Patent Assignment
Reel/Frame 052472/0871
CHANGE OF NAME
Recorded: 2020-04-22
Received: 2020-04-22
Pages: 8
Assignor
UNITED TECHNOLOGIES CORPORATION
Executed: 2020-04-03
Assignee
RAYTHEON TECHNOLOGIES CORPORATION
10 FARM SPRINGS ROAD, FARMINGTON, CT, 06032, UNITED STATES
Covered Applications
(100)
FLUIDIC MACHINING METHOD AND SYSTEM
App. No. 16/100,257
→
GAS TURBINE ENGINE FRONT ARCHITECTURE
App. No. 15/943,100
→
SHOT TUBE FOR DIE-CAST MACHINE
App. No. 15/851,765
→
SEAL ANTI-ROTATION
App. No. 15/841,792
→
TURBINE VANE CLUSTER INCLUDING ENHANCED PLATFORM COOLING
App. No. 15/790,423
→
GAS TURBINE ENGINE AIRFOIL
App. No. 15/727,683
→
GASPATH COMPONENT INCLUDING MINICORE PLENUMS
App. No. 15/629,812
→
AIRFOIL FOR GAS TURBINE ENGINE
App. No. 15/584,846
→
Geared Architecture for High Speed and Small Volume Fan Drive Turbine
App. No. 15/485,512
→
PARTIALLY ADDITIVELY MANUFACTURED HEAT EXCHANGER
App. No. 15/483,379
→
ALUMINUM-CHROMIUM DIFFUSION COATING
App. No. 15/470,949
→
GAS TURBINE ENGINE AIRFOIL COOLING CIRCUIT ARRANGEMENT
App. No. 15/450,087
→
METHOD INCLUDING FIBER REINFORCED CASTING ARTICLE
App. No. 15/448,267
→
CERAMIC MATRIX COMPOSITE TURBINE EXHAUST ASSEMBLY FOR A GAS TURBINE ENGINE
App. No. 15/424,930
→
Classification of Gas Turbine Engine Components and Decision for Use
App. No. 15/412,293
→
Advanced Geared Gas Turbine Engine
App. No. 15/412,102
→
GAS TURBINE ENGINE WITH INTERCOOLED COOLING AIR AND DUAL TOWERSHAFT ACCESSORY GEARBOX
App. No. 15/410,113
→
CONCENTRIC SHAFTS DRIVING ADJACENT FANS FOR AIRCRAFT PROPULSION
App. No. 15/373,101
→
Heat Exchanger Mounted at Rear of Gas Turbine Engine for Challenging Temperature Applications
App. No. 15/369,189
→
ADDITIVELY MANUFACTURED COMPONENT FOR A GAS POWERED TURBINE
App. No. 15/335,761
→
GAS TURBINE ENGINE WITH HEAT EXCHANGER DIAGNOSTICS
App. No. 15/271,274
→
GAS TURBINE ENGINE AIRFOIL WITH SHOWERHEAD COOLING HOLES NEAR LEADING EDGE
App. No. 15/266,855
→
REAL TIME AERODAMPING MEASUREMENT OF TURBOMACHINE
App. No. 15/256,411
→
Heat Exchanger for Gas Turbine Engine Mounted in Intermediate Case
App. No. 15/244,025
→
GAS TURBINE ENGINE AIRFOIL
App. No. 15/116,000
→
THRUST REVERSER STRUCTURE MOUNTED TO FAN CASE
App. No. 15/218,138
→
SILICON OXYCARBIDE-BASED ENVIRONMENTAL BARRIER COATING
App. No. 15/110,819
→
TRAILING EDGE COOLING PEDESTAL CONFIGURATION FOR A GAS TURBINE ENGINE AIRFOIL
App. No. 15/110,904
→
GAS TURBINE ENGINE INNER CASE WITH NON-INTEGRAL VANES
App. No. 15/110,856
→
GAS TURBINE ENGINE STATOR VANE MISTUNING
