发明名称 Split Spiroid
摘要 The spiroid wing tip according to embodiments of the invention including a continuous segmental assembly having a closed loop frontal profile comprising a lower near vertical segment, a horizontal segment, a vertical segment, a second horizontal upper segment, and a near vertical segment. Accordingly to some embodiments of the invention, the spiroid profile is lowered with respect to the wing chord plane, such that a portion of the spiroid wing tip extends below the wing chord plane.
申请公布号 US2012312929(A1) 申请公布日期 2012.12.13
申请号 US201213493915 申请日期 2012.06.11
申请人 GRATZER LOUIS B. 发明人 GRATZER LOUIS B.
分类号 B64C5/08 主分类号 B64C5/08
代理机构 代理人
主权项
地址