Thermal Barrier Coating for Bearing Journal Surfaces of Rotary Shafts
US-2015043848-A1 · Feb 12, 2015 · US
US10801505B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10801505-B2 |
| Application number | US-201616077162-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 8, 2016 |
| Priority date | Mar 28, 2016 |
| Publication date | Oct 13, 2020 |
| Grant date | Oct 13, 2020 |
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A centrifugal compressor according to the present invention includes, as gas flow paths, diffuser flow paths into which process gas flowing from impellers to outside in a radial direction flows, curved flow paths that respectively communicate with the diffuser flow paths and change a flowing direction of the process gas from a direction toward the outside in the radial direction to a direction toward inside in the radial direction, and return flow paths that respectively communicate with the curved flow paths and cause the process gas flowing through the curved flow paths to flow into the impellers. In the present invention, the curved flow path configuring at least one of the gas flow paths is provided between a diaphragm and a flow path forming body that is provided between the diaphragm and the casing.
Opening claim text (preview).
The invention claimed is: 1. A rotary machine, comprising: a casing; a rotor that includes a rotary shaft rotatably supported inside the casing, and a plurality of stages of impellers fixed to an outer periphery of the rotary shaft; diaphragms respectively surrounding the impellers; and gas flow paths through which process gas to be compressed flows, the gas flow paths being provided respectively corresponding to the impellers, wherein the gas flow paths include diffuser flow paths, curved flow paths, and return flow paths, the diffuser flow paths respectively communicate from outlets of the impellers in a radially outward direction to the curved flow paths, the curved flow paths respectively communicate from outlets of the diffuser flow paths and change a flowing direction of the process gas from the radially outward direction toward a radially inward direction to the return flow paths, the return flow paths respectively communicate from outlets of the curved flow paths and cause the process gas flowing through the curved flow paths, to flow into a next stage of the impellers, the curved flow path configuring at least one of the gas flow paths is provided between the diaphragm and a flow path forming body that is provided between the diaphragm and the casing, the flow path forming body provided such as to substitute a part of the casing, the casing includes an annular accommodating groove recessed outward in the radial direction, corresponding to a region provided with the flow path forming body, and the flow path forming body includes an annular shape and is mated with the accommodating groove such that a radial extent of the curved flow path provided between the diaphragm and the flow path forming body is located inside a radial extent of the accommodating groove of the casing. 2. The rotary machine according to claim 1 , wherein the flow path forming body is positioned based on one or both of temperature of the process gas and a range where water injection is performed. 3. The rotary machine according to claim 2 , wherein the curved flow path configuring the gas flow path located in at least a last stage, out of the gas flow paths, is provided between the corresponding diaphragm and the flow path forming body. 4. The rotary machine according to claim 2 , wherein the curved flow paths configuring the gas flow paths located in all stages within the range where the water injection is performed, out of the gas flow paths, are provided between the diaphragms and the flow path forming body. 5. The rotary machine according to claim 2 , wherein the curved flow path configuring the gas flow path located in a rear stage within the range where the water injection is performed, out of the gas flow paths, is provided between the corresponding diaphragm and the flow path forming body. 6. The rotary machine according to claim 1 , wherein the casing is a horizontal divisional casing including a lower half casing and an upper half casing, and the curved flow paths provided between the diaphragms and the flow path forming body are provided on one or both of the lower half casing and the upper half casing. 7. The rotary machine according to claim 1 , wherein the curved flow paths other than the curved flow paths provided between the diaphragms and the flow path forming body, are provided between the diaphragms and the casing. 8. The rotary machine according to claim 1 , wherein the casing is covered with a heat insulation material. 9. The rotary machine according to claim 1 , wherein the casing includes paired bearings supporting the rotary shaft, and bearing chambers respectively accommodating the bearings each include a heat shielding material.
the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors · CPC title
especially adapted for elastic fluid pumps · CPC title
Adding liquids · CPC title
Cooling (of machines or engines in general F01P); Heating; Diminishing heat transfer {(for the motor of air-pump units F04D25/082; cooling of shafts or bearings F04D29/04)} · CPC title
for radial or helico-centrifugal pumps · CPC title
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