App. No. 15/110,889
→
VAPOR DEPOSITION APPARATUS AND METHOD
App. No. 15/202,984
→
POWER SYSTEM FOR AIRCRAFT PARALLEL HYBRID GAS TURBINE ELECTRIC PROPULSION SYSTEM
App. No. 15/200,240
→
AIRCRAFT INCLUDING PARALLEL HYBRID GAS TURBINE ELECTRIC PROPULSION SYSTEM
App. No. 15/200,192
→
CERAMIC COVERED TURBINE COMPONENTS
App. No. 15/108,613
→
ISOTHERMALIZED COOLING OF GAS TURBINE ENGINE COMPONENTS
App. No. 15/182,755
→
ROTOR BLADE PLATFORM COOLING PASSAGE
App. No. 15/100,413
→
FAN BLADE WITH ADHESIVE FABRIC STACKUP
App. No. 15/039,929
→
GAS TURBINE ENGINE COMPONENT MATEFACE SURFACES
App. No. 15/039,945
→
DIE CASTING MACHINE SHOT SLEEVE
App. No. 15/038,853
→
CASTING SYSTEM FOR INVESTMENT CASTING PROCESS
App. No. 15/159,296
→
SHAPED COOLING PASSAGES FOR TURBINE BLADE OUTER AIR SEAL
App. No. 15/157,857
→
ARTICLE HAVING VARIABLE COATING
App. No. 15/036,109
→
REFRACTORY METAL CORE FINISHING TECHNIQUE
App. No. 15/034,612
→
METHOD OF MANUFACTURING FIBER REINFORCED BARRIER COATING
App. No. 15/033,153
→
Simple Heat Exchanger Using Super Alloy Materials for Challenging Applications
App. No. 15/138,491
→
SEAL ARC SEGMENT WITH SLOPED CIRCUMFERENTIAL SIDES
App. No. 15/137,044
→
CASTING CORE AND METHOD FOR TESTING A HOLLOW METAL ARTICLE
App. No. 15/137,183
→
SPLIT-ZONE FLOW METERING T-TUBE
App. No. 15/134,653
→
METHOD AND ASSEMBLY FOR INSPECTING ENGINE COMPONENT
App. No. 15/030,236
→
INTEGRATED GAS TURBINE ENGINE SUPPORT AND SENSOR
App. No. 15/030,128
→
METHOD OF DETECTING CONVERSION QUALITY OF GREEN MATRIX COMPOSITE MATERIAL AND SYSTEM FOR SAME
App. No. 15/027,827
→
IN-SITU DESIZING FOR LIQUID INFUSION PROCESSES
App. No. 15/027,800
→
VARIABLE AREA VANE ENDWALL TREATMENTS
App. No. 15/027,526
→
Endwall Countouring Trench
App. No. 15/027,562
→
ELECTROMAGNETIC ANTI-WINDMILLING SYSTEM
App. No. 15/089,891
→
VANE SEAL SYSTEM AND SEAL THEREFOR
App. No. 15/026,709
→
CMC BLADE WITH MONOLITHIC CERAMIC PLATFORM AND DOVETAIL
App. No. 15/025,949
→
PROCESSING METHOD FOR PIP DERIVED CMC ARTICLE
App. No. 15/026,094
→
ROTATING COMPONENT BALANCE RING
App. No. 15/023,831
→
LINK SETTING ASSEMBLY AND METHOD
App. No. 15/075,386
→
METHOD OF FABRICATING A CERAMIC ARTICLE
App. No. 15/022,680
→
CMC AIRFOIL WITH SHARP TRAILING EDGE AND METHOD OF MAKING SAME
App. No. 15/022,631
→
METHOD OF PRODUCING A CERAMIC ARTICLE, INTERMEDIATE ARTICLE AND COMPOSITION THEREFOR
App. No. 15/022,588
→
GAS TURBINE ENGINE AIRFOIL HAVING SERPENTINE FED PLATFORM COOLING PASSAGE
App. No. 15/022,622
→
