Sliding connection between the floor structure and the hull structure of an aircraft
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United States of America Patent
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Sep 19, 2017
Issued Date -
N/A
app pub date -
May 28, 2015
filing date -
May 30, 2014
priority date (Note) -
In Force
status (Latency Note)
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Abstract
An aircraft structure part comprising a floor structure, a hull structure, and a connecting element. The connecting element comprises a rod attached, at its first end, to one of the hull and the floor; an attachment element, attached to the other of the hull and the floor, and provided with an opening in which the second end of the rod is slidably mounted; and an endstop attached to the rod so as to engage with the attachment element, to limit the sliding amplitude of the rod in the opening. When the connection between the floor and the hull is loaded in tension, the endstop makes it possible to comply with the standards for withstanding acceleration towards the aircraft front. When the connection is loaded in compression, the rod slides freely in the opening, which limits the constraints of withstanding compressive stresses, reducing the weight of the connecting element.
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