IP Library › Assignment 059619/0336
Patent Assignment
Reel/Frame 059619/0336

RELEASE OF SECURITY INTEREST

Recorded: 2022-04-06 Received: 2022-04-06 Pages: 30
Assignor
Assignees
KTT CORE, INC.
1701 MILITARY TRAIL, SUITE 110, 120, 130, JUPITER, FL, 33458, UNITED STATES
FTT AMERICA, LLC
1701 MILITARY TRAIL, SUITE 110, 120, 130, JUPITER, FL, 33458, UNITED STATES
CONSOLIDATED TURBINE SPECIALISTS, LLC
24323 S. 385TH WEST AVENUE, BRISTOW, OK, 74010, UNITED STATES
FLORIDA TURBINE TECHNOLOGIES, INC.
1701 MILITARY TRAIL, SUITE 110, 120, 130, JUPITER, FL, 33458, UNITED STATES
Covered Applications (100)
PROCESS FOR RETROFITTING AN INDUSTRIAL GAS TURBINE ENGINE FOR INCREASED POWER AND EFFICIENCY
App. No. 16/301,560
→
HIGH PRESSURE COMPRESSOR DIFFUSER FOR AN INDUSTRIAL GAS TURBINE ENGINE
App. No. 16/094,378
→
INDUSTRIAL GAS TURBINE ENGINE WITH FIRST AND SECOND STAGE ROTOR COOLING
App. No. 15/998,911
→
Variable Pitch Fan for Gas Turbine Engine
App. No. 16/052,951
→
Cast Integrally Bladed Rotor with Bore Entry Cooling
App. No. 16/048,775
→
TURBOPUMP WITH A SINGLE PIECE HOUSING AND A SMOOTH ENAMEL GLASS SURFACE
App. No. 16/072,087
→
Apparatus and process of forming an integrally bladed rotor with cooled single crystal blades and an equiax nickel disk
App. No. 16/038,252
→
METAL ADDITIVE MANUFACTURING PROCESS OF FORMING AN INTEGRALLY BLEND ROTOR
App. No. 16/015,387
→
Process of forming a metal additive manufactured part with a smooth surface
App. No. 16/014,322
→
GEARED TURBOFAN AERO GAS TURBINE ENGINE WITH SOLID BORE TURBINE DISK
App. No. 15/983,503
→
Gas Turbine Engine Fan Stage with Bearing Cooling
App. No. 15/967,684
→
CAES COMBUSTOR TEST FACILITY
App. No. 15/764,910
→
Apparatus and process for optimizing turbine engine performance via load control through a power control module
App. No. 15/928,543
→
Generator Cooling Impeller and Bearing/Rotor Cooling
App. No. 15/928,489
→
GAS TURBINE ENGINE SECONDARY AIR SYSTEM AND AXIAL THRUST MANAGEMENT SYSTEM FOR A ROTOR OF THE ENGINE
App. No. 15/928,500
→
DEVICE FOR SUSPENDING A TUBULAR FROM A FLOATING VESSEL
App. No. 15/573,133
→
ADVANCED LEAN BURN INJECTOR IGNITER SYSTEM
App. No. 15/704,683
→
High Temperature High Pressure Non-Vitiated Heater
App. No. 15/685,470
→
APPARATUS AND PROCESS OF RETROFITTING A COMBINED CYCLE POWER PLANT
App. No. 15/549,050
→
Gas Turbine Engine with Multiple Electric Generators
App. No. 15/616,590
→
Apparatus and process for testing an aero vehicle at high Mach number
App. No. 15/602,306
→
Aircraft with gas turbine engine having outer bypass elements removed
App. No. 15/600,822
→
Gas turbine engine with axial flow fan with twin stream impeller and variable area bypass nozzle
App. No. 15/597,216
→
Interlocking Axial Labyrinth Seal
App. No. 15/472,350
→
Twin spool industrial gas turbine engine low pressure compressor with diffuser
App. No. 15/444,374
→
Turbine airfoil with thin trailing edge cooling circuit
App. No. 15/433,332
→
TURBOCHARGER WITH AIR JOURNAL BEARING AND THRUST BEARING
App. No. 15/429,212
→
Turbine Stator Vane with Multiple Outer Diameter Pressure Feeds
App. No. 15/405,467
→
Cooled Combustor Case with Over-Pressurized Cooling Air
App. No. 15/340,532
→
