公开(公告)号：US20250115351A1

公开(公告)日：2025-04-10

申请号：US18987088

申请日：2024-12-19

Applicant: DASSAULT AVIATION

Inventor： Jérôme CAPPELLE ,  François PINEAU ,  William FAYSSE

IPC: B64C13/18 ,  B64C13/04

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.

公开(公告)号：US20220219809A1

公开(公告)日：2022-07-14

申请号：US17574677

申请日：2022-01-13

Applicant: DASSAULT AVIATION

Inventor： Jérôme CAPPELLE ,  François PINEAU ,  William FAYSSE

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

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.