Patent Grant
11614088
The present invention relates to a method for controlling the liquid injection of a compressor device.
It is known for example that for the cooling of a compressor device, a liquid, such as oil or water for example, is injected into the compression space of the compressor element.
In this way the temperature at the outlet of the compressor element for example can be kept within certain limits, so that the temperature does not become too low so that the formation of condensate in the compressed air is prevented, and whereby the liquid temperature does not become too high so that the quality of the liquid remains optimum.
The injected liquid can also be used for the sealing and lubrication of the compressor element so that a good operation can be obtained.
It is known that the quantity and temperature of the injected liquid will affect the efficiency of the cooling, the sealing and the lubrication.
Methods are already known for controlling the liquid injection in a compressor device, whereby use is made of a control based on the temperature of the injected liquid, whereby the control consists of getting the temperature of the injected liquid to fall if more cooling is desired, by having the liquid pass through a cooler.
By controlling the temperature, the viscosity of the liquid, and thus the lubricating and sealing properties thereof, can also be adjusted.
A disadvantage of such a method is that the minimum attainable temperature of the injected liquid is limited by the temperature of the coolant that is used in the cooler.
Methods are also known for controlling the liquid injection in a compressor device, whereby use is made of a control based on the mass flow of the injected liquid, whereby the control consists of injecting more liquid if more cooling is desired for example.
By injecting more liquid the temperature will rise less. This enables a higher injection temperature without exceeding the maximum outlet temperature, so that overdimensioning of the cooler is not required in the event of a low coolant temperature.
A disadvantage of such a method is that it will only enable the temperature of the injection liquid to be controlled indirectly.
An additional disadvantage of the known methods is that when a proportion of the injected liquid is used to lubricate the bearings, this liquid will have the same temperature as the liquid that is injected into the compression space for the cooling thereof.
It has turned out in practice that in such compressor devices the lifetime of the bearings is detrimentally affected by the liquid temperature.
An example of such devices can be found in US 2012/237,382 and U.S. Pat. No. 4,780,061 where oil is reaching the compression space or the bearings through a configuration of channels.
The purpose of the present invention is to provide a solution to a least one of the aforementioned and other disadvantages and/or to optimise the efficiency of the compressor device.
The object of the present invention is a method for controlling the liquid injection of a compressor element, whereby the compressor element comprises a housing that comprises a compression space in which at least one rotor is rotatably affixed by means of bearings, whereby liquid is injected into the compressor element, whereby the method comprises the step of providing two independent separated liquid supplies to the compressor element, whereby one liquid supply is injected into the compression space and the other liquid supply is injected at the location of the bearings.
‘Independent separated liquid supplies’ means that the liquid supplies follow a separate path or route, that starts for example from a liquid reservoir and ends in the compression space or at the location of the bearings respectively.
An advantage is that for each liquid supply, the properties of the injected liquid, such as the temperature and/or mass flow for example, can be controlled separately.
In this way an optimum liquid supply can be provided both for the bearings and for the compression space with the rotors.
In this way the compressor element can operate more optimally and more efficiently than the already known compressor elements.
In the most preferred embodiment the method comprises the step of controlling both the temperature of the liquid and the mass flow of the liquid, for both liquid supplies separately.
This means: the temperature and the mass flow are controlled for each liquid supply, whereby the control for the one liquid supply is done independently of the other liquid supply.
This has the advantage that both the temperature and the quantity of liquid are specifically attuned to the needs of the bearings or the compression space, as the control of the one liquid supply is completely independent of the other liquid supply.
Also it is no longer necessary to provide an overdimensioned cooler.
Moreover, the control of both the temperature and the quantity of liquid has the additional advantage that a synergistic effect will occur.
Both the separate optimisation of the temperature and the quantity of injected liquid will have a positive effect on the efficiency of the compressor element.
But when both are optimised, there will be a functional interaction between the two controls that yields an improvement in the efficiency of the compressor element that is greater than the sum of the efficiency improvements of both individual controls, so that the controls concern a combination and not merely an aggregation or juxtaposition.
This functional interaction is partly attributable to de-aeration phenomena that relate to the quantity of air dissolved in the liquid.
By controlling both the temperature and the mass flow, the quantity of air dissolved in the liquid is at least partially eliminated, which will increase the efficiency.
