Patent Publication Number: US-2023142730-A1

Title: Secondary-fluid supply for the diffuser of a compressor stage

Description:
FIELD OF THE INVENTION 
     Embodiments hereof relate to a compressor stage, in particular for a turbocharging system and/or a turbocompound, and a process for operating a compressor stage. 
     BACKGROUND OF THE INVENTION 
     Many applications utilising compression stages include injecting or recirculating a secondary fluid. For example, modern internal combustion engines oftentimes need to apply exhaust gas recirculation (EGR) to comply with current and future environmental regulations. 
     Different techniques have been developed for injecting or recirculating the secondary fluid. For internal combustion engines, low pressure EGR and high pressure EGR are commonly employed, depending on at which pressure level the EGR-gas is re-introduced into the air supply path of the engine. 
     Low pressure EGR comprises introducing the EGR gas at a low pressure level upstream of the impeller of the compression stage, which can lead to severe erosion and corrosion issues, especially with regards to the impeller material. 
     High pressure EGR comprises introducing the EGR gas downstream of the compression stage, which often requires an additional EGR blower to overcome the pressure difference between the secondary fluid from the engine exhaust manifold and a primary fluid from the air receiver. 
     One attempt to overcome the problems associated with high and low pressure EGR is to provide a link between the exhaust gas manifold and the zone right between impeller outlet and diffuser inlet. The high momentum primary fluid exiting the compressor impeller draws in and pressurises the EGR-gas like in a jet pump. 
     Current designs to inject exhaust gas into diffusers comprise slits or holes in the compression stage, which are connected to appropriate supply pipes or channels to inject the secondary fluid into the compressor main flow. The slits or holes are located between impeller outlet and diffuser inlet as this is downstream of the impeller—thus avoiding erosion and corrosion issues of the impeller—and upstream of the diffuser—where the static pressure is low enough to draw in the secondary flow stream. 
     This design, however, leads to operational issues as the diffuser limits the mass flow which can be pushed through the diffuser for given upstream total flow conditions. The diffuser is then either too small for the combined main (primary) and secondary flow (if the secondary flow is switched on) or too large for the main flow only, 
     BRIEF SUMMARY OF THE INVENTION 
     Briefly, a compressor stage and a process for operating a compressor stage are provided to overcome at least some of the abovementioned limitations. This object is accomplished by means of a compressor stage, in particular for a turbocharging system and/or a turbocompound, according to claim  1 , and a process for operating a compressor stage according to claim  15 . In particular, the object of the invention is to provide a compressor stage which allows for injection of a secondary fluid and concurrently is suitable for the combined (primary and secondary) flow rate both when the secondary flow is switched on as well as when it is switched off. 
     According to an embodiment, a compressor stage, in particular for a turbocharging system and/or a turbocompound, is provided. The compressor stage comprises an impeller and a vaned diffuser arranged downstream of the impeller. The vaned diffuser is in fluid connection with an outlet of the impeller. The vaned diffuser further comprises an injection device configured to inject a secondary fluid into the vaned diffuser. The injection device comprises a displaceable port at least partially arranged between an adjacent pair of vanes of the diffuser. 
     According to another embodiment, a process for operating a compressor stage for a turbocharging system and/or a turbocompound, in particular a compressor stage assembly according to any embodiments of the present disclosure, is provided. The process comprises determining a desired mass flow of a secondary fluid, in particular an exhaust gas, and determining an effective cross-section of a vaned diffuser of the compressor to maintain an impeller of the compressor within predetermined operating limits. The process further comprises adjusting a cross-section of the vaned diffuser to the effective cross-section, in particular by displacing a displaceable port of an injection device at least partially arranged between an adjacent pair of vanes of the diffuser. 
     Those skilled in the art will recognise additional features and advantages upon reading the following detailed description, and upon viewing the accompanying drawings. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
       The components in the Figures are not necessarily to scale, instead emphasis being placed upon illustrating the principles of the invention. Moreover, in the Figures, like reference signs designate corresponding parts. In the drawings: 
         FIG.  1 A  illustrates a portion of a compressor stage according to an embodiment of the present disclosure. 
         FIG.  1 B  illustrates a portion of a compressor stage according to an embodiment of the present disclosure. 
         FIG.  2 A  illustrates a portion of a compressor stage according to an embodiment of the present disclosure. 
