IP Library Assignment 066923/0229
Patent Assignment
Reel/Frame 066923/0229

Release of Security Interest

Recorded: 2024-03-27 Pages: 9
Assignor
HPS INVESTMENT PARTNERS, LLC
Executed: 2024-03-27
Assignee
CHROMALLOY GAS TURBINE LLC
4100 RCA BLVD., SUITE 100, PALM BEACH GARDENS, FLORIDA, 33410
Covered Properties (30)
Thermal Barrier Coating Having Low Thermal Conductivity
Patent: 6,764,779 →
Application: 10/372,358 →
Thermal Barrier Coating Having Low Thermal Conductivity
Patent: 6,803,135 →
Application: 10/372,570 →
Publication: US 2004/0166356
Welding Single Crystal Articles
Patent: 6,872,912 →
Application: 10/889,207 →
Process for Repairing Sulfidation Damaged Turbine Components
Patent: 7,146,990 →
Application: 11/189,347 →
Turbine Vane Restoration System
Patent: 8,186,056 →
Application: 11/823,767 →
Publication: US 2009/0000102
Tri-Barrier Ceramic Coating
Patent: 9,017,792 →
Application: 13/066,974 →
Publication: US 2012/0276352
Process and Apparatus to Restore Distorted Features on Gas Turbine Vanes
Patent: 9,138,793 →
Application: 14/208,489 →
Publication: US 2014/0259662
Turbine Blade Platform Undercut with Decreasing Radii Curve
Application: 14/972,575 →
Publication: US 2016/0186572
First Stage Turbine Blade
Application: 16/107,363 →
Publication: US 2020/0063565
Second Stage Turbine Blade
Application: 16/107,401 →
Publication: US 2020/0063570
First Stage Turbine Nozzle
Application: 16/107,408 →
Publication: US 2020/0063579
Second Stage Turbine Nozzle
Application: 16/107,416 →
Publication: US 2020/0063580
Method and Apparatus for Improving Cooling of a Turbine Shroud
Application: 16/173,410 →
Publication: US 2020/0131913
Method and Apparatus for Improving Turbine Blade Sealing in a Gas Turbine Engine
Application: 16/173,714 →
Publication: US 2020/0131915
Method and Apparatus for Mounting a Transition Duct in a Gas Turbine Engine
Application: 16/178,677 →
Publication: US 2020/0141251
Axial Stop Configuration for a Combustion Liner
Application: 16/178,682 →
Publication: US 2020/0141585
Cross Fire Tube Retention System
Application: 16/178,688 →
Publication: US 2020/0141584
System and Method for Providing Compressed Air to a Gas Turbine Combustor
Application: 16/178,768 →
Publication: US 2020/0141252
Turbulator Geometry for a Combustion Liner
Application: 16/179,143 →
Publication: US 2020/0141576
Diffuser Guide Vane with Deflector Panel Having Curved Profile
Application: 16/179,378 →
Publication: US 2020/0141250
Method and Apparatus for Improving Core Manufacturing for Gas Turbine Components
Application: 16/229,425 →
Publication: US 2020/0198180
Nickel-Base Alloy for Gas Turbine Components
Application: 16/242,175 →
Publication: US 2020/0216932
Core Pattern Reformer Tool
Application: 16/413,030 →
Publication: US 2020/0360985
Systems and Methods for Modal Testing of Turbine Blades
Application: 16/458,475 →
Publication: US 2020/0003654
System for Fixturing a Gas Turbine Engine Component for an Electroplating Process
Application: 16/897,857 →
Publication: US 2021/0388522
Method of Repairing An Engine Case Flange
Application: 17/086,609 →
Publication: US 2021/0131310
Core Pattern Reformer Tool
Application: 17/227,895 →
Publication: US 2021/0229164
Spherical Fused Silica Compositions for Injection Molded Ceramic Cores and Methods of Making Parts Using Such Compositions
Application: 17/660,038 →
Publication: US 2023/0339013
Systems and Methods of Bonding Wax Components for Lost Wax Casting
Application: 63/260,524 →
Systems and Methods of Repairing a Hollow Fan Blade
Application: 63/366,707 →
Related Assignments (1)
Other recorded transfers of the patents in this record — the chain of ownership.
Security Interest Mar 27, 2024
From: CHROMALLOY GAS TURBINE LLC
To: ROYAL BANK OF CANADA
Reel/Frame 066926/0565 →