Patent Assignment
Reel/Frame 064714/0001
CHANGE OF NAME
Recorded: 2023-07-27
Received: 2023-07-27
Pages: 623
Assignor
RAYTHEON TECHNOLOGIES CORPORATION
Executed: 2023-07-14
Assignee
RTX CORPORATION
10 FARM SPRINGS ROAD, FARMINGTON, CT, 06032, UNITED STATES
Covered Applications
(100)
LIGHTWEIGHT JOURNAL SUPPORT PIN
App. No. 18/074,560
→
ANTI-VORTEX TUBE RETAINING RING AND BORE BASKET
App. No. 17/886,190
→
LIQUID ENHANCED LASER STRIPPING
App. No. 17/881,224
→
BLEED HOLE FLOW DISCOURAGER
App. No. 17/876,034
→
GAS TURBINE ENGINE COMPONENT
App. No. 17/866,855
→
RATING CONTROL ARCHITECTURE AND METHOD FOR HYBRID ELECTRIC ENGINE
App. No. 17/847,804
→
COMBUSTOR PANELS FOR GAS TURBINE ENGINES
App. No. 17/843,833
→
ADDITIVE MANUFACTURED DUCTED HEAT EXCHANGER SYSTEM
App. No. 17/843,182
→
COOLING SCHEMES FOR AIRFOILS FOR GAS TURBINE ENGINES
App. No. 17/841,839
→
SYSTEM AND PROCESS FOR DESIGNING INTERNAL COMPONENTS FOR A GAS TURBINE ENGINE
App. No. 17/832,898
→
AIRFOIL ASSEMBLY WITH COMPOSITE RINGS AND SEALING SHELF
App. No. 17/832,256
→
FACE SEAL ARRANGEMENT FOR REDUCED FORCE AND PRESSURE
App. No. 17/747,158
→
FAN BLADE REPAIR SYSTEMS AND METHODS
App. No. 17/747,312
→
GAS TURBINE ENGINE ARTICLE WITH BRANCHED FLANGE
App. No. 17/743,521
→
BOOST SPOOL FLOW CONTROL AND GENERATOR LOAD MATCHING VIA LOAD COMPRESSOR
App. No. 17/662,202
→
FLUIDIC VALVE CONFIGURATION FOR BOOST SPOOL ENGINE
App. No. 17/662,199
→
GEARED TURBOFAN ENGINE WITH TARGETED MODULAR EFFICIENCY
App. No. 17/737,179
→
TRANSMISSION AND METHOD FOR CONTROL OF BOOST SPOOL
App. No. 17/662,193
→
SYSTEM FOR AN IMPROVED STATOR ASSEMBLY
App. No. 17/735,327
→
ROTOR STACK BUSHING WITH ADAPTIVE TEMPERATURE METERING FOR A GAS TURBINE ENGINE
App. No. 17/734,644
→
GAS TURBINE ENGINE WITH POWER DENSITY RANGE
App. No. 17/730,782
→
TURBINE ENGINE BLEED WASTE HEAT RECOVERY
App. No. 17/724,904
→
EPICYCLIC GEAR TRAIN
App. No. 17/711,177
→
CMC VANE MATE FACE FLANGES WITH THROUGH-PLY SEAL SLOTS
App. No. 17/709,523
→
TRIANGULAR-FRAME CONNECTION BETWEEN FAN CASE AND CORE HOUSING IN A GAS TURBINE ENGINE
App. No. 17/701,010
→
RADIAL STRUT FRAME CONNECTION BETWEEN FAN CASE AND CORE HOUSING IN A GAS TURBINE ENGINE
App. No. 17/701,026
→
H-FRAME CONNECTION BETWEEN FAN CASE AND CORE HOUSING IN A GAS TURBINE ENGINE
App. No. 17/700,992
→
NICKEL ALLOY COMPOSITION WITH BORON AND NITROGEN
App. No. 17/694,780
→
GAS TURBINE ENGINE FORWARD BEARING COMPARTMENT ARCHITECTURE
App. No. 17/688,957
→
SYSTEMS AND METHODS FOR CONTROLLING BLADE TIP CLEARANCES
App. No. 17/688,094
→
