EP2820307B1 - Volumetric screw compressor - Google Patents
Volumetric screw compressor Download PDFInfo
- Publication number
- EP2820307B1 EP2820307B1 EP13712324.6A EP13712324A EP2820307B1 EP 2820307 B1 EP2820307 B1 EP 2820307B1 EP 13712324 A EP13712324 A EP 13712324A EP 2820307 B1 EP2820307 B1 EP 2820307B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- main body
- oil
- compression chamber
- liquid
- suited
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 230000006835 compression Effects 0.000 claims description 65
- 238000007906 compression Methods 0.000 claims description 65
- 238000000926 separation method Methods 0.000 claims description 33
- 239000007788 liquid Substances 0.000 claims description 30
- 239000000203 mixture Substances 0.000 claims description 30
- 238000002347 injection Methods 0.000 claims description 12
- 239000007924 injection Substances 0.000 claims description 12
- 238000001914 filtration Methods 0.000 claims description 5
- 230000001050 lubricating effect Effects 0.000 claims description 3
- 230000003134 recirculating effect Effects 0.000 claims 1
- 238000011084 recovery Methods 0.000 description 9
- 238000004519 manufacturing process Methods 0.000 description 6
- 239000002245 particle Substances 0.000 description 5
- 238000010276 construction Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 238000007599 discharging Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 230000010354 integration Effects 0.000 description 2
- 238000005461 lubrication Methods 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 238000009435 building construction Methods 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000005065 mining Methods 0.000 description 1
- 238000010120 permanent mold casting Methods 0.000 description 1
- 238000000746 purification Methods 0.000 description 1
- 238000007528 sand casting Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2/00—Rotary-piston machines or pumps
- F04C2/08—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C2/12—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
- F04C2/14—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
- F04C2/16—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/08—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C18/12—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
- F04C18/14—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
- F04C18/16—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/30—Casings or housings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/02—Lubrication; Lubricant separation
- F04C29/026—Lubricant separation
Definitions
- the present invention is related to the technical field of the devices for the generation of compressed gas, preferably compressed air.
- the present invention concerns the technical field of volumetric compressors.
- the present invention concerns an oil-injected volumetric screw compressor.
- compressors are based on the intake of a gas, typically air, and the treatment of the same to increase its pressure while it flows towards an outlet.
- the compressors of the known type are constituted by the so-called oil-injected volumetric screw compressors.
- Said compressors typically comprise a casing that defines a compression chamber provided with a intake duct and a delivery duct. Inside the compression chamber there are two helical rotors, a male (generally driving) rotor and a female (generally driven) rotor that mesh with each other.
- the compression chamber is fed with oil and the air to be compressed.
- the compression of the air-oil mixture takes place in the volume included between the toothing of the two rotors and the casing.
- the contact section included between the profile of the male rotor and that of the female rotor shifts. More particularly, said contact section shifts starting from the intake duct towards the delivery duct. In this way, the air-oil mixture included between the contact section and the delivery duct is compressed.
- the air-oil mixture flowing out of the compression chamber is then subjected to a treatment to separate the oil from the compressed air.
- the separated oil is then recovered in order to be re-used and re-introduced in the compression chamber.
- the separation sector is thus arranged downstream of the compression chamber.
- the separation sector typically comprises a tank.
- the oil particles are separated from the compressed air due to a mechanical effect.
- the air-oil mixture flowing out of the compression chamber is directed towards the tank through a channel, typically a pipe. Inside the tank the separated oil particles are deposited on the bottom of the tank, while the compressed air remains in the upper portion of the same.
- the oil is collected from the bottom of the tank in order to recirculate it, as explained above, while on the other hand the compressed air is collected from the upper portion of the tank, further purified from any oil residues, and then made available to be let out at the desired pressure.
- a drawback posed by the screw compressors of the known type lies in their construction complexity that is due to the need to channel the various flows along pre-determined paths, to feed oil and air into the compression chamber, to convey the oil-air mixture to the separation tank and to recirculate the oil.
- a further drawback of said compressors is constituted by their considerable overall dimensions, in particular due to the size of the oil-air mixture separation tank.
- the main object of the present invention is thus to solve or at least partially overcome the above mentioned problems that characterize the volumetric screw compressors known in the state of the art.
- the present invention is based on the general consideration that the problems found in the art can be at least partially resolved by providing a gas compression device that uses a compression liquid, wherein one or more of the gas and/or liquid conveying elements are integrated in a single block or main body.
- the subject of the present invention is thus a gas compression device of the type comprising:
- the separation means are preferably housed at least partially in the main body. According to a preferred embodiment of the invention, the connection channel is completely made in the main body.
- the separation means preferably comprise an element suited to convey the mixture against a surface of the main body.
- the device comprises a tank arranged downstream of the separation means so as to receive at least the separated liquid of the mixture.
- the tank is suited to be removably associated with the main body.
- the device comprises a liquid recirculation circuit running from the tank to the compression chamber.
- the recirculation circuit comprises a channel for injecting the liquid in the compression chamber, wherein the injection channel is at least partially made in the main body.
- thermostatic valve is properly arranged along the liquid recirculation circuit.
- the thermostatic valve comprises a body carried out in a single piece with the main body.
- Means for filtering the liquid are preferably arranged along the liquid recirculation circuit.
- the liquid filtering means comprise a filter that is accommodated in a supporting seat carried out in a single piece with the main body.
- the device preferably comprises means for injecting the gas in the compression chamber.
- the device comprises a valve body of the intake valve, wherein the valve body is carried out in a single piece with the main body.
- the device preferably comprises conveying means arranged downstream of the separation means in order to convey the separated gas of the mixture to an oil separator filter.
- the conveying means comprise a gas ejection channel, wherein the ejection channel is at least partially made in the main body.
- the device comprises a liquid recovery channel suited to convey the liquid recovered by the oil separator filter to the compression chamber.
- the liquid recovery channel is at least partially made in the main body.
- the device comprises a viewing element for the inspection of the liquid recovery channel.
- the compression means comprise two helical screws meshing with each other.
- the helical screws are advantageously arranged along respective longitudinal rotation axes that are substantially parallel to each other.
- the hydraulic connection channel comprises at least one section aligned along a corresponding axis that intersects one of the rotation axes of the helical springs.
- the device comprises canalization means suited to convey the liquid used to lubricate the moving parts of the device.
- liquid conveying means convey the liquid to the sliding bearings of the helical screws.
- the canalization means preferably comprise one or more channels made inside the main body.
- the liquid is preferably constituted by oil.
- the gas is preferably constituted by air.
- the present invention can be applied in particular to the production of volumetric compressors used in various sectors, for example in the mining sector, in building construction or in the industrial sector.
- the present invention can be especially but not exclusively applied for the production of an oil-injected volumetric screw compressor powered by means of an electric motor.