On the other hand, account has to be taken of the sealing capacity, partly attributable to the viscosity of the injected liquid and partly to the available mass flow of the liquid. For each operating point there is an ideal combination of liquid flow and viscosity, which is a function of the temperature, whereby both parameters strengthen one another.
The invention also concerns a liquid-injected compressor device, whereby this compressor device comprises at least one compressor element, whereby the compressor element comprises a housing that comprises a compression space in which at least one rotor is rotatably affixed by means of bearings, whereby the compressor device is further provided with a gas inlet and an outlet for compressed gas that is connected to a liquid separator, which is connected to the compressor element by means of an injection circuit, whereby the aforementioned injection circuit comprises two separate injection pipes that start from the liquid separator and which open into the compression space and into the housing at the location of the aforementioned bearings respectively.
Such a compressor installation has the advantage that the liquid supplies for the lubrication of the bearings and for the cooling of the compression space can be controlled independently of one another, so that both liquid supplies can be controlled according to the optimum properties that are needed for the bearings and for the compression space respectively at that specific operating point.
The invention also concerns a liquid-injected compressor element with a housing that comprises a compression space in which at least one rotor is rotatably affixed by means of bearings, whereby the compressor element is further provided with a connection for an injection circuit for the injection of liquid into the compressor element, whereby the connection to the injection circuit is realised by means of a number of injection points in the housing, whereby the housing is further provided with separated integrated channels that start from the aforementioned injection points in the housing and open into the compression space and at the aforementioned bearings respectively.
Such a liquid-injected compressor element can be used in a compressor device according to the invention. In this way at least a proportion of the injection pipes of the injection circuit of the compressor device will as it were extend partially separately in the housing of the compressor element in the form of the aforementioned integrated channels.
Such an approach will ensure that the number of injection points that provide the connection of the injection pipes can be kept limited and that for example the division of the liquid supply to the different bearings can be realised by a suitable division of the channels in the housing.
The location of the injection points can also be freely chosen, whereby the channels in the housing will ensure that the oil supply is guided to the appropriate location.
With the intention of better showing the characteristics of the invention, a few preferred variants of a method for controlling the liquid injection of a compressor device and a liquid-injected compressor device thereby applied, are described hereinafter by way of an example, without any limiting nature, with reference to the accompanying drawings, wherein:
The liquid-injected compressor device 1 shown in
The compressor element 2 comprises a housing 3 that defines a compression space 4 with a gas inlet 5 and an outlet 6 for compressed gas.
One or more rotors 7 are rotatably affixed in the housing 3 by means of bearings 8 that are affixed on the shafts 9 of the rotors 7. The rotors 7 are driven, for example, by engine/motor/gearbox 28, which is connected to controller 29.
Furthermore, the housing 3 is provided with a number of injection points 10a, 10b for the injection of a liquid.
This liquid can for example be synthetic oil or water or otherwise, but the invention is not limited to this as such.
The injection points 10a, 10b are placed at the location of the compression space 4 and at the location of the aforementioned bearings 8.
The compressor element 2 is shown in more detail in
According to the invention the housing 3 is provided with separated integrated channels 11 that start from the aforementioned injection points 10a, 10b in the housing 3 and open into the compression space 4 and the aforementioned bearings 8 respectively.
In the example shown in
However, this is not necessarily the case as due to the provision of the separated integrated channels 11, there is more freedom to place the injection points 10a, 10b at a different location.
Furthermore, it is possible to provide a separate injection point 10a, 10b for each channel 11.
However, it is also possible that more than one channel 11 starts from an injection point 10a, 10b.
As can be seen in
Moreover, in this case more than one channel 11 is also provided for the compression space 4. In this case there are two channels 11 that run from the injection points 10a to the compression space 4.
Additionally one or more cavities 12 can be provided in the housing 3.
In the example shown there are three cavities 12.
One cavity 12 acts as a liquid reservoir for liquid for the compression space 4, the other two cavities 12 act as a liquid reservoir for liquid for the bearings 8.
For the bearings 8 one cavity 12 is provided on the inlet side 5 and one cavity 12 on the outlet side 6.
The cavities 12 ensure a connection between the injection points 10a, 10b and one or more of the separated integrated channels 11 connected thereto.
