发明名称 Lift spoiler for parked aircraft
摘要 A lift spoiler for use on the wings of parked aircraft to reduce lift forces produces by the aircraft wings and that are produced during storms and high wind speed conditions. The lift spoiler includes a generally rectangular spoiler panel that is supported relative to the wing upper surface by a pair of holders. The holders include suction-cup-type attachments for securely attaching the lift spoiler relative to the wing upper surface to deflect airflow over the wing surface and thereby reduce the lift effect of the airflow that acts on the wing to otherwise lift the aircraft during high wind speed conditions and cause possible damage to the aircraft while it is parked.
申请公布号 US2008116321(A1) 申请公布日期 2008.05.22
申请号 US20060602592 申请日期 2006.11.22
申请人 TUINDER TIMMY 发明人 TUINDER TIMMY
分类号 B64C3/58 主分类号 B64C3/58
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