IP Library Assignment 054062/0001
Patent Assignment
Reel/Frame 054062/0001

CHANGE OF NAME

Recorded: 2020-09-04 Received: 2020-09-04 Pages: 219
Assignor
UNITED TECHNOLOGIES CORPORATION
Executed: 2020-04-03
Assignee
RAYTHEON TECHNOLOGIES CORPORATION
870 WINTER STREET MA, WALTHAM, MA, 02451-1449, UNITED STATES
Covered Applications (100)
SYSTEM AND METHOD FOR MITIGATING LOADS ACTING ON A ROTOR BLADE OF A WIND TURBINE
App. No. 17/071,126
LASER-PROCESSING APPARATUS, METHODS OF OPERATING THE SAME, AND METHODS OF PROCESSING WORKPIECES USING THE SAME
App. No. 17/047,254
ABRASIVE FLOW MACHINING METHOD AND ARTICLE
App. No. 16/842,050
FIXTURE FOR VAPOR DEPOSITION SYSTEM
App. No. 16/836,337
ADDITIVE MANUFACTURED DUCTED HEAT EXCHANGER SYSTEM
App. No. 16/830,470
FILM-COOLED MULTI-WALLED STRUCTURE WITH ONE OR MORE INDENTATIONS
App. No. 16/827,195
BONDED COMBUSTOR WALL FOR A TURBINE ENGINE
App. No. 16/827,200
TANDEM ROTOR BLADES
App. No. 16/827,135
GEARED TURBOFAN WITH OVERSPEED PROTECTION
App. No. 16/825,370
CUTTING BLADE TIPS
App. No. 16/825,610
LINKAGE ASSEMBLY PREVENTING AXIAL ROTATION OF THE LINK ROD FOR A GAS TURBINE ENGINE
App. No. 16/823,643
RADIAL FUEL SHIFTING AND BIASING IN AN AXIAL STAGED COMBUSTOR FOR A GAS TURBINE ENGINE
App. No. 16/822,926
AIRFOIL WITH PANEL AND SIDE EDGE COOLING
App. No. 16/821,169
GAS TURBINE ENGINE WITH INTERCOOLED COOLING AIR AND TURBINE DRIVE
App. No. 16/821,383
METHOD FOR HEAT TREATING COMPONENTS
App. No. 16/818,127
STRUCTURED MATERIAL ALLOY COMPONENT FABRICATION
App. No. 16/815,502
GAS TURBINE ENGINE DRIVE SYSTEM HEALTH MONITOR
App. No. 16/812,644
PRE-START MOTORING SYNCHRONIZATION FOR MULTIPLE ENGINES
App. No. 16/812,862
GEARED TURBOMACHINE FAN AND COMPRESSOR ROTATION
App. No. 16/812,636
GAS TURBINE ENGINE AND METHOD TO COOL A GAS TURBINE ENGINE CASE ASSEMBLY
App. No. 16/812,807
CALCIUM-MAGNESIUM-ALUMINO-SILICATE RESISTANT THERMAL BARRIER COATINGS
App. No. 16/812,946
COMPRESSOR ROTOR STACK ASSEMBLY FOR GAS TURBINE ENGINE
App. No. 16/811,666
REFRACTORY METAL CORE FINISHING TECHNIQUE
App. No. 16/808,529
THRUST EFFICIENT TURBOFAN ENGINE
App. No. 16/809,092
PILOTED RETAINING PLATE FOR A FACE SEAL ARRANGEMENT
App. No. 16/806,052
STATOR OUTER PLATFORM SEALING AND RETAINER
App. No. 16/805,309
INDUCING AND MONITORING A VIBRATORY RESPONSE IN A COMPONENT
App. No. 16/799,281
DUAL COOLING AIRFLOW TO BLADES
App. No. 16/794,900
INTERNAL COOLING CAVITY WITH TRIP STRIPS
App. No. 16/793,575
HIGH TEMPERATURE IMAGING MEDIA FOR DIGITAL IMAGE CORRELATION
