An aircraft wing slat (20) is formed from composite materials using lay-up and vacuum bagging techniques. The slat lay-up comprises a central honeycomb core (26) sandwiched between upper (22) and lower (24) composite skins, a pre-cured spar (28) and pre-cured stiffeners (30). After the lay-up is cured and removed from a lay-up mold, leading edge strengthening ribs (32) and a preformed composite nose skin (40) are installed to complete the slat.
Composite wing slat for aircraft
Verbundvorflügel für Luftfahrzeug
volet de bord d'attaque de composite
24.04.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |