EP1749992A1 - Multistage motor-compressor for the compression of a fluid, for motor vehicles for example - Google Patents
Multistage motor-compressor for the compression of a fluid, for motor vehicles for example Download PDFInfo
- Publication number
- EP1749992A1 EP1749992A1 EP06101557A EP06101557A EP1749992A1 EP 1749992 A1 EP1749992 A1 EP 1749992A1 EP 06101557 A EP06101557 A EP 06101557A EP 06101557 A EP06101557 A EP 06101557A EP 1749992 A1 EP1749992 A1 EP 1749992A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- motor
- compressor according
- ducts
- section
- transfer
- 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.)
- Granted
Links
- 239000012530 fluid Substances 0.000 title claims abstract description 21
- 230000006835 compression Effects 0.000 title claims abstract description 16
- 238000007906 compression Methods 0.000 title claims abstract description 16
- 238000009987 spinning Methods 0.000 claims abstract 2
- 230000005540 biological transmission Effects 0.000 claims description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B33/00—Engines characterised by provision of pumps for charging or scavenging
- F02B33/32—Engines with pumps other than of reciprocating-piston type
- F02B33/34—Engines with pumps other than of reciprocating-piston type with rotary pumps
- F02B33/40—Engines with pumps other than of reciprocating-piston type with rotary pumps of non-positive-displacement type
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
- F02B39/02—Drives of pumps; Varying pump drive gear ratio
- F02B39/08—Non-mechanical drives, e.g. fluid drives having variable gear ratio
- F02B39/10—Non-mechanical drives, e.g. fluid drives having variable gear ratio electric
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/12—Multi-stage pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
- F04D29/4213—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/50—Inlet or outlet
- F05D2250/51—Inlet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/14—Preswirling
Definitions
- This invention refers to a multistage motor-compressor for the compression of a fluid, for motor vehicles for example.
- the invention refers to a two-stage motor-compressor for the supply of pressurized air to fuel cell systems.
- Motor-compressors of the above-stated type are well known, in which the first-stage scroll is connected to a tangential first section of a transfer duct, while a second axial or radial section of the transfer duct is connected to a fluid conveyor for the second-stage scroll.
- the second section is axial, the fluid flow entering the conveyor undergoes abrupt changes of direction, giving rise to a drop in flow pressure, high operational power consumption and reduced efficiency for the motor-compressor.
- the second section of the transfer duct is radial, it is normally shaped to create a helical flow with the same direction of rotation as that of the second-stage impeller.
- This radial connection has the drawback of reduced efficiency and a low compression ratio at high flow rates.
- Multistage motor-compressors are also known, in which the impellers are arranged in series on the same output side of the driving electric motor's shaft. Since the two impellers are cantilever mounted on the shaft, the latter is subject to stress, which reduces the operating speed.
- the object of the invention is that of embodying a two-stage motor-compressor, which is highly reliable, eliminating the drawbacks and increasing the performance of motor-compressors of known art.
- this object is achieved by a multistage motor-compressor for the compression of a fluid, as defined in claim 1.
- the impellers of the two stages are fixed on two opposite ends of the shaft of a common driving electric motor, for which the motor-compressor is able to operate at high speeds.
- reference 5 generically indicates a multistage motor-compressor for the compression of a fluid, for motor vehicles for example.
- the motor-compressor 5 is of the type with two stages 6 and 7, low pressure and high pressure respectively, and is suitable for the supply of pressurized air in a fuel cell system or for supplying air to internal combustion engines, or for any system in which compressed air is required.
- the low-pressure stage 6 comprises a low-pressure impeller, which henceforth will be called the primary impeller 8 (Figure 3).
- the primary impeller 8 rotates around an axis A and is preceded by a fixed ogival portion 9, placed inside a low-pressure scroll, which henceforth will be called the primary scroll 10.
- the primary impeller 8 is fixed on one end 15' of a shaft of an electric motor 15.