- the present invention is not limited to such application.
- the present invention can be conveniently applied in all the cases requiring the use of a volumetric screw compressor, for example an engine-driven or motor-driven compressor (internal compression engine/motor).
- an engine-driven or motor-driven compressor internal compression engine/motor
- FIG 1 schematically shows the operating principle of a preferred embodiment of the oil-injected screw compressor 1 according to the present invention, hereinafter simply referred to as the "compressor".
- the compressor 1 substantially carries out a compression treatment on an incoming gas flow Fi, typically air, with a compression liquid, typically oil, in order to obtain an outgoing flow of compressed gas Fu.
- the oil-injected screw compressor 1 is a type of machinery of the volumetric rotary type. It is constituted by a compression chamber 2 containing two helical rotors, a male (generally driving) rotor and a female (generally driven) rotor that mesh with each other, as is explained in greater detail below.
- the compression of the gas-oil mixture takes place in the volume included between the toothing of the two rotors and the body that defines the compression chamber 2; during rotation, the contact section included between the profile of the male rotor and the profile of the female rotor shifts starting from an intake side towards a delivery side, so that the quantity of air contained therein is compressed due to the reduction in the available volume.
- the compressor 1 comprises an air intake valve 3, provided with an apposite intake filter 4, suited to convey the air into the compression chamber 2.
- the compressor 1 comprises an oil supply inlet 5 suited to convey the oil into the compression chamber 2.
- Moving means 6 allow the driving rotor to rotate inside the compression chamber 2.
- the compressor 1 also comprises a separation sector 7 arranged downstream of the compression chamber 2, in which the compressed oil-air mixture is subjected to a separation treatment in order to provide, at the outlet, compressed air 8 on one side and oil 9 on the other side.
- the separated oil 9 is recovered in order to be re-introduced in the compression chamber 2 through said supply inlet 5.
- the re-introduction of said oil 9 into the compression chamber 2 is conditional on its previous passage in a thermostatic valve 10 that allows the oil 9 to flow through it towards the supply inlet 5 only if its temperature is below a pre-determined limit temperature. In fact, the oil inside the compression chamber 2 is subjected to a temperature increase.
- the thermostatic valve therefore, allows only oil at the correct temperature to flow through it, while the oil at higher temperature is conveyed to an oil cooler 11 that lowers its temperature before it is re-introduced in the recirculation circuit.
- Upstream of the oil supply inlet 5 there is preferably a filter 12 suited to purify the oil from any impurities.
- the separated compressed air 8 is first conveyed to an oil separator filter 13 that separates any oil residues present in the compressed air.
- the recovered residual oil is re-introduced in the compression chamber 2.
- an oil recovery viewing element 14 that allows the oil to be monitored.
- the purified compressed air flowing out of the oil separator filter 13 passes through a minimum pressure valve 15. Said valve 15 allows the passage of air through it only when the pre-determined rated pressure has been reached.
- the air flowing out of the minimum pressure valve is preferably directed towards a cooler 16 where it is cooled down.
- the cooled air is then conveyed to a usage tank 17, or alternatively directly to the user.
- Part of the purified compressed air flowing out of the oil separator filter 13 is conveyed to the intake valve 3 through an apposite channel 58.
- the air conveyed through said channel 58 represents the feedback signal that signals to the intake valve 3 when the air passage must be closed or opened.
- the intake valve 3 is opened. If, on the contrary, the air pressure in said channel 58 is higher than or equal to the pre-determined rated pressure of the compressor, the intake valve 3 is closed.
- the compressor 1 is described here below with reference to Figures from 2 to 12, indicating the various parts mentioned above.
- the main body 30 is preferably produced by means of a permanent mold casting process, preferably through a metallic material casting process.
- the metallic material preferably comprises aluminium.
- the main body 30 can advantageously be obtained by sand casting of a cast iron alloy.
- a tank 40 suited to collect the air 8 and the oil 9 generated downstream of the separation means 7.
- the oil tank 40 is preferably suited to be connected to the main body 30 by means of screws, as shown in Figure 6 , in such a way as to obtain a removable structure.
- the tank is advantageously provided with an oil discharge valve 80.
- first rotor 21 with helical toothing, or male rotor and a second rotor 22 with helical toothing, or female rotor, which meshes with the first rotor 21.
- the two rotors 21 and 22 are arranged substantially parallel to each other and rotate along corresponding rotation axes substantially parallel to the main axis X of the compression chamber 2.
- the first rotor 21 is the driving rotor and is suited to be connected at one end 24 to the power means 6.
- the second rotor 22 is the driven rotor and is set rotating by the first rotor 21.
- the power means 6 preferably comprise an electric motor directly connected to the end 24 of the first rotor 21.
- the power means may be of a different type, like for example a combustion engine, or they may be provided with an indirect, remote connection to a motor, for example through the interposition of a driving belt or gears.
- the first rotor 21 preferably comprises four lobes suited to be engaged in seats provided in the second rotor 22. Said seats are five in the embodiment illustrated herein.
- the number of lobes and/or seats of the two rotors 21, 22 may be different.
- the top of the main body 30 is associated with the air intake valve 3 with the respective filter 4.
- the air intake valve 3 comprises a valve body 31 that houses internal valve means, fixed to the valve body through suitable connection means, for example through screws.
- the valve body 31 is preferably carried out in a single piece with the main body 30.
- the air intake valve 3 communicates with the compression chamber 2 through an apposite air intake channel 32.
- Said air intake channel 32 is preferably provided in the main body 30, as shown in Figure 9 .
- this is achieved through a recirculation circuit that draws the oil from the bottom of the tank 40 in order to re-introduce it in the compression chamber 2.
- the oil present on the bottom of the tank 40 is drawn, due to the effect of pressure inside the tank 40, through a suction pipe 41, visible in Figure 6 , and then conveyed to the thermostatic valve 10.
- the thermostatic valve 10 directs the oil flow directly to the oil filter 12 and from there to the compression chamber 2. If the oil temperature exceeds the limit temperature, the thermostatic valve 10, instead, directs the oil flow towards a cooler, not illustrated herein, through a duct connected to an apposite outlet 42. The oil cooled by the cooler is re-introduced upstream of the thermostatic valve 10 through a duct connected to an apposite inlet 43.
- the body 46 of the thermostatic valve 10 is preferably carried out in a single piece with the main body 30.
- the supporting seat 55 of the oil filter 12 is preferably carried out in a single piece with the main body 30.
- the oil flowing out of the oil filter 12 is conveyed to the compression chamber 2 through an oil injection channel 47, shown in Figure 8 .
- the oil injection channel 47 is advantageously defined inside the main body 30.
- the oil performs also a lubricating function with regard to some parts of the compressor.
- the sliding elements, or bearings, that support the rotors 21, 22 need lubricating.
- the oil in the system is also properly channelled in such a way as to reach those parts.
