发明名称 Blade damper and method for making same
摘要 A turbine engine blade damper (50) for damping vibrations of blades (12) in a turbine engine. The blade damper (50) includes an elongate body (52) extending between a forward end (54) and a rearward end (56) opposite the forward end (54). The body (52) is sized and shaped for receipt within a gap formed between adjacent platforms (22) of the blades (12) so the body (52) frictionally engages the adjacent platforms (22) to dampen vibrations of the blades (12) and to prevent air from passing through the corresponding gap during engine operation. The damper (50) also includes a retainer (70) mounted on at least one of the forward and rearward ends (56) of the body (52). The retainer (70) is sized and shaped for receipt within a recess (72) formed in at least one of the adjacent blades (12) to hold the body (52) between the blades (12). The retainer (70) is sized and shaped to prevent air from passing between the blades (12) and the retainer (70) during engine operation. <IMAGE>
申请公布号 EP1167691(B1) 申请公布日期 2005.08.10
申请号 EP20010303645 申请日期 2001.04.20
申请人 GENERAL ELECTRIC COMPANY 发明人 GROVER, GARTH KNEELAND;LIOTTA, GARY CHARLES
分类号 F01D5/16;F01D5/10;F01D5/26;F01D5/32;F01D11/00;F01D25/00;F01D25/06 主分类号 F01D5/16
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