Patent Assignment
Reel/Frame 022488/0630
Change of Name
Recorded: 2009-03-31
Pages: 13
Assignor
SIEMENS POWER GENERATION, INC.
Executed: 2008-10-01
Assignee
SIEMENS ENERGY, INC.
4400 ALAFAYA TRAIL, ORLANDO, FLORIDA, 32826
Covered Properties
(434)
Infrared Imaging of Ultrasonically Excited Subsurface Defects in Materials
Patent:
6,236,049 →
Application:
09/397,585 →
High-Temperature Fuel Cell
System and method for identifying a defective component in a network environment
Application:
10/218,720 →
Publication:
US 2003/0097315
Apparatus and methods for sampling and analyzing inlet air associated with combustion turbine
Application:
10/252,214 →
Publication:
US 2004/0055900
Method for Producing a Fully Transposed High Tc Composite Superconductor and a Superconductor Produced by Said Method
Waste Heat Steam Generator
Bolted Assembly and Apparatus and Method for Tensioning the Bolted Assembly
Application:
10/559,370 →
Publication:
US 2009/0151517
Method and Apparatus for Measuring on-Line Failure of Turbine Thermal Barrier Coatings
Device and method for forming support systems for electric generator components
Application:
10/644,562 →
Publication:
US 2005/0034887
Segmented thermal barrier coating and method of manufacturing the same
Application:
10/649,536 →
Publication:
US 2004/0081760
Method for managing tools in a power plant service environment
Application:
10/661,682 →
Publication:
US 2005/0060243
Plasma Sprayed Ceramic-Metal Fuel Electrode
Turbine Component Tracking System
Outer air seal assembly
Application:
10/671,291 →
Publication:
US 2005/0067788
Consumable Insert and Method of Using the Same
Turbine blade tip with optimized abrasive
Application:
10/733,738 →
Publication:
US 2005/0129511
System and Method for Measuring Coating Thickness
Seal Usable Between Thermally Movable Components
Seal for a turbine engine
Application:
10/797,452 →
Publication:
US 2005/0200080
Two Stage Catalytic Combustor
Component Having Wear Coating Applied by Cold Spray Process
Catalytic Oxidation Element for a Gas Turbine Engine
Boron Free Joint for Superalloy Component
Turbine Blade for Monitoring Blade Vibration
System and method for processing inspection data for evaluating degradation of coating on components
Application:
10/910,867 →
Publication:
US 2005/0038817
Current Bus and Power Lead Assemblies for Solid Oxide Fuel Cell Generators
Heat Treatment of Superalloy Components
Repair of Nickel-Based Alloy Turbine Disk
Method to Use a Receiver Operator Characteristics Curve for Model Comparison in Machine Condition Monitoring
Recuperated Atmospheric Sofc/Gas Turbine Hybrid Cycle
Catalytic combustors
Application:
10/992,183 →
Publication:
US 2005/0070431
Combustor Flow Sleeve with Optimized Cooling and Airflow Distribution
Power Plant Life Assessment
Method for Forming Interphase Layers in Ceramic Matrix Composites
Gas turbine combustor
Application:
11/035,560 →
Publication:
US 2006/0156734
Weldability of Alloys with Directionally-Solidified Grain Structure
Turbine Engine Combustor with Bolted Swirlers
Nut cap and method of securing a nut on a bolt
Application:
11/062,283 →
Publication:
US 2006/0188357
Cooled Transition Duct for a Gas Turbine Engine
Manufacture of Specialized Alloys with Specific Properties
Method for Forming Turbine Seal by Cold Spray Process
Processing Method for Solid Core Ceramic Matrix Composite Airfoil
Welding of gamma'-strengthened superalloys
Application:
11/092,793 →
Publication:
US 2006/0219758
Catalytic Oxidation Module for a Gas Turbine Engine
Compression of Resin Impregnated Insulating Tapes
Insulation paper with high thermal conductivity materials
Application:
11/106,846 →
Publication:
US 2005/0274774
Fabrics with High Thermal Conductivity Coatings
Smart component for use in an operating environment
Application:
11/122,566 →
Publication:
US 2005/0198967
Hazard boundary termination box
Application:
11/122,570 →
Publication:
US 2006/0252308
Combined cycle power plant using compressor air extraction
Application:
11/127,476 →
Publication:
US 2006/0254280
Electrically conductive thermal barrier coatings capable for use in electrode discharge machining
Application:
11/145,439 →
Publication:
US 2006/0275553
