发明名称 Gas turbine engine centrifugal impeller
摘要 In one embodiment a centrifugal impeller has an axis of rotation, a plurality of blades, and a plurality of pitches defined between the blades. A cavity may be formed in a back side of the impeller, opposite with at least one of the plurality of pitches. In one form the cavity may not extend below a radius determined according to a stress criteria or stress limitation.
申请公布号 US8241005(B2) 申请公布日期 2012.08.14
申请号 US20080288053 申请日期 2008.10.16
申请人 EMMERSON CALVIN W.;RESS, JR. ROBERT A.;HAMMOND STEPHEN N.;ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC. 发明人 EMMERSON CALVIN W.;RESS, JR. ROBERT A.;HAMMOND STEPHEN N.
分类号 B64C11/24;F01D5/18 主分类号 B64C11/24
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