Patents/Inventors

Frederick M. Schwarz

Glastonbury, CTUS36 patents

39 Patents

US125039812025
Gas Turbine Engine with High Speed Low Pressure Turbine Section and Bearing Support Features
RTX CORPORATION
0 cites
US124219162025
Engine Mount System for a Gas Turbine Engine
RTX CORPORATION
0 cites
US123854092025
Epicyclic Gear Train
RTX CORPORATION
0 cites
US123661792025
Gas Turbine Engine with High Speed Low Pressure Turbine Section and Bearing Support Features
RTX CORPORATION
0 cites
US123586302025
Cryogenic Cooling System for an Aircraft
RTX CORPORATION
0 cites
US123513182025
Cryogenic Cooling System for an Aircraft
RTX CORPORATION
0 cites
US123379742025
Propulsion System Cooling Control
RTX CORPORATION
0 cites
US122581352025
Aircraft Hybrid Propulsion Fan Drive Gear System Dc Motors and Generators
RTX CORPORATION
0 cites
US122474932025
Gas Turbine Engine Front Section
RTX CORPORATION
0 cites
US121799292024
Engine Mount System for a Gas Turbine Engine
RTX CORPORATION
0 cites
US120849782024
Epicyclic Gear Train
RTX CORPORATION
0 cites
US120550932024
Geared Turbofan Engine with a High Ratio of Thrust to Turbine Volume
RTX Corporation
0 cites
US120550962024
Geared Turbofan Engine Gearbox Arrangement
RTX CORPORATION
0 cites
US120441832024
Geared Turbine Engine with Relatively Lightweight Propulsor Module
RTX CORPORATION
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US120068762024
Gas Turbine Engine Front Section
RTX CORPORATION
0 cites
US119709842024
Gas Turbine Engine with Power Density Range
RTX CORPORATION
0 cites
US119204852024
Cooling Air for Gas Turbine Engine with Thermally Isolated Cooling Air Delivery
RTX Corporation
0 cites
US119133492024
Gas Turbine Engine with High Speed Low Pressure Turbine Section and Bearing Support Features
RTX CORPORATION
0 cites
US118595382024
Geared Turbofan Engine with Targeted Modular Efficiency
RTX CORPORATION
0 cites
US118073782023
Alternating Starter Use During Multi-engine Motoring
RTX CORPORATION
0 cites
US117317732023
Engine Mount System for a Gas Turbine Engine
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US117191692023
Gas Turbine Engine with Heat Exchanger Diagnostics
Raytheon Technologies Corporation
0 cites
US116804922023
Epicyclic Gear Train
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US116744112023
Multi-engine Coordination During Gas Turbine Engine Motoring
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US116744132023
Gas Turbine Engine with Gearbox Health Features
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US116618942023
Geared Turbine Engine with Relatively Lightweight Propulsor Module
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US116350252023
Gas Turbine Engine with Forward Moment Arm
Raytheon Technologies Corporation
0 cites
US116350432023
Geared Architecture for High Speed and Small Volume Fan Drive Turbine
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US116140362023
Turbine Section of Gas Turbine Engine
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US116087862023
Gas Turbine Engine with Power Density Range
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US115975272023
Aircraft Hybrid Propulsion Fan Drive Gear System DC Motors and Generators
Raytheon Technologies Corporation
0 cites
US115982232023
Gas Turbine Engine with High Speed Low Pressure Turbine Section and Bearing Support Features
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US115982862023
Geared Gas Turbine Engine Arrangement with Core Split Power Ratio
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US115852682023
Geared Turbofan Engine with Targeted Modular Efficiency
Raytheon Technologies Corporation
0 cites
US115852762023
Gas Turbine Engine with High Speed Low Pressure Turbine Section and Bearing Support Features
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US115786512023
Geared Turbofan Arrangement with Core Split Power Ratio
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US115729282023
Heat Exchanger for Cooled Cooling Air with Adjustable Damper
Raytheon Technologies Corporation
0 cites
US115608512023
Geared Turbofan Engine with High Compressor Exit Temperature
RAYTHEON TECHNOLOGIES CORPORATION
0 cites
US115420162023
Cryogenic Cooling System for an Aircraft
RAYTHEON TECHNOLOGIES CORPORATION
0 cites