App. No. 16/793,675
NANOCELLULAR FOAM DAMPER
App. No. 16/792,511
MULTIPLE INJECTOR HOLES FOR GAS TURBINE ENGINE VANE
App. No. 16/790,890
ADDITIVE MANUFACTURING SYSTEM WITH ULTRASONIC INSPECTION AND METHOD OF OPERATION
App. No. 16/791,385
METHOD FOR FABRICATING A CERAMIC MATERIAL
App. No. 16/791,119
GAS TURBINE ENGINE AIRFOIL
App. No. 16/787,731
AIRFOIL INCLUDING ADHESIVELY BONDED SHROUD
App. No. 16/787,710
AEROMECHANICAL IDENTIFICATION SYSTEMS AND METHODS
App. No. 16/787,611
TURBOFAN ENGINE BEARING AND GEARBOX ARRANGEMENT
App. No. 16/786,421
SYSTEMS AND METHODS FOR OPTIMAL SOURCE MATERIAL DEPOSITION ALONG HOLE EDGES
App. No. 16/786,228
METHOD FOR MAGNETIC FLUX COMPENSATION IN A DIRECTIONAL SOLIDIFICATION FURNACE UTILIZING AN ACTUATED SECONDARY COIL
App. No. 16/781,403
GAS TURBINE ENGINE FORWARD BEARING COMPARTMENT ARCHITECTURE
App. No. 16/779,768
BEVELED COVERPLATE
App. No. 16/776,203
Suspension Plasma Spray Apparatus and Use Methods
App. No. 16/773,098
FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
App. No. 16/747,934
RETENTION CLIP FOR A BLADE OUTER AIR SEAL
App. No. 16/747,028
INTEGRAL CERAMIC MATRIX COMPOSITE FASTENER WITH NON-POLYMER RIGIDIZATION
App. No. 16/744,720
CHROMIUM-ENRICHED DIFFUSED ALUMINIDE COATING
App. No. 16/744,583
LASER POWDER DEPOSITION WELD REWORK FOR GAS TURBINE ENGINE NON-FUSION WELDABLE NICKEL CASTINGS
App. No. 16/743,431
APPARATUS AND METHOD FOR MASKING UNDER PLATFORM AREAS OF AIRFOIL COMPONENTS
App. No. 16/743,276
ADDITIVE MANUFACTURING SYSTEM AND METHOD OF MANUFACTURE
App. No. 16/743,528
GAS TURBINE ENGINE AIRFOIL
App. No. 16/741,918
VARIABLE VANE POSITIONING APPARATUS FOR A GAS TURBINE ENGINE
App. No. 16/742,164
GAS TURBINE ENGINE AIRFOIL
App. No. 16/740,817
MIDDLE THREADED FITTING
App. No. 16/738,873
BOOSTER COMPRESSOR WITH SPEED CHANGE SYSTEM
App. No. 16/736,322
METHOD OF INSPECTING COMPONENT SURFACE WITH MARKING MEDIA
App. No. 16/734,818
IMPINGEMENT COOLING ARRANGEMENT FOR AIRFOILS
App. No. 16/734,464
RETENTION HARDWARE
App. No. 16/734,965
ADDITIVE MANUFACTURING SYSTEM FOR MINIMIZING THERMAL STRESSES
App. No. 16/733,913
PLANETARY GEAR SYSTEM FOR TURBOMACHINE
App. No. 16/730,466
TURBINE ENGINE CASE ATTACHMENT AND A METHOD OF USING THE SAME
App. No. 16/730,497
COMBUSTOR LINER PANEL END RAIL WITH DIFFUSED INTERFACE PASSAGE FOR A GAS TURBINE ENGINE COMBUSTOR
App. No. 16/727,178
COMBUSTOR COOLING PANEL WITH FLOW GUIDE
App. No. 16/724,980
COMBUSTOR PANEL STUD COOLING EFFUSION THROUGH HEAT TRANSFER AUGMENTORS
