发明名称 Tailplane for commercial aircraft
摘要 The upper contour line and both lateral contour lines of the unit each have an inflection point, and the centre box section (23) of the elevator unit penetrates the tail unit in the region of the ribs (20,22) which carry the rudder unit. A transversely oriented tubular strut is located on the side of the tail and accommodates a swivel element together with the centre box section. The swivel element is mounted on plain or roller bearings inside the strut.
申请公布号 DE4404810(A1) 申请公布日期 1995.08.17
申请号 DE19944404810 申请日期 1994.02.16
申请人 DAIMLER-BENZ AEROSPACE AIRBUS GMBH, 21129 HAMBURG, DE 发明人 BUTTKEREIT, VOLKER, DIPL.-ING., 20251 HAMBURG, DE;HEMPEL, JOACHIM, DIPL.-ING., 22559 HAMBURG, DE;KIEKEBUSCH, BURKHARD, DIPL.-ING., 21698 HARSEFELD, DE;SCHOENE, WOLFRAM, DIPL.-ING., 21614 BUXTEHUDE, DE
分类号 B64C1/00;B64C1/26;(IPC1-7):B64C1/00 主分类号 B64C1/00
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