Process for repairing a worn carburized steel surface of a sprag clutch
App. No. 15/339,472
→
Air cooled turbine rotor blade for closed loop cooling
App. No. 15/255,227
→
Turbine stator vane with closed-loop sequential impingement cooling insert
App. No. 15/253,210
→
Turbopump with a single piece housing and a smooth enamel glass surface
App. No. 15/227,031
→
Process for launching a cruise missile from an aircraft
App. No. 15/216,966
→
Integrally bladed rotor with bore entry cooling holes
App. No. 15/203,905
→
PROCESS FOR TESTING A COMPRESSOR OR A COMBUSTOR OF A GAS TURBINE ENGINE USING A LARGE COMPRESSED AIR STORAGE RESERVOIR
App. No. 15/200,102
→
Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoir
App. No. 15/200,125
→
PROCESS FOR TESTING A COMPRESSOR OR A COMBUSTOR OF A GAS TURBINE ENGINE USING A LARGE COMPRESSED AIR STORAGE RESERVOIR
App. No. 15/200,057
→
Apparatus and process for removing support structure from a 3D printed part
App. No. 15/190,229
→
Variable low turbine vane with aft rotation axis
App. No. 15/174,051
→
Apparatus and process for manufacturing a centrifugal pump with a rotor within a single piece housing
App. No. 15/173,773
→
Process for retrofitting an industrial gas turbine engine for increased power and efficiency
App. No. 15/157,269
→
High pressure compressor diffuser for an industrial gas turbine engine
App. No. 15/146,036
→
Identity Management Service Using A Blockchain Providing Identity Transactions Between Devices
App. No. 15/146,872
→
APPARATUS AND PROCESS FOR FORMING AN AIR COOLED TURBINE AIRFOIL WITH A COOLING AIR CHANNEL AND DISCHARGE SLOT IN A THIN WALL
App. No. 15/143,666
→
Low pressure compressor diffuser and cooling flow bleed for an industrial gas turbine engine
App. No. 15/137,280
→
Twin spool industrial gas turbine engine with variable inlet guide vanes
App. No. 15/137,248
→
Industrial gas turbine engine with turbine airfoil cooling
App. No. 15/131,426
→
High pressure ratio twin spool industrial gas turbine engine with dual flow high spool compressor
App. No. 15/092,292
→
HIGH PRESSURE RATIO TWIN SPOOL INDUSTRIAL GAS TURBINE ENGINE
App. No. 15/021,531
→
Apparatus and process for determining a convective heat transfer coefficient between a moving fluid and a bounding surface
App. No. 15/053,008
→
Turbine rotor blade of the spar and shell construction
App. No. 15/009,940
→
Process of forming a metal part from a metal powder using a laser to melt the metal powder over a support surface that can be easily removed after the metal part has been formed
App. No. 14/991,469
→
Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoir
App. No. 14/934,219
→
Apparatus and process for converting an aero gas turbine engine into an industrial gas turbine engine for electric power production
App. No. 14/854,119
→
Apparatus and process for refining features in an additive manufactured part
App. No. 14/805,918
→
Air riding seal for a turbine
App. No. 14/795,095
→
Self-balancing air riding seal for a turbine
App. No. 14/740,317
→
Turbine interstage seal with self-balancing capability
App. No. 14/739,536
→
Sensor for detecting hydrocarbon in a static drain line
App. No. 14/623,007
→
ADVANCED LEAN BURN INJECTOR IGNITER SYSTEM
App. No. 14/614,215
→