GAS TURBINE ENGINE AIRFOIL COMPONENT PLATFORM SEAL COOLING
App. No. 15/022,025
→
INTERCOOLED COOLING AIR USING EXISTING HEAT EXCHANGER
App. No. 15/069,197
→
FEATURE TO PROVIDE COOLING FLOW TO DISK
App. No. 15/021,060
→
COOLING CONFIGURATION FOR ENGINE COMPONENT
App. No. 14/917,855
→
Translating Compressor and Turbine Rotors for Clearance Control
App. No. 14/917,293
→
Turbine Vane With Platform Rib
App. No. 14/917,124
→
GAS TURBINE ENGINE AIRFOIL TURBULATOR FOR AIRFOIL CREEP RESISTANCE
App. No. 14/915,455
→
DIE CASTING SYSTEM AND METHOD
App. No. 15/050,532
→
COMPRESSOR AREA SPLITS FOR GEARED TURBOFAN
App. No. 14/912,187
→
PROTECTIVE PANEL AND FRAME THEREFOR
App. No. 14/912,132
→
THROAT AREA CALCULATION FOR A SECTION OF A GAS TURBINE ENGINE
App. No. 15/013,308
→
VARIABLE PITCH FAN BLADE ARRANGEMENT FOR GAS TURBINE ENGINE
App. No. 15/009,868
→
GAS TURBINE ENGINE NON-ROTATING STRUCTURE WEDGE SEAL
App. No. 14/908,225
→
TURBOFAN ENGINE FRONT SECTION
App. No. 15/007,263
→
BLADE OUTER AIR SEAL HAVING SURFACE LAYER WITH POCKETS
App. No. 15/005,318
→
HEAT FLUX MEASUREMENT SYSTEM
App. No. 15/002,724
→
GAS TURBINE ENGINE WITH FAN CLEARANCE CONTROL
App. No. 14/906,019
→
GAS TURBINE ENGINE CERAMIC COMPONENT ASSEMBLY ATTACHMENT
App. No. 14/904,560
→
COOLED COMPRESSOR
App. No. 14/902,373
→
GAS TURBINE ENGINE WITH ROTATING INLET
App. No. 14/974,195
→
GAS TURBINE ENGINE WITH ONE PIECE ACOUSTIC TREATMENT
App. No. 14/974,220
→
GAS TURBINE ENGINE WITH SHORT INLET AND MISTUNED FAN BLADES
App. No. 14/974,151
→
EXPORT DECOMPOSITION FILTER FOR A MULTI-USER CAX ENVIRONMENT
App. No. 14/972,141
→
ANTI-ICING CORE INLET STATOR ASSEMBLY FOR A GAS TURBINE ENGINE
App. No. 14/959,542
→
COOLING PASSAGES FOR GAS TURBINE ENGINE COMPONENT
App. No. 14/949,047
→
GAS TURBINE ENGINE NACELLE ANTI-ICING SYSTEM
App. No. 14/947,174
→
DIE CASTING OF COMPONENT HAVING INTEGRAL SEAL
App. No. 14/937,988
→
Turbine Vane With Platform Pad
App. No. 14/787,332
→
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BETWEEN INLET AND FAN SIZE
App. No. 14/882,760
→
FIXED-VARIABLE VANE WITH POTTING IN GAP
App. No. 14/880,519
→
GAS TURBINE ENGINE COMPONENT
App. No. 14/878,555
→
GAS TURBINE ENGINE AIRFOIL MISTUNING
App. No. 14/855,956
→
LINK FOR AIRCRAFT COMPONENT MOUNTING
App. No. 14/842,907
→
GAS TURBINE ENGINE AIRFOIL GEOMETRIES AND CORES FOR MANUFACTURING PROCESS
App. No. 14/841,324
→
GAS TURBINE ENGINE TURBINE VANE RAIL SEAL
App. No. 14/770,112
→
TITANIUM ALUMINIDE TURBINE EXHAUST STRUCTURE
App. No. 14/769,801
→