发明名称 Control device for aircraft and airships
摘要 The control device has conical or wedge-shaped bodies (6) at the tail for load-dependent control, with the tip or sharp edge against the slipstream. These bodies or aerodynamic auxiliary bodies (7) attached to them have devices for control of the aircraft. These consist of variably operated shafts (10,11) and appropriately dimensioned rudder and elevator (8,9). The control bodies, rudders and elevators are made of stainless or other steel sheet, aluminium, plastic and a durable adhesive.
申请公布号 DE19543302(A1) 申请公布日期 1997.05.22
申请号 DE19951043302 申请日期 1995.11.21
申请人 SCHUBERT, WERNER, DR.MED., 45468 MUELHEIM, DE 发明人 SCHUBERT, WERNER, DR.MED., 45468 MUELHEIM, DE
分类号 B64C9/00;B64C9/12;(IPC1-7):B64C9/00 主分类号 B64C9/00
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