发明名称 |
MITIGATION OF SURFACE DISCONTINUITIES BETWEEN FLIGHT CONTROL SURFACES AND AN AIRFRAME OF AN AIRCRAFT |
摘要 |
Embodiments provide a transitional element that bridges a gap between an edge of a flight control surface and an edge of a non-movable portion of an airframe. In one embodiment, a transitional element bridges a gap between an edge of a flight control surface and an edge of a non-movable portion of an airframe. The transitional element includes a plurality of ribs that span the gap. Each of the plurality of ribs has a contour that corresponds to the flight control surface and is configured to pivot a portion of a rotated angle of the flight control surface to generate a transitional surface across the gap. |
申请公布号 |
CA2935181(A1) |
申请公布日期 |
2017.02.20 |
申请号 |
CA20162935181 |
申请日期 |
2016.07.05 |
申请人 |
THE BOEING COMPANY |
发明人 |
LOYET, JESSICA;PITT, DALE M. |
分类号 |
B64C9/00;B64C3/18;B64C3/38;B64C9/02 |
主分类号 |
B64C9/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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