Patent Grant
11371507
This application is a National Stage of International Application No. PCT/IB2019/058063 filed Sep. 24, 2019, claiming priority based on Belgian Patent Application No. 2018/5658 filed Sep. 25, 2018.
The present invention relates to an oil-injected multistage compressor.
People are already aware of multistage compressor devices in which gas is compressed in two or more steps or ‘stages’, whereby two or more compressor elements are placed in a series one after the other.
People are also already aware of oil-injected multistage compressor devices in which a coolant, in this case oil, is used to cool the gas.
This makes improved efficiency possible, since the consumption of the second and subsequent stages will decrease by cooling the gas before the second and subsequent stages.
The cooling of the gas, and therefore the improvement in efficiency, could be much better.
The cooling could be improved by, for example, additional active cooling. This entails effectively extracting heat from the system instead of only adding a coolant to the system that takes heat from the gas.
Such active cooling offers much more potential for increasing efficiency.
However, this is not as simple as it would appear since there will be a pressure loss in a cooler, which will undo the improved efficiency.
This pressure loss increases due to the presence of oil in the gas, particularly due to the fact that the oil has a higher viscosity than air. The pressure loss will depend on the quantity of oil in the gas: the more oil in the gas, the greater the pressure loss in the intercooler.
The object of the present invention is to provide a solution to at least one of the aforementioned and other disadvantages by providing an oil-injected multistage compressor device, in which there will be an active cooling for which the aforementioned pressure loss will not be a problem.
The subject of the present invention is an oil-injected multistage compressor device that comprises at least one low-pressure stage compressor element with an inlet and an outlet and a high-pressure stage compressor element with an inlet and an outlet, whereby the outlet of the low-pressure stage compressor element is connected to the inlet of the high-pressure stage compressor element by a conduit, with the characteristic that in the aforementioned conduit between the low-pressure stage compressor element and the high-pressure stage compressor element an intercooler is provided and that the compressor device is also equipped with a restriction for limiting the amount of oil injected into the low-pressure stage compressor element.
An advantage is that the restriction can limit the amount of oil injected into the low-pressure stage compressor element.
This results in the pressure loss in the intercooler being limited.
Therefore, one will achieve all the advantages of the active cooling of the gas for the high-pressure stage, without or with only a limited disadvantage of a pressure loss in the intercooler.
The restriction can be implemented in many ways, such as a local constriction in the relevant oil supply conduit.
The restriction is preferably done by a valve that can regulate the amount of oil injected into the low-pressure stage compressor element, so that always only the minimum amount of the required oil is injected and not more than necessary.
This will limit the aforementioned pressure loss in the cooler even more.
When conditions demand, the valve can allow more oil to be injected in order to avoid overheating. In all other cases, it is possible to switch to the minimum injection.
The presence of the intercooler means that less oil is needed for cooling, since the intercooler can take over part of the cooling that was previously done by the oil. Because less oil is needed and injected, the pressure loss in the intercooler will also be limited.
It is possible for the compressor device to be equipped with an oil separator provided in the conduit upstream from the intercooler in order to separate oil.
The advantage of this is that it can ensure that no, or virtually no, oil will enter the intercooler, such that the problem of pressure loss may be completely eliminated.
This also results in the possibility of separating any condensate forming in the intercooler.
When the oil is not separated before the intercooler, this condensate would end up in the oil and it would then be difficult to separate it apart.
The invention also relates to a method for controlling an oil-injected multistage compressor device that comprises at least one low-pressure stage compressor element with an inlet and an outlet and a high-pressure stage compressor element with an inlet and an outlet, whereby the outlet of the low-pressure stage compressor element is connected to the inlet of the high-pressure stage compressor element via a conduit, with the characteristic that in the aforementioned conduit between the low-pressure stage compressor element and the high-pressure stage compressor element an interncooler is provided and that the compressor device is also equipped with a restriction for limiting the amount of oil injected into the low-pressure stage compressor element and with the characteristic that the method comprises the following steps:
The advantages of such a method are obviously similar to the aforementioned advantages of the oil-injected multistage compressor device.
