignor
GENERAL ELECTRIC TECHNOLOGY GMBH
Executed: 2017-01-09
Assignee
ANSALDO ENERGIA SWITZERLAND AG
ROMERSTRASSE 36, BADEN, 5401, SWITZERLAND
Covered Properties
(462)
Pressure Atomizer Nozzle
Patent:
5,934,555 →
Application:
08/811,006 →
Device for Separating Dust Particles
Patent:
5,837,019 →
Application:
08/891,786 →
Premix Burner
Patent:
6,126,439 →
Application:
08/909,737 →
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 →
Brush Seal and Method for the Manufacture of a Brush Seal
Patent:
6,079,714 →
Application:
09/024,705 →
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 →
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 →
Cooling System for the Trailing Edge Region of a Hollow Gas Turbine Blade
Patent:
6,056,508 →
Application:
09/111,778 →
Pressure Atomizer Nozzle
Patent:
6,045,058 →
Application:
09/114,883 →
Ceramic Liner
Patent:
5,957,067 →
Application:
09/119,585 →
Pressure-Measuring Device
Patent:
6,053,048 →
Application:
09/133,669 →
Burner for Operating a Heat Generator
Patent:
5,944,511 →
Application:
09/153,269 →
Burner for Operating a Heat Generator
Patent:
6,059,565 →
Application:
09/178,578 →
Method and Device for Operating a Premix Burner
Patent:
6,132,202 →
Application:
09/179,462 →
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 and Device for Injecting a Fuel/Liquid Mixture into the Combustion Chamber of a Burner
Patent:
6,491,236 →
Application:
09/208,441 →
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 →
Process for Producing a Casting Core, for Forming Within a Cavity Intended for Cooling Purposes
Patent:
6,374,898 →
Application:
09/268,722 →
Gas Turbine Fuel Distributor Incorporating Separate Regulating Units
Patent:
6,189,321 →
Application:
09/289,492 →
Non-Contact Sealing of Gaps in Gas Turbines
Patent:
6,276,692 →
Application:
09/349,963 →
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 →
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 →
Fluid-Flow Machine for Compressing or Expanding a Compressible Medium
Patent:
6,264,425 →
Application:
09/397,510 →
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 →
Flow Duct with Cross-Sectional Step
Patent:
6,216,644 →
Application:
09/431,179 →
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 →
Full Ring Fuel Distribution System for a Gas Turbine Combustor
Patent:
6,282,904 →
Application:
09/443,916 →
Burner for a Heat Generator
Patent:
6,461,151 →
Application:
09/531,184 →
Casting Furnace with Centrally Located Heating Element for Producing Directionally Solidified Castings
Patent:
6,523,599 →
Application:
09/556,310 →
Cooling Arrangement for Blades of a Gas Turbine
Patent:
6,422,811 →
Application:
09/593,162 →
Combustion Chamber/Venturi Cooling for a Low Nox Emission Combustor
Patent:
6,446,438 →
Application:
09/605,765 →
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 →
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 →
Turbo Machine
Patent:
6,499,944 →
Application:
09/657,304 →
Low Nox Emission Combustion Liner with Circumferentially Angled Film Cooling Holes
Patent:
6,427,446 →
Application:
09/664,898 →
Control of Primary Measures for Reducing the Formation of Thermal Nitrogen Oxides in Gas Turbines
Patent:
6,584,775 →
Application:
09/665,056 →
Pre-Mix Nozzle and Full Ring Fuel Distribution System for a Gas Turbine Combustor
Patent:
6,446,439 →
Application:
09/706,425 →
Three Degrees of Freedom Aft Mounting System for Gas Turbine Transition Duct
Patent:
6,442,946 →
Application:
09/712,735 →
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 →
Iron aluminide coating and method of applying an iron aluminide coating
Blade Arrangement with Damping Elements
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 →
Gas Turbine Airfoill
Turbine Blade with Rub Tolerant Cooling Construction
Premix Burner
Wear Reduction Means for a Gas Turbine Combustor Transition Duct End Frame
Method and Device for Producing Hot Working Gases
Method for Injecting Fuel into a Burner
Method for Operating a Combustion Chamber
Sealing Arrangement Between Components of a Rotating Assembly as Well as a Method for Producing a Sealing Joint
