| 摘要 |
A blisk (20) for use in a turbine engine (10). The blisk (20) includes an annular disk (60), an inner row of blades (70) including a plurality of circumferentially spaced airfoils (72) integrally formed with the disk (60), an annular splitter (80) integrally formed with the inner row of blades (70) and surrounding the tips (76) of the plurality of airfoils (72) thereof, and an outer row of blades (90) including a plurality of circumferentially spaced airfoils (92) integrally formed with the splitter (80). There are more airfoils in the outer row of blades (90) than in the inner row of blades (70).
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