发明名称 |
VTOL micro-aircraft |
摘要 |
VTOL micro-aircraft comprising a first and a second ducted rotor mutually aligned and distanced according to a common axis and whose propellers are driven in rotation in mutually opposite directions. Between the two ducted rotors are positioned a fuselage and a wing system formed by wing profiles forming an X or an H configuration and provided with control flaps.
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申请公布号 |
US2004129833(A1) |
申请公布日期 |
2004.07.08 |
申请号 |
US20030626697 |
申请日期 |
2003.07.25 |
申请人 |
C.R.F. SOCIETA CONSORTILE PER AZIONI |
发明人 |
PERLO PIERO;BOLLEA DENIS;FINIZIO ROBERTO;CARVIGNESE COSIMO;BALOCCO ELENA |
分类号 |
B64C27/20;B64C29/02;B64C39/02;(IPC1-7):B64C39/00 |
主分类号 |
B64C27/20 |
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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