The invention relates to an aircraft flow device and an aircraft comprising the aircraft flow device. The aircraft flow device comprising a rib bounded by and fixedly attached to an outer skin, wherein the outer skin and the rib are configured to plastically deform when the outer skin is subjected to an impact load in a leading edge region of the airflow body, wherein the stiffness of the outer skin is greater than or equal to the stiffness of the rib when deformed by the impact load.
本申请涉及一种飞行器流装置和一种包括该飞行器流装置的飞行器。该飞行器流装置包括翼肋,该翼肋由外部蒙皮限定边界并且固定地附接至外部蒙皮,其中,外部蒙皮和翼肋构造成当外部蒙皮在空气流装置的前缘区域中受到冲击载荷时塑性地变形,其中,当由于冲击载荷而变形时外部蒙皮的刚度大于或等于翼肋的刚度。
Aircraft flow device and aircraft comprising aircraft flow device
飞行器流装置和包括该飞行器流装置的飞行器
2020-07-31
Patent
Electronic Resource
Chinese