发明名称 AIRCRAFT SPIRALLING MECHANISM
摘要 <p>An aircraft (1), e.g. an aeroplane or missile, has fins (6, 17) attached to tube (3) encircling the aircraft fuselage. When fins (6, 17) are pivoted, a predetermined difference in size or pitch of fin (6) relative to fin (17) will cause an aerodynamic imbalance, inducing tube (3) to rotate. This rotation produces a constantly revolving transverse force on the fuselage which induces the craft to automatically follow a spiralling flight path thus evading being hit by anti-aircraft weapons.</p>
申请公布号 WO2002102660(A1) 申请公布日期 2002.12.27
申请号 AU2002000808 申请日期 2002.06.20
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