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Category:Raytheon technologies corporation
Pages in category "Raytheon technologies corporation"
The following 61 pages are in this category, out of 61 total.
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- Raytheon technologies corporation (20240300141). CHEMICAL VAPOR INFILTRATION TOOLING FOR OPTIMIZING INFILTRATION IN CERAMIC MATRIX COMPOSITES simplified abstract
- Raytheon technologies corporation (20240300142). METHODS FOR COMPLEX GEOMETRY MANDREL REMOVAL OF CERAMIC MATRIX COMPOSITE COMPONENTS simplified abstract
- Raytheon technologies corporation (20240300657). AIRCRAFT HYBRID ELECTRIC PROPULSION ARCHITECTURE ENABLING MODES OF OPERATION simplified abstract
- Raytheon technologies corporation (20240300861). METHOD OF REDUCING SURFACE DEFORMATION FROM Z-CHANNEL CREATION simplified abstract
- Raytheon technologies corporation (20240300863). CHEMICAL VAPOR INFILTRATION TOOLING FOR OPTIMIZING INFILTRATION IN CERAMIC MATRIX COMPOSITES simplified abstract
- Raytheon technologies corporation (20240301547). CHEMICAL VAPOR INFILTRATION TOOLING HOLE MODIFICATION FOR OPTIMIZING INFILTRATION IN CERAMIC MATRIX COMPOSITES simplified abstract
- Raytheon technologies corporation (20240301796). Airfoils with Axial Leading Edge Impingement Slots simplified abstract
- Raytheon technologies corporation (20240301797). Airfoils with Mixed Skin Passageway Cooling simplified abstract
- Raytheon technologies corporation (20240301799). AIRFOIL TIP ARRANGEMENT FOR GAS TURBINE ENGINE simplified abstract
- Raytheon technologies corporation (20240301805). BOLTED JOINT OF GAS TURBINE ENGINE simplified abstract
- Raytheon technologies corporation (20240301808). HEAT EXCHANGER(S) FOR RECOVERING WATER AND/OR HEAT ENERGY FROM TURBINE ENGINE COMBUSTION PRODUCTS simplified abstract
- Raytheon technologies corporation (20240301819). RECOVERING WATER AND/OR HEAT ENERGY FROM POWERPLANT COMBUSTION PRODUCTS simplified abstract
- Raytheon technologies corporation (20240301823). HEAT EXCHANGER(S) FOR RECOVERING WATER AND/OR HEAT ENERGY FROM TURBINE ENGINE COMBUSTION PRODUCTS simplified abstract
- Raytheon technologies corporation (20240301830). HEAT EXCHANGER(S) FOR RECOVERING WATER AND/OR HEAT ENERGY FROM TURBINE ENGINE COMBUSTION PRODUCTS simplified abstract
- Raytheon technologies corporation (20240302042). TURBINE ENGINE COMBUSTOR WALL WITH APERTURE DEFLECTOR simplified abstract
- Raytheon technologies corporation (20240302044). CANTED FUEL INJECTOR ASSEMBLY FOR A TURBINE ENGINE simplified abstract
- Raytheon technologies corporation (20240302101). HEAT EXCHANGER WITH CROSSING HEAT EXCHANGE TUBES simplified abstract
- Raytheon technologies corporation (20240307965). MITIGATING DOWN SKIN EFFECTS IN ADDITIVE MANUFACTURING simplified abstract
- Raytheon technologies corporation (20240307973). SPINDLES PEENING OFFSET FIXTURE FOR CNC TURNING simplified abstract
- Raytheon technologies corporation (20240308015). MULTI-HEAD DESIGN FOR ULTRASONIC IMPACT GRINDING OF CMCS simplified abstract
- Raytheon technologies corporation (20240308680). AIRCRAFT FUEL SYSTEM WITH REMOVABLE FUEL TANK simplified abstract
- Raytheon technologies corporation (20240308921). SHEATHED METALLIC NEEDLES FOR PRODUCING Z-CHANNELS IN FIBROUS PREFORMS simplified abstract
- Raytheon technologies corporation (20240308922). TOOLING FOR PRODUCING Z-CHANNELS IN CERAMIC FIBER PREFORMS simplified abstract
- Raytheon technologies corporation (20240308927). THREE-DIMENSIONAL WEAVE WITH SACRIFICIAL Z-FIBERS FOR IMPROVED CERAMIC MATRIX COMPOSITE MICROSTRUCTURE simplified abstract
- Raytheon technologies corporation (20240309764). ALTERING STRUCTURAL RESPONSE OF TWO-PIECE HOLLOW-VANE ASSEMBLY simplified abstract
- Raytheon technologies corporation (20240309765). ALTERING STRUCTURAL RESPONSE OF TWO-PIECE HOLLOW-VANE ASSEMBLY BY CHANGING THE COVER COMPOSITION simplified abstract
