本发明公开了用于飞行器的机头结构和制造飞行器的方法。轮舱组件联接到机架并且形成机头起落架舱的一部分。轮舱组件包括压力舱面,该压力舱面从机架的右侧延伸到机架的左侧并且形成界定加压空间和非加压空间的压力边界的一部分。地板面板支撑件由压力舱面支撑在加压空间中。压力舱面和地板面板支撑件形成飞行器的驾驶舱地板的一部分。多个传输元件位于地板面板支撑件与压力舱面之间。多个传输元件与飞行器的至少一个高级系统相关联。
A nose structure (160) of an aircraft (100) includes an airframe (102). A wheel well assembly (194) is coupled to the airframe (102) and forms a portion of a nose landing gear bay (124). The wheel well assembly (194) includes a pressure deck (118) that extends from a right side (198) of the airframe to a left side (200) of the airframe and that forms a portion of a pressure boundary (104) delimiting a pressurized space (106) and a non-pressurized space (108). A floor-panel support (110) is supported by the pressure deck (118) in the pressurized space. The pressure deck and the floor-panel support form a portion of a flight deck floor (120) of a flight deck (122) of the aircraft (100). A plurality of transport elements (112) is located between the floor-panel support and the pressure deck. The plurality of transport elements is associated with at least one high-level system (114) of the aircraft (100).
用于飞行器的机头结构和制造飞行器的方法
2025-07-22
Patent
Electronic Resource
Chinese