LIQUID RING COMPRESSOR

Abstract: The invention applies to a liquid ring compressor in which there is annular space (10) between the rotor (6) and the rotor axle (5), the annular space being connected with the rotor compression zone through two or more discharge openings (20, 15).

Description: Liquid rinσ compres sor The obj ect of the invention i s a liquid ring compres sor and vacuum pump . The known liquid ring compressor has a casing with a rotor inside, mounted off-centre. The casing contains liqui which is caused by the centrifugal force of the rotor to rotate along the periphery of the casing. Since the rotor i mounted off-centre, the inner surface of the liquid ring moves up and down in the rotor vane slots as the rotor turns. The slots are connected to the gas inlet when the liquid ring moves outwards, away from the bottom of slot. The slots are connected to the outlet when the distance between the liquid ring and the bottom of the slot is at minimum. During the compression phase the opening at the bottom of the slot is closed whereupon the liquid penetrating the slot compresses the gas. Since small amount of liquid leave the compressor along with the gas, a corresponding amount has to be continuously replaced. Liquid ring compressors are used in the processing industry, in particular for transferring large amounts of gas. These pumps are particularly useful when the gas contains solid impurities. One liquid ring compressor is presented in the publication US 3154240. The known liquid ring compressors have an in-built, essentially constant pressure ratio. This implies a need for extra power when the compressor is operated at a pressure ratio deviating from the design value. Furthermore, a constant pressure ratio causes problems when starting the pump, if there is no pressure difference between the inlet and the outlet. Now the liquid ring compressors defined more closely in the patent claim have been invented. The rotor of the now-invented liquid ring compressor is equipped with a flange to which the vanes are attached. At the opposite end, the vanes are connected to each other with a ring flange. The gas to be compressed is led from the compression zone of the rotor to a walled-off annular space, between the axle and rotor and from there to the outlet. One of the characteristics of the invention is that, preceding the actual discharge, there are in the walls of the annular space a number of intermediate outlets equipped with a valve. One of the characteristics of the invention is that the compressor casing is a drum rotating in the same direction as the rotor. One of the characteristics of the invention is that vanes become separated from the liquid ring at the induction zone. One of the characteristics of the invention is that the compressor is equipped with a cooling system with which liquid coolant can be injected into the vane slots. One of the characteristics of the invention is that there is an interconnection equipped with a valve from the outlet side of the compressor to the inlet side. One of the characteristics of the invention is that there are guide plates in the casing outside the rotor. One of the characteristics of the invention is that the slots in the induction phase are connected via grooves to the induction chamber. Some of the advantageous characteristics of the invention are described in detail below. The schematic figures are side projections in which - figure 1 displays a liquid ring compressor as per the invention, as seen parallel to the axle, i.e. from the front, - figure 2 is an alternative detail of the compressor in fig. 1 as seen from the front, - figure 3a displays another compressor as per the invention, as seen from the side, - figure 3b shows the compressor in fig. 3a as seen from th front, - figure 4 is a magnification of a detail from figure 3a, - figure 5 shows a third compressor as per the invention as seen from the front, - figure 6 shows a fourth compressor as per the invention as seen from the side, - figure 7 shows a fifth compressor as per the invention as seen from the front, - figure 8 shows the connections of compressors as per the invention. The liquid ring compressor shown in fig. 1 has a fixed cylindrical casing 1, and the casing a rotor 6 placed on an eccentrically moving axle 5. The rotor has an end flange to which the vanes 8, which are parallel to the axle, are attached. The other ends of the vanes 8 are connected with a ring flange 9. Between the vanes 8 and the axle 5 there is an annular space, which is separated with a wall from the axle 5 and from the slots between the vanes. The annular space is divided with the walls 23 into three sector-like spaces. Section 10.1 is connected to the inlet channel, section 10.3 to the outlet channel and section 10.2 to a separate outlet channel in which the pressure can be lower than in the outlet channel 10.3 There is liquid in the casing 1. As the rotor 6 revolves, the centrifugal force causes the liquid to form a ring on the periphery of the casing 1. The volume of the liquid is such that when the rotor 6 revolves, the tips of the vanes 8, when in the lowest position, barely penetrate the liquid. In the upper position the liquid touches the bottom of the vane slot. The inner surface of the liquid ring is represented by the line 19. The gas to . be compressed .is led along the induction channel to the section 10.1 of the annular space, which in turn is connected with the vane slots in the induction phase. As the vane slots turn from the induction phase to the compression phase, the liquid moving into the slot starts compressing the gas. When in the highest position, the slot passes the discharge opening 15 leading to the annular space 10.3. Ahead of the actual discharge opening are a number of intermediate outlets 20 equipped with valve 21, some of the issuing to the annular space 10.3 and others to the annular space 10.2. The valves can be non-return valves or positively controlled valves. The valves prevent the gas being compressed to a pressure essentially higher than the pressure in the outlet channel. The makes the starting easier, particularly when the compressor is used as a vacuu pump. From a compressor as . shown in fig. 1 some of the gas to be compressed can be discharged at a pressure lower than th final pressure. Figure 2 shows an alternative annular space which is divided with the discharge wall 23 into two sections. The first section 10.2 is connected with the compression zone via the intermediate discharge opening 20'. Some of the gas to be compressed can be discharged via the first section at a pressure lower than the final pressure. This is an essential benefit in many circulating processes. Using this arrangement, it is, for example, possible to improve the efficiency of a heat pump. Fig. 2 shows an example of the non-return valve 21. It has a conical opening tapering towards the outer surface of the wall and the corresponding breech 24. The breech 24 is controlled by the spring 25. When the pressure in the annular