- Raytheon technologies corporation (20240309779). COMPRESSOR CASE WITH A COOLING CAVITY simplified abstract
- Raytheon technologies corporation (20240309806). MODULATING FLUID FLOW WITHIN A TURBINE ENGINE USING STEAM simplified abstract
- Raytheon technologies corporation (20240309807). ASYMMETRIC INTRODUCTION OF STEAM INTO TURBINE ENGINE COMBUSTION CHAMBER simplified abstract
- Raytheon technologies corporation (20240309808). INTRODUCING STEAM WITH QUENCH AIR INTO TURBINE ENGINE COMBUSTOR simplified abstract
- Raytheon technologies corporation (20240309809). INJECTING STEAM INTO HOOD CAVITY OF TURBINE ENGINE COMBUSTOR simplified abstract
- Raytheon technologies corporation (20240309810). INTRODUCING STEAM INTO CORE AIR UPSTREAM OF TURBINE ENGINE DIFFUSER PLENUM simplified abstract
- Raytheon technologies corporation (20240309811). STEAM COOLING TURBINE ENGINE COMBUSTOR WALL simplified abstract
- Raytheon technologies corporation (20240309813). STEAM COOLING TURBINE STATOR VANE ARRAY simplified abstract
- Raytheon technologies corporation (20240309814). SELECTIVE STEAM DISTRIBUTION TO STEAM COOLED ZONES IN A TURBINE ENGINE simplified abstract
- Raytheon technologies corporation (20240309815). PROTECTIVE TREATMENT AND METHOD OF APPLYING THE SAME simplified abstract
- Raytheon technologies corporation (20240310042). INJECTING FUEL-STEAM MIXTURE INTO TURBINE ENGINE COMBUSTOR simplified abstract
- Raytheon technologies corporation (20240310246). MULTI-MEASUREMENT PROBE ASSEMBLY simplified abstract
- Raytheon technologies corporation (20240310599). COUPLING OPTICAL FIBERS AND FLUID PASSAGES simplified abstract
- Raytheon technologies corporation (20240313811). ARCHITECTURE FOR HIGH TEMPERATURE RADIO FREQUENCY SMART NODE simplified abstract
- Raytheon technologies corporation (20240408561). APPARATUS AND METHOD FOR ISOLATING HYDROGEN FROM WATER
- Raytheon technologies corporation (20240408676). DETERMINING QUALITY OF REUSED BUILD POWDER FOR ADDITIVE MANUFACTURING
- Raytheon technologies corporation (20240408979). POWER AND ENERGY MANAGEMENT FOR DISTRIBUTED HYBRID PROPULSION
- Raytheon technologies corporation (20240409400). APPARATUS AND METHOD FOR ISOLATING HYDROGEN FROM WATER
- Raytheon technologies corporation (20240409401). APPARATUS AND METHOD FOR ISOLATING HYDROGEN FROM WATER
- Raytheon technologies corporation (20240410283). AIRFOIL COOLING CIRCUIT
- Raytheon technologies corporation (20240410284). TURBINE VANE BAFFLE CHIMNEY
- Raytheon technologies corporation (20240410287). INTEGRAL COMPOSITE STATOR LABYRINTH SEAL
- Raytheon technologies corporation (20240410313). WATER COOLED EXHAUST DUCT
- Raytheon technologies corporation (20240410314). WATER ACTIVE TURBINE CLEARANCE CONTROL
- Raytheon technologies corporation (20240410392). HYBRID SHROUD IMPELLER
- Raytheon technologies corporation (20240410393). COMPRESSOR VARIABLE VANE SPINDLE MOUNT WITH FLOATING SEAL
- Raytheon technologies corporation (20240410587). GAS TURBINE ENGINE WITH IMPROVED HIGH PRESSURE COMPRESSOR LEAKAGE PATH GUIDE STRUCTURE
- Raytheon technologies corporation (20240410656). COMPOSITE HEAT EXCHANGE APPARATUS FOR A TURBINE ENGINE
- Raytheon technologies corporation (20240410787). MULTI INSTRUMENT EGRESS FOR GAS TURBINE ENGINE
- Raytheon technologies corporation (20240411962). METHOD AND SYSTEM FOR OPTIMIZING THE ASSEMBLY OF ROTATING HARDWARE IN GAS TURBINE ENGINES USING ARTIFICIAL NEURAL NETWORKS
- Raytheon technologies corporation (20240412409). INVERTING NEURAL RADIANCE FIELDS FOR PART AND SCENE POSE ESTIMATION
- Raytheon technologies corporation (20240413704). AIRCRAFT POWERPLANT WITH BOOSTED GAS TURBINE ENGINE
- RAYTHEON TECHNOLOGIES CORPORATION patent applications on December 12th, 2024
- Raytheon Technologies Corporation patent applications on September 12th, 2024
- Raytheon Technologies Corporation patent applications on September 19th, 2024