Aircraft fluid control system having a pressure sensor
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United States of America Patent
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Nov 5, 2019
Grant Date -
Oct 4, 2018
app pub date -
Apr 3, 2017
filing date -
Apr 3, 2017
priority date (Note) -
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Abstract
A pressure sensor for fluid control system for an aircraft includes an enclosure, a piston assembly, and a bellows. The enclosure has a body that extends between a first end and a second end. A first fluid line extends to the first end. The piston assembly has a piston head that is movably disposed within the enclosure and a piston rod that extends from the piston head and through the second end. The bellows is disposed within the body that extends between and is operatively connected to the piston head and the first end.
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