         FIG.  2 B  illustrates a portion of a compressor stage according to an embodiment of the present disclosure. 
         FIG.  3 A  illustrates a portion of a compressor stage according to an embodiment of the present disclosure. 
         FIG.  3 B  illustrates a portion of a compressor stage according to an embodiment of the present disclosure. 
     
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     In the following detailed description, reference is made to the accompanying drawings, which form a part hereof, and in which are shown by way of illustration specific embodiments of the invention. 
     As used herein, the terms “having”, “containing”, “including”, “comprising” and the like are open ended terms that indicate the presence of stated elements or features, but do not preclude additional elements or features. 
     It is to be understood that other embodiments may be utilised, and structural or logical changes may be made without departing from the scope of the present invention. The following detailed description, therefore, is not to be taken in a limiting sense, and the scope of the present invention is defined by the appended claims. The embodiments described herein use specific language, which should not be construed as limiting the scope of the appended claims. Each embodiment and each aspect so defined may be combined with any other embodiment or with any other aspect unless clearly indicated to the contrary. 
     According to an embodiment, a compressor stage  100 , in particular for a turbocharging system and/or a turbocompound, is provided. 
     The compressor stage  100  includes an impeller  110  having an inlet section and an outlet section or exit and a diffuser  120  having a diffuser inlet section  111 . The diffuser  120  is arranged downstream of the impeller  110 . The diffuser inlet section  111  is in fluid communication with the outlet section of the impeller. The compressor stage  100  is configured to suck in a primary fluid, typically air, at the impeller inlet section and compress and convey the primary fluid through the compressor stage  100 . This path through the compressor stage  100  may also be referred to as flow channel. The compressor stage  100  may be a centrifugal compressor stage. 
     The diffuser  120  is a vaned diffuser including a plurality of vanes  121 ,  122 ,  123 . The vaned diffuser  120  has a housing, wherein the vanes  121 ,  122 ,  123  are typically fixed to the housing or integrally formed with the housing. The housing may include side walls, in particular a shroud side and/or a hub side. The vanes  121 ,  122 ,  123  extend between two opposing side walls of the housing. 
       FIG.  1 A  shows a portion of a compressor stage  100  according to an embodiment of the present disclosure. The large unfilled arrow illustrates the flow of the primary fluid being conveyed from the impeller  110  (only the location of the impeller is indicated in  FIG.  1 A ) to the diffuser inlet section  111  and further into the vaned diffuser  120 . The section of the compressor stage  100  displayed in  FIG.  1 A  includes two vanes  121 ,  122 , however, typically many additional vanes are arranged within the vaned diffuser  120 . 
     Each pair of vanes  121 ,  122 ,  123  defines a throat section  150 . The throat section  150  is to be understood as a constricted section which limits the mass flow rate of a fluid conveyed through the compressor stage  100 . The vaned diffuser  120  typically includes a plurality of throat sections  150 , each defined by a respective adjacent pair of vanes  121 ,  122 ,  123 . 
     According to an embodiment, the throat section  150  includes an up-stream portion  151  adjacent to the diffuser inlet  111 . At some operating points, the up-stream portion  151  may also be referred to as cross-section reducing portion as the stream-tube cross-section for a fluid conveyed through the vaned diffuser  120  may be increasingly reduced within the up-stream portion  151  of the throat section  150 . The throat section  150  further comprises a throat location  152 , The throat location  152  is the location adjacent to the respective pair of vanes with the geometrically lowest cross-sectional area, typically the throat location  152  includes the lowest cross-sectional area of the entire vaned diffuser  120  (aside from other throat locations  152  defined by other adjacent pairs of vanes). The throat section  150  comprises a down-stream portion  153 , located downstream of the throat location  152 . At some operating points, the down-stream portion may also be referred to as cross-section expanding portion as the stream-tube cross-section for a fluid conveyed through the vaned diffuser  120  may continuously increase downstream of the throat location  152 . The throat section  150  is therefore to be understood as a section largely defined by and largely arranged within an adjacent pair of vanes, however, it is not restricted to a single location. The mass flow rate of a fluid conveyed through the vaned diffuser is particularly affected or limited by the throat location  152 , Illustratively,  FIGS.  1 B and  3 B  sketch the throat section  150 , the up-stream portion  151 , the throat location  152  and the down-stream portion  153 . 
