公开(公告)号：US11214348B2

公开(公告)日：2022-01-04

申请号：US16453119

申请日：2019-06-26

Applicant: Airbus Operations S.A.S.

Inventor： Marie-Anne De Smet

IPC: B64C1/06 ,  B64C7/00 ,  G01D11/24

Abstract: A sensor is fixed on an aircraft structure by a joining system which includes at least one enclosure in which is positioned at least one transducer, at least one passage configured to allow at least one conducting element to pass through the enclosure, at least one flexible connection connecting each transducer present in the enclosure to said enclosure and at least one binder joining together the enclosure and the structure. This joining system makes it possible to limit the spread of the deformations of the structure toward the transducer or transducers and ultimately the risks of malfunction.

公开(公告)号：US20200010165A1

公开(公告)日：2020-01-09

申请号：US16453119

申请日：2019-06-26

Applicant: Airbus Operations S.A.S.

Inventor： Marie-Anne De Smet

IPC: B64C1/06

Abstract: A sensor is fixed on an aircraft structure by a joining system which includes at least one enclosure in which is positioned at least one transducer, at least one passage configured to allow at least one conducting element to pass through the enclosure, at least one flexible connection connecting each transducer present in the enclosure to said enclosure and at least one binder joining together the enclosure and the structure. This joining system makes it possible to limit the spread of the deformations of the structure toward the transducer or transducers and ultimately the risks of malfunction.