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公开(公告)号：US11312509B2
公开(公告)日：2022-04-26
申请号：US16785890
申请日：2020-02-10
Applicant: Airbus Operations S.A.S.
Inventor： Hervé Lasserre , Xavier Alquier , Aymeric Plo
Abstract: A mobile machine includes a fuselage having at least one door, inside which is located a unit for processing measurements taken by at least one measurement device installed outside said fuselage. The system for communication between the processing unit and the measurement device includes a flex circuit that is affixed at least partially flat in the door corner between the door and the rim of the opening formed in the fuselage with which the door is associated and one of the ends, the internal end, of which is located inside the fuselage and the other, external, end of which is located outside. Since the flex circuit makes it possible to pass through the wall of the fuselage via the opening for doors, the need to make substantial modifications to the aircraft is avoided.
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2.发明申请公开(公告)号：US20200269996A1
公开(公告)日：2020-08-27
申请号：US16785890
申请日：2020-02-10
Applicant: Airbus Operations S.A.S.
Inventor： Hervé Lasserre , Xavier Alquier , Aymeric Plo
Abstract: A mobile machine includes a fuselage having at least one door, inside which is located a unit for processing measurements taken by at least one measurement device installed outside said fuselage. The system for communication between the processing unit and the measurement device includes a flex circuit that is affixed at least partially flat in the door corner between the door and the rim of the opening formed in the fuselage with which the door is associated and one of the ends, the internal end, of which is located inside the fuselage and the other, external, end of which is located outside. Since the flex circuit makes it possible to pass through the wall of the fuselage via the opening for doors, the need to make substantial modifications to the aircraft is avoided.
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公开(公告)号：US20180366982A1
公开(公告)日：2018-12-20
申请号：US16005322
申请日：2018-06-11
Applicant: Airbus Operations (S.A.S.)
Inventor： Aymeric Plo , Xavier Alquier
Abstract: A portable measuring system including an electronic acquisition device, at least one sensor linked to the acquisition device, and a power supply module. The power supply module includes at least one electric torus to be mounted on electrical wiring in order to generate a current by induction, and an electric power management device that delivers a voltage-stabilized current in order to power the acquisition device. An assembly includes an external data centralizer. Such a system or assembly is easy to install, has potentially unlimited autonomy, and is particularly well suited to use in an aircraft.
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