发明名称 Turbofan flow path trenches
摘要 <p>An integrally bladed disk (24A, 24B, 24C) includes a rim (30) and blades (34a, 34b). The blades are circumferentially spaced and extend integrally outward from the rim to define a flow path (50a, 50b, 50c) therebetween. The periphery of the rim forms a flow surface (36) and includes a trench (42a, 42b, 42c) that is disposed adjacent the blades.</p>
申请公布号 EP2372088(A2) 申请公布日期 2011.10.05
申请号 EP20100251606 申请日期 2010.09.16
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BARNES, ROLAND R.;YILMAZ, CAGDAS
分类号 F01D5/14;F01D5/34 主分类号 F01D5/14
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