App. No. 16/725,116
COMBUSTOR COOLING PANEL STUD
App. No. 16/725,049
GAS TURBINE ENGINE AIRFOIL
App. No. 16/722,164
ABRADABLE LAYER WITH GLASS MICROBALLOONS
App. No. 16/717,458
COMPRESSOR FLOWPATH
App. No. 16/715,528
CABLE ASSEMBLY WITH STRAIN RELIEF
App. No. 16/711,907
COOLING SYSTEMS FOR GAS TURBINE ENGINES
App. No. 16/712,458
LIGHTWEIGHT JOURNAL SUPPORT PIN
App. No. 16/705,479
METHOD OF RESONANT INSPECTION FOR ADDITIVE MANUFACTURING
App. No. 16/703,467
FILM COOLING A COMBUSTOR WALL OF A TURBINE ENGINE
App. No. 16/703,211
ADDITIVELY MANUFACTURED CORE
App. No. 16/701,614
LUBRICATION OF EPICYCLIC GEAR SYSTEM FOR GAS TURBINE ENGINE
App. No. 16/700,090
ADDITIVE MANUFACTURED CONGLOMERATED POWDER REMOVAL FROM INTERNAL PASSAGES
App. No. 16/695,877
GAS TURBINE ENGINE SYSTEM WEAR REDUCTION
App. No. 16/695,290
DEPOSITED MATERIAL STRUCTURE WITH INTEGRATED COMPONENT
App. No. 16/688,824
ADDITIVE MANUFACTURING PROCESS DISTORTION MANAGEMENT
App. No. 16/686,951
METHOD FOR PYROLYZING PRECERAMIC POLYMER MATERIAL USING ELECTROMAGNETIC RADIATION
App. No. 16/687,149
GEARED GAS TURBINE ENGINE WITH OIL DEAERATOR AND AIR REMOVAL
App. No. 16/684,926
GEARED TURBOFAN ARRANGEMENT WITH CORE SPLIT POWER RATIO
App. No. 16/684,968
METHOD OF MANUFACTURING BOAS ENHANCED HEAT TRANSFER SURFACE
App. No. 16/682,671
MULTIFUNCTIONAL NANOCELLULAR SINGLE CRYSTAL NICKEL FOR TURBINE APPLICATIONS
App. No. 16/681,043
GAS TURBINE ENGINE AIRFOIL
App. No. 16/681,187
HIGH THRUST GEARED GAS TURBINE ENGINE
App. No. 16/676,788
ENVIRONMENTAL COOLING SYSTEMS FOR AIRCRAFT
App. No. 16/675,585
INTERNALLY COOLED AIRFOIL
App. No. 16/675,879
ADDITIVE MANUFACTURING METHOD FOR THE ADDITION OF FEATURES WITHIN COOLING HOLES
App. No. 16/673,062
FAN AND LOW PRESSURE COMPRESSOR GEARED TO LOW SPEED SPOOL OF GAS TURBINE ENGINE
App. No. 16/671,432
SEAL FACE PLATE COOLING
App. No. 16/670,531
TURBINE ENGINE COMPONENT INCLUDING AN AXIALLY ALIGNED SKIN CORE PASSAGE INTERRUPTED BY A PEDESTAL
App. No. 16/669,698
GAS TURBINE ENGINE WITH DOVE-TAILED TOBI VANE
App. No. 16/668,773
FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
App. No. 16/667,154
LOW NOISE COMPRESSOR ROTOR FOR GEARED TURBOFAN ENGINE
App. No. 16/667,326
LOW NOISE COMPRESSOR AND TURBINE FOR GEARED TURBOFAN ENGINE
App. No. 16/667,334
GAS TURBINE ENGINE AIRFOIL
App. No. 16/667,321
SEALING PROCESS FOR AN ANODIZED ALUMINUM-ALLOY SURFACE
App. No. 16/666,693
TOOL FOR REMOVING COLLARS
App. No. 16/665,395
AIRFOIL WITH SEAL BETWEEN ENDWALL AND AIRFOIL SECTION
App. No. 16/665,339