An aircraft high lift airfoil arrangement guiding element includes a first part configured to be fixed to a first edge member or rib of the airfoil arrangement, and a second part including a track support element to movably support a track device of a second edge member or slat of the airfoil arrangement. The second part is mounted to the first part to move from a first to a second position. A biasing device biases the track support element in the spanwise direction towards the track device. The airfoil arrangement is produced by providing the first edge member or rib, rigidly attaching thereto guiding elements to guide the movable track device supporting the second edge member or slat, and attaching the track device to the first edge member. During installation, a surface of the track device is pressed against a movable track support element biased against the track device.
GUIDING ELEMENT FOR A HIGH LIFT AIRFOIL ARRANGEMENT OF AN AIRCRAFT, HIGH LIFT AIRFOIL ARRANGEMENT AND PRODUCTION METHOD
16.09.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2023
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NTIS | 1981
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