发明名称 |
Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity |
摘要 |
Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity are provided. In this regard, a representative turbine stage for a gas turbine engine includes a first set of rotatable blades operative to be positioned downstream of and adjacent to a first set of vanes, a number of blades of the first set of blades being less than a number of vanes of the first set of vanes.
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申请公布号 |
US7984607(B2) |
申请公布日期 |
2011.07.26 |
申请号 |
US20070850787 |
申请日期 |
2007.09.06 |
申请人 |
UNITED TECHNOLOGIES CORP. |
发明人 |
SHARMA OM P.;BLAIR MICHAEL F. |
分类号 |
F02K3/00 |
主分类号 |
F02K3/00 |
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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