Oil-injected multi-stage compressor system and procedure for controlling such a compressor system

US12018678B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12018678-B2
Application numberUS-201917273422-A
CountryUS
Kind codeB2
Filing dateSep 24, 2019
Priority dateSep 25, 2018
Publication dateJun 25, 2024
Grant dateJun 25, 2024

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

An oil-injected multi-stage compressor system that comprises at least a low-pressure stage compressor element (2) with an inlet (4a) and an outlet (5a) and a high-pressure stage compressor element (3) with an inlet (4b) and an outlet (5b), whereby the outlet (5a) of the low-pressure stage compressor element (2) is connected to the inlet (4b) of the high-pressure stage compressor element (3) through a pipeline (6), characterized in that the compressor elements (2, 3) are provided with their own drive in the form of an electric motor (2a, 3a), whereby the compressor elements (2, 3) are connected to the electric motor (2a, 3a) either directly or through a gearbox and that an intercooler (9) is provided in the aforementioned pipeline (6) between the low-pressure stage compressor element (2) and the high-pressure stage compressor element (3).

First claim

Opening claim text (preview).

The invention claimed is: 1. An oil-injected multi-stage compressor system that comprises at least a low-pressure stage compressor element ( 2 ) with an inlet ( 4 a ) and an outlet ( 5 a ) and a high-pressure stage compressor element ( 3 ) with an inlet ( 4 b ) and an outlet ( 5 b ), whereby the outlet ( 5 a ) of the low-pressure stage compressor element ( 2 ) is connected to the inlet ( 4 b ) of the high-pressure stage compressor element ( 3 ) through a pipeline ( 6 ), wherein the compressor elements ( 2 , 3 ) are provided with their own drive in the form of an electric motor ( 2 a , 3 a ), whereby the compressor elements ( 2 , 3 ) are connected to the electric motor ( 2 a , 3 a ) either directly or through a gearbox and that an intercooler ( 9 ) is provided in the aforementioned pipeline ( 6 ) between the low-pressure stage compressor element ( 2 ) and the high-pressure stage compressor element ( 3 ), whereby the intercooler ( 9 ) is adjustable, whereby the compressor system ( 1 ) is also equipped with a control unit or regulator ( 11 ) to control or regulate the intercooler ( 9 ), so that the temperature at the inlet ( 4 b ) of the high-pressure stage compressor element ( 3 ) is above the dew point, whereby the intercooler ( 9 ) is an air-cooling system, which is adjustable by a fan, whereby the flow rate of the air can be controlled by adjusting the speed of the fan, whereby the intercooler ( 9 ) can additionally be regulated by changing the temperature of the air by a bypass pipeline that bypasses the intercooler. 2. The oil-injected multi-stage compressor system according to claim 1 , wherein the compressor system ( 1 ) is provided with a sensor ( 12 ) that is connected to the control unit or regulator ( 11 ) to measure the environmental parameters, where the control unit or regulator ( 11 ) can determine or calculate the dew point based on the measurements of the sensor ( 12 ). 3. The oil-injected multi-stage compressor system according to claim 1 , wherein the compressor system ( 1 ) is also provided with a humidity sensor ( 13 ) at the inlet ( 4 b ) of the high-pressure stage compressor element ( 3 ) that is connected to the control unit or regulator ( 11 ), which humidity sensor ( 13 ) can measure or determine the humidity, whereby the control unit or regulator ( 11 ) can determine or calculate the dew point on the basis of the measurements of the sensor ( 13 ). 4. The oil-injected multi-stage compressor system according to claim 1 , wherein the compressor system ( 1 ) is also provided with a temperature sensor ( 14 ) at the inlet ( 4 b ) of the high-pressure stage compressor element ( 3 ) that is connected to the control unit or regulator ( 11 ), which temperature sensor ( 14 ) can measure or determine the temperature, whereby the control unit or regulator ( 11 ) is provided with an algorithm that allows determining the dew point based on the course of the temperature measured by the temperature sensor ( 14 ). 