Patent ID: 11971277
Assignee: TEXTRON INNOVATIONS INC.
Field: Transport (Mechanical engineering)
Classification: CPC B  G | IPC B  G

Claim 7:
8. A rotor-hub-flap anisotropic-sensor arrangement comprising:
a plurality of anisotropic sensors coupled to a flight control computer and a rotor hub; and
at least one magnet associated with the plurality of anisotropic sensors;
wherein:
the at least one magnet is a single magnet;
the plurality of anisotropic sensors comprises a first anisotropic sensor and a second anisotropic sensor;
the first anisotropic sensor is arranged on a first side of the single magnet;
the second anisotropic sensor is arranged on the first side of the single magnet at a distance farther from the single magnet than the first anisotropic sensor; and
the first anisotropic sensor and the second anisotropic sensor are mounted on opposite sides of an intermediate circuit board.