发明名称 Sealing ring for gas turbine engines
摘要 A sealing ring for controlling gas leakage through the annular space between two rotating concentric members; for example engine shafts. The sealing ring 20 has a generally trapezoidal cross section and an overlapping scarf joint. The sealing ring improves sealing by providing continuous lines of contact at edges between inner and outer coaxial shaft members.
申请公布号 US5344162(A) 申请公布日期 1994.09.06
申请号 US19930007962 申请日期 1993.01.22
申请人 ROLLS-ROYCE PLC 发明人 KERNON, JOHN D.;KNIGHT, MARK J.
分类号 F01D11/00;F02C7/28;F16J9/14;F16J15/16;F16J15/44;(IPC1-7):F16J15/42 主分类号 F01D11/00
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