发明名称 Alternating Vane Asymmetry
摘要 A vane assembly for a gas turbine engine may include a plurality of vanes being arranged in vane groupings symmetrically spaced circumferentially from each other. Each vane grouping may include at least a first and a second vane. The at least first and second vanes may be spaced from each other at a first pitch. Each vane grouping may be spaced from each other at a second pitch. The first pitch may be dissimilar from the second pitch.
申请公布号 US2016146040(A1) 申请公布日期 2016.05.26
申请号 US201514933497 申请日期 2015.11.05
申请人 United Technologies Corporation 发明人 Simpson Alex J.;Dube Bryan P.;Paul John E.
分类号 F01D25/06;F04D29/32;F01D5/02;F01D9/04 主分类号 F01D25/06
代理机构 代理人
主权项 1. A vane assembly for a gas turbine engine, the vane assembly comprising: a plurality of vanes being arranged in vane groupings symmetrically spaced circumferentially from each other, each vane grouping including at least a first and a second vane, the at least first and second vanes being spaced from each other at a first pitch, each vane grouping being spaced from each other at a second pitch, the first pitch being dissimilar from the second pitch.
地址 Farmington CT US
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