space 10.2 is higher, the breech is pressed against the edges of the opening. The compressor is also provided with the cooling system 22 with which cold liquid, preferably the same liquid that the liquid ring consists of, can be injected in a vane slot during the compression phase. The cooling system 22 includes a tube passing through the annular space 10.2, with a mouth and nozzle which are attached to the wall of the annular space. The efficiency of the compressor can be essentially improved by fitting, as shown in figs. 3a and 3b, a drum 3 on the axle 2 rotating between the casing 1 and the rotor. This way the friction of the liquid ring periphery is essentially diminished, since the speed of the liquid ring relative to the casing can be reduced. When the drum 3 and rotor 6 are rotating at the same circumferential velocity, the only difference in speed is the slip caused by the eccentricity. When the friction is decreased, the rotational speed can be correspondingly increased. Thus it is possible to use - higher pressure ratios and higher back pressure. Furthermore, higher centrifugal force makes it possible to regulate the speed over a higher capacity range, but the pressure difference causes no essential variations in the thickness of the liquid ring between the outlet and the inlet. The compressor shown in figures 3a and 3b has a fixed cylindrical casing 1, a drum axle 2 attached to the casing with a bearing, and a cylindrical drum 3 rotating in the casing fixed at the end of the axle. In the centre of the end furthest away from the drum axle there is an opening 4 On the opposite side is a rotor axle 5, which is placed above drum axle 2. Rotating on this axle is a rotor 6 which is placed inside the drum. The rotor 6 is equipped with end flange 7 attached to the end of the axle 5. The vanes 8 pointing towards the opening 4 are fixed to the flange 7. The opposite ends of the vanes 8 are connected to each othe with the ring flange 9. Between the vanes 8 and the axle 5 there is an annular space 10 connected to the drum through the openings 11 in the end flange 7. The inlet socket 12 of the gas to be compressed is attached to the casing 1. The gas enters the drum 3 through the openings 13 in the drum end close to the axle. Placed in the annular space 10 is the discharge channel 14 which is connected via 15 with the uppermost slot of the rotor 6. Separated from the discharge channel with a wall, the lower part of annular space 10 forms inlet channel 16 which is connected via 17 to the slots of the rotor in the induction phase. The height of the vanes 8 is higher at the bearing end of the axle 5 of the rotor 6 than at the other end, whereby the annular space is conical. This means that the inner surface 19 of the liquid ring at the topmost part of the casing 3 at the opposite end of the axle is below the botto edge of the flange 6 and the vanes 8 (fig. 4). This feature is used for sealing the space between the flange 6 and the 8 wall 18 of the discharge 14 by making threads on the lower edge of the flange. These threads tend to force water from the drum into the compression space. The seals 25 and 27 of the axles 2 and 5 are placed so that they can be serviced from outside the casing. The gas entering the drum 3 flows through the openings 11 to the annular space 10 and from there via the inlet opening 17 to the slots of vanes 8 in the induction phase. As the slots turn away from the opening 17, the liquid penetrating the slots starts compressing the gas until the slot reaches the topmost position at the discharge opening 15 through which the gas flows into the discharge channel 14. The applications shown in the figs. 3a and 3b can also have intermediate outlets (fig. 3b) closed with a valve in the compression zone of the rotor 6. The last discharge opening can also be closed with a valve. The intermediate openings can be used for bleeding gas at different pressures into separate discharge channels. In order to reduce the slip, the rotor and the drum are provided with ribs 45 and 46. Alternatively, the drum and the rotor may be rotated as positively guided in relation to each other. In the application as shown in the fig. 5, the off-set between the rotor 6 and the drum 3 has been increased and the rotor diameter has been correspondingly decreased whereby the tips of the vanes 8 lose contact with the liquid ring in the induction zone. In this case, the gas can be supplied over the periphery of the rotor. Even with this arrangement it is of course possible to use intermediate outlets, cooling 22 and rotary drum 3. In the application as shown in the fig. 5, there are groove-like vacuum relief channels 28 on the outer surface of the annular space 10 in the vacuum building area after the discharge. These channels 28 connect the induction zon with the slots that have just passed the outlet. This way the evaporation of the sealing liquid is prevented and the running is more even. In the arrangement where the liquid ri'rtg is disconnecte from the rotor 6 in the induction zone and the gas is led t the periphery of the rotor, several rotors 6 can be placed in the same drum 3. Such application is shown in figure 6. In it there are three rotors 6 in the drum 3. In the application as shown in the fig. 6, guide plates 29 attached to the casing 1 are used for improving the volumetric efficiency. These guide plates are placed immediately ahead of the rotor 6 compression zone so that the rear edge of the plate is in contact with the liquid ring. The inner edge 31 of the guide plate 29 is curved and it rests against the outer periphery of the rotor 6. The purpose of the guide plate 29 is to prevent the gas being compressed from discharging from the slot that is not yet sealed by the liquid ring. The guide plate 29' can also be used in construction as shown in fig. 5. In the arrangement shown in fig. 7, the axle 2 of the rotary drum is attached to the casing 1 with bearings at both ends. The drum 3 is fixed in the centre of the axle 2 with two flanges 32. The space between the flanges 32 is connected to the casing 1 via 33 and inside the drums 3 via 34. In both drums 3 thus created there are three rotors 6, placed off-set from each other. Figure 8 shows one arrangement for connecting the liquid ring compressor. The gas to be compressed is fed from the line 36 to the compressor 35. The replacement liquid is supplied from line 38 equipped" with control valve 37. The compressed gas and the sealing liquid contained in are supplied to the separating tank 39. In it the sealing liquid is separated from the gas and returned to the compressor 35 via the cooler 40. The gas is supplied from the separating tank 39 to the discharge line 42 equipped with a non-return valve 41. The discharge line 42 is connected via the interconnection 43 to the supply line 36. The interconnection is provided with a throttle valve 44. The throttle valve 44 is open when the compressor is started. When the valve 44 is gradually throttled, the compressor reaches the desired discharge pressure.

