Compressor assembly for turbocharger burst containment
A compressor assembly is disclosed. The compressor assembly may have a compressor housing and a compressor impeller disposed within the compressor housing. The compressor impeller may have a hub extending from a hub front end to a hub rear end and an exducer blade disposed on the hub adjacent the hub rear end. The compressor impeller may further include a hub extension extending outward from the hub rear end. The compressor assembly may also have an impeller cap disposed on the hub extension. Further, the compressor assembly may have a windage seal disposed on the impeller cap. The windage seal may be separated from a blade rear surface by an axial gap. In addition, the compressor assembly may have a compressor diffuser disposed within the compressor housing. The compressor diffuser may have a diffuser inner surface separated from an outer rim of the exducer blade by a radial gap.
1. A compressor assembly, comprising:
a compressor housing;
a compressor impeller disposed within the compressor housing, the compressor impeller including:
a hub extending from a hub front end to a hub rear end;
an exducer blade disposed on the hub adjacent the hub rear end, the exducer blade having a blade rear surface; and
a hub extension extending outward from the hub rear end;
an impeller cap disposed on the hub extension;
a windage seal including:
a windage seal bore,
an outer surface of the impeller cap being disposed within the windage seal bore,
a seal hub,
a seal web extending generally radially from the seal hub, and
a seal shield extending generally axially towards the blade rear surface from a radially outermost portion of the seal web, the seal shield including a shield front face disposed opposite to and axially spaced apart from the blade rear surface by a first axial distance; and
a compressor diffuser disposed within the compressor housing, the compressor diffuser having a diffuser inner surface separated from an outer rim of the exducer blade by a radial gap, wherein
the exducer blade has a balancing ring projecting outwards from the blade rear surface, the balancing ring having an balancing ring end,
the seal shield has an inner radius larger than a radius of the balancing ring, and
the first axial distance is smaller than a second axial distance between the balancing ring end and the blade rear surface.
2. The compressor assembly of claim 1 , wherein the compressor housing includes:
a compressor outer volute configured to be connected to a bearing housing;
a compressor inner volute; and
an inlet flow guide attached to the compressor inner volute and the compressor outer volute and configured to direct air into the compressor impeller.
3. The compressor assembly of claim 2 , wherein
the compressor outer volute includes an outer volute rear wall,
the compressor inner volute includes an inner volute rear wall, and
the compressor diffuser is disposed between the outer volute rear wall and the inner volute rear wall.
4. The compressor assembly of claim 3 , wherein
the radial gap is a first radial gap,
the compressor outer volute includes an extension having an inner surface, and
the compressor diffuser is separated from the inner surface by a second radial gap.
5. The compressor assembly of claim 3 , wherein the compressor diffuser is centered on the compressor outer volute by a plurality of alignment pins disposed circumferentially relative to a rotational axis of the compressor assembly.
6. The compressor assembly of claim 1 , wherein
the seal web and the seal shield have an outer surface, and
the windage seal includes a groove disposed on the outer surface.
7. The compressor assembly of claim 6 , wherein
the seal web has a web front face and a web rear face opposite to the web front face,
the seal shield extends outwards from the web front face, and
the groove is disposed nearer the web front face as compared to the web rear face.
8. A turbocharger, comprising:
a turbine housing;
a turbine wheel disposed within the turbine housing and configured to be driven by exhaust received from an engine;
a compressor housing;
a compressor impeller disposed within the compressor housing, the compressor impeller including:
a hub extending from a hub front end to a hub rear end;
an exducer blade disposed on the hub adjacent the hub rear end, the exducer blade having a blade rear surface; and
a hub extension extending outward from the hub rear end;
an impeller cap disposed on the hub extension;
a windage seal including:
a windage seal bore,
an outer surface of the impeller cap being disposed within the windage seal bore,
a seal hub,
a seal web extending generally radially from the seal hub, and
a seal shield extending generally axially towards the blade rear surface from a radially outermost portion of the seal web, the seal shield including a shield front face disposed opposite to and axially spaced apart from the blade rear surface by a first axial distance;
a compressor diffuser disposed within the compressor housing, the compressor diffuser having a diffuser inner surface separated from an outer rim of the exducer blade by a radial gap; and
a shaft connecting the impeller cap and the turbine wheel, wherein
the exducer blade has a balancing ring projecting outwards from the blade rear surface, the balancing ring having an balancing ring end,
the seal shield has an inner radius larger than a radius of the balancing ring, and
the first axial distance is smaller than a second axial distance between the balancing ring end and the blade rear surface.
9. The turbocharger of claim 8 , wherein the compressor housing includes:
a compressor outer volute configured to be connected to a bearing housing;
a compressor inner volute; and
an inlet flow guide attached to the compressor inner volute and the compressor outer volute and configured to direct air into the compressor impeller.
10. The turbocharger of claim 9 , wherein
the compressor outer volute includes an outer volute rear wall,
the compressor inner volute includes an inner volute rear wall, and
the compressor diffuser is disposed between the outer volute rear wall and the inner volute rear wall.
11. The turbocharger of claim 10 , wherein
the radial gap is a first radial gap,
the compressor outer volute includes an extension having an inner surface, and
the compressor diffuser is separated from the inner surface by a second radial gap.
12. The turbocharger of claim 10 , wherein the compressor diffuser is centered on the compressor outer volute by a plurality of alignment pins disposed circumferentially relative to a rotational axis of the turbocharger.
13. The turbocharger of claim 8 , wherein
the seal web and the seal shield have an outer surface, and
the windage seal includes a groove disposed on the outer surface.
14. The turbocharger of claim 13 , wherein
the seal web has a web front face and a web rear face opposite to the web front face,
the seal shield extends outwards from the web front face, and
the groove is disposed nearer the web front face as compared to the web rear face.