It is clear that the injection point 10a at the location of the compression space 4 connects to the cavity 12 for liquid for the compression space 4.
The channels 11 that open into the compression space 4 also connect to this cavity 12.
Analogously, the injection points 10b at the location of the bearings 8 and the channels 11 that open into the bearings 8 connect to the cavities 12 for liquid for the bearings 8.
It is clear that it is also possible that if the design of the compressor element 2 and the housing 3 so allows, only one injection point 10b is provided and one cavity 12 for liquid for the bearings 8. In this case the liquid will be brought to all bearings 8 using the channels 11.
Furthermore, the liquid-injected compressor device 1 comprises a liquid separator 13, whereby the outlet 6 for compressed gas is connected to the inlet 14 of the liquid separator 13.
The liquid separator 13 comprises an outlet 15 for compressed gas, from where the compressed gas can be guided to a consumer network for example, not shown in the drawings.
The liquid separator 13 further comprises an outlet 16 for the separated liquid.
The liquid separator 13 is connected to the aforementioned outlet 16 by means of an injection circuit 17 connected to the compressor element 2.
This injection circuit 17 comprises two separate separated injection pipes 17a, 17b, which both start from the liquid separator 13.
The injection pipes 17a, 17b will ensure two separate separated liquid supplies to the compressor element 2.
The injection points 10a, 10b in the housing 3 ensure the connection of the compressor element 2 to the injection circuit 17.
A first injection pipe 17a leads to the aforementioned injection point 10a at the location of the compression space 4.
The second injection pipe 17b leads to the injection points 10 that are placed at the location of the bearings 8.
As already mentioned above in this case, but not necessarily, there are two injection points 10b for the bearings 8, i.e. one for each end of the shaft 9 of the rotor 7.
To this end the second injection pipe 17b will be split into two sub-pipes 18a, 18b, whereby one sub-pipe 18a, 18b will come out at each end of the shaft 9.
If there is only one injection point 10b for the bearings, the channels 11 will take over the function of the sub-pipes 18a, 18b, or in other words: then these sub-pipes 18a, 18b are integrated in the housing 3 in the form of two separated integrated channels 11 that run from the injection point 10b to the bearings 8.
It is clear that for the aforementioned channels 11, as shown in
A cooler 19 is provided in the first injection pipe 17a. This cooler 19 can for example, but not necessarily for the invention, be provided with a fan for cooling the liquid that flows through this first injection pipe 17a. Of course the invention is not limited as such and another type of cooler 19 can also be used, for example with a cooling liquid such as water or similar.
A controllable valve 20 is also provided, in this case, but not necessarily, a throttle valve.
By means of this throttle valve the quantity of liquid that is injected in the compression space 4 can be adjusted.
A cooler 21 is also provided in the second injection pipe 17b, whereby in this case use can be made of a cooling fluid, such as water for example, to cool the liquid or it can be cooled by a fan.
Furthermore, in this case two controllable valves 22 are provided in the second injection pipe 17b, one in each sub-pipe 18a, 18b.
It is also possible that one single controllable valve 22 is provided, for example in the form of a three-way valve at the location of the connecting point P between the two sub-pipes 18a, 18b.
It is also possible to replace the two valves 22 by one valve 22 that is not a three-way valve, but for example is an ordinary (two-way) control valve, that is provided upstream from the division of the injection pipe 17b into the sub-pipes 18a, 18b.
The operation of the compressor device 1 is very simple and as follows.
During the operation of the compressor device 1 a gas, for example air, will be drawn in via the gas inlet 5 that will be compressed by the action of the rotors 7 and leave the compressor element 2 via the outlet.
As liquid is injected into the compression space 4 during the operation, this compressed air will contain a certain quantity of the liquid.
The compressed air is guided to the liquid separator 13.
There the liquid will be separated and collected underneath in the liquid separator 13.
The compressed air, now free of liquid, will leave the liquid separator 13 via the outlet 15 for compressed gas and can be guided to a compressed gas consumer network, for example, not shown in the drawings.
The separated liquid will be carried back to the compressor element 2 by means of the injection circuit 17.
