发明名称 |
Nedslipbart forseglingssystem |
摘要 |
A gas turbine engine abradeable seal system is provided comprising a seal assembly and a cooperating interacting turbine blade. The turbine blade has a tip portion containing cubic boron nitride abrasive particles and the seal assembly has a superalloy substrate with a bond coat thereon having a surface roughness of at least 300 RA and a porous ceramic abradeable seal material on the bond coat having a porosity of from 5 to 15 volume %. |
申请公布号 |
NO20035427(D0) |
申请公布日期 |
2003.12.05 |
申请号 |
NO20030005427 |
申请日期 |
2003.12.05 |
申请人 |
CHROMALLOY GAS TURBINE CORP |
发明人 |
HOWARD, PETER;SHANKAR, RAVI |
分类号 |
F01D5/28;C23C28/00;F01D11/12;F02C7/00;F02C7/28;F16K5/02 |
主分类号 |
F01D5/28 |
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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