     The vaned diffuser  120  further includes an injection device  130 . The injection device is configured to inject a secondary fluid into the vaned diffuser  120 . In several applications, the secondary fluid is or includes exhaust gas. The injection device  130  comprises a displaceable port  131  at least partially arranged between an adjacent pair of vanes  121 ,  122 ,  123  of the diffuser  120 . Illustratively, the displaceable port  131  may be limited in one dimension (e.g. perpendicular to the flow of the primary fluid) by the pair of adjacent vanes, i.e. may not extend beyond the pair of adjacent vanes in that dimension. In a second dimension (e.g. parallel to the flow of the primary fluid), the displaceable port  131  may extend between an upstream end of one vane, and a downstream end of the adjacent vane, or even extend from an upstream end of one vane to a downstream end of the adjacent vane. The displaceable port  131  may also be entirely arranged between an adjacent pair of vanes  121 ,  122 ,  123  of the diffuser  120 . The displaceable port  131  is displaceable in the sense that the relative positioning of at least portions of the port  131  with respect to the vaned diffuser may be changed. For example, the port  131  may be displaced by a rotational or translational movement. 
     According to another embodiment, the injection device  130  comprises a displaceable port  131  at least partially arranged between a plurality of adjacent pairs of vanes  121 ,  122 ,  123 . A downstream end portion or downstream end of the displaceable port  131  may extend over a full or partial circumference of the vaned diffuser  120 . For example, as an alternative to the embodiment shown in  FIG.  2 A , the displaceable port  131  may be partially arranged between adjacent vanes  121 ,  122  and partially arranged between adjacent vanes  122 ,  123  and extend along vane  122  at the downstream end portion of the displaceable port  131  (or in other words, the displaceable port  131 —shown as several separate ports  131  in  FIG.  2 A —may comprise sections connected or integrally formed at the downstream end portion, in particular approximately perpendicular to the flow of the primary fluid). 
     The injection device  130  may be configured to inject the secondary fluid into the vaned diffuser  120  when the displaceable port  131  is in an open position and to block a flow of the secondary fluid into the vaned diffuser  120  when the displaceable port  131  is in a closed position. The arrangement of the displaceable port  131  partially between adjacent pairs of vanes enables injection of the secondary fluid at a location of low backpressure of the primary fluid. The static pressure of the primary fluid is relatively low, enabling the secondary flow stream to be drawn in by the primary fluid. 
     In one embodiment, the injection device  130  is configured to inject the secondary fluid into the throat section  150 , preferably within the up-stream portion  151  and/or within the throat location  152  of the throat section. This embodiment enables injection of the secondary fluid at a location of lowest backpressure of the primary fluid. Preferably, the secondary fluid is injected at a position in the vicinity of or even at the highest Mach number of the primary fluid between the diffuser inlet section  111  and a downstream end of the vanes, or even within the vaned diffuser  120 . 
       FIG.  1 A  displays an embodiment of the displaceable port  131  arranged between an adjacent pair of vanes  121 ,  122  of the diffuser  120 .  FIG.  3 B  is a close up of the compressor stage  100  shown in  FIG.  1 A . The contours indicate the Mach number of the primary fluid at a particular operating point. In this particular example, i.e. at this particular operating point, a highest Mach number is obtained in the up-stream portion  151  slightly upstream of the throat location  152 . At other operating points, the highest Mach number may be obtained at the throat location  152 , for example. The displaceable port  131  is arranged such that an injection location  135  is at a position in the vicinity of the highest Mach number of the primary fluid. 
     Embodiments of the present disclosure advantageously enable introducing the secondary gas downstream of the impeller, thus avoiding erosion and corrosion to the impeller while concurrently allowing for injection of the secondary fluid at a location of low backpressure of the primary fluid. An additional blower for the secondary fluid is therefore not required. The high momentum primary fluid exiting the compressor impeller  110  draws in and pressurises the secondary fluid like in a jet pump. 
     The displaceable port  131  according to the present disclosure is configured to adjust an effective cross-section (or effective cross-sectional area) of the vaned diffuser  120 . In particular, the effective cross-section between the vanes  121 ,  122 ,  123  or the throat section  150  is adjustable by displacement of the port  131 . Advantageously, adjustment of the cross-section of the throat section  150  results in an adjustment of the cross-section of the throat location  152 . The effective cross-section of the throat location ( 152 ) is adjustable by displacement of the port ( 131 ). 
