发明名称 | Split spiroid | ||
摘要 | An airplane, including a wing and a spiroid wing tip coupled to an end of the wing. The wing includes a wing leading edge and a wing trailing edge. The spiroid wing-tip includes an enclosed loop, which includes a beginning section, an ending section, and a middle section. The beginning section includes a leading edge generally continuous with the wing leading edge. The ending section includes a trailing edge swept rearward with respect to the wing trailing edge. The middle section is between the beginning section and the ending section, and includes a portion extending above a chord plane of the wing. | ||
申请公布号 | US9580170(B2) | 申请公布日期 | 2017.02.28 |
申请号 | US201615256719 | 申请日期 | 2016.09.05 |
申请人 | Aviation Partners, Inc. | 发明人 | Gratzer Louis B. |
分类号 | B64C23/06 | 主分类号 | B64C23/06 |
代理机构 | Rutan & Tucker, LLP | 代理人 | Rutan & Tucker, LLP |
主权项 | 1. An airplane, comprising: a wing including a wing leading edge and a wing trailing edge; a spiroid wing tip coupled to an end of the wing, the spiroid wing tip including an enclosed loop, the enclosed loop comprising: a beginning section including a leading edge generally continuous with the wing leading edge;an ending section including a trailing edge swept rearward with respect to the wing trailing edge; anda middle section between the beginning section and the ending section, the middle section including a portion extending above a chord plane of the wing. | ||
地址 | Seattle WA US |