Patent Assignment
Reel/Frame 048521/0081
SUPPLEMENT NO. 1 TO AMENDED AND RESTATED INTELLECTUAL PROPERTY SECURITY AGREEMENT
Recorded: 2019-03-06
Received: 2019-03-06
Pages: 35
Assignors
CONSOLIDATED TURBINE SPECIALISTS LLC
Executed: 2019-03-01
ELWOOD INVESTMENTS LLC
Executed: 2019-03-01
FLORIDA TURBINE TECHNOLOGIES INC.
Executed: 2019-03-01
FTT AMERICA, LLC
Executed: 2019-03-01
KTT CORE, INC.
Executed: 2019-03-01
S&J DESIGN LLC
Executed: 2019-03-01
TURBINE EXPORT, INC.
Executed: 2019-03-01
Assignee
SUNTRUST BANK
303 PEACHTREE STREET NE, 25TH FLOOR, ATLANTA, GA, 30308, UNITED STATES
Covered Applications
(100)
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
→
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
→
Turbine rotor cooling air static collector
App. No. 15/131,110
→
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
→
Circulating fluidized bed cooling for an industrial gas turbine engine
App. No. 13/835,692
→
Split ring floating air riding seal for a turbine
App. No. 13/793,853
→
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
→
TURBINE BLADE TIP PORTION WITH TRENCHED COOLING HOLES
App. No. 13/459,130
→
Turbine blade with radial cooling passage having continuous discrete turbulence air mixers
App. No. 13/458,342
→
Turbine vane with endwall cooling
App. No. 13/445,078
→
Turbine stator vane with near wall integrated micro cooling channels
App. No. 13/427,277
→