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 |