发明名称 FACE SEAL FOR GAS TURBINE ENGINE
摘要 A face seal for a gas turbine engine comprises a seal body that has a contact face to engage a rotating surface. The contact face is defined as an area extending radially between an inner diameter of the seal body and an outer diameter of the seal body at one seal end providing a radial width. The radial width is between greater than 0.15 inch (3.81 mm).
申请公布号 US2009230628(A1) 申请公布日期 2009.09.17
申请号 US20090472553 申请日期 2009.05.27
申请人 DOBEK LOUIS J;SONOKAWA MASAYOSHI;SHAFFER HAROLD K;STORY MARK 发明人 DOBEK LOUIS J.;SONOKAWA MASAYOSHI;SHAFFER HAROLD K.;STORY MARK
分类号 F16J15/34 主分类号 F16J15/34
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