发明名称 SYSTEM, METHOD AND APPARATUS FOR WINDBLAST REDUCTION DURING RELEASE OR EJECTION FROM AIRCRAFT
摘要 The invention reduces the impact of flowfield forces on objects launched from high speed aircraft during flight. For example, the invention provides a solution for overcoming ejection windblast injuries to pilots and increases the probability of injury-free or low-injury ejection. The gas flow is used to rapidly create a very short duration protective "bubble" in the incoming air flow ahead of the ejecting pilot. The bubble reduces the local flow velocity and aerodynamic forces on the pilot during the injury-critical time period of ejection. The invention also is suitable for reducing the intensity of flowfield forces that act on released military aircraft ordnance, such as bombs and missiles.
申请公布号 US2009321570(A1) 申请公布日期 2009.12.31
申请号 US20080145558 申请日期 2008.06.25
申请人 LOCKHEED MARTIN CORPORATION 发明人 JONES MIKE I.;BAIRD GLENN W.;CHARLTON ERIC F.
分类号 B64D25/115;B64D1/12 主分类号 B64D25/115
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