Patent Assignment
Reel/Frame 075029/0769
RELEASE OF PATENT SECURITY INTEREST RECORDED AT R/F 59664/0917
Recorded: 2026-03-04
Received: 2026-03-04
Pages: 41
Assignor
TRUIST BANK
Executed: 2026-02-20
Assignees
FLORIDA TURBINE TECHNOLOGIES, INC.
10680 TREENA STREET, SUITE 600, SAN DIEGO, CA, 92131, UNITED STATES
GICHNER SYSTEMS GROUP, INC.
10680 TREENA STREET, SUITE 600, SAN DIEGO, CA, 92131, UNITED STATES
KRATOS ANTENNA SOLUTIONS CORPORATION
10680 TREENA STREET, SUITE 600, SAN DIEGO, CA, 92131, UNITED STATES
KRATOS INTEGRAL HOLDINGS, LLC
10680 TREENA STREET, SUITE 600, SAN DIEGO, CA, 92131, UNITED STATES
KRATOS TECHNOLOGY & TRAINING SOLUTIONS, INC.
10680 TREENA STREET, SUITE 600, SAN DIEGO, CA, 92131, UNITED STATES
KRATOS UNMANNED AERIAL SYSTEMS, INC.
10680 TREENA STREET, SUITE 600, SAN DIEGO, CA, 92131, UNITED STATES
MICRO SYSTEMS, INC.
10680 TREENA STREET, SUITE 600, SAN DIEGO, CA, 92131, UNITED STATES
Covered Applications
(100)
SYSTEMS AND METHODS FOR PROCESSING VARIABLE CODING AND MODULATION (VCM) BASED COMMUNICATION SIGNALS USING FEEDFORWARD CARRIER AND TIMING RECOVERY
App. No. 17/580,074
→
PROGRAMMATICALLY DETERMINING NEXT-HOP MAC ADDRESS
App. No. 17/521,688
→
SOFTWARE-BASED ORCHESTRATION OF COMMUNICATION PAYLOADS IN SATELLITES
App. No. 17/347,068
→
SYSTEMS AND METHODS FOR CHANNEL SIMULATION OF SIGNALS REPRESENTATIVE OF A COMMUNICATION SIGNAL
App. No. 17/332,675
→
SYSTEMS AND METHODS FOR SIGNAL MODULATION OF A PLURALITY OF DOWNLINK SIGNAL REPRESENTATIVE OF A COMMUNICATION SIGNAL
App. No. 17/332,285
→
SYSTEMS AND METHODS FOR POST-DETECT COMBINING OF A PLURALITY OF DOWNLINK SIGNALS REPRESENTATIVE OF A COMMUNICATION SIGNAL
App. No. 17/332,349
→
SYSTEM AND METHOD FOR PROCESSING SIGNALS USING FEED FORWARD CARRIER AND TIMING RECOVERY
App. No. 17/031,507
→
APPARATUS AND PROCESS OF FORMING AN INTEGRALLY BLADED ROTOR WITH COOLED SINGLE CRYSTAL BLADES AND AN EQUIAX NICKEL DISK
App. No. 16/781,191
→
High Speed Shaft Flexible Coupling
App. No. 16/566,434
→
APPARATUS AND PROCESS FOR TESTING A LARGE COMBUSTOR USING A CAES FACILITY
App. No. 16/491,850
→
TURBOCHARGED GAS TURBINE ENGINE WITH ELECTRIC POWER GENERATION FOR SMALL AIRCRAFT ELECTRIC PROPULSION
App. No. 16/484,645
→
Axial Thrust Foil Air Bearing with Thrust Sensor
App. No. 16/446,948
→
Ceramic Radial Turbine
App. No. 16/446,970
→
Self-Metering Hydrostatic Thrust Bearing
App. No. 16/375,999
→
INSULIN ANALOGS WITH REDUCED AFFINITY TO INSULIN RECEPTOR AND USE THEREOF
App. No. 16/335,490
→
Gas Turbine Engine Bearing with Fuel Lubrication and Cooling
App. No. 16/288,704
→
SYSTEM AND METHOD FOR PROCESSING SIGNALS USING FEED FORWARD CARRIER AND TIMING RECOVERY
App. No. 16/230,993
→
PROCESS FOR RETROFITTING AN INDUSTRIAL GAS TURBINE ENGINE FOR INCREASED POWER AND EFFICIENCY
App. No. 16/301,560
→
SYSTEM AND METHOD FOR OPTIMIZING SATELLITE GATEWAY DIVERSITY
App. No. 16/164,618
→
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
→
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
→
ADVANCED LEAN BURN INJECTOR IGNITER SYSTEM
App. No. 15/704,683
→
High Temperature High Pressure Non-Vitiated Heater
App. No. 15/685,470
→
SYSTEM AND METHOD FOR INTERFERENCE REDUCTION IN RADIO COMMUNICATIONS
App. No. 15/670,996
→
APPARATUS AND PROCESS OF RETROFITTING A COMBINED CYCLE POWER PLANT
App. No. 15/549,050
→
SYSTEMS AND METHODS FOR SIGNAL CANCELLATION IN SATELLITE COMMUNICATION
App. No. 15/649,408
→
Gas Turbine Engine with Multiple Electric Generators
App. No. 15/616,590
→
GAS TURBINE ENGINE WITH AXIAL THRUST BALANCE
App. No. 15/603,911
→
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
→
TURBOCHARGER WITH AIR JOURNAL BEARING AND THRUST BEARING
App. No. 15/429,212
→
Process for repairing a worn carburized steel surface of a sprag clutch
App. No. 15/339,472
→
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
→
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
→
AUTONOMOUS VEHICLE APPLIQUE
App. No. 15/066,943
→
Apparatus and process for determining a convective heat transfer coefficient between a moving fluid and a bounding surface
App. No. 15/053,008
→
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
→
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
→
SYSTEM AND METHOD FOR INCREASING SPOT BEAM SATELLITE BANDWIDTH
App. No. 14/602,073
→
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
→
PACKETIZED RADIO FREQUENCY TRANSPORT SYSTEM
App. No. 14/509,710
→
Small turbine stator vane with impingement cooling insert
App. No. 14/291,510
→
ECCENTRICITY CONTROL FOR GEOSYNCHRONOUS SATELLITES
App. No. 14/282,717
→
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
→
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
→
ENVELOPE FEEDBACK INTERFERENCE REDUCTION AND DATA THROUGHPUT MAXIMIZATION
App. No. 13/843,393
→
Split ring floating air riding seal for a turbine
App. No. 13/793,853
→
SEQUENTIAL COOLING INSERT FOR TURBINE STATOR VANE
App. No. 13/685,053
→
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
→
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
→
PROCESS FOR RE-DESIGNING A DISTRESSED COMPONENT USED UNDER THERMAL AND STRUCTURAL LOADING
App. No. 13/478,005
→
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 airfoil with pressure side trailing edge cooling slots
App. No. 13/427,250
→
Turbine vane with dirt separator
App. No. 13/415,022
→
Method of Manufacturing a Shrouded Centrifugal Impeller for High Speed Use
App. No. 13/412,989
→