发明名称 Hybrid aircraft e.g. helicopter, has two wings arranged laterally at casing and engaging together with casing by rotating around axis using rotating mechanism, rotation symmetric and mirror symmetrical configuration
摘要 <p>The aircraft has a rotationally symmetric, lenticular casing (1) with a volume in which air gas is filled. Two wings (3.1, 3.2) having a symmetrical profile are arranged laterally at the casing. The wings engage together with the casing by rotating around an axis using a rotating mechanism (5), a rotation symmetric and mirror symmetrical configuration, where the mechanism is provided in a middle of the casing.</p>
申请公布号 DE102006028885(A1) 申请公布日期 2007.03.22
申请号 DE20061028885 申请日期 2006.06.21
申请人 SINGER, CSABA 发明人
分类号 B64B1/20;B64C3/50;B64C9/36;B64C27/18;B64C27/24;B64C29/00 主分类号 B64B1/20
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