| 摘要 |
A turbofan engine (10) includes a fan (14) mounted to a fan frame (32) inside a fan nacelle (30). A booster compressor (16) is joined to the fan (14) inboard a flow splitter (34). A booster bleed system (54) is disposed inside the splitter (34), and includes an inlet (58) at the compressor outlet (52), and an outlet (60) joined to the bypass duct (36) following the fan (14). |
