Chock for Steering Mechanism of an Aircraft Nose Landing Gear
Number of patents in Portfolio can not be more than 2000
United States of America
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Issued Date -
Nov 14, 2024
app pub date -
May 8, 2023
filing date -
May 8, 2023
priority date (Note) -
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status (Latency Note)
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Abstract
A device to engage with a steering mechanism of a nose landing gear of an aircraft to limit steering rotation of the nose landing gear. The device includes a first chock sized to fit within a first space formed in the nose landing gear at a first cylinder of a steering mechanism, and a second chock sized to fit within a second space formed in the nose landing gear at a second cylinder. The first chock is configured to engage with the first cylinder and to compress to prevent retraction of the first cylinder beyond a first predetermined length. The second chock is configured to engage with the second cylinder and to compress to prevent retraction of the second cylinder beyond a second predetermined length.
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