公开(公告)号：US12067811B2

公开(公告)日：2024-08-20

申请号：US17574644

申请日：2022-01-13

Applicant: DASSAULT AVIATION

Inventor： Patrick Dignimont ,  Jérôme Cappelle ,  Serge Bruillot

IPC: G07C5/00 ,  B64D45/00 ,  B64D47/00 ,  G07C5/08

CPC classification number: G07C5/008 ,  B64D45/00 ,  B64D47/00 ,  G07C5/0841 ,  B64D2045/0085

Abstract: A system for secure transfer of digital aircraft data comprising redundant data producer systems includes a first data producer, capable of producing first data, at successive moments, and a second data producer, redundant to the first system. The second data producer is capable of producing an integrity check result relating at least to second data which it produces in a manner redundant to the first data, the integrity check result being transmitted to a data consumer. The data consumer is capable of retrieving the first data and the integrity check result produced by the second system, to produce a new integrity check result from the first data and compare the new integrity check result with the integrity check result produced by the second system.

公开(公告)号：US12252236B2

公开(公告)日：2025-03-18

申请号：US17574677

申请日：2022-01-13

Applicant: DASSAULT AVIATION

Inventor： Jérôme Cappelle ,  François Pineau ,  William Faysse

IPC: B64C13/50 ,  B64D31/04 ,  B64D31/06

Abstract: A system for piloting an aircraft includes a throttle, a flight parameter sensor system, and an engine calculator controlling thrust parameters of an engine of the aircraft. The piloting system includes a flight control unit connected to the engine calculator, the sensors and the throttle. The flight control unit generates a thrust control vector from a flight control law and sends a digital signal including the generated thrust control vector to the engine calculator. The engine calculator controlling said thrust parameters of the engine depending on the generated thrust control vector received.