公开(公告)号：US20170183085A1

公开(公告)日：2017-06-29

申请号：US15385966

申请日：2016-12-21

Applicant: DASSAULT AVIATION

Inventor： Arnaud BRANTHOMME ,  Guy SCHALLER ,  Lorianne BOUTZEN

IPC: B64C17/10 ,  B64C13/16 ,  G06F3/14 ,  B64C13/04

CPC classification number: B64C17/10 ,  B64C13/042 ,  B64C13/16 ,  B64D37/00 ,  B64D43/00 ,  F02C9/26 ,  G06F3/14

Abstract: A system for controlling and monitoring pieces of equipment of an aircraft, each piece of equipment being able to be switched between two logic activation state values, comprising a man-machine interface, a module for configuration of a functional activation state of a function able to be performed on at least pieces of equipment of a system of the aircraft, the functional activation state being configurable between an active state and an inactive state, the configuration module being adapted for detecting an action of selection of a functional activation state of the function by an operator, and a control and monitoring module configured for determining a logic activation state of each of the pieces of equipment of the system, so that, when each of the pieces of equipment is in the determined logic activation state, the function is in the selected functional activation state.