公开(公告)号：US20220265187A1

公开(公告)日：2022-08-25

申请号：US17676128

申请日：2022-02-19

Applicant: DASSAULT AVIATION

Inventor： François SALMON-LEGAGNEUR ,  Valentin LIGIER ,  Cyril SAINT REQUIER

IPC: A61B5/18 ,  A61B5/00

Abstract: A system for monitoring the operational status of an aircraft crew comprises a unit for determining at least one pilot state based on first monitoring data of a high design assurance level and second monitoring data of a lower design assurance level. The determination unit comprises a first evaluation module capable of obtaining a high-level pilot state from the first data, regardless of the second data; a second evaluation module capable of determining a low-level pilot state, from at least the second data; and a consolidation module for determining a consolidated pilot state. The consolidated pilot state is obtained as a function of the high-level pilot state and the low-level pilot state.

公开(公告)号：US20200017233A1

公开(公告)日：2020-01-16

申请号：US16508268

申请日：2019-07-10

Applicant: DASSAULT AVIATION

Inventor： Cyril SAINT REQUIER ,  Gilles CONSTANT ,  Guy SCHALLER ,  Arnaud BRANTHOMME ,  Magali THOREL

IPC: B64D45/00 ,  G08G5/00

Abstract: An aircraft operational state monitoring system is provided that includes a module for acquiring a logic state of a plurality of components of the aircraft, the components belonging to airplane systems. The aircraft operational state monitoring system includes a module for determining the operability status of a plurality of macroscopic functions of the aircraft, each macroscopic function being defined independently of the components and airplane systems necessary for the performance of the macroscopic function, the operability status being determined based on logic states of the plurality of components between an operational status and at least one nonoperational status. The aircraft operational state monitoring system includes a display and at least one graphic display management assembly on the display, configured for displaying, on the display, summary indicators of the operability status of the macroscopic functions of the aircraft.

公开(公告)号：US20190164440A1

公开(公告)日：2019-05-30

申请号：US16199045

申请日：2018-11-23

Applicant: DASSAULT AVIATION

Inventor： Benjamin BRIAND ,  Cédric CARLE ,  Stéphane DRINAL ,  Cyrille GRIMALD ,  Jean-François SAEZ ,  Cyril SAINT REQUIER ,  Jean-Baptiste VALLART

IPC: G08G5/00 ,  G01C23/00

Abstract: An aircraft mission computing system includes an aircraft mission path computing engine, and a mission deck comprising a display and a display management assembly configured for displaying, on the display, at least one button for defining an operational specification of the mission. The computing engine is configured to be activated after defining the choice of operational specification using the definition button to determine at least one possible path of the aircraft based on the or each choice of defined operational specification using the or each definition button. The display management assembly is configured to display, on the display, after the activation of the computing engine, at least one outcome indicator providing mission feasibility information while respecting the or each operational specification choice.