- One of said lubrication channels 49 shown in Figure 9 , allows a minimum quantity of oil taken from the oil injection channel 47 to be conveyed to one end of the compression chamber, in the area where there are the bearings of the rotors 21, 22.
- said lubrication channel 49 is defined inside the main body 30.
- the oil-air mixture is thrust from the compression chamber 2 towards an outlet opening 50 by the combined action of the two rotors 21 and 22, as shown in Figure 9 .
- the mixture is channelled from said outlet opening 50 towards the separation means 7.
- the canalization of the mixture takes place through a hydraulic connection channel 51.
- the hydraulic connection channel 51 is advantageously made in the main body 30.
- the hydraulic connection channel 51 is substantially aligned along an inclined axis Y. Said axis Y of the hydraulic connection channel 51 intersects the main axis X of the compression chamber 2, as visible in Figure 9 , and thus intersects also the respective rotation axes of the first and second rotor 21 and 22.
- the separation means 7, as illustrated in Figures 9 , 10 and 11 , are arranged under the compression chamber 2 and are preferably confined in a hollow portion 33 of the main body 30.
- the hollow portion 33 is defined by a side perimeter wall 34 of the main body 30.
- the side perimeter wall 34 is advantageously made in a single piece with the main body 30.
- the separation means 7 comprise an injection element 52 suited to receive the pressurized mixture from the hydraulic connection channel 51 and to convey said mixture against the internal surface of the side perimeter wall 34.
- the oil particles are separated from the compressed air due to a mechanical effect.
- the flow of the mixture is directed towards a given route, indicatively shown by the arrow D1 in Figure 11 .
- the special geometric configuration of the side wall 34 makes it possible to reduce the flow speed and thus to separate the oil particles from the air.
- the compressed air separated from the oil instead, remains in the upper portion 40a of the tank 40.
- the separation means 7 are partially defined by the lower portion of the main body 30 and positioned in proximity to the compression chamber 2.
- the injection element may come in different shapes, and it may also be made in a single piece with the main body 30.
- the separated compressed air 8 is in the upper portion 40a of the tank 40.
- the compressed air is drawn from said area 40a through an ejection channel 60 in order to be conveyed to the oil separator filter 13.
- Said filter 13 allows the purification of the compressed air through the elimination of residual oil particles left therein after the separation step.
- the first portion 60a of the air ejection channel 60 is advantageously carried out inside the main body 30.
- the oil separator filter 13 comprises a first outlet 61 for the purified compressed air and a second outlet 62 for the oil recovered after filtering, as can be seen in Figure 12 .
- the recovered oil is re-introduced in the compression chamber 2 through a suitable oil recovery channel 62.
- the oil recovery channel 62 is partially carried out inside the main body 30.
- the oil recovery viewing element 14 is advantageously positioned along the oil recovery channel 62. Said viewing element 14 makes it possible to monitor the presence of oil inside the oil recovery channel 62 and thus inside the compressor 1.
- the purified air flowing out of the oil separator filter 13 passes through the minimum pressure valve 15.
- the outgoing flow of compressed air Fu can be preferably stored in a suitable air tank for future use.
- the presence of a main body 30 provided with channels for the flow of oil and/or air and/or the air-oil mixture makes it possible to reduce to a minimum the length of the routes covered by said fluids and thus to reduce the pressure drops in the corresponding flows.
- a further advantage obtained through the present invention derives from the integration of several parts of the compressor in the main body 30.
- elements like the side perimeter wall 34 of the separation means 7, the valve body 31 of the air intake valve 3, the body 46 of the thermostatic valve 10, the supporting seat 55 of the oil filter 12 are advantageously carried out in a single piece with the main body 30.
- the tank 40 can be associated with the main body 30 of the compressor 1 through screws. Furthermore, the separation means 7 are substantially confined in the overall volume of the main body 30. Said characteristics make the tank 40 easy to replace to equip the compressor with a tank having a different shape and/or volume.
- the tank may be configured so that it can be placed in a remote position with respect to the main body 30, and in this case a collection element may be provided that can be applied to the underside of the main body 30 downstream of the separation means 7, for example a funnel-shaped element that collects the separated oil and conveys it to the remote tank.
- a suitable suction unit will then be provided to bring the oil from the remote tank back to the compression chamber 2 so as to allow recirculation.
- Figures 13 and 14 show a variant embodiment of the invention.
- valve body 131 of the intake valve 3 constitutes a separate element that can be applied to the main body 130.
- the other elements, that is, the side perimeter wall 34 of the separation means 7, the valve body 46 of the thermostatic valve 10 and the supporting seat 55 of the oil filter 12 are advantageously carried out in a single piece with the main body 130.
- FIGS 15 and 16 show another variant embodiment of the invention.
- the supporting seat of the oil filter 12 constitutes a separate element with respect to the main body 230.
- the supporting seat of the oil filter 12 can be applied directly to the main body 230 in an apposite channel 231.
- the supporting seat of the oil filter 12 is suited to be connected to the main body 230 through a duct connected to the same channel 231.
- the other elements that is, the side perimeter wall 34 of the separation means 7 and the body 46 of the thermostatic valve 10, are advantageously carried out in a single piece with the main body 230.
- Figures 17 and 18 show a further variant embodiment of the invention.
- Said embodiment differs from the one previously described with reference to Figures 15 and 16 in that the body of the thermostatic valve, not illustrated herein, constitutes a separate element that can be applied to the main body 330.
- the side perimeter wall 34 of the separation means 7 is advantageously made in a single piece with the main body 330.
- the compressor that is the subject of the invention achieves all the set objects, and in particular achieves the object to provide a volumetric screw compressor having reduced size and weight compared to the compressors of the known type, though ensuring higher reliability and efficiency.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
- Refuse Collection And Transfer (AREA)
- Separation By Low-Temperature Treatments (AREA)
- Supercharger (AREA)
- Compressor (AREA)
Description
- The present invention is related to the technical field of the devices for the generation of compressed gas, preferably compressed air.
- In particular, the present invention concerns the technical field of volumetric compressors.
- In detail, the present invention concerns an oil-injected volumetric screw compressor.
- The use of devices for the generation of compressed gas is known in several sectors, typically in the industrial field but also in other fields.
- These compressed gas generation devices, hereinafter simply referred to as "compressors", are based on the intake of a gas, typically air, and the treatment of the same to increase its pressure while it flows towards an outlet.
- The compressors of the known type are constituted by the so-called oil-injected volumetric screw compressors.
- Said compressors typically comprise a casing that defines a compression chamber provided with a intake duct and a delivery duct. Inside the compression chamber there are two helical rotors, a male (generally driving) rotor and a female (generally driven) rotor that mesh with each other. The compression chamber is fed with oil and the air to be compressed. The compression of the air-oil mixture takes place in the volume included between the toothing of the two rotors and the casing. During the rotation of the two rotors, the contact section included between the profile of the male rotor and that of the female rotor shifts. More particularly, said contact section shifts starting from the intake duct towards the delivery duct. In this way, the air-oil mixture included between the contact section and the delivery duct is compressed.
