Patent Assignment
Reel/Frame 055659/0001
CORRECTIVE ASSIGNMENT TO CORRECT THE AND REMOVE PATENT APPLICATION NUMBER 11886281 AND ADD PATENT APPLICATION NUMBER 14846874. TO CORRECT THE RECEIVING PARTY ADDRESS PREVIOUSLY RECORDED AT REEL: 054062 FRAME: 0001. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF ADDRESS.
Recorded: 2021-03-04
Received: 2021-03-04
Pages: 429
Assignor
UNITED TECHNOLOGIES CORPORATION
Executed: 2020-04-03
Assignee
RAYTHEON TECHNOLOGIES CORPORATION
10 FARM SPRINGS ROAD, FARMINGTON, CT, 06032-2568, UNITED STATES
Covered Applications
(100)
SYSTEM AND METHOD FOR LOCATION BASED DYNAMIC REDIRECTION OF ADVERTISER AFFILIATE LINKS FOR ONLINE ADVERTISING
App. No. 17/205,698
→
SEMICONDUCTOR MEMORY DEVICE
App. No. 16/856,679
→
SEMICONDUCTOR MEMORY DEVICE
App. No. 16/854,394
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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
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BONDED COMBUSTOR WALL FOR A TURBINE ENGINE
App. No. 16/827,200
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TANDEM ROTOR BLADES
App. No. 16/827,135
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FILM-COOLED MULTI-WALLED STRUCTURE WITH ONE OR MORE INDENTATIONS
App. No. 16/827,195
→
GEARED TURBOFAN WITH OVERSPEED PROTECTION
App. No. 16/825,370
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CUTTING BLADE TIPS
App. No. 16/825,610
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LINKAGE ASSEMBLY PREVENTING AXIAL ROTATION OF THE LINK ROD FOR A GAS TURBINE ENGINE
App. No. 16/823,643
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RADIAL FUEL SHIFTING AND BIASING IN AN AXIAL STAGED COMBUSTOR FOR A GAS TURBINE ENGINE
App. No. 16/822,926
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AIRFOIL WITH PANEL AND SIDE EDGE COOLING
App. No. 16/821,169
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GAS TURBINE ENGINE WITH INTERCOOLED COOLING AIR AND TURBINE DRIVE
App. No. 16/821,383
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METHOD FOR HEAT TREATING COMPONENTS
App. No. 16/818,127
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STRUCTURED MATERIAL ALLOY COMPONENT FABRICATION
App. No. 16/815,502
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GAS TURBINE ENGINE DRIVE SYSTEM HEALTH MONITOR
App. No. 16/812,644
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GAS TURBINE ENGINE AND METHOD TO COOL A GAS TURBINE ENGINE CASE ASSEMBLY
App. No. 16/812,807
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CALCIUM-MAGNESIUM-ALUMINO-SILICATE RESISTANT THERMAL BARRIER COATINGS
App. No. 16/812,946
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PRE-START MOTORING SYNCHRONIZATION FOR MULTIPLE ENGINES
App. No. 16/812,862
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GEARED TURBOMACHINE FAN AND COMPRESSOR ROTATION
App. No. 16/812,636
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COMPRESSOR ROTOR STACK ASSEMBLY FOR GAS TURBINE ENGINE
App. No. 16/811,666
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THRUST EFFICIENT TURBOFAN ENGINE
App. No. 16/809,092
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REFRACTORY METAL CORE FINISHING TECHNIQUE
App. No. 16/808,529
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PILOTED RETAINING PLATE FOR A FACE SEAL ARRANGEMENT
App. No. 16/806,052
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STATOR OUTER PLATFORM SEALING AND RETAINER
App. No. 16/805,309
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SEMICONDUCTOR MEMORY DEVICE
App. No. 16/800,180
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INDUCING AND MONITORING A VIBRATORY RESPONSE IN A COMPONENT
App. No. 16/799,281
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DUAL COOLING AIRFLOW TO BLADES
App. No. 16/794,900
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INTERNAL COOLING CAVITY WITH TRIP STRIPS
App. No. 16/793,575
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HIGH TEMPERATURE IMAGING MEDIA FOR DIGITAL IMAGE CORRELATION
App. No. 16/793,675
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NANOCELLULAR FOAM DAMPER
App. No. 16/792,511
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MULTIPLE INJECTOR HOLES FOR GAS TURBINE ENGINE VANE
App. No. 16/790,890
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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
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AEROMECHANICAL IDENTIFICATION SYSTEMS AND METHODS
App. No. 16/787,611
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AIRFOIL INCLUDING ADHESIVELY BONDED SHROUD
App. No. 16/787,710
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GAS TURBINE ENGINE AIRFOIL
App. No. 16/787,731
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SYSTEMS AND METHODS FOR OPTIMAL SOURCE MATERIAL DEPOSITION ALONG HOLE EDGES
App. No. 16/786,228
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TURBOFAN ENGINE BEARING AND GEARBOX ARRANGEMENT
App. No. 16/786,421
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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