Method for Producing a Cast Part, Model Mold, and Ceramic Insert for Use in This Method
Gas Turbine Set
Device for Cooling a Shroud of a Gas Turbine Blade
Burner with High Flame Stability
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
Combustion Chamber/Venturi Cooling for a Low Nox Emission Combustor
Process for the Operation of an Annular Combustion Chamber, and Annular Combustion Chamber
Re-Fired Gas Turbine Engine
Advanced Crossfire Tube Cooling Scheme for Gas Turbine Combustors
Gas Turbine
Catalytic Burner
Catalyzer
Burner System
Fully Premixed Secondary Fuel Nozzle
Fully Premixed Secondary Fuel Nozzle with Dual Fuel Capability
Fully Premixed Secondary Fuel Nozzle with Improved Stability and Dual Fuel Capability
Rotor for a Gas Turbine
Patent:
6,808,362 →
Application:
10/204,479 →
Insulated Cooling Passageway for Cooling a Shroud of a Turbine Blade
Turbogroup of a Power Generating Plant
Combustion Device for Generating Hot Gases
Deformable Brush Seal Support
Advanced Cooling Configuration for a Low Emissions Combustor Venturi
Pressure Ram Device on a Gas Turbine Combustor
Method for Operating a Burner and Burner with Stepped Premix Gas Injection
Secondary Fuel Nozzle with Readily Customizable Pilot Fuel Flow Rate
Fully Premixed Pilotless Secondary Fuel Nozzle
Gas Turbine Combustor Hybrid Dynamic-Static Probe
Patent:
6,742,394 →
Application:
10/341,573 →
Fluidic Control of Fuel Flow
Combustion Liner Cap Assembly Attachment and Sealing System
Transition Duct Support Bracket Wear Cover
Low Emissions Hydrogen Blended Pilot
Coated Crossfire Tube Assembly
Sealing Arrangement
Advanced Fuel Nozzle Design with Improved Premixing
Catalytic Burner
Turbine Blade Airfoil
Patent:
6,769,878 →
Application:
10/434,691 →
Dual Fuel Fin Mixer Secondary Fuel Nozzle
Damping Arrangement for Reducing Combustion-Chamber Pulsation in a Gas Turbine System
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
Burner and Pilot Burner
Annular Combustor for a Gas Turbine
Premix Burner and Method of Operation
Gas Turbine Set
Fully Premixed Pilotless Secondary Fuel Nozzle with Improved Tip Cooling
Process for Operation of a Burner with Controlled Axial Central Air Mass Flow
Seal Assembly
Gas Turbine Combustor End Cover
Turbine Blade Airfoil Having Improved Creep Capability
Sealing Arrangements
Combustion Method and Burner for Carrying Out the Method
Turbine Blade Attachment Lightening Holes
Combustion Chamber
Process for Strengthen Grain Boundaries of an Article Made from a Ni Based Superalloy
Turbine Blade Shroud Cutter Tip
Seal System
Primary Fuel Nozzle Having Dual Fuel Capability
Axial-Flow Thermal Turbomachine
Axial-Flow Thermal Turbomachine
Gas Turbine Having Exhaust Recirculation
Turbomachine
Turbomachine
Apparatus and Method for Reducing the Heat Rate of a Gas Turbine Powerplant
Transition Duct Apparatus Having Reduced Pressure Loss
Gas Turbo Set
Combustion Liner Having Improved Cooling and Sealing
Hot Gas Path Assembly
Catalytic Reactor and Associated Operating Method
Burner Arrangement for the Annular Combustion Chamber of a Gas Turbine
Vane Platform Rail Configuration for Reduced Airfoil Stress
Method of Operating a Combustion System for Increased Turndown Capability
Patent:
7,137,256 →
Application:
10/906,631 →
Gas Turbine and Associated Cooling Method
Cooled Turbine Blade or Vane
Turbine Rotor Blade for Gas Turbine Engine
Method for Casting a Directionally Solidified Article
Compressor Rotor Blade
Flange for Flame Observation
Method for Operating a Compressor
Rotor with Core Surrounded by Shielding Rings
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 Combustion of a Fuel
Rope Seal for Gas Turbine Engines
Airflow Distribution to a Low Emissions Combustor
Method for Operating a Gas Turbine and a Gas Turbine for Implementing the Method
Apparatus and Method for Testing Combustion
Tile and Exo-Skeleton Tile Structure
Method for Operating an Air-Breathing Engine
Parametric Production of Drilled Cooling Holes
Fuel Injection System and Purging Method
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
Premix Burner with a Swirl Generator Delimiting a Conical Swirl Space and Having Sensor Monitoring