- The air-oil mixture flowing out of the compression chamber is then subjected to a treatment to separate the oil from the compressed air.
- The separated oil is then recovered in order to be re-used and re-introduced in the compression chamber.
- The separation sector is thus arranged downstream of the compression chamber. According to the known art, the separation sector typically comprises a tank. The oil particles are separated from the compressed air due to a mechanical effect. The air-oil mixture flowing out of the compression chamber is directed towards the tank through a channel, typically a pipe. Inside the tank the separated oil particles are deposited on the bottom of the tank, while the compressed air remains in the upper portion of the same.
- On the one hand, the oil is collected from the bottom of the tank in order to recirculate it, as explained above, while on the other hand the compressed air is collected from the upper portion of the tank, further purified from any oil residues, and then made available to be let out at the desired pressure.
- The screw compressors belonging to the state of the art, however, pose some drawbacks.
- A drawback posed by the screw compressors of the known type lies in their construction complexity that is due to the need to channel the various flows along pre-determined paths, to feed oil and air into the compression chamber, to convey the oil-air mixture to the separation tank and to recirculate the oil.
- First of all, this leads to a high production cost of the various parts making up the compressor and to considerable assembly time and costs.
- Another drawback posed by said compressors and related to their construction complexity is constituted by their limited reliability which is due to the presence of several parts that may get damaged over time.
- This construction complexity also leads to the need for complicated and costly operations for the maintenance and/or replacement of any damaged parts.
- A further drawback of said compressors is constituted by their considerable overall dimensions, in particular due to the size of the oil-air mixture separation tank.
- Another drawback of said compressors is represented by pressure drops along the channels of the oil, air and oil/air flows, which reduce the overall efficiency of the compressor.
- The main object of the present invention is thus to solve or at least partially overcome the above mentioned problems that characterize the volumetric screw compressors known in the state of the art.
- In particular, it is one object of the present invention to provide a volumetric screw compressor that is more efficient than the compressors of the known type. It is another object of the present invention to provide a volumetric screw compressor having reduced size and weight compared to the compressors of the known type.
- It is further object of the present invention to provide a volumetric screw compressor that is more reliable than the compressors of the known type.
- It is another object of the present invention to provide a volumetric screw compressor having reduced production and/or maintenance times and/or costs compared to the compressors of the known type.
- It is a further object of the present invention to provide a volumetric screw compressor that can be easily adapted to different power ranges and/or to different needs in terms of overall dimensions.
- The present invention is based on the general consideration that the problems found in the art can be at least partially resolved by providing a gas compression device that uses a compression liquid, wherein one or more of the gas and/or liquid conveying elements are integrated in a single block or main body.
- According to a first embodiment, the subject of the present invention is thus a gas compression device of the type comprising:
- a main body suited to define a compression chamber provided with an inlet for said gas;
- a liquid for the compression of said gas, suited to be injected in said compression chamber in order to obtain a mixture comprising said liquid and said gas;
- compression means arranged in said compression chamber and suited to compress said mixture towards an outlet of said compression chamber;
- separation means arranged downstream of said outlet and suited to receive said mixture and separate said liquid from said gas included in said mixture;
- connection means suited to connect said outlet to said separation means,
- The separation means are preferably housed at least partially in the main body. According to a preferred embodiment of the invention, the connection channel is completely made in the main body.
- The separation means preferably comprise an element suited to convey the mixture against a surface of the main body.
- Advantageously, the device comprises a tank arranged downstream of the separation means so as to receive at least the separated liquid of the mixture. According to a preferred embodiment of the invention, the tank is suited to be removably associated with the main body.
- Preferably, the device comprises a liquid recirculation circuit running from the tank to the compression chamber.
- According to an advantageous embodiment of the invention, the recirculation circuit comprises a channel for injecting the liquid in the compression chamber, wherein the injection channel is at least partially made in the main body.
- A thermostatic valve is properly arranged along the liquid recirculation circuit. According to a preferred embodiment of the invention, the thermostatic valve comprises a body carried out in a single piece with the main body.
- Means for filtering the liquid are preferably arranged along the liquid recirculation circuit.
- According to a preferred embodiment of the invention, the liquid filtering means comprise a filter that is accommodated in a supporting seat carried out in a single piece with the main body.
- The device preferably comprises means for injecting the gas in the compression chamber.
- In a preferred embodiment of the invention, the device comprises a valve body of the intake valve, wherein the valve body is carried out in a single piece with the main body.
- The device preferably comprises conveying means arranged downstream of the separation means in order to convey the separated gas of the mixture to an oil separator filter.
- According to a preferred embodiment of the invention, the conveying means comprise a gas ejection channel, wherein the ejection channel is at least partially made in the main body.
- Advantageously, the device comprises a liquid recovery channel suited to convey the liquid recovered by the oil separator filter to the compression chamber.
- Preferably, the liquid recovery channel is at least partially made in the main body.
- More preferably, the device comprises a viewing element for the inspection of the liquid recovery channel.
- In a preferred embodiment of the invention, the compression means comprise two helical screws meshing with each other.
- The helical screws are advantageously arranged along respective longitudinal rotation axes that are substantially parallel to each other.
- In a preferred embodiment of the invention, the hydraulic connection channel comprises at least one section aligned along a corresponding axis that intersects one of the rotation axes of the helical springs.
- Advantageously, the device comprises canalization means suited to convey the liquid used to lubricate the moving parts of the device.
- In a preferred embodiment of the invention the liquid conveying means convey the liquid to the sliding bearings of the helical screws.
- The canalization means preferably comprise one or more channels made inside the main body.
- The liquid is preferably constituted by oil.
- The gas is preferably constituted by air.