Claims: Patent claims 1. A liquid ring compressor consisting of: - a cylindrical casing (1/3), with at least one of the ends provided with an opening in the centre, - an axle (5) parallel to the longitudinal axis of the casing, placed off-centre through an opening in the casing, - on the axle a rotor (6) designed to rotate in the casing; on the rotor an end flange (7) attached to the axle and; attached to the rotor vanes (8) parallel to the axle connected at the other end with a ring flange (9), - an annular space (10) between the rotor and the axle; the annular space is separated from the casing with a cylindrical outer wall and end walls, - the casing is filled with a liquid which the rotating rotor forces to form a ring on the periphery of the casing, - a discharge opening (15) in the wall of the annular space at the end of the compression zone; the compression zone is the zone in which the inner surface of the liquid ring (19) approaches in the direction, of rotation the outer wall of the annular space, - a discharge channel (14) leading from the annular space through the opening at the end of the casing, and - a system for supplying gas into the casing to the rotor vane slots that are in the induction zone; the induction zone is the zone in which the inner surface, in the direction of rotation, moves away from the outer wall of annular space (10), c h a r a c t e r i z e d in that - in the wall of the annular space (10) there is at least one intermediate outlet (20) equipped with a valve and located ahead of the discharge opening (15). 2. A liquid ring compressor as per the patent claim no. 1, in which - the casing is a rotating drum (3), and - the rotor turns in the same direction as the drum. 3. A liquid ring compressor as per the patent claim no. 1 or 2, c h a r a c t e r i z e d in that - there is such an amount of liquid in the casing that the rotor vanes in the induction zone become separated from the inner surface of the liquid ring. 4. A liquid ring compressor as per one of the patent claims no. 1 to no. 4, c h a r a c t e r i z e d in that at least one of the intermediate outlets is a separate intermediate outlet (20') leading from the annular space to a intermediate discharge space separated with the outlet wall (23), from which intermediate outlet space there is a separate outlet channel leading thorough the opening in the end of the casing. 5. A liquid ring compressor as per one of the patent claims no. 1 to no. 4, c h a r a c t e r i z e d in that it is equipped with a cooling system (22) with which liquid can be injected into at least one vane slot in the compression or induction phase for the purpose of cooling down the gas to be compressed or the liquid ring. 6. A liquid ring compressor as per one of the patent claims no. I to o. 5, c h a r a c t e r i z e d in that there is an interconnection (43) equipped with a valve (4 from the outlet side to the inlet side of the pump. 7. A liquid ring compressor as per one of the patent claims no. 2 to no. 6, c h a r a c t e r i z e d in that rotor or the drum is equipped with ribs or wings to reduc the slip between the rotor and the drum or that the both rotate as positively guided in relation to each other. 8. A liquid ring compressor as per one of the patent claims no. 2 to no. 7, c h a r a c t e r i z e d in that the casing there are two drums attached on the same axle. 9. A liquid ring compressor as per one of the patent claims no. 1 to no. 8, c h a r a c t e r i z e d in that there is a guide plate (29) fitted outside the rotor periphery to improve the volumetric efficiency. 10. A liquid ring compressor as per one of the patent claims no. I to no. 9, c h a r a c t e r i z e d in that vane slots in the induction phase are connected via the grooves (28) with the inlet space. 11. A liquid ring compressor as per one of the patent claims no. 3 to no. 10, c h a r a c t e r i z e d in that there are two or more rotors in the casing.

Inventors: JUHOLA PENTTI, JUHOLA, PENTTI
Applicants: PENTAMO OY
Application year: 1989
Main classification: F04C19
IPC codes: F04C19, F04C29