Three axis active magnetic levitation for inertial sensing systems
AssigneeEcole Polytechnique Federale De Lausanne (Epfl)
InventorsAlexis Boletis, François Barrot, Roland Moser
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AssigneeEcole Polytechnique Federale De Lausanne (Epfl)
InventorsAlexis Boletis, François Barrot, Roland Moser
Estimating the term…
The invention relates to an inertial sensor based on the magnetic levitation of an inertial mass comprising an active magnetic bearing unit arranged in such a way as to levitate the inertial mass and characterized by the fact that it furthermore comprises additional active magnetic bearings units arranged in such a way as to control the position of said inertial mass along three independent axis and to create, for any of said independent axis, restoring forces that can be oriented in any of the two directions of these independent axis.
An inertial sensor based on the magnetic levitation of a ferromagnetic spherical or cylindrical inertial mass and comprising:
An inertial sensor based on the magnetic levitation of a ferromagnetic inertial mass and comprising:
Dependencies are inferred from the claim text.
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Suspensions; Bearings: using magnetic or electrostatic fields
Measuring inclination
By measuring the force required to restore a proofmass subjected to inertial forces to a null position: with electromagnetic counterbalancing means
Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration: in two or more dimensions
Term ended 15 Jan 2024 (estimated)
This application is the U.S. national phase of international application PCT/CH2003/000597 filed 2 Sep. 2003 which designated the U.S. and claims benefit of PCT/CH02/00481, dated 2 Sep. 2002, the entire content of which is hereby incorporated by reference.
The present invention relates to non-contact inertial sensing systems, that is to say inertial sensors where the inertial mass is never in contact with the rest of the instrument. The contact less suspension of said mass is assured by magnetic bearings.
Current inertial sensing systems such as seismometers, accelerometers, gravimeters and tiltmeters are based on the relative displacement between an inertial mass and the base of the instrument when the said base is subject to an external disturbance (vibration, modification of the “g” level, angle); and gyroscopes, which are another kind of inertial sensing systems, are made of an inertial mass which is rotated about one of its axis of inertia and the measurement principle relies on the relative movement between the said axis and the base of the instrument, or on the force generated by the said axis on the base of the instrument, when the said base is subject to an external movement.
For a greater understanding of the nature and objects of the invention, reference should be made to the following detailed description and the accompanying drawings, in which:
FIG. 1 shows complete view of the first embodiment of the inertial sensing system with: 1) End cap 2) Support structure 3) Horizontal pair of electromagnets 4) Vertical pair of electromagnets 5) Ferromagnetic inertial mass 6) Holding structure for the horizontal electromagnets 7) High precision position sensors 8) Coil armature
FIG. 2 shows a horizontal cut (O,X,Y) of the first embodiment of the inertial sensing system with: 3a), 3b), 3c), 3d) Coils 7a), 7b), 7c), 7d) High precision position sensors
Implementation 1a (FIG. 1, FIG. 2, FIG. 3)
Six electromagnets 3, 4, 3a, 3b, 3c, 3d are diametrically disposed in pairs along three orthogonal axis.
A small size ferromagnetic inertial mass 5 is levitated and its position controlled along three axis.