ADAPTIVE BLEED SCHEDULE IN A GAS TURBINE ENGINE
App. No. 17/682,313
→
METHOD FOR REMOVING REFRACTORY METAL CORES
App. No. 17/676,430
→
CONTROLLING LUBRICANT FLOW IN EPICYCLIC GEARBOX
App. No. 17/676,520
→
CRYOGENICALLY ASSISTED EXHAUST CONDENSATION
App. No. 17/669,680
→
REDUCING CONTRAILS FROM AN AIRCRAFT POWERPLANT
App. No. 17/670,090
→
LINE-OF-SIGHT COATING FIXTURE AND APPARATUS
App. No. 17/668,591
→
TURBOEXPANDER INTER-STAGE HEATING AND NH3 CRACKING
App. No. 17/665,063
→
ENGINE ARTICLE WITH INTEGRAL LINER AND NOZZLE
App. No. 17/591,054
→
OFF-SET DUCT HEAT EXCHANGER
App. No. 17/588,541
→
TANGENTIALLY BOWED AIRFOIL
App. No. 17/585,760
→
HYDROGEN POWERED GEARED TURBO FAN ENGINE WITH AN OFF-SET REDUCED CORE
App. No. 17/581,375
→
GEAR TRAIN WITH VARIABLE INPUT DIRECTION OF ROTATION AND CONSTANT OUTPUT DIRECTION OF ROTATION
App. No. 17/578,818
→
RADIO FREQUENCY WAVEGUIDE SYSTEM FOR MIXED TEMPERATURE ENVIRONMENTS
App. No. 17/578,751
→
FEATHER SEAL FOR CMC BOAS
App. No. 17/573,921
→
SUPERCRITICAL FLUID SYSTEMS
App. No. 17/559,281
→
RESTRAINING PLUG
App. No. 17/557,844
→
GEARED TURBINE ENGINE WITH RELATIVELY LIGHTWEIGHT PROPULSOR MODULE
App. No. 17/555,606
→
SPALL PLATE FOR CONSUMABLE COMBUSTOR SUPPORT STRUCTURES
App. No. 17/550,703
→
Pressure-Balanced Carbon Seal
App. No. 17/541,712
→
MACHINING OF CERAMIC MATRIX COMPOSITE DURING PREFORMING AND PARTIAL DENSIFICATION
App. No. 17/541,826
→
RING GEAR MOUNTING ARRANGEMENT WITH OIL SCAVENGE SCHEME
App. No. 17/540,400
→
GEARED GAS TURBINE ENGINE ARRANGEMENT WITH CORE SPLIT POWER RATIO
App. No. 17/538,048
→
REMOVING DEBRIS FROM AN ENGINE COMPONENT
App. No. 17/535,101
→
THRUST EFFICIENT GAS TURBINE ENGINE
App. No. 17/533,607
→
METHOD OF ASSEMBLY FOR GEAR SYSTEM WITH ROTATING CARRIER
App. No. 17/532,085
→
TURBINE SECTION OF GAS TURBINE ENGINE
App. No. 17/530,544
→
AIRFOIL WITH BODY AND COVER PANEL
App. No. 17/529,392
→
GAS TURBINE ENGINE WITH NON-EPICYCLIC GEAR REDUCTION SYSTEM
App. No. 17/527,549
→
AIRFOIL WITH SERPENTINE FIBER PLY LAYUP
App. No. 17/524,809
→
AIRFOIL WITH FIBER PLIES HAVING INTERDIGITATED FINGERS IN TRAILING END
App. No. 17/525,005
→
MACHINABLE COATINGS FABRICATED BY SLURRY METHODS FOR USE ON CERAMIC MATRIX COMPOSITES
App. No. 17/517,984
→
SEAL ASSEMBLY WITH SECONDARY RETENTION FEATURE
App. No. 17/513,995
→
FRONT SECTION STIFFNESS RATIO
App. No. 17/512,824
→
LOW DENSITY HYBRID KNIFE SEAL
App. No. 17/509,418
→
VANE ARC SEGMENT WITH CURVED RADIAL FLANGE
App. No. 17/504,627
→
LOW NOISE TURBINE FOR GEARED GAS TURBINE ENGINE