With the insight to better demonstrate the features of the invention, the following describes, as a non-exhaustive example, some preferred embodiments of an oil-injected multistage compressor device according to the invention and method in order to control such a compressor device, with reference to the accompanying drawings, in which:
The
Both compressor elements 2, 3 are, for example, screw compressor elements, but this is not necessary for the invention.
Both compressor elements 2, 3 are also provided with an oil circuit for the injection of oil in compressor elements 2, 3. For clarity, these oil circuits are not or only partially shown in the FIGURE.
Low-pressure stage compressor element 2 has an inlet 4a for gas and an outlet 5a for compressed gas.
Gas outlet 5a is connected to inlet 4b of high-pressure stage compressor element 3 via a conduit 6.
High-pressure stage compressor element 3 is also equipped with an outlet 5b, whereby outlet 5b is connected to a liquid separator 7.
It is possible for outlet 8 of this liquid separator 7 to be connected to an aftercooler.
An intercooler 9 is included in the aforementioned conduit 6 between low-pressure stage compressor element 2 and high-pressure stage compressor element 3.
Compressor device 1 is also equipped with a restriction 10 for limiting the quantity of oil injected into low-pressure stage compressor element 2.
In this case, but not necessarily for the invention, this restriction 10 is carried out with a valve 10, which will allow the regulation of the amount of oil to be injected.
Of course it is not excluded that a passive or non-regulatable restriction 10 is applied instead of a valve 10, for example in the form of a narrowing in the conduit at the point where valve 10 is usually located.
The aforementioned valve 10 can be an open-closed regulatable valve or a continuously regulatable valve.
A control unit or regulator 11 is provided for controlling or regulating this valve 10.
In this case, a temperature sensor 12 is also provided which may determine or measure the temperature at outlet 5a of low-pressure stage compressor element 2. This sensor 12 is connected to the aforementioned control unit or regulator 11.
It is also possible to use a power meter or an efficiency meter instead of a temperature sensor 12.
In this case, but not necessarily for the invention, compressor device 1 is equipped with an oil separator 13, which is provided in conduit 6 upstream from intercooler 9 for separating the oil that is injected into low-pressure stage compressor element 2. An oil conduit 14 is also provided which runs from this oil separator 13 towards low-pressure stage compressor element 2 in order to direct the oil separated by oil separator 13 via this oil conduit 14 to low-pressure stage compressor element 2 to be injected into the low-pressure stage compressor element 2 there.
This means that this oil conduit 14 runs towards the aforementioned valve 10.
Alternatively, it is also possible for this oil conduit 14 to run from oil separator 13 to liquid separator 7 downstream from high-pressure stage compressor element 3.
This is shown schematically using the dotted line 14a, which represents this oil conduit 14a.
Such an oil conduit 14a will guide the oil separated by oil separator 13 via this oil conduit 14a to liquid separator 7. It is not excluded for an oil pump 14b or the like to be used for displacing the oil.
In this case, both an oil cooler 15 and a filter 16 will be provided in oil conduit 14.
The filter 16 can filter out any impurities in the oil before the oil is reinjected into compressor element 2.
An oil return conduit 17 is also provided, which leaves from liquid separator 7 with a branch 17a to high-pressure stage compressor element 3 and a branch 17b to low-pressure stage compressor element 2.
As can be seen in
Naturally, this is not necessarily the case and both the oil cooler 15 and filter 16 can be included downstream from point P in oil conduit 14, so that both the oil from liquid separator 7 and the oil from oil separator 13 are cooled and filtered by oil cooler 15 and filter 16 respectively.
If oil conduit 14a is provided, it can also be provided with an oil cooler 15 and a filter 16.
The operation of the oil-injected multistage compressor device 1 is very simple and is as follows:
During operation, compressed gas, e.g. air, will be sucked in via inlet 4a of low-pressure stage compressor element 2 and will undergo a first compression stage.
The partially compressed gas will flow through conduit 6 to intercooler 9, where it will be cooled and then flow to inlet 4b of high-pressure stage compressor element 3, where it will undergo a subsequent compression.
Oil will be injected in both low-pressure stage 2 and high-pressure stage compressor element 3, which will ensure the lubrication and cooling of compressor elements 2, 3.
The compressed gas will leave high-pressure stage compressor element 3 via outlet 5b and be guided to oil separator 7.
The injected oil will be separated and the compressed gas can then possibly be guided to an aftercooler before being sent to consumers.
