撞车
考试(生物学)
碰撞试验
翼
计算机科学
比例(比率)
航空学
航空航天工程
工程类
程序设计语言
物理
地质学
古生物学
量子力学
作者
Ivan Colamartino,Andrea Renzo,Marco Anghileri,Fabrizio Turconi
标识
DOI:10.4050/f-0080-2024-1222
摘要
The AW609 tiltrotor features a unique high-mounted wing with rotatable nacelles positioned at the wing tips, it is capable of operating both in airplane and vertical flight mode. To achieve suited protection of the occupants during emergency landing, the wing - which is particularly stiff in order to sustain the heavy weights at the tips, where rotors, engines and transmissions are positioned - implements a controlled failure mechanism at root, so that during emergency landings it breaks and unloads the fuselage of the weight of wingbox and nacelles, thus avoiding catastrophic collapse. As the effectiveness of such mechanism was never demonstrated under impact conditions, certification agencies requested an empirical validation through experimental testing. The test was carried out July 2022 at Polytechnic of Milan, Italy; the present work details the Test activity, from its preliminary phases to the Test Day, to the analyses of its outcomes.
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