论文部分内容阅读
机体结构和机载设备“欧洲鲫”是一种三座悬臂式下单翼飞机,全金属半硬壳结构。机翼略带上反角,翼面积26.8平方米。机翼中段为双梁结构,与机身结为一体,并装有主起落架和挂弹架。机翼外段采用前文所述的“米斯塔尔”结构。每侧机翼后缘装有1.93平方米的副翼舵面和1.65平方米的开裂式襟翼(手动操纵,最大可偏转45°)。机身横截面为卵形,采用隔框加桁条结构,中部有斜撑加固。机身隔框由硬铝板制成。机身蒙皮为光滑的硬铝板,受力部分的蒙皮靠内侧波纹板加强。飞行员和
Body structure and airborne equipment “European crucian carp ” is a three cantilever monoplane, all-metal semi-hard shell structure. The wing slightly dorsal angle, wing area of 26.8 square meters. The middle wing is a double-beam structure that is integrated with the fuselage and equipped with a main landing gear and a hanger. The wing outer segment uses the “Mystall” structure described earlier. 1.93 square meters of aileron rudder and 1.65 square meters of dehiscent flaps (manual override, maximum deflectable 45 °) on each wing’s trailing edge. The cross section of the fuselage is oval, using the frame plus stringer structure, the middle of the bracing reinforcement. The fuselage frame is made of hard aluminum. The fuselage skin is a smooth hard aluminum, reinforced by the inner corrugated part of the force part. Pilot and