公开(公告)号：US20220381801A1

公开(公告)日：2022-12-01

申请号：US17747353

申请日：2022-05-18

Applicant: Airbus Operations S.A.S.

Inventor： Jean-Luc Vialatte ,  Karounen Veerabadran ,  Thomas Boisson ,  Laurent Malard ,  Ivan Garcia Hallo ,  Florent Montet

IPC: G01P13/02 ,  G01P13/00

Abstract: The measuring device includes a substrate intended to be arranged on an aerodynamic surface; a profiled element connected at one of its ends to the substrate, and configured to be oriented, under the effect of the fluid flow; a magnet that is secured to the profiled element and is configured to generate a magnetic field; and a measuring element that is configured to measure a value of the magnetic field and to convert this measured value of the magnetic field into an angle value indicating the direction of the fluid flow; the measuring device thus making it possible to measure and provide, in real-time, a numerical angle value with which it is possible to define with high precision the direction of the fluid flow relative to the aerodynamic surface.