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Suspension Plasma Spray Apparatus and Use Methods
App. No. 16/773,098
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SEMICONDUCTOR MEMORY DEVICE
App. No. 16/749,710
→
FLEXIBLE SUPPORT STRUCTURE FOR A GEARED ARCHITECTURE GAS TURBINE ENGINE
App. No. 16/747,934
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RETENTION CLIP FOR A BLADE OUTER AIR SEAL
App. No. 16/747,028
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INTEGRAL CERAMIC MATRIX COMPOSITE FASTENER WITH NON-POLYMER RIGIDIZATION
App. No. 16/744,720
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CHROMIUM-ENRICHED DIFFUSED ALUMINIDE COATING
App. No. 16/744,583
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LASER POWDER DEPOSITION WELD REWORK FOR GAS TURBINE ENGINE NON-FUSION WELDABLE NICKEL CASTINGS
App. No. 16/743,431
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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
→
VARIABLE VANE POSITIONING APPARATUS FOR A GAS TURBINE ENGINE
App. No. 16/742,164
→
GAS TURBINE ENGINE AIRFOIL
App. No. 16/741,918
→
GAS TURBINE ENGINE AIRFOIL
App. No. 16/740,817
→
MIDDLE THREADED FITTING
App. No. 16/738,873
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BOOSTER COMPRESSOR WITH SPEED CHANGE SYSTEM
App. No. 16/736,322
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METHOD OF INSPECTING COMPONENT SURFACE WITH MARKING MEDIA
App. No. 16/734,818
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IMPINGEMENT COOLING ARRANGEMENT FOR AIRFOILS
App. No. 16/734,464
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RETENTION HARDWARE
App. No. 16/734,965
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ADDITIVE MANUFACTURING SYSTEM FOR MINIMIZING THERMAL STRESSES
App. No. 16/733,913
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SEMICONDUCTOR MEMORY DEVICE AND MEMORY SYSTEM
App. No. 16/733,491
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PLANETARY GEAR SYSTEM FOR TURBOMACHINE
App. No. 16/730,466
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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
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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
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GAS TURBINE ENGINE AIRFOIL
App. No. 16/722,164
→
SEMICONDUCTOR MEMORY DEVICE
App. No. 16/719,585
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ABRADABLE LAYER WITH GLASS MICROBALLOONS
App. No. 16/717,458
→
COMPRESSOR FLOWPATH
App. No. 16/715,528
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COOLING SYSTEMS FOR GAS TURBINE ENGINES
App. No. 16/712,458
→
SEMICONDUCTOR MEMORY
App. No. 16/707,646
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LIGHTWEIGHT JOURNAL SUPPORT PIN
App. No. 16/705,479
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FILM COOLING A COMBUSTOR WALL OF A TURBINE ENGINE
App. No. 16/703,211
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METHOD OF RESONANT INSPECTION FOR ADDITIVE MANUFACTURING
App. No. 16/703,467
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ADDITIVELY MANUFACTURED CORE
App. No. 16/701,614
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THREE-DIMENSIONAL SEMICONDUCTOR MEMORY DEVICE INCLUDING SLIT WITH LATERAL SURFACES HAVING PERIODICITY
App. No. 16/701,981
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LUBRICATION OF EPICYCLIC GEAR SYSTEM FOR GAS TURBINE ENGINE
App. No. 16/700,090
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MEMORY SYSTEM FOR RESTRAINING THRESHOLD VARIATION TO IMPROVE DATA READING
App. No. 16/697,540
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GAS TURBINE ENGINE SYSTEM WEAR REDUCTION
App. No. 16/695,290
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ADDITIVE MANUFACTURED CONGLOMERATED POWDER REMOVAL FROM INTERNAL PASSAGES
App. No. 16/695,877
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DEPOSITED MATERIAL STRUCTURE WITH INTEGRATED COMPONENT
App. No. 16/688,824
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SEMICONDUCTOR STORAGE DEVICE
App. No. 16/688,368
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METHOD FOR PYROLYZING PRECERAMIC POLYMER MATERIAL USING ELECTROMAGNETIC RADIATION
App. No. 16/687,149
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ADDITIVE MANUFACTURING PROCESS DISTORTION MANAGEMENT
App. No. 16/686,951
→
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
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GAS TURBINE ENGINE AIRFOIL
App. No. 16/681,187
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HIGH THRUST GEARED GAS TURBINE ENGINE
App. No. 16/676,788
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ENVIRONMENTAL COOLING SYSTEMS FOR AIRCRAFT
App. No. 16/675,585
→
INTERNALLY COOLED AIRFOIL
App. No. 16/675,879
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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
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VOLTAGE GENERATION CIRCUIT WHICH IS CAPABLE OF EXECUTING HIGH-SPEED BOOST OPERATION
App. No. 16/670,862
→
SEAL FACE PLATE COOLING
App. No. 16/670,531
→