System for Introducing Fuel to a Fluid Flow Upstream of a Combustion Area
Process for Producing a Three-Dimensional Object
High thermal conductivity materials incorporated into resins
Application:
11/152,983 →
Publication:
US 2005/0277349
Structured Resin Systems with High Thermal Conductivity Fillers
High thermal conductivity materials aligned within resins
Application:
11/152,985 →
Publication:
US 2005/0277721
High Thermal Conductivity Materials with Grafted Surface Functional Groups
Vibration stress relief of superalloy components
Application:
11/156,320 →
Publication:
US 2006/0283920
Turbine Blade Tip Clearance Control
Combustion Transition Duct Providing Stage 1 Tangential Turning for Turbine Engines
Illuminated Inspection Apparatus and Method of Employing the Same
Controlled Pilot Oxidizer for a Gas Turbine Combustor
Method of joining ceramic parts and articles so formed
Pin-Loaded Mounting Apparatus for a Refractory Component in a Combustion Turbine Engine
Radially Expanding Turbine Engine Exhaust Cylinder Interface
Cold Spray Method for Producing Gas Turbine Blade Tip
Refractory Component with Ceramic Matrix Composite Skeleton
Method of Instrumenting a Component
Method of Measuring in Situ Differential Emissivity and Temperature
High temperature erosion resistant coating and material containing compacted hollow geometric shapes
Application:
11/235,494 →
Publication:
US 2007/0237667
Utilization of Discontinuous Fibers for Improving Properties of High Temperature Insulation for Ceramic Matrix Composites
Method of sealing a free edge of a composite material
Application:
11/243,147 →
Publication:
US 2007/0075455
System for restoring turbine vane attachment systems in a turbine engine
Application:
11/243,148 →
Publication:
US 2007/0077148
Support System for Transition Ducts
Apparatus and Method of Monitoring Operating Parameters of a Gas Turbine
Apparatus and Method of Detecting Wear in an Abradable Coating System
Method and Apparatus for Measuring Compression in a Stator Core
Exhaust heat augmentation in a combined cycle power plant
Application:
11/297,063 →
Publication:
US 2007/0130952
Stepped Gradient Fuel Electrode and Method for Making the Same
Combustor Flow Sleeve Attachment System
Seamless solid oxide fuel cell
Application:
11/326,700 →
Publication:
US 2007/0160886
Ceramic Wash-Coat for Catalyst Support
Attachment for Ceramic Matrix Composite Component
Pilot Fuel Flow Tuning for Gas Turbine Combustors
System and Method for Improving the Heat Rate of a Turbine
System for recovering water from flue gas
Application:
11/345,724 →
Publication:
US 2007/0175333
Gas Turbine Engine Curved Diffuser with Partial Impingement Cooling Apparatus for Transitions
Advanced integration for improved integrated gasification combined cycle efficiency
Application:
11/350,560 →
Publication:
US 2007/0181854
Fuel Flow Tuning for a Stage of a Gas Turbine Engine
Gas Turbine Engine Transitions Comprising Closed Cooled Transition Cooling Channels
Advanced Asu and Hrsg Integration for Improved Integrated Gasification Combined Cycle Efficiency
Supercritical Pressurization of Fuel Slurry
Removable Diffusion Stage for Gas Turbine Engine Fuel Nozzle Assemblages
Monitoring Health of a Combustion Dynamics Sensing System
Axial diffusor for a turbine engine
Application:
11/378,028 →
Publication:
US 2007/0214792
Coatings for molybdenum-based substrates
Application:
11/390,744 →
Publication:
US 2007/0231595
Seeding Resins for Enhancing the Crystallinity of Polymeric Substructures
Mix of Grafted and Non-Grafted Particles in a Resin
Composite Insulation Tape with Loaded Htc Materials
Patterning on Surface with High Thermal Conductivity Materials
Seeding of Htc Fillers to Form Dendritic Structures
Air Flow Conditioner for a Combustor Can of a Gas Turbine Engine
Vane Shroud Through-Flow Platform Cover
Sulfur detector for gaseous fuels
Application:
11/403,568 →
Publication:
US 2007/0243108
High power density seal-less tubular solid oxide fuel cell by means of a wide interconnection
Application:
11/403,636 →
Publication:
US 2007/0243445
Self Regenerating Desulfurizer for Gaseous Fuels
Turbine airfoil with integral chordal support ribs
Application:
11/415,597 →
Publication:
