A structural system for accommodating the thermal expansion of a nacelle lip skin and supporting structure has a lip skin and a first angle element attached to the lip skin. The first angle element has a free edge that is scalloped to accommodate thermal stresses. A bulkhead is attached to the first angle element.
Un système structurel pour compenser la dilatation thermique dun revêtement de bord de nacelle et dune structure de support comporte un revêtement de bord et un premier élément dangle fixé au revêtement de bord. Le premier élément dangle comporte un bord libre qui est festonné pour compenser les contraintes thermiques. Une cloison est fixée au premier élément dangle.
METHOD OF ATTACHING NACELLE STRUCTURE TO MINIMIZE FATIGUE LOADING
METHODE DE FIXATION D'UNE STRUCTURE DE NACELLE SERVANT A MINIMISER LA CHARGE DE FATIGUE
2018-07-10
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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