- Further advantages, objects and characteristics, as well as further embodiments of the present invention are defined in the claims and will be illustrated in the following description, with reference to the enclosed drawings; in the drawings, corresponding or equivalent characteristics and/or components of the present invention are identified by the same reference numbers. In particular:
-
Figure 1 shows a schematic view of the operating principle of a compressor according to a first embodiment of the invention; -
Figure 2 shows a side view of a compressor according to a first embodiment of the invention; -
Figure 3 shows a plan view of the compressor shown inFigure 2 in which some elements have been removed; -
Figure 4 shows an axonometric view of some parts of the compressor shown inFigure 2 ; -
Figure 5 showsFigure 4 from a different point of view; -
Figure 6 shows a partially exploded side view ofFigure 2 in which some elements have been removed; -
Figure 7 shows an enlarged detail ofFigure 4 ; -
Figure 8 shows a sectional view ofFigure 2 along line VIII-VIII in which some elements have been removed; -
Figure 9 shows a sectional view ofFigure 3 along line IX-IX; -
Figure 10 shows an axonometric view from below of the detail shown inFigure 7 ; -
Figure 11 shows a plan view from below of the detail shown inFigure 7 ; -
Figure 12 shows a sectional view ofFigure 3 along line XII-XII; -
Figure 13 shows a variant embodiment of the compressor shown inFigure 4 ; -
Figure 14 shows an enlarged detail ofFigure 13 ; -
Figure 15 shows another variant embodiment of the compressor shown inFigure 4 ; -
Figure 16 shows an enlarged detail ofFigure 15 ; -
Figure 17 shows a further variant embodiment of the compressor shown inFigure 4 ; -
Figure 18 shows an enlarged detail ofFigure 17 . - Although the present invention is described below with reference to its embodiments illustrated in the drawings, the present invention is not limited to the embodiments described below and illustrated in the drawings. On the contrary, the embodiments described below and illustrated in the drawings clarify some aspects of the present invention, the scope of which is defined in the claims.
- The present invention can be applied in particular to the production of volumetric compressors used in various sectors, for example in the mining sector, in building construction or in the industrial sector. In particular, the present invention can be especially but not exclusively applied for the production of an oil-injected volumetric screw compressor powered by means of an electric motor. It should however be noted that the present invention is not limited to such application. On the contrary, the present invention can be conveniently applied in all the cases requiring the use of a volumetric screw compressor, for example an engine-driven or motor-driven compressor (internal compression engine/motor). Here below is the description of some embodiments of the compressor according to the present invention; in the figures, similar or equivalent characteristics and/or component parts are identified by the same reference numbers.
-
Figure 1 schematically shows the operating principle of a preferred embodiment of the oil-injected screw compressor 1 according to the present invention, hereinafter simply referred to as the "compressor". - The compressor 1 substantially carries out a compression treatment on an incoming gas flow Fi, typically air, with a compression liquid, typically oil, in order to obtain an outgoing flow of compressed gas Fu.
- The oil-injected screw compressor 1 is a type of machinery of the volumetric rotary type. It is constituted by a
compression chamber 2 containing two helical rotors, a male (generally driving) rotor and a female (generally driven) rotor that mesh with each other, as is explained in greater detail below. The compression of the gas-oil mixture takes place in the volume included between the toothing of the two rotors and the body that defines thecompression chamber 2; during rotation, the contact section included between the profile of the male rotor and the profile of the female rotor shifts starting from an intake side towards a delivery side, so that the quantity of air contained therein is compressed due to the reduction in the available volume. - The compressor 1 comprises an
air intake valve 3, provided with anapposite intake filter 4, suited to convey the air into thecompression chamber 2. The compressor 1 comprises anoil supply inlet 5 suited to convey the oil into thecompression chamber 2. - Moving means 6 allow the driving rotor to rotate inside the
compression chamber 2. The compressor 1 also comprises aseparation sector 7 arranged downstream of thecompression chamber 2, in which the compressed oil-air mixture is subjected to a separation treatment in order to provide, at the outlet,compressed air 8 on one side andoil 9 on the other side. - The separated
oil 9 is recovered in order to be re-introduced in thecompression chamber 2 through saidsupply inlet 5. The re-introduction of saidoil 9 into thecompression chamber 2 is conditional on its previous passage in athermostatic valve 10 that allows theoil 9 to flow through it towards thesupply inlet 5 only if its temperature is below a pre-determined limit temperature. In fact, the oil inside thecompression chamber 2 is subjected to a temperature increase. The thermostatic valve, therefore, allows only oil at the correct temperature to flow through it, while the oil at higher temperature is conveyed to an oil cooler 11 that lowers its temperature before it is re-introduced in the recirculation circuit. Upstream of theoil supply inlet 5 there is preferably afilter 12 suited to purify the oil from any impurities. - The separated
compressed air 8 is first conveyed to anoil separator filter 13 that separates any oil residues present in the compressed air. - The recovered residual oil is re-introduced in the
compression chamber 2. Along the re-introduction circuit provided for the recovered oil there is preferably an oilrecovery viewing element 14 that allows the oil to be monitored. - The purified compressed air flowing out of the
oil separator filter 13 passes through aminimum pressure valve 15. Saidvalve 15 allows the passage of air through it only when the pre-determined rated pressure has been reached. - The air flowing out of the minimum pressure valve is preferably directed towards a cooler 16 where it is cooled down. The cooled air is then conveyed to a
usage tank 17, or alternatively directly to the user. - Part of the purified compressed air flowing out of the
oil separator filter 13 is conveyed to theintake valve 3 through anapposite channel 58. The air conveyed through saidchannel 58 represents the feedback signal that signals to theintake valve 3 when the air passage must be closed or opened. In particular, if the air pressure in saidchannel 58 is lower than the pre-determined rated pressure of the compressor 1, theintake valve 3 is opened. If, on the contrary, the air pressure in saidchannel 58 is higher than or equal to the pre-determined rated pressure of the compressor, theintake valve 3 is closed. - Further elements, not specifically indicated, are preferably provided in the compressor 1, like for example valves for discharging oil from the
separation sector 7, or safety valves, or valves for discharging the condensation present in theair tank 17 etc. - The compressor 1 is described here below with reference to Figures from 2 to 12, indicating the various parts mentioned above.
- In the compressor 1 it is first of all possible to identify a
main body 30, shown in particular inFigure 7 , inside which thecompression chamber 2 is defined. - The
main body 30 is preferably produced by means of a permanent mold casting process, preferably through a metallic material casting process. The metallic material preferably comprises aluminium. In variant embodiments of the invention, themain body 30 can advantageously be obtained by sand casting of a cast iron alloy. - On the underside of the
main body 30 there is atank 40 suited to collect theair 8 and theoil 9 generated downstream of the separation means 7. - The
oil tank 40 is preferably suited to be connected to themain body 30 by means of screws, as shown inFigure 6 , in such a way as to obtain a removable structure. - The tank is advantageously provided with an
oil discharge valve 80. - In the
compression chamber 2 there are, arranged longitudinally along a main axis X, afirst rotor 21 with helical toothing, or male rotor, and asecond rotor 22 with helical toothing, or female rotor, which meshes with thefirst rotor 21. The tworotors compression chamber 2. - In the embodiment illustrated herein, the
first rotor 21 is the driving rotor and is suited to be connected at oneend 24 to the power means 6. Thesecond rotor 22 is the driven rotor and is set rotating by thefirst rotor 21. - The power means 6 preferably comprise an electric motor directly connected to the
end 24 of thefirst rotor 21. - In variant embodiments of the invention the power means may be of a different type, like for example a combustion engine, or they may be provided with an indirect, remote connection to a motor, for example through the interposition of a driving belt or gears.