US 2007/0258814
Combustor Liner for Gas Turbine Engine
Heat recovery gas turbine in combined brayton cycle power generation
Application:
11/418,862 →
Publication:
US 2007/0256424
Pilot Nozzle Heat Shield Having Internal Turbulators
Anode Gas Stack Start-Up Heater and Purge Gas Generator
Fluid Flow Distributor Apparatus for Gas Turbine Engine Mid-Frame Section
Fuel Heating System for Turbine Engines
Combined Cycle Power Plant
Abradable labyrinth tooth seal
Application:
11/441,895 →
Publication:
US 2007/0273104
Advanced Processing of Active Thermography Signals
Combustion Apparatus Using Pilot Fuel Selected for Reduced Emissions
Fuel Oil Bi-Directional Flow Divider
Combined 2D and 3D Nondestructive Examination
Systems and Methods for Integration of Gasification and Reforming Processes
Coating method for non-destructive examination of articles of manufacture
Cantilevered Framework Support for Turbine Vane
Rapid prototyping of ceramic articles
Leakage Flow Control and Seal Wear Minimization System for a Turbine Engine
Method and Apparatus for Monitoring Particles in a Gas Turbine Working Fluid
System for Modulating Fuel Supply to Individual Fuel Nozzles in a Can-Annular Gas Turbine
Method and Apparatus for Detecting a Flashback Condition in a Gas Turbine
Cmc with Multiple Matrix Phases Separated by Diffusion Barrier
Ring seal for a turbine engine
Application:
11/492,589 →
Publication:
US 2008/0025838
Turbine Engine Ring Seal
Combustor Liner with Reverse Flow for Gas Turbine Engine
Hollow Cmc Airfoil with Internal Stitch
Abradable Coating System
Weld Repair of Superalloy Materials
Micro-Combustor for Gas Turbine Engine
Turbine Airfoil with Near Wall Inflow Chambers
Slidable Spring-Loaded Transition-to-Turbine Seal Apparatus and Heat-Shielding System, Comprising the Seal, at Transition/Turbine Junction of a Gas Turbine Engine
At Least One Combustion Apparatus and Duct Structure for a Gas Turbine Engine
Axially Staged Combustion System for a Gas Turbine Engine
Rotor Disc Assembly with Abrasive Insert
Turbine Airfoil Cooling System with Platform Cooling Channels with Diffusion Slots
Turbine airfoil cooling system with near wall pin fin cooling chambers
Application:
11/506,080 →
Publication:
US 2010/0221121
Vortex Cooled Turbine Blade Outer Air Seal for a Turbine Engine
Inner Ring with Independent Thermal Expansion for Mounting Gas Turbine Flow Path Components
Resonator Device at Junction of Combustor and Combustion Chamber
Turbine Airfoil Cooling System with Axial Flowing Serpentine Cooling Chambers
Turbine Airfoil Cooling System with Bifurcated and Recessed Trailing Edge Exhaust Channels
Combustion turbine having a single compressor with inter-cooling between stages
Application:
11/510,242 →
Publication:
US 2008/0047276
Cooling Arrangement for Cmc Components with Thermally Conductive Layer
High Temperature Insulation and Insulated Article
Turbine blade tip gap reduction system for a turbine engine
Application:
11/518,018 →
Publication:
US 2008/0063513
Low coefficient of friction, wear resistant coating for steam turbine blade contact areas
Application:
11/518,019 →
Adjustable Turbine Exhaust Flow Guide and Bearing Cone Assemblies
Instrumented Component for Use in an Operating Environment
Instrumented Component for Combustion Turbine Engine
High Thermal Conductivity Dielectric Tape
Extended Life Fuel Nozzle
Turbine engine cooling fluid feed system
Application:
11/526,255 →
Stacked Laminate Bolted Ring Segment
Turbine Airfoil Cooling System with Platform Edge Cooling Channels
Morphological forms of fillers for electrical insulation
Application:
11/529,181 →
Publication:
US 2007/0026221
Superconducting Coil Support Structures
Nano and Meso Shell-Core Control of Physical Properties and Performance of Electrically Insulating Composites
Gas Turbine: Seal Between Adjacent Can Annular Combustors
Turbine airfoil cooling system with enhanced tip corner cooling channel
Application:
11/543,523 →
Publication:
US 2008/0085193
Turbine Airfoil with Submerged Endwall Cooling Channel
Thermal barrier coating system for a turbine airfoil usable in a turbine engine
Application:
11/543,649 →
Publication:
US 2008/0085191
Transition Duct for Gas Turbine Engine.
