发明名称 |
Integrated aircraft windshields and associated methods |
摘要 |
Aircraft having cab portions with integrated windshields are disclosed. The cab portion can include a rounded nose and a windshield positioned above and aft of a forward extremity of the rounded nose. A contour of the cab portion extending from the nose over the windshield aft of the nose can have a generally continuously smooth, unkinked shape. In particular embodiments, the portion of the contour corresponding to the windshield can be convex when viewed from a position external to the cab portion, and the shape of the windshield can form a portion of a conical surface.
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申请公布号 |
US2004069903(A1) |
申请公布日期 |
2004.04.15 |
申请号 |
US20030681790 |
申请日期 |
2003.10.08 |
申请人 |
RETZ KEVIN M.;VOOGT NICHOLAAS;FRIEND MICHAEL G.;HOLTORF CHRISTOPHER R.;WALLACE MANNON L.;SONES ANDREW |
发明人 |
RETZ KEVIN M.;VOOGT NICHOLAAS;FRIEND MICHAEL G.;HOLTORF CHRISTOPHER R.;WALLACE MANNON L.;SONES ANDREW |
分类号 |
B64C1/00;B64C1/06;B64C1/26;B64C25/04;B64C25/10;B64C30/00;B64D9/00;B64D11/00;B64D27/18;B64D37/04;(IPC1-7):B64C1/00 |
主分类号 |
B64C1/00 |
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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