发明名称 Area ruled fan blade ends for turbofan jet engine.
摘要 <p>An annular casing (12) axially conducts fluid through, defining a central longitudinal axis (A). A hub (26) is rotatably supported about the axis within the casing. Rotor blades (50) are spaced about and radiate from the hub, each of the rotor blades including a part-span damper (56) circumferentially interconnecting the next adjacent rotor blade. An area rule (58) is formed in one of the hub (26) and casing (12) for reducing drag between the casing and hub caused by the part-span dampers (56) at transonic speed. The area rule comprises an annularly troughed contour (60). The troughed contour is radially aligned with the part-span dampers.</p>
申请公布号 EP0622526(A1) 申请公布日期 1994.11.02
申请号 EP19940300924 申请日期 1994.02.08
申请人 TELEFLEX INCORPORATED 发明人 ROBERTS, WILLIAM B.
分类号 F01D5/14;F01D5/20;F01D5/22;F01D11/12;(IPC1-7):F01D5/14;F01D5/24;F02C7/04 主分类号 F01D5/14
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