发明名称 Sicherungsmethode für einen Turbinenfutter
摘要 The liner segments are retained within an outer casing by a flanged connection. The system includes a T-shaped pin retained within the flanged connection radially and circumferentially by engagement with a slot formed in the outer casing, and axially be engagement with a notch formed in the adjacent liner segment. Thus the liner segment overlaps the positioning pin. In a preferred embodiment, each liner segment is notched and held in place by a pin which, in turn, is retained within a slot in the compressor casing.
申请公布号 DE69402730(D1) 申请公布日期 1997.05.28
申请号 DE1994602730 申请日期 1994.01.14
申请人 GENERAL ELECTRIC CO., SCHENECTADY, N.Y., US 发明人 WALKER, ROGER CLAYTON, MIDDLETOWN, OHIO 45044, US;GLYNN, CRISTOPHER CHARLES, HAMILTON, OHIO 45013, US
分类号 F02C7/00;F01D25/24;F02C7/20 主分类号 F02C7/00
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