发明名称 HIGH STRENGTH TO WEIGHT HORIZONTAL AND VERTICAL AIRCRAFT STABILIZER
摘要 A minimum weight horizontal and vertical stabilizer (188) which a primary torque box is formed within the skins (202, 204) and extends transversely from the most forwardly spars (190, 212) to the most rearwardly spar (196) to occupy spaces between all of the spars (190, 212, 192, 194, 196).
申请公布号 WO8501489(A1) 申请公布日期 1985.04.11
申请号 WO1983US01551 申请日期 1983.09.29
申请人 THE BOEING COMPANY 发明人 HAMM, ROBERT, ALTON;SOUDAK, URI
分类号 B64C3/20;(IPC1-7):B64C3/20 主分类号 B64C3/20
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