- the primary impeller 8 also comprises a series of substantially radial, shaped blades 11, of known type.
- the primary scroll 10 is composed of a shaped casing 12, connected in a removable manner, via bolts and at least one half-ring 13, to a fixed plate 20 carried on an external casing 32 of the motor 15, which has a substantially cylindrical shape.
- the shaped casing 12 has a central air-inlet opening 14 to the low-pressure stage 6.
- the primary scroll 10 also has at least one curved, fluid-delivery duct 16, which has a substantially spiral shape placed substantially on plane P perpendicular to axis A.
- the primary scroll 10 is equipped with three curved ducts 16 arranged at 120° to each other, for the purpose of having a balanced load on the primary scroll 10.
- the annular chamber 17 is in communication with the central opening 14, through an annular inlet opening 18 facing towards axis A, while on the other side it is in communication with the curved ducts 16 through corresponding outlet openings 19, facing towards the outside of the annular chamber 17.
- the shaped blades 11 of the impeller 8 are suitable for conveying incoming air from the central opening 14 to the curved ducts 16.
- the axial direction of the airflow to be compressed is optimized by the ogival portion 9.
- each curved duct 16 has an increasing section from the outlet opening 19 of the annular chamber 17 to the outlet opening 25, which is defined by the terminal radial section of the curved duct 16.
- the spiral shape of the curved duct 16 induces a fluid flow that turns in the same direction of rotation as the impeller 8.
- the high-pressure stage 7 of the motor-compressor 5 comprises a high-pressure impeller, which henceforth will be called the secondary impeller 21 ( Figure 3), rotating around its axis.
- This axis can advantageously coincide with axis A of the primary impeller 8.
- the secondary impeller 21 is fixed on the end 15" of the shaft of the motor 15 opposite from that of the primary impeller 8, thereby providing a balanced load on the shaft of the motor 15 such that the group of impellers 8 and 21 can be spun at high speed.
- the secondary impeller 21 is equipped with its own ogival portion 22, suitable for optimizing the direction of the axial flow.
- the ogival portion 22 is placed inside a high-pressure scroll, which henceforth will be called the secondary scroll 23.
- the secondary impeller 21 also comprises a series of substantially radial, shaped blades 24.
- the secondary scroll 23 is composed of a shaped casing 26 connected in a removable manner, via bolts and at least one half-ring 27, to another fixed plate 33, carried on the external casing 32 of the motor 15.
- the shaped casing 26 of the secondary scroll 23 has a sleeve 31 with a central air-inlet opening 28 to the high-pressure stage 7.
- the secondary scroll 23 has at least one curved duct 29, substantially placed on another plane R perpendicular to axis A.
- the secondary scroll 23 (see also Figure 7) advantageously has just one curved duct 29, which also has a substantially spiral course and terminates with a straight section 30.
- the spiral of the curved duct 29 is such as to generate a fluid flow that also turns in the same direction as the secondary impeller 21.
- the fixed plate 33 together with the shaped casing 26 forms an annular chamber 34, one side of which is in communication with the central opening 28, through an annular inlet opening 36 facing towards axis A.
- the annular chamber 34 is in communication with the curved duct 29, through an opening 37 facing towards the outside, which forms the inlet opening of the curved duct 29.
- the shaped blades 24 of the impeller 21 are suitable for conveying incoming air from the central opening 28 to the annular chamber 34.
- the curved duct 29 has an increasing section from the portion adjacent to its inlet opening 37 to a corresponding outlet opening 38 ( Figure 5) defined by the terminal radial section of the curved duct 29, which is equal to that of the straight section 30.
- the motor-compressor 5 also comprises a conveyor 39 with an outer wall 40 and a central opening 41 ( Figure 3), in which the sleeve 31 of the secondary scroll 23 engages in a sealed manner.
- the conveyor 39 is also provided with three inlet openings 42 associated with the three outlet openings 25 of the curved ducts 16 of the primary scroll 10.