Ceramic Matrix Composite Turbine Engine Components with Unitary Stiffening Frame
Igcc Design and Operation for Maximum Plant Output and Minimum Heat Rate
Gas Turbine Belly Band Seal Anti-Rotation Structure
A Method for Removing the Endplate of an Electric Generator
Repair Fixture
Closed Loop Turbine Cooling Fluid Reuse System for a Turbine Engine
Turbine Vane Id Support
Turbine Airfoil Cooling System with Spanwise Equalizer Rib
Reusable inflatable shipping packing system
Application:
11/589,000 →
Publication:
US 2008/0099365
Stacked Laminate Fiber Wrapped Segment
System and Method for Separation and Control of Entrained Gas Mixture
System and Method for Generation of High Pressure Air in an Integrated Gasification Combined Cycle System
Ceramic matrix composite surfaces with open features for improved bonding to coatings
Application:
11/600,709 →
Publication:
US 2010/0119777
Transonic compressor rotors with non-monotonic meanline angle distributions
Application:
11/600,710 →
Publication:
US 2008/0118362
Air Seal Unit Adapted to Be Positioned Adjacent Blade Structure in a Gas Turbine
System and Method Employing Direct Gasification for Power Generation
Cooling of Turbine Blade Suction Tip Rail
Remote Viewing Apparatus
High temperature insulation with enhanced abradability
Application:
11/607,344 →
Publication:
US 2008/0274336
Three Dimensional Reinforced Cmc Articles by Interlocking Two Dimensional Structures
Blade Clearance System for a Turbine Engine
Axial tangential radial on-board cooling air injector for a gas turbine
Application:
11/639,859 →
Publication:
US 2008/0141677
Tip Clearance Control
Turbine Airfoil with Controlled Area Cooling Arrangement
Impact Resistant Thermal Barrier Coating System
Cooling Arrangement for a Tapered Turbine Blade
Aero-Mixing of Rotating Blade Structures
Rotor Winding Shield for a Superconducting Electric Generator
Damage Tolerant Gas Turbine Component
Power Generation System Incorporating Multiple Rankine Cycles
Advanced Cooling Method for Combustion Turbine Airfoil Fillets
Sprayed Weld Strip for Improved Weldability
Gas Turbine Engine
Anti-Flashback Features in Gas Turbine Engine Combustors
Multi-Layered Platelet Structure
Treatment of Micropores in Mica Materials
Ceramic matrix composite turbine engine component
Application:
11/698,225 →
Publication:
US 2009/0324393
Cmc to Metal Attachment Mechanism
Blade Assembly in a Combustion Turbo-Machine Providing Reduced Concentration of Mechanical Stress and a Seal Between Adjacent Assemblies
Method of Suppressing Combustion Instabilities Using a Resonator Adopting Counter-Bored Holes
Turbine Seal Plate Locking System
Low leakage spring clip/ring combinations for gas turbine engine
A-TIG welding of copper alloys for generator components
Application:
11/703,472 →
Publication:
US 2007/0181550
External Profile for Turbine Blade Airfoil
Thermally insulated CMC structure with internal cooling
Application:
11/707,191 →
Publication:
US 2008/0199661
Airfoil for a Gas Turbine
Ring Seal for a Turbine Engine
Flexible, High-Temperature Ceramic Seal Element
Turbine Blade Having a Convergent Cavity Cooling System for a Trailing Edge
Blade for a Gas Turbine
Ceramic matrix composite abradable via reduction of surface area
Application:
11/709,698 →
Publication:
US 2008/0206542
Optimized fabric lay-up for improved ceramic matrix composites
Application:
11/709,699 →
Publication:
US 2008/0207075
Transition Support System for Combustion Transition Ducts for Turbine Engines
System and Method for Oxygen Separation in an Integrated Gasification Combined Cycle System
Process and apparatus for cooling a metal part during a welding operation
Cmc Airfoil with Thin Trailing Edge
Blade Shroud Vibration Monitor
Fluid Pump Having Multiple Outlets for Exhausting Fluids Having Different Fluid Flow Characteristics
Cmc Wall Structure with Integral Cooling Channels
Thermally Balanced Near Wall Cooling for a Turbine Blade
Intensively Cooled Trailing Edge of Thin Airfoils for Turbine Engines
Wavy Flow Cooling Concept for Turbine Airfoils
Airfoil for a Gas Turbine Engine
Transition-To Turbine Seal Apparatus and Transition-to-Turbine Seal Junction of a Gas Turbine Engine
