A guiding element (60) for a high lift airfoil arrangement of an aircraft comprises a first part (62) configured for being fixed to a first edge member or rib (34) of a high lift airfoil arrangement, and a second part (63) comprising at least one track support element (66) for movably supporting a track device (28) of a second edge member or slat (16) of the airfoil arrangement. The second part (63) is movably mounted to the first part (62) and configured for moving from a first position to a second position. A biasing device (73) is configured for biasing the track support element (66) in the spanwise direction towards the track device (28). A high lift airfoil arrangement is produced by providing a first edge member or rib (34), rigidly attaching thereto guiding elements for guiding a movable track device supporting a second edge member or slat (16), and attaching the track device (28) to the first edge member. During installation of the track device (28), a surface (29) of the track device (28) is pressed against a movable track support element (66) which is biased against the track device (28).
GUIDING ELEMENT FOR A HIGH LIFT AIRFOIL ARRANGEMENT OF AN AIRCRAFT, HIGH LIFT AIRFOIL ARRANGEMENT AND PRODUCTION METHOD
FÜHRUNGSELEMENT FÜR EINE HOCHAUFTRIEBSPROFILANORDNUNG EINES FLUGZEUGS, HOCHAUFTRIEBSPROFILANORDNUNG UND HERSTELLUNGSVERFAHREN
ÉLÉMENT DE GUIDAGE POUR UN AGENCEMENT DE PROFIL AÉRODYNAMIQUE HYPERSUSTENTATEUR D'UN AVION, AGENCEMENT DE PROFIL AÉRODYNAMIQUE HYPERSUSTENTATEUR ET PROCÉDÉ DE PRODUCTION
2023-07-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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NTIS | 1981
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