This paper presents a new kind of inductive force sensor that gives th
e amplitude and the direction of the force in a plane, and that is dif
ferent from the lately developped technologies utilizing the magnetost
rictive or magnetoresistive effect. It is constituted of a magnetic ci
rcuit with airgaps that varie in length with the applied force. When a
force is exerted, a bar is bent and one of the airgaps becomes wider,
the reluctance of the corresponding magnetic circuit increases and th
e inductance of the coil located on this circuit decreases; the other
airgap becomes narrower. The bending of the bar is proportional to the
applied force, so, the inductance variations are an image of this for
ce. The use of two coils leads to a differential structure. The same c
onstruction is done to measure the force in the orthogonal direction.
This structure gives the two components of a force in a plane. The sen
sor is studied first to optimize its geometry with regard to the dimen
sional parameters. An optimum is found that gives the maximum airgap v
ariations for a given force, and so the maximum signal variations. A m
agnetic study is done with finite elements calculations. A prototype w
as built to measure lift and drag of a rudder on a ship.