Multi-Pass Cooling for Turbine Airfoils
Nondestructive Inspection Heads for Components Having Limited Surrounding Space
Concentric Tube Support Assembly
Engine Brake for Part Load Co Reduction
Fiber Optic Generator Condition Monitor
Gas Turbine Engine
Stacked Laminate Gas Turbine Component
System for Applying a Continuous Surface Layer on Porous Substructures of Turbine Airfoils
Heat Treatment System for a Composite Turbine Engine Component
System for Forming a Gas Cooled Airfoil for Use in a Turbine Engine
Superalloy forming highly adherent chromia surface layer
Application:
11/784,987 →
Publication:
US 2008/0253923
Co-Forged Steel Rotor Component for Steam and Gas Turbine Engines
Co-Forged Nickel-Steel Rotor Component for Steam and Gas Turbine Engines
Rare earth modified corrosion resistant superalloy with enhanced oxidation resistance and coating compatibility
Application:
11/788,238 →
Publication:
US 2007/0202002
Rare earth modified high strength oxidation resistant superalloy with enhanced coating compatibility
Application:
11/788,295 →
Publication:
US 2007/0202003
Corrosion resistant superalloy with improved oxidation resistance
Application:
11/788,299 →
Publication:
US 2007/0199629
Apparatus for mixing fuel and air in a combustion system
Oxidation resistant superalloy
Application:
11/788,301 →
Publication:
US 2008/0260571
Corrosion and oxidation resistant directionally solidified superalloy
Application:
11/788,302 →
Publication:
US 2008/0260572
Airfoil for a Turbine of a Gas Turbine Engine
Abradable Cmc Stacked Laminate Ring Segment for a Gas Turbine
System and method of evaluating uncoated turbine engine components
Application:
11/800,789 →
Publication:
US 2008/0101683
Turbine Airfoil with Enhanced Cooling
Patterned Reduction of Surface Area for Abradability
Impingement Jets Coupled to Cooling Channels for Transition Cooling
Multivane Segment Mounting Arrangement for a Gas Turbine
Wear Minimization System for a Compressor Diaphragm
Process for Applying a Thermal Barrier Coating to a Ceramic Matrix Composite
Enterprise-wide data standardization structure and method
Application:
11/804,403 →
Publication:
US 2008/0288269
Blade for a Gas Turbine Engine
Near Wall Cooling for a Highly Tapered Turbine Blade
Mems Emissions Sensor System for a Turbine Engine
Gas Turbine Transition Duct Coupling Apparatus
Turbine Airfoils with Near Surface Cooling Passages and Method of Making Same
Turbine vane with divided turbine vane platform
Application:
11/807,390 →
Publication:
US 2008/0298973
Eccentric Polygonal Main Lead Flexible Connector Assembly
Temperature Monitor for Bus Structure Flex Connector
Turbine Rotor Blade Groove Entry Slot Lock Structure
Regenerative Static Excitation System for Superconducting Rotor
Atomic Layer Epitaxy Processed Insulation
Combined Cycle Power Generation
Ceramic Matrix Composite Attachment Apparatus and Method
Turbine Airfoil Cooling System with Rotor Impingement Cooling
Method of constructing a hollow fiber reinforced structure
Application:
11/825,691 →
Publication:
US 2009/0014926
Angled honeycomb seal between turbine rotors and turbine stators in a turbine engine
Application:
11/825,692 →
Publication:
US 2009/0014964
Turbine Vane Securing Mechanism
Gas Turbine Engine Adapted for Use in Combination with an Apparatus for Separating a Portion of Oxygen from Compressed Air
Method and System for Limiting a Current in an Alternating Current Generator
Application:
11/850,951 →
Publication:
US 2009/0067101
Wavy Cmc Wall Hybrid Ceramic Apparatus
Non-Rectangular Resonator Devices Providing Enhanced Liner Cooling for Combustion Chamber
Crack-Free Erosion Resistant Coatings on Steels
Gas Turbine Component with Reduced Cooling Air Requirement
Integral Single Crystal/Columnar Grained Component and Method of Casting the Same
High Thermal Conductivity Mica Paper Tape
Application:
11/860,635 →
Publication:
US 2008/0050580
Electrical Insulation Tape with Controlled Bonding and Resin Impregnation Properties
Method of on-Line Turbine Blade Slope and Sensor Position Verification
