Aircraft shock strut having a fluid level monitor

Details Aircraft shock strut having a fluid level monitor Aircraft shock strut having a fluid level monitor

G - Physics

01

M

G01M 17/00 (2006.01) B64C 25/58 (2006.01) G01F 25/00 (2006.01)

Patent

CA 2715766

A system for monitoring a liquid level in an aircraft shock strut includes a cylinder having an internal chamber sealed by a piston telescopically movable within the cylinder. The chamber contains a gas and a liquid, and a sensor assembly is provided for monitoring a condition of a level of the liquid in the chamber. The sensor assembly includes at least one probe within the chamber, and a fitting assembly allows one or more leads from the probe to pass through the wall of the strut while maintaining pressure in the chamber. The fitting assembly includes a plug molded to the one or more leads extending from the probe. The fitting assembly also includes a retainer for holding the plug in sealed relationship with a through passage in the strut.

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