MICRO-TURBINE GAS GENERATOR AND PROPULSIVE SYSTEM
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United States of America Patent
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N/A
Issued Date -
Feb 15, 2024
app pub date -
Mar 15, 2023
filing date -
Dec 4, 2015
priority date (Note) -
Published
status (Latency Note)
Importance
Abstract
A propulsion system includes a first compressor in fluid communication with a fluid source. A first conduit is coupled to the first compressor, and a heat exchanger is in fluid communication with the first compressor via the first conduit. A second conduit is positioned proximal to the heat exchanger. A combustor is in fluid communication with the heat exchanger via the second conduit and is configured to generate a high-temperature gas stream. A third conduit is coupled to the combustor, and a first thrust augmentation device is in fluid communication with the combustor via the third conduit. The heat exchanger is positioned within the gas stream generated by the combustor.
First Claim
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