An aircraft equipped with a distributed ductless fan propulsion system is provided. In one aspect, an aircraft includes a body defining a transverse centerline that divides the body into a first side and a second side. One or more first ductless fans are mounted to a first side of the body. The one or more first ductless fans are rotatable in a first direction. One or more second ductless fans are mounted to a second side of the body. The one or more second ductless fans are rotatable in a second direction opposite the first direction.
提供了一种配备有分布式无导管风扇推进系统的飞行器。一方面,飞行器包括限定横向中心线的主体,该横向中心线将主体分成第一侧和第二侧。一个或多个第一无导管风扇安装到主体的第一侧。一个或多个第一无导管风扇可沿第一方向旋转。一个或多个第二无导管风扇安装到主体的第二侧。一个或多个第二无导管风扇可沿与第一方向相反的第二方向旋转。
Aircraft equipped with distributed counter-rotating ductless fan propulsion system
配备有分布式反向旋转无导管风扇推进系统的飞行器
01.03.2022
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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