VARIABLE ENGINE-INLET BYPASS CONTROL SYSTEMS AND METHOD
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United States of America Patent
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Issued Date -
Oct 20, 2022
app pub date -
Apr 20, 2021
filing date -
Apr 20, 2021
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Abstract
A system for optimizing engine air-mass-flow intake of an aircraft includes a forward-facing airframe-inlet duct interoperably coupled to an inlet of an engine of the aircraft, an air-mass-flow bypass mechanism coupled to the forward-facing airframe-inlet duct and adjustable to allow a selected amount of air entering an inlet of the forward-facing airframe-inlet duct to bypass the inlet of the engine, and an air-pressure sensor arranged in the forward-facing airframe-inlet duct adjacent to the inlet of the engine. A measured value (“PT1”) from the air-pressure sensor is used to determine a degree to which the air-mass-flow bypass mechanism is to be opened.
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