Method and Apparatus for Tracking a Rotating Blade Tip for Blade Vibration Monitor Measurements
Non-Synchronous Vibrational Excitation of Turbine Blades Using a Rotating Excitation Structure
Solid Oxide Fuel Cell Generator with Mid-Stack Fuel Feed
Integrated Fuel Gas Characterization System
Maximum Blade Surface Temperature Estimation for Advanced Stationary Gas Turbines in Near-Infrared (with Reflection)
Method of Coalescing Information About Inspected Objects
Method and System for Interactive Virtual Inspection of Modeled Objects
Solid Oxide Fuel Cell Generator Including a Glass Sealant
Wear Prevention Spring for Turbine Blade
Rotating Apparatus Disk
Vane Assembly with Metal Trailing Edge Segment
Method of Matching Sensors in a Multi-Probe Turbine Blade Vibration Monitor
Stacked Lamellae Ceramic Gas Turbine Ring Segment Component
Ring Segment Coolant Seal Configuration
Turbine Blade Tip Cooling System
Turbine Airfoil Cooling System with Recessed Trailing Edge Cooling Slot
Sequential Combustion Firing System for a Fuel System of a Gas Turbine Engine
Turbine Blade Tip Cooling System
Thermally Protective Multiphase Precipitant Coating
Turbine Vane for a Gas Turbine Engine
Rotor Pole Crossover Connection
Thermally Insulating Layer Incorporating a Distinguishing Agent
Airfoil Seal System for Gas Turbine Engine
Centerline Suspension for Turbine Internal Component
Airfoil with Cooling Hole Having a Flared Section
Application:
12/018,994 →
Publication:
US 2009/0074588
Sealing Band Having Bendable Tang with Anti-Rotation in a Turbine and Associated Methods
Application:
12/019,002 →
Publication:
US 2009/0191050
Method of Layered Fabrication
Application:
12/019,900 →
Publication:
US 2009/0188097
Engine Portions with Functional Ceramic Coatings and Methods of Making Same
Imparting Functional Characteristics to Engine Portions
Automated Remote Carriage for Tightening Generator Wedges
Turbine Disc Sealing Assembly
Metal Injection Joining
Multi-Stage Axial Combustion System
Horizontal Assembly of Stator Core Using Keybar Extensions
Method and Apparatus for Forming Insulated Rotor Conductors
Method for Removing a Half Turn of a Coil from a Slot of a Dynamoelectric Machine
Airfoil Structure Shim
Superalloy Component Welding at Ambient Temperature
Electronic Ground Detection Apparatus for Use on Ground Detector Ring of Power Generating System
Winding for Use in High Temperature Superconducting Generator
Gas Turbine Engine Including Temperature Control Device and Method Using Memory Metal
Application:
12/044,017 →
Publication:
US 2009/0226327
Real-Time Body Segmentation System
Igniter Assembly for a Gas Turbine
Method of Producing a Turbine Component with Multiple Interconnected Layers of Cooling Channels
Power Generator and Power Generator Auxiliary Monitoring
Mechanically Affixed Turbine Shroud Plug
Method of in Slot Tightness Measuring of Stator Coil
Method of Increasing Service Interval Periods in a Steam Turbine
Fastener Assembly with Cyclone Cooling
Method of Forming a Catalyst Element Having a Thermal Barrier Coating as the Catalyst Substrate
Turbine Blade Tip Gap Reduction System
Hybrid Ceramic Structure with Internal Cooling Arrangements
Sealing Arrangement for Turbine Engine Having Ceramic Components
Anisotropic Soft Ceramics for Abradable Coatings in Gas Turbines
Application:
12/101,460 →
Publication:
US 2009/0258247
Apparatus Comprising a Cmc-Comprising Body and Compliant Porous Element Preloaded Within an Outer Metal Shell
Combustion Turbine Including a Diffuser Section with Cooling Fluid Passageways and Associated Methods
Electrical Machine Including Axial Connector Assemblies and Related Methods
Cmc Anchor for Attaching a Ceramic Thermal Barrier to Metal
Fuel Cell Generator with Fuel Electrodes That Control on-Cell Fuel Reformation
Method of Restoring Near-Wall Cooled Turbine Components
Application:
12/117,954 →
Publication:
US 2009/0324841
Gas Turbine Exhaust Sound Suppressor and Associated Methods
Electric Machine Having Electrically Conductive Member and Associated Insulation Assembly and Related Methods
System and Method for Selective Catalytic Reduction of Nitrogen Oxides in Combustion Exhaust Gases
