Subsea compressor cleaning method wherein the cleaning liquid is retrieved from the multiphase process fluid
US-9518588-B2 · Dec 13, 2016 · US
US10458438B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10458438-B2 |
| Application number | US-201515503621-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 17, 2015 |
| Priority date | Sep 19, 2014 |
| Publication date | Oct 29, 2019 |
| Grant date | Oct 29, 2019 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A centrifugal compressor includes: a rotational shaft; a main casing surrounding at least a part of the rotational shaft, the main casing having an inlet and an outlet separated from each other in an axial direction of the rotational shaft and an annular space surrounding a section of the rotational shaft at a side of the inlet and communicating with the inlet; at least one impeller disposed in a fixed state to the rotational shaft inside the main casing; a flow guide member disposed inside the annular space and extending along the axial direction of the rotational shaft; a plurality of injection holes disposed along the flow guide member and separated from one another along the axial direction of the rotational shaft; and a flow path which extends inside the annular space and through which a cleaning fluid to be supplied to the plurality of injection holes is capable of flowing.
Opening claim text (preview).
The invention claimed is: 1. A centrifugal compressor, comprising: a rotational shaft; a main casing surrounding at least a part of the rotational shaft, the main casing having an inlet and an outlet separated from each other in an axial direction of the rotational shaft and an annular space surrounding a section of the rotational shaft at a side of the inlet and communicating with the inlet, wherein a fluid to be compressed before compression flows in the annular space; at least one impeller disposed in a fixed state to the rotational shaft inside the main casing; a flow guide member disposed inside the annular space and extending along the axial direction of the rotational shaft, the flow guide member having a flow guide element extending along a radial direction of the rotational shaft and having a predetermined blade width in the axial direction of the rotational shaft; a plurality of injection holes disposed along the flow guide member and separated from one another along the axial direction of the rotational shaft; and a flow path which extends inside the annular space and through which a cleaning fluid to be supplied to the plurality of injection holes is capable of flowing. 2. The centrifugal compressor according to claim 1 , wherein the flow guide member is disposed on a side opposite from the inlet in a circumferential direction of the rotational shaft. 3. The centrifugal compressor according to claim 1 , wherein at least a part of the plurality of injection holes is disposed on a surface of the flow guide element. 4. The centrifugal compressor according to claim 3 , wherein the flow guide element constitutes a part of an inlet guide-vane row disposed in the annular space. 5. The centrifugal compressor according to claim 1 , wherein the flow guide member has a blade element which reduces a flow-path cross sectional area of the annular space from the inlet toward the flow guide element. 6. The centrifugal compressor according to claim 1 , wherein at least a part of the plurality of injection holes is arranged in a line along the axial direction of the rotational shaft. 7. The centrifugal compressor according to claim 1 , wherein at least a part of the plurality of injection holes is arranged in a staggered fashion along the axial direction of the rotational shaft.
rotating diffusers · CPC title
Axial inlet and radial outlet · CPC title
Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles · CPC title
Adding liquids · CPC title
Cleaning of turbomachines · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.