A ducted aircraft (100) and a duct (10) thereof, the ducted aircraft (100) comprising the duct (10), a fuselage (20) and a power assembly (30), the duct (10) comprising at least two duct monomers (11), the duct monomers (11) having duct holes (111), the fuselage (20) being connected to the duct (10), the power assembly (30) being connected to the fuselage (20), the power assembly (30) being at least partially located within the duct holes (111), the power assembly (30) cooperating with the duct (10) to provide aerodynamic lift, at least part of each duct single body (11) is of a hollow structure. According to the ducted aircraft (100), the weight of the duct (10) can be effectively reduced, the force effect of the system is improved, and the endurance time is prolonged.
一种涵道飞行器(100)及其涵道(10),其中,涵道飞行器(100)包括涵道(10)、机身(20)和动力组件(30),涵道(10)包括至少两个涵道单体(11),涵道单体(11)具有涵道孔(111),机身(20)与涵道(10)连接,动力组件(30)与机身(20)连接,动力组件(30)至少部分位于涵道孔(111)内,动力组件(30)与涵道(10)配合提供气动升力,其中,涵道单体(11)至少部分为中空结构。提出的涵道飞行器(100),可以有效降低涵道(10)的重量,提高系统的力效,以延长续航时间。
Ducted aircraft and duct thereof
涵道飞行器及其涵道
2025-04-01
Patent
Electronic Resource
Chinese
IPC: | B64U |