     The vaned diffuser  120  may be designed such that the cross-sectional area of the throat location  152 , or in other words a mass flow rate, is sufficient for the primary fluid when the secondary fluid is not injected and the displaceable port  131  is in the closed position. Displacement of the port  131  allows for the secondary fluid to be injected, which in turn results in a higher mass flow. Concurrently, the effective cross-sectional area of the throat location  152  is increased in the open position, which advantageously allows for the combined primary and secondary flow to pass the throat section  150  without impeding the compressor stage  100  performance. The impeller can deliver the same mass flow rate with and without the secondary fluid being injected and can operate at its optimum performance both when the secondary air flow is switched on and off. By adjusting the effective cross-sectional area to the amount of secondary flow to be injected, an ideal cross-sectional area can be assured for each operation point. 
     The secondary fluid may be injected without being limited by the mass flow rate of the secondary fluid. The displaceable port  131  thus allows for flexible flow conditions, which can be adapted according to a required or desired flow rate of the secondary fluid. The compressor stage according to the present disclosure overcomes the drawbacks of prior art constant geometry configurations of the diffuser. Embodiments disclosed herein allow for adjusting the diffuser geometry for a large range of secondary fluid streams to be injected into the primary stream. Further, it is assured that the increased mass flow can pass the diffuser without pushing the impeller into surge. Additionally, displacement of the port allows for adjusting the change in flow area along the streamlines within the diffuser  120 . 
       FIG.  1 B  illustrates a section of the compressor stage  100  of  FIG.  1 A  along the line A-A, The flow of the primary fluid is indicated by the large unfilled arrow on the right hand side of  FIG.  1 B . In this embodiment, the displaceable port  131  is convertible or movable from a closed position—the displaceable port  131  is illustrated as bold lines—to an open position—the displaceable port  131  is illustrated as dashed lines. The arrow drawn below the throat location  152  indicates the increase of the cross-sectional area in the open position compared to the closed position. 
     According to one aspect, the injection device  130  includes an actuating mechanism configured to move or translate the displaceable port  131  between the open position and the closed position. For example, the actuating mechanism may include a hydraulic, a mechanic, a pneumatic, or a sensor controlled actuator.  FIGS.  2 B and  3 A  illustrate examples of a compressor stage including an actuating mechanism (the actuating mechanism is not shown in the Figures). The left-right arrows in  FIGS.  2 B and  3 A  indicate a translation of the displaceable port  131  approximately perpendicular to the flow of the primary fluid. In  FIG.  3 A , the displaceable port  131  is illustrated as bold lines in the closed position and as dashed lines in the open position. The left arrow in  FIG.  28    indicates a flow direction of the secondary fluid. 
     According to another aspect, the injection device  130  includes a pivoting mechanism configured to pivot the displaceable port  131  between the open position and the closed position.  FIG.  1 B  illustrates an example of a compressor stage including a pivoting mechanism. The injection device  130  may further include one or more joints  134 , which pivotably mounts the displaceable port  131  to the vaned diffuser  120 . The joint  134  is preferably arranged downstream of the throat location  152 , such that pivoting the displaceable port  131  leads to a substantial increase in the cross-sectional area in the vicinity of the throat location  152 . According to this aspect, the port may also be referred to as flap. 
     According to one aspect, the injection device  130  is configured to inject the secondary fluid substantially parallel to the flow of the primary fluid in the vaned diffuser  120 . The injection device may include a secondary fluid channel  132 . The secondary fluid channel may be in fluid connection with a secondary fluid supply  133 . The secondary fluid channel  132  may be arranged at a small angle with respect to the flow of the primary fluid. The injection device  130  may further include a flow regulator or valve. The flow regulator may be arranged within the secondary fluid channel  132  or further upstream of the secondary fluid channel  132 . The flow regulator may be configured to regulate the mass flow of the secondary fluid. The mass flow of the secondary fluid may then be controlled by the flow regulator while the effective cross-sectional area may be controlled by the port  131 , thereby decoupling the two functionalities. However, the compressor stage of the present disclosure does not require the flow regulator or valve. The mass flow of the secondary fluid may also be controlled or regulated by the displacement of the port  131 . 
