发明名称 |
Cabin air compressor diffuser vane drive ring |
摘要 |
A cabin air compressor drive ring includes an outer ring defining an axis, an inner ring co-axial with the outer ring, a plurality of webbings connecting the inner ring to the outer ring, and a plurality of vane engagement pins axially protruding from the outer ring. The vane engagement pins are spaced circumferentially about the outer ring, and the inner ring includes a drive ring bearing interface. |
申请公布号 |
US9341193(B2) |
申请公布日期 |
2016.05.17 |
申请号 |
US201313856504 |
申请日期 |
2013.04.04 |
申请人 |
Hamilton Sundstrand Corporation |
发明人 |
Beers Craig M.;Rosen Seth E. |
分类号 |
F01D17/12;F04D29/46;F16C35/00 |
主分类号 |
F01D17/12 |
代理机构 |
Carlson, Gaskey & Olds, P.C. |
代理人 |
Carlson, Gaskey & Olds, P.C. |
主权项 |
1. A cabin air compressor drive ring comprising:
an outer ring defining an axis; an inner ring co-axial with the outer ring said inner ring defining a bearing interface track operable to mount said drive ring to a cabin air compressor bearing, said bearing interface track comprising a first and second facing wall, each of said first and second facing walls are perpendicular to the axis, and a bearing interface base surface, said bearing interface base surface is parallel to the axis; a plurality of webbings connecting the inner ring to the outer ring; a plurality of vane engagement pins axially protruding from the outer ring, wherein said vane engagement pins are spaced circumferentially about the outer ring; said inner ring comprises a drive ring bearing interface; and a first clearance cut protruding radially into said bearing interface base surface and axially into a first of said facing walls at a joint between said first of said facing walls and said bearing interface base surface. |
地址 |
Windsor Locks CT US |