- the three inlet openings 42 are also arranged at 120° to each other.
- a corresponding transfer duct, generically indicated by reference 44, is placed between each outlet opening 25 of the primary scroll 10 and the corresponding inlet opening 42 of the conveyor 39.
- each transfer duct 44 is shaped so as to create a flow entering the conveyor 39 with a substantially helical course and a direction of rotation opposite to the direction of rotation of the secondary impeller 21.
- each transfer duct 44 comprises a first section 52 ( Figures 1, 4 and 6) connected to the corresponding curved duct 16 and substantially tangential to the primary impeller 8, a second section 56 ( Figures 2, 5 and 8) connected to the corresponding opening 42 of the conveyor 39 and substantially tangential to the secondary impeller 21, and a longitudinal intermediate section 54 and 57.
- each transfer duct 44 comprises a first connector section 53, substantially helical in form and placed between the first tangential section 52 and the intermediate section 54 and 57.
- Each transfer duct also comprises a second curved connector section 58 placed between the second tangential section 56 and the intermediate section 54 and 57.
- the transfer ducts 44 are advantageously placed on the outside of the casing 32 and are each formed by two segments 46 and 47 ( Figures 1 and 2), connected in a removable manner to the primary scroll 10 and the conveyor 39 respectively.
- the two segments 46 and 47 terminate with corresponding flanges 48 and 49, which mate together on a plane S ( Figure 3) perpendicular to axis A, and are connected to each other in a sealed and removable manner, for example by bolts 51.
- each transfer duct 44 comprises the said first section 52, the corresponding substantially helical connection section 53, and a straight portion 54, which forms a portion 54 of the intermediate section 54 and 57.
- segment 47 of each transfer duct 44 comprises the said second section 56, the curved connection section 58 and another straight portion 57 of the intermediate section 54 and 57.
- All of the ducts 16, 29 and 44 of the motor-compressor 5 are outwardly sealed to support the pressurized fluid, via toroidal gaskets for example, pastes or in any other known manner.
- the shaped casing 12 of the primary scroll 10 is provided with a series of cooling ribs or fins 59.
- the shaped casing 26 of the secondary scroll 23 and the conveyor 39 are provided with corresponding series of cooling ribs or fins 61 and 62.
- the fins 59, 61 and 62 serve to increase the heat-exchange surface area with the external environment, to cool the compressed fluid efficiently, increasing the density and therefore increasing the efficiency of the motor-compressor 5.
- the transfer ducts 44 have an elliptic section to contain the radial bulk of the motor-compressor 5.
- the two impellers 8 and 21 are coaxial and are driven by a single electric motor 15.
- the arrows 63 and 64 represent the direction of rotation of the motor 15, while the black arrows on the transfer ducts 44 represent the flow of fluid.
- Figure 4 clearly shows that the direction of rotation of the flow in the segments 46 is consistent with that of the motor 15 (arrow 63), while Figure 5 shows that the direction of rotation of the flow in the sections 57 of the segments 47 is opposite to that of the motor 15 (arrow 64).
- the motor-compressor 5 comprises just one delivery duct 16 and just one transfer duct 44 to the conveyor 39.
- the motor-compressor 5 comprises two delivery ducts 16 and two transfer ducts 44, placed diametrically opposite each other.
- the two variants have a number of outlets 25 for the scroll 10 and inlets 42 to the conveyor 39 equal to the number of transfer ducts 44.
- the shape of the transfer ducts 44 in Figures 9 and 10 is identical to that of the transfer ducts 44 in Figure 2.
- Figures 9 and 10 parts that are the same or similar to those in Figure 2 are indicated with the same reference numbers, and so the two variants will not be described any further.
- Figure 11 shows a curve 66 of the compression ratio ⁇ as a function of flow Q of the motor-compressor 5.
