发明名称 TURBINE EXHAUST SEAL
摘要 A turbine assembly for a turbocharger can include a C-shaped seal that includes an inner diameter, an outer diameter, an axis aligned parallel to a rotational axis of a turbine wheel, a lower lip that contacts a lower axial face of an outer surface of a shroud component along an annular portion of the shroud component, an upper lip that contacts a lower axial face of an inner surface of a turbine housing, and a wall portion that extends between the lower lip and the upper lip. Various other examples of devices, assemblies, systems, methods, etc., are also disclosed.
申请公布号 US2015003957(A1) 申请公布日期 2015.01.01
申请号 US201313927217 申请日期 2013.06.26
申请人 Honeywell International Inc. 发明人 Gerard Arnaud;Solanki Shankar Pandurangasa;Morand Nicolas;Mulot Sylvain;Eumont Vincent;Abel Francis;Sibille Stephane
分类号 F04D29/10 主分类号 F04D29/10
代理机构 代理人
主权项 1. A turbine assembly for a turbocharger comprising: a turbine wheel that comprises a base, a nose, blades, and a rotational axis that extends from the base to the nose; a turbocharger shaft operatively coupled to the turbine wheel; an annular component that comprises an opening that receives at least a portion of the turbine wheel; a shroud component that comprises an axis aligned with the rotational axis of the turbine wheel and an annular portion and a cylindrical portion that comprise an outer surface and an inner shroud surface wherein the outer surface comprises a lower axial face and an upper axial face; mounts that extend from the annular component to locations at the shroud component wherein the mounts form an axial clearance between the annular component and the shroud component; a turbine housing that comprises an axis aligned with the rotational axis of the turbine wheel, a lower axial face, an upper axial face and an inner surface that extends between the lower axial face and the upper axial face; and a C-shaped seal that comprises an inner diameter, an outer diameter, an axis aligned parallel to the rotational axis of the turbine wheel, a lower lip that contacts the lower axial face of the outer surface of the shroud component along the annular portion of the shroud component, an upper lip that contacts the lower axial face of the inner surface of the turbine housing, and a wall portion that extends between the lower lip and the upper lip.
地址 Morristown NJ US