     According to one aspect, the displaceable port  131  is arranged within the housing of the vaned diffuser  120 . The port  131  may be a wall section of the vaned diffuser  120 . In the closed position, the port may be flush with the remaining side wall of the vaned diffuser  120 . In other words, the displaceable port  131  does not protrude into the flow channel of the primary fluid of the vaned diffuser  120  in the closed position and does not affect the flow of the primary fluid. The port  131  is convertible from the closed position to the open position by displacing the port  131  away from the flow channel. The port  131  also does not protrude into the flow channel of the primary fluid in the open position. An opening motion of the port  131  corresponds to a partial retraction of the port  131  behind the remaining side wall of the vaned diffuser  120 . The port  131  may be arranged within a shroud side and/or hub side of the housing. In case the injection device  130  includes a pivoting mechanism, a downstream end of the port  131  may be flush with the remaining side wall of the vaned diffuser  120  in the open position. 
     In an alternative aspect, the displaceable port  131  is arranged within the vanes  121 ,  122 ,  123  of the vaned diffuser  120 . Typically, the vanes of a vaned diffuser have a rather limited extent perpendicular to the flow of the primary fluid. This embodiment is particularly suitable when a modest variation of the cross-sectional area by means of the port  131  is sufficient. 
     The compressor stage  100  may further include a conical diffuser section  140  or volute (reference is made for example to  FIG.  3 A ). The conical diffuser section  140  is arranged downstream of the vaned diffuser  120 , and in particular downstream of the down-stream portion  153  and upstream of a compressor stage outlet section. The length of the down-stream portion  153  along the flow channel of the primary fluid may be more than or equal to the distance between the throat location  152  and the downstream end of the port  131  along the flow direction of the primary fluid. 
     The compressor stage  100  may further include a control unit. The control unit may be configured to displace the port  131  (e.g. by controlling the actuating mechanism or by controlling the pivoting mechanism) enabling injection of the secondary fluid and/or adjusting the effective cross-section of the throat section  150  to a predetermined level. The control unit may also be configured to control the mass flow of the secondary fluid (e.g. by controlling the flow regulator). 
     The vaned diffuser may include a plurality of displaceable ports  131 . Each of the plurality of displaceable ports  131  may be at least partially arranged between an adjacent pair of vanes  121 ,  122 ,  123 .  FIG.  2 A  displays a portion of the vaned diffuser  120 , wherein three vanes  121 ,  122 ,  123  and three ports  131  are shown. According to one exemplary embodiment, the vaned diffuser  120  includes a port  131  arranged between every adjacent pair of vanes  121 ,  122 ,  123 . According to another exemplary embodiment, the plurality of ports  131  may be arranged in a pattern. For example, ports  131  may be arranged between every second adjacent pair of vanes  121 ,  122 ,  123 . The control unit may be configured to displace the plurality of ports  131  and/or control the mass flow of the secondary fluid individually, i.e. independent of each other. 
     According to an embodiment, a turbocharging system is provided. The turbocharging system includes a compressor stage according to any of the embodiments disclosed herein. The turbocharger system includes one or more turbocharger stages. At least one of the turbocharger stages includes the compressor stage according to any of the embodiments disclosed herein. In one exemplary aspect, each turbocharger stage includes the compressor stage according to any of the embodiments disclosed herein. In another exemplary aspect, one turbocharger stage includes the compressor stage according to any of the embodiments disclosed herein, whereas the other turbocharger stages may not be configured for injection of a secondary fluid. 
     According to an embodiment, an engine is provided. The engine includes a turbocharging system according to any of the embodiments disclosed herein. In one aspect, the engine is an internal combustion engine. The injection device  130 , and in particular the secondary fluid channel  132 , may be in fluid connection with an exhaust gas manifold of the engine. 
     According to another embodiment, a gas engine, in particular a hydrogen combustion engine, is provided. The gas engine includes a compressor stage according to any of the embodiments disclosed herein. The injection device  130 , and in particular, the secondary fluid channel  132  may be in fluid connection with an exhaust gas outlet of the gas engine. 
