发明名称 Aircraft having a canard wing configuration
摘要 In the case of an aircraft having a canard wing configuration, the canard wing which is arranged at a distance from the main wing is arranged over a shaft. This shaft runs in the longitudinal axis of the aircraft and originates from the tip of the main wing (mainplane), the canard wing being arranged in the sense of increasing the wing span. <IMAGE>
申请公布号 DE3133957(A1) 申请公布日期 1983.03.10
申请号 DE19813133957 申请日期 1981.08.27
申请人 VEREINIGTE FLUGTECHNISCHE WERKE GMBH 发明人 HANSEN,HEINZ,DIPL.ING.
分类号 B64C5/08;B64C39/12;(IPC1-7):B64C5/08 主分类号 B64C5/08
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