Catalytic Process for Control of Nox Emissions Using Hydrogen
Electrical-Discharge-Inhibiting Conformable Layer for Use in Inner-Cooled Coils
Shaft Seal Assembly for Hydrogen Cooled Turbine Generator
Apparatus for Impact Testing for Electric Generator Stator Wedge Tightness
Method and System for Monitoring Partial Discharge Within an Electric Generator
Application:
12/132,708 →
Publication:
US 2009/0302862
Method and Apparatus for Checking Stator Core Alignment
Apparatus and Method for the Installation of a Pre-Assembled Stator Core
Method of Analyzing Non-Synchronous Vibrations Using a Dispersed Array Multi-Probe Machine
Fuel Injector for Low Nox Furnace
Application:
12/154,972 →
Publication:
US 2009/0297996
Polymer Brushes
Stator Coil with Improved Heat Dissipation
Fabrication of Copper-Based Anodes via Atmosphoric Plasma Spraying Techniques
Solid Oxide Fuel Cell with Transitioned Cross-Section for Improved Anode Gas Management at the Open End
Corrosion Resistant Alloy Compositions with Enhanced Castability and Mechanical Properties
Application:
12/173,983 →
Publication:
US 2009/0041615
Forward-Section Resonator for High Frequency Dynamic Damping
Process of Producing an Abradable Thermal Barrier Coating with Solid Lubricant
Application:
12/174,219 →
Publication:
US 2010/0015350
Ceramic Matrix Composite Wall with Post Laminate Stitching
Electrical Partial Discharge Pulse Marker Discrimination
Elimination of Plate Fins in Combustion Baskets by Cmc Insulation Installed by Shrink Fit
Fuel Heating via Exhaust Gas Extraction
Structure and Method for Protecting a Hybrid Ceramic Structure from Moisture Attack in a High Temperature Environment
Method of Forming a Turbine Engine Component Having a Vapor Resistant Layer
Application:
12/177,567 →
Publication:
US 2010/0021643
Method of Manufacturing a Thermal Insulation Article
Integral Flow Sleeve and Fuel Injector Assembly
Turbine Engine Flow Sleeve
Turbine Engine Component with Cooling Passages
Injection Molded Component
Method for Spacing Electrical Conductors and Related Devices
Process for Applying a Shape Memory Alloy Erosion Resistant Protective Structure Onto an Airfoil of a Turbine Blade
Transition with a Linear Flow Path with Exhaust Mouths for Use in a Gas Turbine Engine
Transition with a Linear Flow Path for Use in a Gas Turbine Engine
Canted Outlet for Transition in a Gas Turbine Engine
Methodology and Tooling Arrangements for Strengthening a Surface Bond in a Hybrid Ceramic Matrix Composite Structure
Application:
12/194,108 →
Publication:
US 2010/0047512
Subsurface Inclusion of Spheroids and Methodology for Strengthening a Surface Bond in a Hybrid Ceramic Matrix Composite Structure
Application:
12/194,135 →
Publication:
US 2010/0047526
Method of Making Rare-Earth Strengthened Components
Combustion Turbine Component Having Rare Earth Nicocral Coating and Associated Methods
Combustion Turbine Component Having Rare Earth Conicral Coating and Associated Methods
Combustion Turbine Component Having Rare Earth Nicral Coating and Associated Methods
Combustion Turbine Component Having Rare Earth Fecral Coating and Associated Methods
Apparatus and Method for Controlling the Secondary Injection of Fuel
Combustion Turbine Component Having Bond Coating and Associated Methods
Grid Ceramic Matrix Composite Structure for Gas Turbine Shroud Ring Segment
Apparatus and Method for Monitoring Wear of Components
Deconstructable Assembly and Method
Gas Turbine Transition Duct Apparatus
Integrated Fuel Gas Characterization System
Method of Making a Combustion Turbine Component Using Thermally Sprayed Transient Liquid Phase Forming Layer
Application:
12/198,464 →
Publication:
US 2011/0171394
Method of Forming Molybdenum Based Wear Resistant Coating on a Workpiece
Application:
12/198,478 →
Publication:
US 2010/0055339
Turbine Engine Cover Plate Assembly Stand
Bimetallic Bond Layer for Thermal Barrier Coating on Superalloy
Circumferential Shroud Inserts for a Gas Turbine Vane Platform
Compressor Blade Having a Ratio of Leading Edge Sweep to Leading Edge Dihedral in a Range of 1:1 to 3:1 Along the Radially Outer Portion.
