Engine thrust reverser lock
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United States of America Patent
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Oct 17, 2017
Grant Date -
Oct 1, 2015
app pub date -
Jun 12, 2015
filing date -
Mar 14, 2013
priority date (Note) -
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Abstract
In some aspects, an aircraft engine thrust reverser lock system includes a pin-capturing member. The pin-capturing member includes a body that is rotatable about an axis defined by a pivot extending through the body. The body includes an interior surface that defines a slot. The slot has an opening that is sized to receive a pin into the slot. One side of the slot includes a protruded sidewall surface that protrudes into the slot toward an another sidewall surface of the slot. The protruded sidewall surface defines an apex between the open and closed ends of the slot. Between the apex and the closed end of the slot, the protruded sidewall surface faces the rotational axis.
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