Turbocharger with oil-free hydrostatic bearing
App. No. 14/607,846
→
LIQUID ROCKET ENGINE WITH HYBRID ELECTRIC MOTOR DRIVEN PUMP
App. No. 14/548,598
→
Air riding seal with purge cavity
App. No. 14/548,492
→
Turbine stator vane with insert and flexible seal
App. No. 14/534,489
→
Multiple Wall Impingement Plate for Sequential Impingement Cooling of an Endwall
App. No. 14/533,239
→
TURBINE LAST STAGE ROTOR BLADE WITH FORCED DRIVEN COOLING AIR
App. No. 14/512,070
→
Sequential cooling insert for turbine stator vane
App. No. 14/511,211
→
Gas turbine engine with liquid metal cooling
App. No. 14/450,944
→
Small turbine stator vane with impingement cooling insert
App. No. 14/291,510
→
Multiple staged compressor with last stage airfoil cooling
App. No. 14/246,166
→
TURBOCHARGER WITH OIL-FREE HYDROSTATIC BEARING
App. No. 14/245,199
→
Sequential cooling insert for turbine stator vane
App. No. 14/176,730
→
Turbine rotor blade with super cooling
App. No. 14/163,535
→
Process for forming an air cooled turbine airfoil
App. No. 14/101,761
→
APPARATUS AND PROCESS FOR TESTING AN INDUSTRIAL GAS TURBINE ENGINE AND COMPONENTS THEREOF
App. No. 14/008,308
→
Floating air riding seal for a turbine
App. No. 14/066,364
→
Gas turbine engine with liquid metal cooling
App. No. 14/056,992
→
Turbine with radial acting seal
App. No. 14/030,102
→
MULTIPLE STAGED COMPRESSOR WITH LAST STAGE AIRFOIL COOLING
App. No. 13/946,003
→
MULTIPLE STAGED COMPRESSOR WITH LAST STAGE AIRFOIL COOLING
App. No. 13/904,629
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Circulating fluidized bed cooling for an industrial gas turbine engine
App. No. 13/835,692
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Split ring floating air riding seal for a turbine
App. No. 13/793,853
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HIGH SPEED INDUSTRIAL GAS TURBINE ENGINE WITH CO-ROTATING GENERATOR FOR HIGH SPEED USE
App. No. 13/759,808
→
Turbine rotor blade with tip cooling
App. No. 13/687,009
→
SEQUENTIAL COOLING INSERT FOR TURBINE STATOR VANE
App. No. 13/685,053
→
TURBINE BLADE WITH MICRO SIZED NEAR WALL COOLING CHANNELS
App. No. 13/681,848
→
IR DETECTION OF SMALL CRACKS DURING FATIGUE TESTING
App. No. 13/664,489
→
Method for testing variable cooling geometries in a turbine vane
App. No. 13/652,509
→
ADVANCED HOT SECTION MATERIALS AND COATINGS TEST RIG
App. No. 13/646,674
→
INDUSTRIAL STATOR VANE WITH SEQUENTIAL IMPINGEMENT COOLING INSERTS
App. No. 13/623,291
→
Thin walled turbine blade and process for making the blade
App. No. 13/622,551
→
SPRING LOADED COMPLIANT SEAL FOR HIGH TEMPERATURE USE
App. No. 13/585,891
→
EXTENDABLE NOZZLE FOR ROCKET ENGINE
App. No. 13/572,809
→
TURBINE BLADE WITH NEAR WALL COOLING CHANNELS
App. No. 13/539,714
→
TURBINE BLADE WITH COUNTER FLOWING NEAR WALL COOLING CHANNELS
App. No. 13/539,720
→
MULTIPLE STAGED COMPRESSOR WITH LAST STAGE AIRFOIL COOLING
App. No. 13/526,601
→
SMALL GAS TURBINE ENGINE WITH MULTIPLE BURN ZONES
App. No. 13/481,089
→
PROCESS FOR RE-DESIGNING A DISTRESSED COMPONENT USED UNDER THERMAL AND STRUCTURAL LOADING
App. No. 13/478,005
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TURBINE BLADE TIP PORTION WITH TRENCHED COOLING HOLES
App. No. 13/459,130
→