Patent Assignment
Reel/Frame 066926/0565
SECURITY INTEREST
Recorded: 2024-03-27
Received: 2024-03-27
Pages: 16
Assignor
CHROMALLOY GAS TURBINE LLC
Executed: 2024-03-27
Assignee
ROYAL BANK OF CANADA
20 KING STREET WEST, 4TH FLOOR, TORONTO, CAX, M5H1C4, CANADA
Covered Applications
(46)
Masking Systems
App. No. 18/443,244
→
System for Securing Component for an Electrically-Driven Process
App. No. 18/443,250
→
Masking System
App. No. 18/433,679
→
TOOLING AND METHOD FOR MASKING A TURBINE COMPONENT SUCH AS A BLADE OR VANE
App. No. 18/430,364
→
TURBINE COMPONENT HOLDER FOR IMAGING
App. No. 18/422,446
→
Multi-Component Masking System
App. No. 18/415,750
→
Multi-Component Masking Systems for High Temperature Applications
App. No. 18/529,944
→
Plating Tool Tooling System
App. No. 18/529,258
→
ADDITIVELY MANUFACTURED PROTECTIVE COVER FOR GAS TURBINE COMPONENTS
App. No. 18/491,574
→
Additively Manufactured Masking System
App. No. 18/478,126
→
Systems and Methods for Repairing Compressor Blades Using Hybrid Manufacturing Techniques
App. No. 18/475,094
→
Method and Apparatus for Improving Core Manufacturing for Gas Turbine Components
App. No. 18/458,820
→
Repair of Aircraft Fan Blade
App. No. 18/446,923
→
Additively Manufactured Tooling for Coating Components Using Electrically Driven Aqueous Processes
App. No. 18/337,807
→
Fastening System for Securing a Component to a Mounting Device for a High-Temperature Process
App. No. 18/298,703
→
Systems and Methods of Bonding Wax Components for Lost Wax Casting
App. No. 18/041,759
→
Repair of Aircraft Fan Blade
App. No. 18/156,466
→
Method for Fixturing a Gas Turbine Engine Component for an Electroplating Process
App. No. 18/155,187
→
Systems and Methods for Repairing Compressor Blades Using Hybrid Manufacturing Techniques
App. No. 17/931,500
→
Spherical Fused Silica Compositions for Injection Molded Ceramic Cores and Methods of Making Parts Using Such Compositions
App. No. 17/660,038
→
Core Pattern Reformer Tool
App. No. 17/227,895
→
Method of Repairing An Engine Case Flange
App. No. 17/086,609
→
SYSTEM FOR FIXTURING A GAS TURBINE ENGINE COMPONENT FOR AN ELECTROPLATING PROCESS
App. No. 16/897,857
→
SYSTEMS AND METHODS FOR MODAL TESTING OF TURBINE BLADES
App. No. 16/458,475
→
CORE PATTERN REFORMER TOOL
App. No. 16/413,030
→
NICKEL-BASE ALLOY FOR GAS TURBINE COMPONENTS
App. No. 16/242,175
→
METHOD AND APPARATUS FOR IMPROVING CORE MANUFACTURING FOR GAS TURBINE COMPONENTS
App. No. 16/229,425
→
METHOD AND APPARATUS FOR MOUNTING A TRANSITION DUCT IN A GAS TURBINE ENGINE
App. No. 16/178,677
→
CROSS FIRE TUBE RETENTION SYSTEM
App. No. 16/178,688
→
SYSTEM AND METHOD FOR PROVIDING COMPRESSED AIR TO A GAS TURBINE COMBUSTOR
App. No. 16/178,768
→
DIFFUSER GUIDE VANE WITH DEFLECTOR PANEL HAVING CURVED PROFILE
App. No. 16/179,378
→
AXIAL STOP CONFIGURATION FOR A COMBUSTION LINER
App. No. 16/178,682
→
TURBULATOR GEOMETRY FOR A COMBUSTION LINER
App. No. 16/179,143
→
METHOD AND APPARATUS FOR IMPROVING TURBINE BLADE SEALING IN A GAS TURBINE ENGINE
App. No. 16/173,714
→
METHOD AND APPARATUS FOR IMPROVING COOLING OF A TURBINE SHROUD
App. No. 16/173,410
→
FIRST STAGE TURBINE NOZZLE
App. No. 16/107,408
→
SECOND STAGE TURBINE BLADE
App. No. 16/107,401
→
SECOND STAGE TURBINE NOZZLE
App. No. 16/107,416
→
FIRST STAGE TURBINE BLADE
App. No. 16/107,363
→
TURBINE BLADE PLATFORM UNDERCUT WITH DECREASING RADII CURVE
App. No. 14/972,575
→
PROCESS AND APPARATUS TO RESTORE DISTORTED FEATURES ON GAS TURBINE VANES
App. No. 14/208,489
→
TRI-BARRIER CERAMIC COATING
App. No. 13/066,974
→
TURBINE VANE RESTORATION SYSTEM
App. No. 11/823,767
→
METHOD FOR THE PRODUCTION OF A HOLE AND DEVICE
App. No. 10/574,724
→
PROCESS FOR REPAIRING SULFIDATION DAMAGED TURBINE COMPONENTS
App. No. 11/189,347
→
WELDING SINGLE CRYSTAL ARTICLES
App. No. 10/889,207
→