公开(公告)号：US20160023749A1

公开(公告)日：2016-01-28

申请号：US14807014

申请日：2015-07-23

Applicant: Airbus Operations S.A.S.

Inventor： Mathieu CARTON ,  Pierre DEBUSSCHERE ,  David CHABE

IPC: B64C13/00 ,  B64D39/00 ,  G05D1/08

CPC classification number: B64C13/00 ,  B64D39/00 ,  G05D1/0607 ,  G05D1/0808

Abstract: The system comprises at least one lift generator element that is able to modify directly the lift of the aircraft and means for defining a deflection instruction upon actuation by a pilot of the aircraft of a control column of the aircraft generating a vertical load factor control value and applying it to an elevator and simultaneously defining a command instruction and applying it to the lift generator element to generate a direct lift.

Abstract translation: 该系统包括至少一个提升发电机元件，该升降机发电机元件能够直接修改飞行器的升降机，以及用于在飞行器的飞行员致动之后定义偏转指令的装置，该飞行器的飞行器产生垂直载荷系数控制值， 将其施加到电梯并同时定义命令指令并将其施加到电梯发电机元件以产生直接电梯。