Turbomachine
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
Combustor Liners
Inlet Bleed Heat and Power Augmentation for a Gas Turbine Engine
Hook Ring Segment for a Compressor Vane
Combustion Chamber
Combustion Chamber for a Gas Turbine
Blade with Shroud
Burner for a Gas Turbine
Vane Platform Rail Configuration for Reduced Airfoil Stress
Method and Device for Burning Hydrogen in a Premix Burner
Premix Burner with Mixing Section
Method of Producing a Hot Gas Component of a Turbomachine Including an Embedded Channel
Cross Flange Seal for a Pressure Vessel, Especially for a Turbomachine Casing
Sealing Element for Use in a Fluid-Flow Machine
Premixing Burner for Generating an Ignitable Fuel/Air Mixture
Premix Burner for Operating a Combustion Chamber
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
Transition Duct Cooling Feed Tubes
Gas Turbine Fuel Nozzle Having Improved Thermal Capability
Low Residence Combustor Fuel Nozzle
Guide Vane Arrangement of a Turbomachine
Gas Turbine Engine Controls for Minimizing Combustion Dynamics and Emissions
Operating Method for a Turbogroup
Vane Arrangement of a Turbo Machine
Gas Turbogroup
Gas Turbine Integrated with Fuel Catalytic Partial Oxidation
Combustion Chamber with Burner and Associated Operating Method
Apparatus for the Combustion of a Fuel-Oxidizer Mix
Gas Turbine with Axial Thrust Balance
Compressor Airfoil
Transition Duct Assembly
Method for Designating a Component Having a Heat Insulation Layer and for Determining Its Operating Time
Fuel Lance for a Gas Turbine Installation and a Method for Operating a Fuel Lance
Altering a Natural Frequency of a Gas Turbine Transition Duct
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
Combustor End Cap Assembly
Combustion Liner Damper
Method for Operating a Burner
Compound Variable Elliptical Airfoil Fillet
Turbine Blade Platform Trailing Edge Undercut
Method of Depositing a Wear Resistant Seal Coating and Seal System
Fuel Distribution System for a Gas Turbine with Multistage Burner Arrangement
Operation of a Gas Turbine
Methods for the Protection of a Thermal Barrier Coating System and Methods for the Renewal of Such a Protection
Burner and Fuel Lance for a Gas Turbine Installation
Continuous-Flow Machine, Turbine, or Compressor
Combustor with Reduced Carbon Monoxide Emissions
Burner with Lance
Alignment of Machine Components Within Casings
High-Temperature Alloy
Creep-Resistant Steel
Shiplap Arrangement
Stator Heat Shield
Method of Operating a Gas Turbine, and Gas Turbine with Water Injection
Compressor Stator Vane
Cool Flame Combustion
Application:
12/618,136 →
Publication:
US 2010/0089066
High Temperature and Oxidation Resistant Material
Hot Gas Component of a Turbomachine Including an Embedded Channel
Turbine Blades
Conical Gas Turbine Burner Having a Fuel Lance with Inclined Side Nozzles
Load Rejection and Recovery Using a Secondary Fuel Nozzle
Burner for a Gas Turbine and Method for Feeding a Gaseous Fuel in a Burner
Cooling of a Gas Turbine Engine Downstream of Combustion Chamber
Injection Nozzle Having Constant Diameter Pin and Method for Operating the Injection Nozzle
Welding Additive Material
Burner of a gas turbine
Lamellar Seal for a Turbomachine
Gas Turbine Stator/Rotor Expansion Stage Having Bumps Arranged to Locally Increase Static Pressure
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
Method for Operating a Gas Turbine Plant
Burner Arrangement, and Use of Such a Burner Arrangement
Method and Burner Arrangement for the Production of Hot Gas, and Use of Said Method
Tunable Transition Duct Side Seals in a Gas Turbine Engine
Abradable Coating System
Leaf Seals
Application:
12/940,497 →
Publication:
US 2011/0182729
Sequential Combustor Gas Turbine Including a Plurality of Gaseous Fuel Injection Nozzles and Method for Operating the Smae
Leaf Seal
Nickel-Base Superalloy with Improved Degradation Behavior
Method for Adjusting a Helmholtz Resonator and an Adjustable Helmholtz Resonator
Gas Turbine and Method for Its Operation
Unflared Compressor Blade
Blade for a Gas Turbine
Combined Cycle Power Plant with Flue Gas Recirculation
