| 发明名称 |
Non-integral platform and damper for an airfoil |
| 摘要 |
A section of a gas turbine engine includes a damper which extends from a disk between a first blade and a second blade to provide a dissipating vibratory motion energy in the form of friction heating.
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| 申请公布号 |
US8066479(B2) |
申请公布日期 |
2011.11.29 |
| 申请号 |
US20100753934 |
申请日期 |
2010.04.05 |
| 申请人 |
EL-AINI YEHIA M.;KLEIN MYRON L.;PRATT & WHITNEY ROCKETDYNE, INC. |
发明人 |
EL-AINI YEHIA M.;KLEIN MYRON L. |
| 分类号 |
F01D5/10 |
主分类号 |
F01D5/10 |
| 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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