A proportion of the liquid will be transported to the compression space 4 via the first injection pipe 17a and the channels 11 connected thereto, another proportion to the bearings 8 via the second injection pipe 17b, the two sub-pipes 18a, 18b and the channels 11 connected thereto.
Hereby the coolers 19, 21 and the controllable valves 20, 22 will be controlled according to a method that consists of first controlling the mass flow of the liquid supplies, i.e. the controllable valves 20, 22, and then controlling the temperature of the liquid supplies, i.e. the coolers 19, 21.
The aforementioned control is thus a type of master-slave control, whereby the master control, in this case the control of the controllable valves 20, 22, is always done first.
It is important to note here that the coolers 19, 21 and controllable valves 20, 22 are controlled independently of one another, this means that the control of the one cooler 19 is not affected in any way by the control of the other cooler 21 or that the control of the one controllable valve 20 has no effect on the control of the other controllable valves 22.
The control will be such that the properties of the liquid are attuned to the requirements for the compression space 4 and for the bearings 8 respectively.
As mentioned above, by applying both controls a synergistic effect will occur as a result of a functional interaction between the two controls.
Preferably the method consists of controlling the temperature and mass flow of the liquid supplies such that the specific energy requirement of the liquid-injected compressor device 1 is a minimum.
The specific energy requirement (SER) is the ratio of the power (P), e.g., electrical power consumption by the motor 28, of the compressor device 1, which can be determined by the controller 29, to the flow rate (FAD) supplied by the compressor device 1 compared to the standard operating conditions of the compressor element 2. By comparing the SER to the specification of the compressor element 2, the efficiency of the compressor element can be determined.
Although in the examples shown the injection circuit 17 is formed by two separated independent injection pipes 17a, 17b, it is not excluded that a third independent injection pipe is provided, which leads to the drive of the compressor device 1.
A cooler 19, 21 and a controllable valve 20, 22 can also be incorporated in this third injection pipe.
This third injection pipe will ensure the lubrication and cooling of the drive, whereby this drive can take on the form of a motor with the necessary transmissions and gear wheels.
The control of the cooler 19, 21 and the controllable valve 20, 22 in this third injection pipe can be controlled in the same way as for the other two injection pipes 17a, 17b, whereby in this case it will be ensured that the quantity and temperature of the injected liquid are optimised for the requirements of the drive.
Although in the example shown the injection circuit 17 comprises two separate separated injection pipes 17a, 17b both of which start from the liquid separator 13, it is not excluded that only one injection pipe 17a, 17b starts from the liquid separator 13, whereby this injection pipe 17a, 17b is split at a location downstream from the liquid separator 13 and upstream from the controllable valve 20. This location can be between the cooler 19 and the controllable valve 20, for example.
An advantage of this is that only one connection between the injection circuit 17 and the liquid separator 13 has to be provided and that the cooler 21 may be omitted.
In this case a three-way valve 24 is provided at the tap-off of the bypass pipe 23 upstream from the cooler 19 to control the quantity of liquid that can flow via the bypass pipe 23 and via the cooler 19.
The operation of the compressor device 1 is largely analogous to the operation of the embodiment of
Only the control of the controllable valve 20 and the cooler 19 for the temperature and the flow rate of the liquid supply to the compression space 4 will be done differently in this embodiment.
When the temperature T at the outlet 6 is still lower than the set value Tset, the three-way valve 24 will send a proportion of the liquid supply through the bypass pipe 23 instead of through the cooler 19. The liquid that flows through the bypass pipe 23 will not be cooled so that the cooling capacity of the injected liquid in the compression space 4 will decrease.
If necessary, an ever greater proportion of the liquid supply will be sent through the bypass pipe 23 to decrease the cooling capacity and let the temperature T rise above the set value Tset.
When all the liquid is sent through the bypass pipe 24 and the temperature T is still too low, the quantity of liquid that is injected will be reduced by closing the three-way valve 24 so that less liquid is allowed through.
The quantity of liquid will be decreased until the temperature T is at least equal to the set value Tset.
Using the cooler 19 and the three-way valve 24 whereby the oil 15 can be sent partly through the bypass pipe 23 and partly through the cooler 19, the cooling capacity can be controlled continuously without the quantity of injected liquid, i.e. the flow rate of the liquid supply, having to be changed for this purpose.