App. No. 17/503,814
→
HYBRID GAS TURBINE ENGINE SYSTEM POWERED WARM-UP
App. No. 17/501,051
→
RADIO FREQUENCY WAVEGUIDE SYSTEM NODES
App. No. 17/497,616
→
AUXILIARY COMPONENT MOUNTING SYSTEM FOR GAS TURBINE ENGINES
App. No. 17/492,417
→
FAN DRIVE GEAR SYSTEM
App. No. 17/484,331
→
AIRFOIL TIP POCKET WITH AUGMENTATION FEATURES
App. No. 17/482,478
→
FLEXIBLE COUPLING FOR GEARED TURBINE ENGINE
App. No. 17/480,503
→
VANE ARC SEGMENT FORMED OF FIBER-REINFORCED COMPOSITE
App. No. 17/480,511
→
BAFFLE WITH TWO DATUM FEATURES
App. No. 17/480,325
→
SMOOTHING ROUND INTERNAL PASSAGES OF ADDITIVELY MANUFACTURED PARTS USING METALLIC SPHERES
App. No. 17/477,873
→
SEAL ASSEMBLY WITH REDUCED PRESSURE LOAD ARRANGEMENT
App. No. 17/476,566
→
TANDEM BLADE ROTOR DISK
App. No. 17/472,236
→
COMPOSITE FAN BLADE
App. No. 17/470,638
→
GAS TURBINE ENGINE BUFFER SYSTEM
App. No. 17/469,025
→
INTEGRATED ELECTRO-AERO-THERMAL TURBINE ENGINE
App. No. 17/465,251
→
MONOLITHIC COMBUSTOR FOR ATTRITIABLE ENGINE APPLICATIONS
App. No. 17/465,244
→
PREFERENTIAL FLOW DISTRIBUTION FOR GAS TURBINE ENGINE COMPONENT
App. No. 17/460,520
→
ELECTRO-PNEUMATIC ENVIRONMENTAL CONTROL SYSTEM AIR CIRCUIT
App. No. 17/411,529
→
FRAME CONNECTION BETWEEN FAN CASE AND CORE HOUSING IN A GAS TURBINE ENGINE
App. No. 17/407,275
→
HYDRAULIC STARTER ASSEMBLY FOR A GAS TURBINE ENGINE
App. No. 17/406,652
→
ENERGY BEAM POSITIONING DURING FORMATION OF A COOLING APERTURE
App. No. 17/401,931
→
FORMING LINED COOLING APERTURE(S) IN A TURBINE ENGINE COMPONENT
App. No. 17/401,906
→
FORMING COOLING APERTURE(S) USING ELECTRICAL DISCHARGE MACHINING
App. No. 17/401,974
→
GEARED GAS TURBINE ENGINE WITH REDUCED FAN NOISE
App. No. 17/399,309
→
MULTI-ENVIRONMENTAL BARRIER COATING, PROCESSES FOR COATING ARTICLES, AND THEIR COATED ARTICLES
App. No. 17/395,992
→
GAS TURBINE ENGINE WITH BLADE CHANNEL VARIATIONS
App. No. 17/396,029
→
MORPHING STRUCTURES FOR FAN INLET VARIABLE VANES
App. No. 17/396,050
→
Turbine Blade Trailing Edge Cooling Feed
App. No. 17/429,097
→
ARTIFICIAL ICE FOR AN AIRCRAFT COMPONENT
App. No. 17/396,076
→
HOURGLASS AIRFOIL COOLING CONFIGURATION
App. No. 17/392,573
→
GEARED TURBOFAN ARRANGEMENT WITH CORE SPLIT POWER RATIO
App. No. 17/383,512
→
AIRFOIL ASSEMBLY WITH FIBER-REINFORCED COMPOSITE RINGS AND TOOTHED EXIT SLOT
App. No. 17/377,618
→
CERAMIC COMPONENT HAVING SILICON LAYER AND BARRIER LAYER
App. No. 17/378,005
→
SEAL SYSTEM HAVING SILICON LAYER AND BARRIER LAYER
App. No. 17/377,591
→
ENGINE BLEED AIR DUCTING INTO HEAT EXCHANGER
App. No. 17/377,951
→