A slat track device (7) for an aircraft wing (1), comprising a beam-shaped main load bearing track structure (9) configured to be connected to a slat (5) and to be movably connected to a main wing (3), a guidance surface (11) provided at the track structure (9), for being guided along a corresponding guidance device (19) provided at a main wing (3), a connection device (13) provided at the track structure (9) for connecting the track structure (9) to a slat (5), and an engagement device (15) provided at the track structure (9) and configured for engagement with a drive member (33) of a drive unit (37) provided at a main wing (3). The object of the present invention, to provide a slat track device comprising two redundant main load paths, is achieved in that the track structure (9) comprises a first track member (41) and a second track member (43) formed separately from one another and each being connected to both the connection device (13) and the engagement device (15).
НАПРАВЛЯЮЩЕЕ УСТРОЙСТВО ДЛЯ ПРЕДКРЫЛКА КРЫЛА ВОЗДУШНОГО СУДНА
22.03.2019
Patent
Elektronische Ressource
Russisch
IPC: | B64C AEROPLANES , Flugzeuge |
СПОСОБ И УСТРОЙСТВО ДИСТАНЦИОННОГО ОСМОТРА СОСТОЯНИЯ ДВИГАТЕЛЯ ВОЗДУШНОГО СУДНА
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