发明名称 AIRCRAFT BODY MOUNTED ENERGY ABSORBING RUB STRIP
摘要 An energy absorbing rub strip having a core material and a fairing positioned over the core material. The core material may be configured to buckle under the application of a predetermined amount of force and the fairing may be configured to be attached to a fuselage of an aircraft. The fairing may be made out of an abrasive-resistant material such as titanium or a nickel-based metal. The core material may be comprised of an aluminum honeycomb. The core material may be comprised of a dual density material. The length of the rub strip may extend beyond potential contact points on the fuselage during landing and takeoff. Upon a ground contact event, the thickness of deformed/buckled core material may be measured to determine if the ground contact event may have caused structural damage to the aircraft.
申请公布号 US2015336654(A1) 申请公布日期 2015.11.26
申请号 US201414249576 申请日期 2014.04.10
申请人 The Boeing Company 发明人 Cottet Justin D;Kepner Roger S;Drake Michael L
分类号 B64C1/06 主分类号 B64C1/06
代理机构 代理人
主权项 1. An energy absorbing rub strip, the rub strip comprising: a core material, the core material being configured to buckle under an application of a predetermined amount of force; and a fairing positioned over the core material, the fairing being configured to be attached to a fuselage of an aircraft.
地址 Seal Beach CA US