Combined Cycle Power Plant with Flue Gas Recirculation
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
Thermally Loaded, Cooled Component
Process for Producing a Single-Crystal Component Made of a Nickel-Based Superalloy
Gas Turbine Engine and Method for Cooling the Compressor of a Gas Turbine Engine
Method and Device for Ascertaining the Approach of the Lean Blow Off of a Gas Turbine Engine
Combustion Device
Burner Arrangement with Deflection Elements for Deflecting Cooling Air Flow
Power Plant and Method for Its Operation
Method for Controlling a Gas Turbine and Gas Turbine for Implementing the Method
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
Nickel-Based Superalloy
Filler Material for Welding
Application:
13/346,830 →
Publication:
US 2012/0187093
Sealing Arrangement for a Thermal Machine
System and Method for Blade Retention
Method for Combusting Hydrogen-Rich, Gaseous Fuels in a Burner, and Burner for Performing Said Method
Gas Turbine Generator Set
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
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
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
Retaining Collar for a Gas Turbine Combustion Liner
Axial Compressor with an Injection Device for Injecting a Fluid
Method for Injecting Water into a Multistage Axial Compressor of a Gas Turbine
Vibration Damper for Rotating Parts
Method for Switching Over a Combustion Device Between a First Fuel and a Second Fuel
Self-Adjusting Device for Controlling the Clearance Between Rotating and Stationary Components of a Thermally Loaded Turbo Machine
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
Light Weight Shroud Fin for a Rotor Blade
Axial Compressor for Fluid-Flow Machines
Diffuser, in Particular for an Axial Flow Machine
Application:
13/678,676 →
Publication:
US 2013/0129498
Damping System for Combustor
Flushing the Exhaust Gas Recirculation Lines of a Gas Turbine
Repair Of A Shrouded Blade
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
Mixing Element for Gas Turbine Units with Flue Gas Recirculation
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
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
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
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
Adjusted Rotating Airfoil
Adjusted Stationary Airfoil
Gas Turbine Temperature Measurement
Damping Device for a Gas Turbine Combustor
Method and Gas Turbine Combustion System for Safely Mixing H2-Rich Fuels with Air
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
Rotary Flow Machine and Method for Disassembling the Same
Deep Trailing Edge Repair
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 Rotor Positioning Device
Can Combustor for a Can-Annular Combustor Arrangement in a Gas Turbine
Sensor Mounting Attachment
Method and Device for Suppressing the Formation of Ice on Structures at the Air Intake of a Turbomachine
Gas Turbine Engine and Operations
Application:
14/317,758 →
Publication:
US 2015/0016964
Maintenance Assembly Adaptable Within Gas Turbine Engine
Gas Turbine with Improved Part Load Emissions Behavior
Rotor Shaft for a Turbomachine
Shaft Coupling Assembly and Method for Coupling Shafts
Fixation Device for Turbine and Method for Applying Fixation
Sequential Combustion with Dilution Gas Mixer
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
Method of Operating a Gas Turbine Power Plant with Exhaust Gas Recirculation and Corresponding Gas Turbine Power Plant
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
Annular Helmholtz Damper
Simultaneous Broadband Damping at Multiple Locations in a Combustion Chamber
Strip Seal and Method for Designing a Strip Seal
Cooled Wall
Gas Turbine Power Plant with Non-Homogeneous Input Gas
Carrier Ring
Mixing Arrangement for Mixing a Fuel with a Stream of Oxygen Containing Gas
Gas Turbine Combustor
Application:
14/494,984 →
Publication:
US 2015/0007571
Method for Determining the Temperature Inside a Combustor
Gas Turbine with Sequential Combustion Arrangement
Acoustic Damping Device
Impingement Cooling Arrangement
Combustor Cooling Structure
