LOAD ADJUSTABLE AND REUSABLE MECHANICAL RESTRAINT FOR AIRCRAFT EVACUATION SLIDE/RAFT SYSTEMS
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United States of America
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Issued Date -
Jan 20, 2022
app pub date -
Dec 18, 2020
filing date -
Dec 18, 2020
priority date (Note) -
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Abstract
A releasable restraint for an evacuation system includes a plug body and a socket body. A ball, a plunger, a first spring member, and an adjustable fastener are disposed at least partially within the plug body. A spring force of the first spring member is adjustable in response to moving the adjustable fastener with respect to the plug body. The first spring member urges the plunger against the ball, and in response, the ball extends through a sidewall of the plug body and at least partially through a sidewall of the socket body to lock the plug body to the socket body. In response to a tensile force applied to the releasable restraint, the ball is configured to retract at least partially into the plug body, against the urging of the first spring member, to release the socket body from the plug body.
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