- The
first rotor 21 preferably comprises four lobes suited to be engaged in seats provided in thesecond rotor 22. Said seats are five in the embodiment illustrated herein. - In variant embodiments of the invention, however, the number of lobes and/or seats of the two
rotors - The top of the
main body 30 is associated with theair intake valve 3 with therespective filter 4. - The
air intake valve 3 comprises avalve body 31 that houses internal valve means, fixed to the valve body through suitable connection means, for example through screws. - The
valve body 31 is preferably carried out in a single piece with themain body 30. - The
air intake valve 3 communicates with thecompression chamber 2 through an appositeair intake channel 32. Saidair intake channel 32 is preferably provided in themain body 30, as shown inFigure 9 . - Regarding the oil supply to the
compression chamber 2, this is achieved through a recirculation circuit that draws the oil from the bottom of thetank 40 in order to re-introduce it in thecompression chamber 2. - The oil present on the bottom of the
tank 40 is drawn, due to the effect of pressure inside thetank 40, through asuction pipe 41, visible inFigure 6 , and then conveyed to thethermostatic valve 10. - If the oil temperature is correct, meaning below a limit temperature, the
thermostatic valve 10 directs the oil flow directly to theoil filter 12 and from there to thecompression chamber 2. If the oil temperature exceeds the limit temperature, thethermostatic valve 10, instead, directs the oil flow towards a cooler, not illustrated herein, through a duct connected to anapposite outlet 42. The oil cooled by the cooler is re-introduced upstream of thethermostatic valve 10 through a duct connected to anapposite inlet 43. - The
body 46 of thethermostatic valve 10 is preferably carried out in a single piece with themain body 30. - Also the supporting
seat 55 of theoil filter 12 is preferably carried out in a single piece with themain body 30. - The oil flowing out of the
oil filter 12 is conveyed to thecompression chamber 2 through anoil injection channel 47, shown inFigure 8 . - The
oil injection channel 47 is advantageously defined inside themain body 30. - As is known, in oil-injected screw compressors the oil performs also a lubricating function with regard to some parts of the compressor. In particular, the sliding elements, or bearings, that support the
rotors lubrication channels 49, shown inFigure 9 , allows a minimum quantity of oil taken from theoil injection channel 47 to be conveyed to one end of the compression chamber, in the area where there are the bearings of therotors lubrication channel 49 is defined inside themain body 30. - The oil-air mixture is thrust from the
compression chamber 2 towards anoutlet opening 50 by the combined action of the tworotors Figure 9 . The mixture is channelled from said outlet opening 50 towards the separation means 7. - According to the present invention, the canalization of the mixture takes place through a
hydraulic connection channel 51. Thehydraulic connection channel 51 is advantageously made in themain body 30. - The
hydraulic connection channel 51 is substantially aligned along an inclined axis Y. Said axis Y of thehydraulic connection channel 51 intersects the main axis X of thecompression chamber 2, as visible inFigure 9 , and thus intersects also the respective rotation axes of the first andsecond rotor - The separation means 7, as illustrated in
Figures 9 ,10 and 11 , are arranged under thecompression chamber 2 and are preferably confined in ahollow portion 33 of themain body 30. In particular, thehollow portion 33 is defined by aside perimeter wall 34 of themain body 30. Theside perimeter wall 34 is advantageously made in a single piece with themain body 30. - In this way the
hydraulic connection channel 51 is advantageously carried out completely in themain body 30. - In particular, the separation means 7 comprise an
injection element 52 suited to receive the pressurized mixture from thehydraulic connection channel 51 and to convey said mixture against the internal surface of theside perimeter wall 34. - The oil particles are separated from the compressed air due to a mechanical effect. The flow of the mixture is directed towards a given route, indicatively shown by the arrow D1 in
Figure 11 . The special geometric configuration of theside wall 34 makes it possible to reduce the flow speed and thus to separate the oil particles from the air. - Following this separation, the oil falls downwards due to gravity and it is collected in the
tank 40. - The compressed air separated from the oil, instead, remains in the
upper portion 40a of thetank 40. - Advantageously, according to the present invention the separation means 7 are partially defined by the lower portion of the
main body 30 and positioned in proximity to thecompression chamber 2. - This makes it possible to reduce to a minimum the length of the
hydraulic connection channel 51 between thecompression chamber 2 and the separation means 7, more particularly between theoutlet opening 50 and theinjection element 52. - This advantageously makes it possible to reduce the pressure drops in the mixture to a minimum.
- In other embodiments of the invention, the injection element may come in different shapes, and it may also be made in a single piece with the
main body 30. - As already explained, the separated
compressed air 8 is in theupper portion 40a of thetank 40. The compressed air is drawn from saidarea 40a through anejection channel 60 in order to be conveyed to theoil separator filter 13. Saidfilter 13 allows the purification of the compressed air through the elimination of residual oil particles left therein after the separation step. - The
first portion 60a of theair ejection channel 60 is advantageously carried out inside themain body 30. - The
oil separator filter 13 comprises afirst outlet 61 for the purified compressed air and asecond outlet 62 for the oil recovered after filtering, as can be seen inFigure 12 . - The recovered oil is re-introduced in the
compression chamber 2 through a suitableoil recovery channel 62. - Advantageously, the
oil recovery channel 62 is partially carried out inside themain body 30. - The oil
recovery viewing element 14 is advantageously positioned along theoil recovery channel 62. Saidviewing element 14 makes it possible to monitor the presence of oil inside theoil recovery channel 62 and thus inside the compressor 1. - The purified air flowing out of the
oil separator filter 13 passes through theminimum pressure valve 15. - The outgoing flow of compressed air Fu is available at the outlet of the
minimum pressure valve 15. - The outgoing flow of compressed air Fu can be preferably stored in a suitable air tank for future use.
- According to the present invention, the presence of a
main body 30 provided with channels for the flow of oil and/or air and/or the air-oil mixture makes it possible to reduce to a minimum the length of the routes covered by said fluids and thus to reduce the pressure drops in the corresponding flows. - This increases the overall efficiency of the compressor 1 and reduces its dimensions. This results in a compact structure of the compressor.
- Furthermore, such a type of canalization makes it possible to avoid the use of ducts to create the channels for the passage of the fluids, reducing to a minimum the moving parts of the compressor and also minimizing the risk of breakage and/or damage.
- This makes the compressor more reliable and reduces the time and costs required for the maintenance and/or production of the compressor.
- Furthermore, said techniques for making the main body allow the compressor's production time and costs to be reduced.
- A further advantage obtained through the present invention derives from the integration of several parts of the compressor in the
main body 30. In particular, elements like theside perimeter wall 34 of the separation means 7, thevalve body 31 of theair intake valve 3, thebody 46 of thethermostatic valve 10, the supportingseat 55 of theoil filter 12 are advantageously carried out in a single piece with themain body 30. - This results in the compact structure of the compressor, its reduced size, its reduced overall weight and greater reliability due to the integration of said elements.
