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Aircraft has front longitudinal section to receive cockpit area, rear longitudinal section to receive rear body section and central longitudinal section to receive intermediate region of body between cockpit area and rear body section

机译:飞机的前纵向部分用于接收驾驶舱区域,后纵向部分用于接收后机身部分,中央纵向部分用于接收在驾驶舱区域和后机身部分之间的机身中间区域

摘要

The aircraft has a body (10), made of metallic materials and composite materials, is provided with wings (30), where multiple openings (21,22,23,24,25,26,27) in the body. Coupling points (31,41,51) are provided for wings on the body, where the body is divided into three longitudinal sections. The front longitudinal section receives a cockpit area (11), where the rear longitudinal section receives a rear body section (13) of the body. The central longitudinal section receives an intermediate region (12) of the body between the cockpit area and the rear body section.
机译:飞机具有由金属材料和复合材料制成的机体(10),其具有机翼(30),机体内有多个开口(21、22、23、24、25、26、27)。机体上的机翼设有连接点(31、41、51),其中机体分为三个纵向部分。前纵向部分容纳驾驶舱区域(11),后纵向部分容纳车身的后车身部分(13)。中央纵向部分在驾驶舱区域和后部车身部分之间接收车身的中间区域(12)。

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