| 摘要 |
On-board device for monitoring the load of an aeroplane, which can be used on each axle of a landing gear. It comprises: in the axis of the axle 1 a rigid rod 5 which is not subjected to deformation, and is carried by two thin deformable supports 6, 7; and in the vertical plane of the rod 5, two inductive sensors 8, 9 attached to the axle 1, disposed on either side of the central part of the rod 5 in order to allow differential detection of the variations of the relative position of the rod and the axle so as to calculate therefrom the load applied to the axle. <IMAGE>
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