The parafoil aircraft has a mechanism for increasing lift on landing, high surface loading, a landing frame (7), an automatic device (8) for measuring distance (9) to the ground and a controller (5) or triggering the lift enhancing mechanism at a defined ground separation (12). The parafoil (2) has a surface loading of more than 20 daN/m2. The landing frame is skid shaped and its base surface has track guides. The ground distance measurement device is mounted on the landing frame.
申请公布号
DE19634017(A1)
申请公布日期
1998.02.26
申请号
DE19961034017
申请日期
1996.08.23
申请人
DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT, 81663 MUENCHEN, DE
发明人
RIEGER, ULRICH, DIPL.-ING., 83620 FELDKIRCHEN-WESTERHAM, DE