A fluid propulsion system includes a fuselage and at least one main wing having an upper surface, at least one recess in the upper surface, and at least one conduit in fluid communication with the at least one recess. At least one ejector is disposed within the at least one recess and is configured to receive compressed air via the at least one conduit.
本公开涉及一种流体推进系统,包括机身和至少一个主翼,该主翼具有上表面、上表面中的至少一个凹部以及与该至少一个凹部流体连通的至少一个导管。至少一个喷射器布置在该至少一个凹部内并且构造成经由该至少一个导管接收压缩空气。
Fluid propulsion system
流体推进系统
2024-12-27
Patent
Electronic Resource
Chinese