According to the invention, high lift leading-edge slats (13) and high lift flaps (14) are simultaneously deployed, when the speed of the aircraft is equal to and less than an AES threshold.
申请公布号
WO2007144485(A1)
申请公布日期
2007.12.21
申请号
WO2007FR00940
申请日期
2007.06.07
申请人
AIRBUS FRANCE;AIRBUS DEUTSCHLAND GMBH;DELAPLACE, FRANCK;RICHTER, MARTIN;LANG, DIETER