To ensure that there is not a big pressure loss in intercooler 9, valve 10 will be controlled by control unit 11 so that temperature Toutlet at outlet 5a of low-pressure stage compressor element 2 remains below a specific value Tmax.
For this, the first step will be to determine the temperature Toutlet.
This temperature Toutlet will in this case be measured directly with sensor 12.
However, it is clear that there are other ways to determine this temperature Toutlet. For example, it can also be determined or calculated from the temperature after intercooler 9 or based on environmental parameters and working conditions of low-pressure stage compressor element 2.
The method for controlling valve 10 is then further as follows:
In this way, oil or additional oil can be injected when needed so that the temperature does not increase too much.
At times when the temperature is low enough, the oil injection can be reduced or stopped again.
If valve 10 is an open-closed valve, oil will either be injected or not.
If valve 10 is continuously regulatable, the flow rate of the oil can be precisely adjusted to meet the current requirement.
This ability to regulate ensures that a minimum oil injection is always obtained.
Although the regulation of valve 10 in the example described above is carried out on the basis of the temperature Toutlet, it is not excluded for the control to be based on the power or efficiency.
In such cases, valve 10 will be controlled by control unit 10 so that the power or efficiency remains above a certain value Pmax or Emax, to ensure that there is no large loss of pressure in intercooler 9.
In addition to the control of valve 10, the method in this case will also include the step of separating oil downstream of low-pressure stage compressor element 2 and upstream of intercooler 9 with the help of oil separator 13.
This separated oil will then be discharged to low-pressure stage compressor element 2 via oil conduit 14.
Oil conduit 14 will meet branch 17b of return conduit 17 at point P in order to go to valve 10 and ultimately to low-pressure stage compressor element 2.
Alternately, if compressor device 1 is equipped with an oil conduit 14a, the method can include the step of separating the oil downstream from low-pressure stage compressor element 2 and upstream from intercooler 9 using oil separator 13 and subsequently pumping this to liquid separator 7 downstream from high-pressure stage compressor element 3.
Due to this additional step, even the minimum injected oil in low-pressure stage compressor element 2 will be removed from the gas, so that there is minimal pressure loss in intercooler 9.
In this way, the gas can always be actively cooled with intercooler 9 before it goes to high-pressure stage compressor element 3 without this being accompanied by significant pressure loss and therefore a loss of efficiency.
The actively cooled air will then be further compressed in high-pressure stage compressor element 3 with a much higher performance than when no intercooler 9 is present.
Another aspect of the invention is that the compressor device is only provided with oil separator 13 with additional oil conduit or 14a and not with valve 10 which regulates the oil injection.
In this case, there will therefore be no minimum oil injection, but only all the oil injected in low-pressure stage compressor element 2 will be separated by oil separator 13 before the gas is led to intercooler 9.
The present invention is by no means limited to the embodiments described as examples and shown in the figures, but an oil-injected multistage compressor device according to the invention, and a method for controlling such a compressor device can be achieved following different variants without going beyond the scope of the invention.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2018/5658 | Sep 2018 | BE | national |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/IB2019/058063 | 9/24/2019 | WO | 00 |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2020/065505 | 4/2/2020 | WO | A |
| Number | Name | Date | Kind |
|---|---|---|---|
| 3759052 | Inoue | Sep 1973 | A |
| 6506027 | Timuska | Jan 2003 | B1 |
| 8277207 | Kishi | Oct 2012 | B2 |
| 8313312 | Fujimoto | Nov 2012 | B2 |
| 20040217180 | Lu | Nov 2004 | A1 |
| Number | Date | Country |
|---|---|---|
| 204716541 | Oct 2015 | CN |
| 105275810 | Jan 2016 | CN |
| 107002683 | Aug 2017 | CN |
| 05-044678 | Feb 1993 | JP |
| 0225115 | Mar 2002 | WO |
| Entry |
|---|
| International Search Report for PCT/IB2019/058063 dated Dec. 16, 2019 (PCT/ISA/210). |
| Written Opinion for PCT/IB2019/058063 dated Dec. 16, 2019 (PCT/ISA/237). |
| Number | Date | Country | |
|---|---|---|---|
| 20210246900 A1 | Aug 2021 | US |
