Aircraft high lift system and method for determining an operating condition of an aircraft high lift system

摘要

The present disclosure relates to an aircraft high lift system with at least one load station for actuating a flap of a wing, preferably a landing flap and/or a leading-edge flap, at least one transmission with transmission portions located between branch transmissions, wherein by means of the branch transmissions actuating energy can be branched off from the transmission to the load station, and to a method for determining an operating condition of an aircraft high lift system.

主权项

1. An aircraft high lift system comprising at least two load stations for actuating a flap of a wing, a central drive unit converting aircraft supply energy into mechanical actuating energy, the actuating energy transmitted from the central drive unit to a transfer gear, the transfer gear distributing the actuating energy to at least one transmission, each transmission comprising at least one transmission portion, each transmission portion arranged between respective branch transmissions of two load stations associated to the flap, wherein via each branch transmission, actuating energy is selectively transmitted from the transmission to the corresponding load station, the system further comprising a detection sensor arranged in each transmission portion by which an operating condition of the transmission or of one or more of the two load stations is determined.