Apparatus for transferring energy between a rotating element and fluid
US-2015377251-A1 · Dec 31, 2015 · US
US2017191487A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2017191487-A1 |
| Application number | US-201715462192-A |
| Country | US |
| Kind code | A1 |
| Filing date | Mar 17, 2017 |
| Priority date | Nov 20, 2012 |
| Publication date | Jul 6, 2017 |
| Grant date | — |
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A compressor end head for providing a thermal barrier to a mechanical seal includes an inner end head having an inner end head opening, inner end head grooves in the inner end head opening, configured to place and seal an end portion of a compressor shaft; and an outer end head having an outer end head opening configured to enclose the inner end head.
Opening claim text (preview).
1 . A compressor end head for providing a thermal barrier to a mechanical seal, the compressor end head comprising: an inner end head having: an inner end head opening; inner end head grooves in the inner end head opening, configured to place and seal an end portion of a compressor shaft; and an outer end head having an outer end head opening configured to enclose the inner end head. 2 . The compressor end head of claim 1 , comprising an interference fit between the inner end head and the outer end head. 3 . The compressor end head of claim 1 , wherein the inner end head is welded to the outer end head. 4 . The compressor end head of claim 1 , wherein the mechanical seal comprises a dry gas seal (DGS). 5 . The compressor end head of claim 1 , wherein the inner end head comprises an inlet; and the outer end head comprises an inlet chamber connected to the inlet, an outlet, an outlet chamber connected to the outlet, and straight axial channels connecting the inlet chamber and the outlet chamber. 6 . The compressor end head of claim 5 , wherein the inlet chamber and the outlet chamber comprise a radial thermal barrier around the mechanical seal. 7 . The compressor end head of claim 5 , wherein the straight axial channels comprise an axial thermal barrier around the mechanical seal. 8 . The compressor end head of claim 5 , comprising a flow path on an outer surface of the inner end head connected between the inlet and the outlet. 9 . The compressor end head of claim 8 , wherein the flow path comprises a flow path for hot oil or gas. 10 . A compressor, comprising: a shaft; an inner end head having: an inner end head opening ; a plurality of inner end head grooves adjacent the inner end head opening configured to place and seal an end portion of the shaft; and an outer end head having an outer end head opening configured to enclose the inner end head. 11 . The compressor of claim 10 , comprising a plurality of impellers connected to the shaft. 12 . The compressor of claim 10 , wherein the inner end head comprises an inlet; and the outer end head comprises an inlet chamber connected to the inlet, an outlet, an outlet chamber connected to the outlet, and straight axial channels connecting the inlet chamber and the outlet chamber. 13 . The compressor of claim 12 , wherein the inlet chamber and the outlet chamber comprise a radial thermal barrier around the mechanical seal. 14 . The compressor of claim 12 , wherein the straight axial channels comprise an axial thermal barrier around the mechanical seal. 15 . The compressor of claim 12 , comprising a flow path on an outer surface of the inner end head connected between the inlet and the outlet. 16 . The compressor of claim 15 , wherein the flow path comprises a flow path for hot oil or gas.
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