WING LOAD SUPPORT STRUCTURE OF THE FUSELAGE
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United States of America Patent
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Issued Date -
Oct 10, 2024
app pub date -
Nov 21, 2023
filing date -
Apr 4, 2023
priority date (Note) -
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status (Latency Note)
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Abstract
A wing load support structure of a fuselage includes a first joint on a front spar of a wing unit of the fuselage, a center bulk head including a first spar joint coupled to the first joint and configured to support a vertical load of the front spar transmitted by the wing unit, a second joint mounted on a rear spar of the wing unit, a spar cover including a second spar joint coupled to the second joint and connected to a rear bulk head by a bulk head upper support, and a support unit configured to support the spar cover and the rear bulk head inside the fuselage and configured to support a vertical load of the rear spar transmitted by the wing unit.
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