A fitting for attaching the horizontal tail stabilizer of an aircraft, allowing the formation of a lighter component, without a fatigue failure mode and with a significant reduction in the installation time. The fitting comprises: a core piece having a regular thickness, the core piece having a U configuration, according to a plan view, thereby being composed of two lateral areas and a central area located between the lateral areas, at least one central reinforcement having a regular thickness and joined to one side of the central area and comprising a flange located on an inner edge of the core piece, at least two lateral reinforcements having a regular thickness and each lateral reinforcement being joined to one side of a different lateral area and comprising a flange located on the inner edge of the core piece.
FITTING FOR ATTACHING THE HORIZONTAL TAIL STABILIZER OF AN AIRCRAFT
06.02.2020
Patent
Elektronische Ressource
Englisch
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