Combustor Device and Transition Duct Assembly
Application:
12/204,087 →
Publication:
US 2010/0050649
Multilayered Ceramic Matrix Composite Structure Having Increased Structural Strength
Turbine Vane with High Temperature Capable Skins
Stationary Turbine Component with Laminated Skin
Turbine Transition Duct Apparatus
Combustion Turbine Component Having Rare-Earth Elements and Associated Methods
Application:
12/205,956 →
Publication:
US 2010/0061875
Method and System for Controlling Fuel to a Dual Stage Nozzle
Composite Blade and Method of Manufacture
Segmented Annular Combustor
Asymmetric Heat Sink Welding Using a Penetration Enhancing Compound
Ceramic Matrix Composite Structure
Method and System for Monitoring the Condition of Generator End Windings
Method of Forming Metallic Carbide Based Wear Resistant Coating on a Combustion Turbine Component
Application:
12/210,346 →
Publication:
US 2010/0068405
Flashback Resistant Pre-Mixer Assembly
Secondary Fuel Delivery System
Combustor Assembly Comprising a Combustor Device, a Transition Duct and a Flow Conditioner
Cooling Structure for Outer Surface of a Gas Turbine Case
Shaft Cover Structure for Use in an Exciter
Solution Heat Treatment and Overage Heat Treatment for Titanium Components
Pilot Burner for Gas Turbine Engine
Gas Turbine Airfoil
Combustor Apparatus in a Gas Turbine Engine
Ultrasonic Coating Removal Method
Application:
12/234,763 →
Publication:
US 2010/0275949
Subsurface Inclusion of Fugitive Objects and Methodology for Strengthening a Surface Bond in a Hybrid Ceramic Matrix Composite Structure
Alternately Swirling Mains in Lean Premixed Gas Turbine Combustors
Combustion Turbine Component Having Rare-Earth Strengthened Alloy and Associated Methods
Application:
12/236,631 →
Publication:
US 2010/0278680
Spiral Cooled Fuel Nozzle
Method of Making a Combustion Turbine Component from Metallic Combustion Turbine Subcomponent Greenbodies
Application:
12/238,774 →
Publication:
US 2009/0183850
Formation of Imprints and Methodology for Strengthening a Surface Bond in a Hybrid Ceramic Matrix Composite Structure
Application:
12/238,897 →
Publication:
US 2010/0080953
Segmented Thermal Barrier Coating
Multiple Piece Turbine Engine Airfoil with a Structural Spar
Related Assignments
(3)
Other recorded transfers of the patents in this record — the chain of ownership.
Confirmatory License
Sep 19, 2007
From: SIEMENS POWER GENERATION, INC.
To: US DEPARTMENT OF ENERGY
Reel/Frame 019846/0453 →
Assignment of Assignor's Interest
Feb 16, 2009
From: SIEMENS ENERGY, INC. (FORMERLY KNOWN AS SIEMENS POWER GENERATION, INC., FORMERLY KNOWN AS SIEMENS WESTINGHOUSE POWER CORPORATION
To: SIEMENS AKTIENGESELLSCHAFT
Reel/Frame 022265/0613 →
Confirmatory License
Jun 6, 2014
From: SIEMENS ENERGY, INC.
To: ENERGY, UNITED STATES DEPARTMENT OF
Reel/Frame 033148/0956 →