The invention relates to an air inlet for gas-turbine jet engines on high-performance aircraft, which device is provided for obtaining (irrespective of the respective flight condition) the required air mass flow rate with an air catchment lip which is arranged on the lower leading edge of the air inlet such that it can pivot about a lateral axis and can be controlled by means of a functional transmitter. <IMAGE>
申请公布号
DE3835669(A1)
申请公布日期
1990.04.26
申请号
DE19883835669
申请日期
1988.10.20
申请人
MESSERSCHMITT-BOELKOW-BLOHM GMBH, 8012 OTTOBRUNN, DE