     According to another embodiment, a fuel cell, in particular a hydrogen fuel cell, is provided. The fuel cell includes a compressor stage according to any of the embodiments disclosed herein. The injection device  130 , and in particular the secondary fluid channel  132 , may be in fluid connection with an exhaust gas outlet of the fuel cell. In one aspect, the fuel cell is a proton exchange membrane fuel cell or polymer electrolyte membrane fuel cell (PEMFC). The injection device  130 , and in particular the secondary fluid channel  132 , is in fluid connection with a secondary fluid supply  133 . The secondary fluid is preferably water (liquid water and/or water vapour), and the secondary fluid supply  133  is a water supply. Injection of water by the injection device  130  allows for supplying moisture or humidification of at least one membrane of the fuel cell. Advantageously, supplying water for humidification through the compressor stage to the at least one membrane of the fuel cell allows for an improved distribution—and even management—of the water within the fuel cell core. Simultaneously, injection of the water downstream of the impeller of the compression stage avoids or at least mitigates erosion and corrosion issues of the impeller. 
     According to another embodiment, a fuel cell, in particular a hydrogen fuel cell, is provided. The fuel cell includes a compressor stage according to any of the embodiments disclosed herein. The injection device  130 , and in particular the secondary fluid channel  132 , may be in fluid connection with one or more (dedicated) tank(s). In one aspect, the fuel cell is a proton exchange membrane fuel cell or polymer electrolyte membrane fuel cell (PEMFC). The injection device  130 , and in particular the secondary fluid channel  132 , is in fluid connection with a secondary fluid supply  133 . The secondary fluid is preferably water (liquid water and/or water vapour), and the secondary fluid supply  133  is a water supply. Injection of water by the injection device  130  allows for supplying moisture or humidification of at least one electrolyte membrane of the fuel cell. Advantageously, supplying water for humidification through the compressor stage to the at least one membrane of the fuel cell allows for an improved distribution—and even better management—of the water within the fuel cell core. Simultaneously, injection of the water downstream of the impeller of the compression stage avoids or at least mitigates erosion and corrosion issues of the impeller. At least one of the tank(s) may be connected to one or several condenser(s) of the fuel cell and/or one or several separator(s) of the fuel cell to recover water from any water source of the fuel cell. At least one of the tank(s) may preferably be partially or completed filled with water from an external source from the fuel) cell. The injection device  130  may be configured for supplying water directly from any of the one or several condenser(s) and/or from any of the one or several separator(s) and/or from any of the one or more water tank(s). 
     The compressor stage and/or the turbocharger system according to any of the embodiments disclosed herein may be used for a variety of applications, including vehicles or industrial applications. Although the background section emphasises exhaust gas recirculation in internal combustion engines as one intended field of application, embodiments disclosed herein are not limited to applications in internal combustion engines or even to exhaust gas. The compressor stage disclosed herein also enables injecting other secondary fluids, such as air, gaseous fuel, or an air-fuel mixture. 
     According to another embodiment, a process for operating a compressor stage for a turbocharging system and/or a turbocompound is provided. The compressor stage may be any compressor stage described herein. 
     The process includes determining a desired mass flow of a secondary fluid. Typically, the desired mass flow corresponds to a value predetermined by a user or manufacturer. For example, for applications utilising internal combustion engines, the desired mass flow may be a required mass flow of exhaust gas determined such that compliance with environmental regulations is ensured. 
     The process further includes determining an effective cross-section of a vaned diffuser  120  of the compressor to maintain an impeller  110  of the compressor stage  100  within predetermined operating limits. Typically, the impeller  110  can only be operated within certain operating limits without impeding the impeller  110  performance, In case the mass flow of the secondary fluid is substantially increased without changing other parameters of the impeller, such as the geometry of the flow path of the primary fluid, the increased mass flow may push the impeller into surge, A required effective cross-section is determined based on the desired mass flow of the secondary fluid and the predetermined operating limits. 
     The process further includes adjusting a cross-section of the vaned diffuser  120  to the effective cross-section. The cross-sectional area may be adjusted by displacing a displaceable port  131  of an injection device  130  according to any embodiment described herein. The displaceable port  131  may be at least partially arranged between an adjacent pair of vanes  121 ,  122 ,  123  of the diffuser  120 . 
     LIST OF REFERENCE SIGNS 
     
         
           100  compressor stage 
           110  impeller 
           111  diffuser inlet section 
           120  vaned diffuser 
           121 ,  122 ,  123  vanes 
           130  injection device 
           131  displaceable port 
           132  secondary fluid channel 
           133  secondary fluid supply 
           134  joint 
           140  conical diffuser section/volute 
           150  throat section 
           151  up-stream portion 
           152  throat location 
           153  down-stream portion.