LATCH ASSEMBLY FOR AIRCRAFT MONUMENT
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United States of America Patent
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Issued Date -
Aug 13, 2020
app pub date -
Aug 28, 2018
filing date -
Aug 30, 2017
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Abstract
A latch assembly for selectively preventing a relative movement between first and second components of an aircraft cabin monument, including a latch having a first connection member and a striker plate having a second connection member complementary to and selectively engageable with the first connection member. The engaged latch and striker plate in use are subjected to a load having a use threshold value and a decompression threshold value. The striker plate is designed to have a failure load higher than the use threshold value and lower than the decompression threshold value. The latch has a failure load higher than the use threshold value and higher than the decompression threshold value. A method of tailoring a failure of a latch assembly selectively preventing a relative movement between first and second components of an aircraft cabin monument is also discussed.
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