发明名称 遠心圧縮機のディフューザのベーンレット
摘要 A system, in certain embodiments, includes a centrifugal compressor diffuser including a flow path having a first surface and a second surface defining opposite axial sides of the flow path. The centrifugal compressor diffuser also includes multiple vanes extending from the first surface to the second surface of the flow path. A first profile of each vane varies along an axial direction. The centrifugal compressor diffuser further includes multiple vanelets extending from the first surface toward the second surface in the axial direction. A first axial extent of each vanelet is less than a second axial extent of the flow path. In addition, a second profile of each vanelet varies along the axial direction and/or the vanelets form a non-periodic pattern around a circumference of the flow path.
申请公布号 JP5727519(B2) 申请公布日期 2015.06.03
申请号 JP20120551965 申请日期 2010.11.30
申请人 キャメロン インターナショナル コーポレイション 发明人 チェスター ブイ.スウィアテック;ミカイル グリゴリーブ;ジェイムズ ヒット;ノエル ブレア,ジュニア
分类号 F04D29/44 主分类号 F04D29/44
代理机构 代理人
主权项
地址