Damping Device for a Combustor of a Gas Turbine
Application:
14/522,994 →
Publication:
US 2015/0113991
Damper with Bent Neck for 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
Sequential Combustion Arrangement with Dilution Gas
Method of Operating a Gas Turbine Assembly and the Gas Turbine Assembly
Brazeless End Cover for a Combustion System
Application:
14/621,908 →
Publication:
US 2015/0226127
Sequential Combustion with Dilution Gas Mixer
Acoustic Damping Device for Chambers with Grazing Flow
Combustion Chamber with Cooling Sleeve
Application:
14/660,269 →
Publication:
US 2015/0267918
Rotor Shaft with Cooling Bore Inlets
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
Fuel Nozzle for Axially Staged Fuel Injection
Fuel Nozzle with Hemispherical Dome Air Inlet
Fuel Nozzle With Multiple Flow Divider Air Inlet
Application:
14/669,089 →
Publication:
US 2016/0281978
Flow Sleeve Deflector for Use in Gas Turbine Combustor
Method for Premixing Air with a Gaseous Fuel and Burner Arrangement for Conducting Said Method
Sequential Combustion with Dilution Gas Mixer
Airfoil with Improved Cooling
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
Exhaust Gas Liner for a Gas Turbine and Gas Turbine with Such an Exhaust Gas Liner
Combustor Cooling Structure
Damper for Gas Turbine
Axial Swirler
Sequential Combustor Arrangement with a Mixer
Method for the Control and Protection of a Gas Turbine and Gas Turbine Using Such Method
Compressor Assembly for Gas Turbine
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
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
Cooling Scheme for a Turbine Blade of a Gas Turbine
Application:
14/858,285 →
Publication:
US 2016/0090847
Method of Electron Beam Welding
Application:
14/861,751 →
Publication:
US 2017/0080530
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
Lobe Lance for a Gas Turbine Combustor
Fuel Lance Cooling for a Gas Turbine with Sequential Combustion
Detection of Deficient Sensors in a Gas Turbine System
Frame Segment for a Combustor Turbine Interface
Combustor with Annular Bluff Body
Application:
14/950,601 →
Publication:
US 2016/0146464
Burner of a Gas Turbine with a Lobed Shape Vortex Generator
First Stage Turbine Vane Arrangement
Combustor Liner
Application:
14/951,308 →
Publication:
US 2016/0146467
Sequential Burner for an Axial Gas Turbine
Abrasive Coated Substrate and Method for Manufacturing Thereof
Method of Operating a Multi-Stage Flamesheet Combustor
Damper of a Gas Turbine with a Gap
Rotor Heat Shield and Method for Securing the Same into a Rotor Assembly
Rotating Gas Turbine Blade and Gas Turbine with Such a Blade
Arrangement of a Rotor and at Least a Blade
Compensation Assembly for a Damper of a Gas Turbine
Axially Staged Mixer with Dilution Air Injection
Rotating Blade for a Gas Turbine
Separate Feedings of Cooling and Dilution Air
Mixer for Admixing a Dilution Air to the Hot Gas Flow
Gas Turbine Vane
Gas Turbine Fuel Pipe Comprising a Damper
Engine and Method for Operating Said Engine
Application:
14/979,152 →
Publication:
US 2016/0177833
Wall for a Hot Gas Channel in a Gas Turbine
Turbulator Structure on Combustor Liner
Centering Arrangement of Two Parts Relative to Each Other
Rotating Machine
Application:
15/007,542 →
Publication:
US 2016/0138410
Sequential Combustor Arrangement with a Mixer
Turbine Blade, Set of Turbine Blades, and Fir Tree Root for a Turbine Blade
Fuel Injection Device for a Gas Turbine Having Streamlined Bodies with Lobe Structure
Sequential Liner for a Gas Turbine Combustor
Method for Operating a Gas Turbine Arrangement
Method and Device for Flame Stabilization in a Burner System of a Stationary Combustion Engine
Welded Fuel Nozzle and Method of Fabricating a Fuel Nozzle
Application:
62/257,575 →
Related Assignments
(11)
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
Sep 11, 2013
From: ALSTOM
To: ALSTOM TECHNOLOGY LTD
Reel/Frame 031186/0561 →
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 →
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 →
Change of Name
Mar 22, 2016
From: ALSTOM TECHNOLOGY LTD
To: GENERAL ELECTRIC TECHNOLOGY GMBH
Reel/Frame 038216/0193 →