5. The oil-injected multi-stage compressor system according to claim 1 , wherein the intercooler ( 9 ) is provided with a heat pump ( 10 ). 6. The oil-injected multi-stage compressor system according to claim 5 , wherein the heat pump ( 10 ) is adjustable. 7. The oil-injected multi-stage compressor system according to claim 1 , wherein oil is injected into the pipeline ( 6 ) that is downstream from the intercooler ( 9 ). 8. A procedure controlling an oil-injected multi-stage compressor system ( 1 ) comprising at least a low-pressure stage compressor element ( 2 ) with an inlet ( 4 a ) and an outlet ( 5 a ) and a high-pressure stage compressor element ( 3 ) with an inlet ( 4 b ) and an outlet ( 5 b ), whereby the outlet ( 5 a ) of the low-pressure stage compressor element ( 2 ) is connected to the inlet ( 4 b ) of the high-pressure stage compressor element ( 3 ) through a pipeline ( 6 ), wherein the compressor elements ( 2 , 3 ) are provided with their own drive in the form of an electric motor ( 2 a , 3 a ), whereby the compressor elements ( 2 , 3 ) are connected either directly or by a gearbox to the electric motor ( 2 a , 3 a ) and that an intercooler ( 9 ) is installed in the above pipeline ( 6 ) between the low-pressure stage compressor element ( 2 ) and the high-pressure stage compressor element ( 3 ), whereby this intercooler ( 9 ) is adjustable, whereby the compressor system ( 1 ) is also provided with a control unit or regulator ( 11 ) for controlling or regulating the intercooler ( 9 ) so that the temperature at the inlet ( 4 b ) of the high-pressure stage compressor element ( 3 ) is above the dew point, and that the procedure comprises the following steps: calculating or determining the dew point at the inlet ( 4 b ) of the high-pressure stage compressor element ( 3 ); and additionally regulating the intercooler ( 9 ) so that the temperature at the inlet ( 4 b ) of the high-pressure stage compressor element ( 3 ) is above the dew point by at least partly bypassing the intercooler ( 9 ). 9. The procedure according to claim 8 , wherein the calculation or determination of the dew point is done by measuring environmental parameters such as pressure, temperature and/or humidity. 10. The procedure according to claim 8 , wherein the calculation or determination of the dew point is done by measuring the humidity at the inlet ( 4 b ) of the high-pressure stage compressor element ( 3 ). 11. The procedure according to claim 8 , wherein the calculation or determination of the dew point is carried out by following the course of the temperature at the inlet ( 4 b ) of the high-pressure stage compressor element ( 3 ).

Assignees

Inventors

Classifications

  • Pumps characterised by combination with, or adaptation to, specific driving engines or motors · CPC title

  • Heating; Cooling (of machines or engines in general F01P) · CPC title

  • Lubrication (of machines or engines in general F01M) · CPC title

  • Rotary-piston machines or pumps, with non-parallel axes of movement of co-operating members, e.g. of screw type (with the working-chamber walls at least partly resiliently deformable F04C5/00; rotary-piston pumps with non-parallel axes of movement of co-operating members specially adapted for elastic fluids F04C18/48) · CPC title

  • Controlled or regulated · CPC title

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What does patent US12018678B2 cover?
An oil-injected multi-stage compressor system that comprises at least a low-pressure stage compressor element (2) with an inlet (4a) and an outlet (5a) and a high-pressure stage compressor element (3) with an inlet (4b) and an outlet (5b), whereby the outlet (5a) of the low-pressure stage compressor element (2) is connected to the inlet (4b) of the high-pressure stage compressor element (3) thr…
Who is the assignee on this patent?
Atlas Copco Airpower Nv
What technology area does this patent fall under?
Primary CPC classification F04C23/001. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jun 25 2024 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).