- Said advantages with respect to the known art are at least partially obtained even if not all of the said elements are integrated in the main body, but only one or more of the same, as is explained below with reference to other embodiments of the invention.
- As explained above, the
tank 40 can be associated with themain body 30 of the compressor 1 through screws. Furthermore, the separation means 7 are substantially confined in the overall volume of themain body 30. Said characteristics make thetank 40 easy to replace to equip the compressor with a tank having a different shape and/or volume. - This makes it possible to customize the compressor based on the different characteristics required from time to time, which may vary according to the compressor power required or simply in order to adapt the external shape of the tank in case special sizes are needed or to satisfy specific aesthetic requirements. Again, the tank may be configured so that it can be placed in a remote position with respect to the
main body 30, and in this case a collection element may be provided that can be applied to the underside of themain body 30 downstream of the separation means 7, for example a funnel-shaped element that collects the separated oil and conveys it to the remote tank. A suitable suction unit will then be provided to bring the oil from the remote tank back to thecompression chamber 2 so as to allow recirculation. -
Figures 13 and 14 show a variant embodiment of the invention. - Said embodiment differs from the one previously described with reference to Figures from 2 to 12 in that the
valve body 131 of theintake valve 3 constitutes a separate element that can be applied to themain body 130. The other elements, that is, theside perimeter wall 34 of the separation means 7, thevalve body 46 of thethermostatic valve 10 and the supportingseat 55 of theoil filter 12 are advantageously carried out in a single piece with themain body 130. -
Figures 15 and 16 show another variant embodiment of the invention. - Said embodiment differs from the one previously described with reference to
Figures 13 and 14 in that the supporting seat of theoil filter 12, not illustrated herein, constitutes a separate element with respect to themain body 230. In a preferred embodiment of the invention, the supporting seat of theoil filter 12 can be applied directly to themain body 230 in anapposite channel 231. In other embodiments of the invention the supporting seat of theoil filter 12 is suited to be connected to themain body 230 through a duct connected to thesame channel 231. The other elements, that is, theside perimeter wall 34 of the separation means 7 and thebody 46 of thethermostatic valve 10, are advantageously carried out in a single piece with themain body 230. -
Figures 17 and 18 show a further variant embodiment of the invention. - Said embodiment differs from the one previously described with reference to
Figures 15 and 16 in that the body of the thermostatic valve, not illustrated herein, constitutes a separate element that can be applied to themain body 330. Theside perimeter wall 34 of the separation means 7 is advantageously made in a single piece with themain body 330. - The above clearly shows, therefore, that the compressor that is the subject of the invention achieves all the set objects, and in particular achieves the object to provide a volumetric screw compressor having reduced size and weight compared to the compressors of the known type, though ensuring higher reliability and efficiency.
- While the present invention has been described with reference to the particular embodiments shown in the figures, it should be noted that the present invention is not limited to the specific embodiments illustrated and described herein; on the contrary, further variants of the embodiments described herein fall within the scope of the present invention, which is defined in the claims.
Claims (18)
- Gas compression device (1), of the type comprising:- a main body (30; 130, 230; 330) suited to define a compression chamber (2) provided with an inlet (32) for said gas, said main body being a single block;- a compression liquid for said gas, suited to be injected in said compression chamber (2) in order to obtain a mixture comprising said liquid and said gas;- compression means (21, 22) arranged in said compression chamber (2) and suited to compress said mixture towards an outlet (50) of said compression chamber (2);- separation means (7) arranged downstream of said outlet (50) and suited to receive said mixture and separate said liquid from said gas included in said mixture;- a connection channel (51) suited to directly connect said outlet (50) to said separation means (7);characterized in that said connection channel (51) is completely made in said main body (30; 130,230; 330).
- Device according to claim 1, characterized in that said separation means (7) are at least partially housed in said main body (30; 130, 230; 330).
- Device (1) according to any of the preceding claims, characterized in that said separation means (7) comprise an element (52) suited to convey said mixture against a surface of said main body (30; 130,230; 330).
- Device (1) according to any of the preceding claims, characterized in that it comprises a tank (40) arranged downstream of said separation means (7) in order to receive at least said separated liquid of said mixture.
- Device (1) according to claim 4, characterized in that said tank (40) can be removably associated with said main body (30; 130, 230; 330).
- Device (1) according to claim 4 or 5, characterized in that it comprises a circuit for recirculating said liquid from said tank (40) to said compression chamber (2).
- Device (1) according to claim 6, characterized in that said recirculation circuit comprises an injection channel (47) for injecting said liquid in said compression chamber (2), said injection channel (47) being at least partially carried out in said main body (30; 130,230; 330).
- Device (1) according to claim 6 or 7, characterized in that a thermostatic valve (10) is arranged along said recirculation circuit of said liquid.
- Device (1) according to claim 8, characterized in that said thermostatic valve (10) comprises a body (46) carried out in a single piece with said main body (30; 130,230).
- Device (1) according to any of the claims from 6 to 9, characterized in that means (12) for filtering said liquid are arranged along said recirculation circuit.
- Device (1) according to claim 10, characterized in that said filtering means comprise a filter (12) that is housed in a supporting seat (55) carried out in a single piece with the main body (30; 130).
- Device (1) according to any of the preceding claims, characterized in that it comprises injection means (3) suited to inject said gas in said compression chamber (2).
- Device (1) according to claim 12, characterized in that said injection means (3) comprise an intake valve (3) for said gas.
- Device (1) according to claim 13, characterized in that it comprises a valve body (31) of said intake valve (3), said valve body (31) being carried out in a single piece with said main body (30).
- Device (1) according to any of the preceding claims, characterized in that it comprises conveying means (60) arranged downstream of said separation means (7) in order to convey said separated gas of said mixture to an oil separator filter (13).
- Device (1) according to any of the preceding claims, characterized in that it comprises canalization means (49) suited to convey said liquid for lubricating the moving parts of said device (1).
- Device (1) according to claim 16, characterized in that said canalization means comprise one or more channels (49) made inside said main body (30; 130, 230; 330).
