TANGENTIAL TURBOFAN PROPULSION SYSTEM
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United States of America Patent
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Issued Date -
May 18, 2023
app pub date -
Jan 4, 2023
filing date -
Jan 4, 2023
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The present invention is a turbofan propulsion system, based on a tangential gas turbine that is structurally a part of the propulsion system's centrifugal compressor, wherein the gas turbine's combustion chambers with nozzles are placed to rotate around a larger radius circle at a supersonic circumferential speed, and the fan blades are placed to rotate around a smaller radius circle at a subsonic circumferential speed, therefore increasing the efficiency of the propulsion system.
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