Moreover, only in the last instance is the quantity of injected liquid reduced so that the lubrication and the seal between the rotors 7 and/or the rotors 7 and the housing 3 by the liquid is not reduced.
An analogous control can also be used to ensure that the temperature T at the outlet 6 is not higher than a set value Tmax.
This set value Tmax is limited by an ISO standard and its maximum value is for example equal to the degradation temperature Td of the liquid. If need be, the set value Tmax can be a few degrees less than this degradation temperature Td in order to build in a certain safety, for example 1° C., 5° C. or 10° C., depending on the level of extra safety that is desired or necessary.
If the temperature T at the outlet 6 is higher than the set value Tmax, the three-way valve 24 will increase the flow of the liquid supply that is injected via the bypass pipe 23 into the compression chamber 4 until the temperature T at the outlet 6 falls to the set value Tmax.
If the maximum quantity of liquid is already being injected or if the temperature T at the outlet 6 is still too high when the maximum quantity of liquid is being injected, the three-way valve 24 will send at least a proportion of the liquid supply through the cooler 19.
If this was already the case or if it is insufficient, a larger proportion of the liquid supply will gradually be sent through the cooler 19 until the temperature T falls sufficiently.
When it turns out to be necessary to send the entire liquid supply through the cooler 19 and the cooling capacity is still insufficient to bring the temperature T down to the set value Tmax, then the cooler 19 will switch on, whereby the cooling capacity is increased.
As a result the liquid in the cooler 19 will be cooled more.
The cooling capacity of the cooler 19 is increased until the temperature T at the outlet 6 is, at a maximum, equal to the set value Tmax.
Through a combination of both methods for controlling the temperature, it can be ensured that the temperature T is kept within certain limits in order to increase the lifetime of the liquid and the compressor installation 1.
Moreover, such a method will ensure that the cooler 19 is always switched off first or switched on last when the cooling capacity of the injection circuit 17 has to be decreased or increased respectively, which will provide an energy saving.
In this case the aforementioned bypass pipe 23 only extends across the controllable valve 20, which is constructed as a throttle valve for example.
The bypass pipe 23 acts as a safety device if the controllable valve 20 fails so that it can always be ensured that a liquid supply to the compression space 4 is possible.
In this case a third independent injection pipe 17c is provided that starts from the liquid separator 13 and leads to the inlet 5.
A cooler 25 is also incorporated in this third injection pipe 17c. In this case a controllable valve 26 is also provided to control the liquid flow rate.
Atomisation 27 is also provided in the third injection pipe 17c at the location of the inlet 5.
This atomisation 27 will atomise, i.e. spray or nebulise, the liquid supply so that the liquid will go into the inlet 5 as small droplets.
Due to this atomisation the heat transfer between the gas and the liquid will be optimum because a greater contact area between the two is created.
The magnitude of the heat transfer will be determined, among others, by the size of the liquid droplets and their distribution in the gas flow.
The atomisation 27 can comprise a number of high frequency vibrating rods and injection nozzles. An alternative can be an atomisation 27 based on the jet expansion of gas/liquid mixtures.
Preferably the atomisation 27 can be controlled in order to control the size of the droplets and to be able to adapt the distribution of the droplets.
For the third injection pipe 17c the temperature of the liquid supply can be controlled by means of the cooler 25, and the flow rate by means of the controllable valve 26, and the spray by means of the atomisation 27.
This will enable the liquid to be injected and atomised in the inlet 5 with an optimum distribution of small liquid droplets and with the desired temperature and flow rate whereby it can respond to the changing (environmental) parameters and requirements regarding lubrication, sealing and cooling.
According to the invention the aforementioned liquid can be oil or water.
The present invention is by no means limited to the embodiments described as an example and shown in the drawings, but such a method for controlling the liquid injection of a compressor device and a liquid-injected compressor device can be realised according to different variants without departing from the scope of the invention.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2016/5147 | Mar 2016 | BE | national |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/BE2016/000044 | 8/23/2016 | WO |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2017/096438 | 6/15/2017 | WO | A |
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| Number | Date | Country | |
|---|---|---|---|
| 20180363652 A1 | Dec 2018 | US |
| Number | Date | Country | |
|---|---|---|---|
| 62266092 | Dec 2015 | US |