- Device (1) according to any of the preceding claims, characterized in that said compression means comprise two helical screws (21, 22) meshing with each other.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT000036A ITVI20120036A1 (en) | 2012-02-14 | 2012-02-14 | VOLUMETRIC SCREW COMPRESSOR. |
PCT/IB2013/000088 WO2013121257A1 (en) | 2012-02-14 | 2013-01-24 | Volumetric screw compressor |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2820307A1 EP2820307A1 (en) | 2015-01-07 |
EP2820307B1 true EP2820307B1 (en) | 2016-03-09 |
Family
ID=46001613
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13712324.6A Active EP2820307B1 (en) | 2012-02-14 | 2013-01-24 | Volumetric screw compressor |
Country Status (8)
Country | Link |
---|---|
US (1) | US20150023825A1 (en) |
EP (1) | EP2820307B1 (en) |
CN (1) | CN104114868A (en) |
BR (1) | BR112014018802B1 (en) |
ES (1) | ES2569902T3 (en) |
IT (1) | ITVI20120036A1 (en) |
RU (1) | RU2610871C2 (en) |
WO (1) | WO2013121257A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105673498A (en) * | 2016-04-01 | 2016-06-15 | 浙江开山凯文螺杆机械有限公司 | Screw compressor with normally-open intake valve, and start method thereof |
DE202019104823U1 (en) | 2018-09-14 | 2019-11-07 | Atlas Copco Airpower, N.V. | Housing of a liquid separation device for separating a liquid from a gas-liquid mixture |
BE1026613B9 (en) | 2018-09-14 | 2020-06-08 | Atlas Copco Airpower Nv | Casing of a liquid separator for separating a liquid from a gas-liquid mixture |
DE202019104824U1 (en) | 2018-09-14 | 2019-10-24 | Atlas Copco Airpower, N.V. | Housing of a liquid separation device for separating a liquid from a gas-liquid mixture |
BE1027152B1 (en) | 2019-04-01 | 2020-10-26 | Atlas Copco Airpower Nv | Liquid separator for separating a liquid from a gas-liquid mixture |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3073514A (en) * | 1956-11-14 | 1963-01-15 | Svenska Rotor Maskiner Ab | Rotary compressors |
DE3149245A1 (en) * | 1981-12-11 | 1983-06-16 | Isartaler Schraubenkompressoren GmbH, 8192 Geretsried | "COMPRESSOR SYSTEM" |
JPH0642476A (en) * | 1992-07-24 | 1994-02-15 | Daikin Ind Ltd | Screw compressor |
DE19739279C2 (en) * | 1997-09-08 | 2001-02-01 | Maid Ludwig | Compressor system |
JP3994220B2 (en) * | 2000-09-01 | 2007-10-17 | 株式会社日立製作所 | Screw compressor |
JP4012706B2 (en) * | 2001-07-30 | 2007-11-21 | 株式会社日立産機システム | Oil-cooled screw compressor |
BE1014611A3 (en) * | 2002-02-08 | 2004-01-13 | Atlas Copco Airpower Nv | Method for oil return of driving in an oil injected screw compressor and thus controlled screw compressor. |
JP4102891B2 (en) * | 2003-01-31 | 2008-06-18 | 株式会社日立製作所 | Screw compressor |
JP4043433B2 (en) * | 2003-11-14 | 2008-02-06 | 株式会社神戸製鋼所 | air compressor |
-
2012
- 2012-02-14 IT IT000036A patent/ITVI20120036A1/en unknown
-
2013
- 2013-01-24 CN CN201380009325.XA patent/CN104114868A/en active Pending
- 2013-01-24 US US14/374,965 patent/US20150023825A1/en not_active Abandoned
- 2013-01-24 EP EP13712324.6A patent/EP2820307B1/en active Active
- 2013-01-24 ES ES13712324.6T patent/ES2569902T3/en active Active
- 2013-01-24 WO PCT/IB2013/000088 patent/WO2013121257A1/en active Application Filing
- 2013-01-24 RU RU2014137103A patent/RU2610871C2/en active
- 2013-01-24 BR BR112014018802-5A patent/BR112014018802B1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
RU2610871C2 (en) | 2017-02-17 |
ITVI20120036A1 (en) | 2012-05-15 |
CN104114868A (en) | 2014-10-22 |
RU2014137103A (en) | 2016-04-10 |
US20150023825A1 (en) | 2015-01-22 |
ES2569902T3 (en) | 2016-05-13 |
BR112014018802A2 (en) | 2017-06-20 |
EP2820307A1 (en) | 2015-01-07 |
WO2013121257A1 (en) | 2013-08-22 |
BR112014018802A8 (en) | 2017-07-11 |
BR112014018802B1 (en) | 2021-11-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2820307B1 (en) | Volumetric screw compressor | |
CN102635553B (en) | Water injection type screw compressor | |
JP4102891B2 (en) | Screw compressor | |
CN1209558C (en) | Spiral compressor | |
CN103511279A (en) | Rotary compressor and refrigeration equipment with the rotary compressor | |
CN203655636U (en) | Low-backpressure compressor | |
CN109477484A (en) | The rotary-vane vaccum pump of oil lubrication | |
US6991443B2 (en) | Oil injected screw compressor | |
EP2895745B1 (en) | Oil separator device for a volumetric compressor and volumetric compressor | |
JP5668371B2 (en) | Turbo compressor | |
CN204921363U (en) | Vortex formula air compressor machine | |
CN103775343A (en) | Horizontal compressor | |
CN104929931B (en) | A kind of vortex air compressor machine and its control method | |
CN203548231U (en) | Oil supply device of refrigeration helical-lobe compressor | |
CN200996380Y (en) | Sliding-valve vacuum pump with single-stage and multi-cylinders | |
CN201507449U (en) | Small flow capacity assembly type air compressor | |
CN104632619B (en) | Natural gas pressurizing and conveying system | |
CN114412643B (en) | Multi-stage oil return device integrating oil-gas separation function | |
EP3294992A1 (en) | Improved volumetric screw compressor | |
RU107295U1 (en) | INPUT MODULE OF SUBMERSIBLE PUMP UNIT WITH SLOT FILTER | |
CN116724174A (en) | Oil-cooled compressor | |
JPH055486A (en) | Oil injection type closed type scroll compressor | |
CN117511590A (en) | Atmospheric recovery device and recovery process thereof | |
RU33395U1 (en) | SLIMMER MODERNIZED NAGIYEVA (NOISE-N) | |
WO2002077461A1 (en) | Water-injected volumetric compressor |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20140903 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAX | Request for extension of the european patent (deleted) | ||
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
INTG | Intention to grant announced |
Effective date: 20150916 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 779747 Country of ref document: AT Kind code of ref document: T Effective date: 20160315 Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602013005390 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2569902 Country of ref document: ES Kind code of ref document: T3 Effective date: 20160513 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20160309 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160610 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160609 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160709 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160711 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602013005390 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 5 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 |
|
26N | No opposition filed |
Effective date: 20161212 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160609 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20170124 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170131 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170131 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170124 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170124 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 6 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170124 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170124 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20130124 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: UEP Ref document number: 779747 Country of ref document: AT Kind code of ref document: T Effective date: 20160309 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160309 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20231229 Year of fee payment: 12 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20240208 Year of fee payment: 12 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 20231227 Year of fee payment: 12 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20231228 Year of fee payment: 12 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20231218 Year of fee payment: 12 |