Fitting for attaching the horizontal tail stabilizer of an aircraft, allowing to obtain a lighter component, without fatigue failure mode and with a significant reduction in the installation time, wherein the fitting comprises:- a core piece (1) having a regular thickness, the core piece (1) having U configuration, according to a plan view, thereby being composed by two lateral areas (1') and a central area (1") located between the arm areas (1'),- at least one central reinforcement (2) having a regular thickness and joined to one side of the central area (1") and comprising a flange (2') located in an inner edge (1"') of the core piece (1),- at least two lateral reinforcements (3) having a regular thickness and each lateral reinforcement (3) being joined to one side of a different lateral area (1') and comprising a flange (3') located in the inner edge (1"') of the core piece (1).
FITTING FOR ATTACHING THE HORIZONTAL TAIL STABILIZER OF AN AIRCRAFT
BESCHLAG ZUR BEFESTIGUNG DES HORIZONTALEN HÖHENLEITWERKSTABILISATORS EINES FLUGZEUGS
FERRURE POUR FIXER LE STABILISATEUR D'EMPENNAGE HORIZONTAL D'UN AÉRONEF
2022-01-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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