公开(公告)号：US20210253275A1

公开(公告)日：2021-08-19

申请号：US17175905

申请日：2021-02-15

Applicant: DASSAULT AVIATION

Inventor： Virginie MARCELOT ,  Rémi BREBAN

IPC: B64F5/60 ,  B64D43/00 ,  B64D45/00 ,  G07C5/08

Abstract: A system for monitoring the operational status of an aircraft between successive missions of the aircraft includes a computer able to determine at least one operational impact measurement on at least one future mission of the aircraft related to the aircraft and/or to an aircraft equipment and/or to a consumable and/or to the aircraft crew, the operational impact measurement being determined as a function of the flight logbook and/or technical logbook data of at least one already completed mission of the aircraft and/or a context of the future mission. The system includes a display and a display manager on the display, able to display on the display at least one operational impact indicator related to the aircraft and/or to the equipment and/or to the consumable and/or to the crew, as a function of the operational impact measurement determined by the computer.

公开(公告)号：US20170217602A1

公开(公告)日：2017-08-03

申请号：US15418705

申请日：2017-01-28

Applicant: DASSAULT AVIATION

Inventor： Rémi BREBAN

IPC: B64D45/00

CPC classification number: B64D45/00 ,  G05B23/0272

Abstract: A system for assisting in a dispatch decision of an aircraft and related process are provided. The system includes a synthesis module, configured to generate at least one dispatch status for the aircraft, based on at least one defect and/or fault datum of the aircraft received from the acquisition module and at least data contained in a first database and in a second minimum equipment list database; and a display, configured to display at least one synthesis window containing at least one defect and/or fault identification indicator of the aircraft developed from the or each defect and/or fault datum, and at least one dispatch status indicator based on the dispatch status determined by the synthesis module.