发明名称 |
TURBINE BLADE SEAL ASSEMBLY |
摘要 |
A seal assembly for an axial flow gas turbine engine includes a rotatable component having a radially extending mate face, a seal slot formed in the mate face, and a seal member slidably disposed in the seal slot. The seal slot includes a radially outer wall and an opposing radially inner wall extending into the component in a circumferential direction from the mate face. The radially outer wall is angled radially inwardly from the mate face toward an inner end portion of the seal slot. Rotation of the seal assembly during operation of the engine produces a centrifugal force on the seal member to effect movement of the seal member in the circumferential direction out of the seal slot. |
申请公布号 |
US2012049467(A1) |
申请公布日期 |
2012.03.01 |
申请号 |
US201113151363 |
申请日期 |
2011.06.02 |
申请人 |
STEWART JEFFREY B.;RUDOLPH RONALD J.;AFANASIEV GENNADIY |
发明人 |
STEWART JEFFREY B.;RUDOLPH RONALD J.;AFANASIEV GENNADIY |
分类号 |
F16J15/02 |
主分类号 |
F16J15/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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