A structural system for accommodating the thermal expansion of a nacelle lip skin and supporting structure has a lip skin (24) and a first angle element (62) attached to the lip skin (24). The first angle element (62) has a free edge (82) that is scalloped to accommodate thermal stresses. A bulkhead (60) is attached to the first angle element (62).
METHOD OF ATTACHING NACELLE STRUCTURE TO MINIMIZE FATIGUE LOADING
VERFAHREN ZUM ANBRINGEN EINER GONDELSTRUKTUR ZUR MINIMIERUNG VON DAUERBEANSPRUCHUNG
PROCÉDÉ DE FIXATION DE STRUCTURE DE NACELLE POUR RÉDUIRE UNE CHARGE DE FATIGUE
01.05.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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