Verfahren und Vorrichtung für die Betriebssteuerung der Motoren eines Luftfahrzeugs während der Startphase

Details

Veröffentlichungs-Nr.

EP2508735

Aktenzeichen

EP12162425

Anmeldetag

30. März 2012

Veröffentlichung

6. Januar 2016

Erteilung

6. Januar 2016

Rechtsraum

EP

IPC

F02C9/00B64D31/12G05D1/02

Abstract

The method involves measuring current values (N1c1-N1c4) of driving parameters associated to external engines (M1, M4) and internal engines (M2, M3). Detection is made whether difference between the current values of the driving parameters associated with each engine and a determined intermediate setpoint value (N1x) is equal to a predefined threshold. Operating speed of the engines is raised to determined take-off speed such that the driving parameters associated with the engine reach a takeoff setpoint value when the difference is equal to the predefined threshold. An independent claim is also included for a device for controlling operating speed of engines of an aircraft during take-off phase.

Anmelder

Firma

Airbus Opérations SAS

Land

🇫🇷 Frankreich

Fachgebiete