- a predetermined compression curve 66 is obtained. If instead the second section 56 of each transfer duct 44 provokes an opposite helical flow to that of the motor 15, the outcome is a displacement of the curve 66 to the right in Figure 11, which indicates that a greater compression ratio is achieved at high flow-rates.
- the functioning of the motor-compressor 5 is as follows.
- the conveyor 39 then channels the fluid flow, via the central opening 28 of the sleeve 31, to the inlet opening 37 of the secondary scroll 23, where it undergoes a second compression imparted by the secondary impeller 21 and then passes into the curved duct 29 of the secondary scroll 23. Finally, the pressurized fluid is conveyed to where utilized by the straight section 30.
- the advantages of the motor-compressor 5 according to the invention with respect to motor-compressors of known art are evident.
- the transfer ducts 44 avoid energy loss in the flow and improve the efficiency of the motor-compressor 5.
- the fixing of the two impellers 8 and 21 on the two ends 15' and 15" of the shaft of the common motor 15 renders operation of the impellers 8 and 21 well balanced, avoiding the generation of vibration and thereby allowing an increase in the speed of rotation.
- each transfer duct 44 could be in a single piece, and be connected to the scroll 10 and to the conveyor 39 in a removable manner, via a bolted flange for example.
- the two impellers 8 and 21 could be spun by independent electric motors and the respective axes A could be parallel, oblique or coplanar, but with a predetermined angle formed between them.
- the two impellers 8 and 21 are preferably rotated by a common electric motor, possibly via at least one drive transmission group, of known type.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Motor Or Generator Cooling System (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
Description
- This invention refers to a multistage motor-compressor for the compression of a fluid, for motor vehicles for example. In particular, the invention refers to a two-stage motor-compressor for the supply of pressurized air to fuel cell systems.
- Motor-compressors of the above-stated type are well known, in which the first-stage scroll is connected to a tangential first section of a transfer duct, while a second axial or radial section of the transfer duct is connected to a fluid conveyor for the second-stage scroll. In the case where the second section is axial, the fluid flow entering the conveyor undergoes abrupt changes of direction, giving rise to a drop in flow pressure, high operational power consumption and reduced efficiency for the motor-compressor.
- In the case in which the second section of the transfer duct is radial, it is normally shaped to create a helical flow with the same direction of rotation as that of the second-stage impeller. This radial connection has the drawback of reduced efficiency and a low compression ratio at high flow rates.
- Multistage motor-compressors are also known, in which the impellers are arranged in series on the same output side of the driving electric motor's shaft. Since the two impellers are cantilever mounted on the shaft, the latter is subject to stress, which reduces the operating speed.
- The object of the invention is that of embodying a two-stage motor-compressor, which is highly reliable, eliminating the drawbacks and increasing the performance of motor-compressors of known art.
- According to the invention, this object is achieved by a multistage motor-compressor for the compression of a fluid, as defined in claim 1.
- According to a variant of the invention, the impellers of the two stages are fixed on two opposite ends of the shaft of a common driving electric motor, for which the motor-compressor is able to operate at high speeds.
- For a better understanding of the invention, a preferred embodiment is described herein, provided by way of example with the aid of the enclosed drawings, in which:
- Figure 1 is a right-hand perspective view of a two-stage motor-compressor according to a first variant of the invention,
- Figure 2 is a left-hand perspective view of the motor-compressor in Figure 1,
- Figure 3 is a diametrical section of the motor-compressor in Figure 1,
- Figure 4 is a view along line IV-IV in Figure 3,
- Figure 5 is a view along line V-V in Figure 3,
- Figure 6 is a left-hand perspective view of part of the motor-compressor in Figure 1,
- Figure 7 is a left-hand perspective view of another part of the motor-compressor in Figure 1,
- Figure 8 is a right-hand perspective view of a further part of the motor-compressor in Figure 1,
- Figures 9 and 10 are two due perspective views similar to that in Figure 2, regarding two variants of the motor-compressor, and
- Figure 11 is a graph of the motor-compressor's compression ratio.
- With reference to Figures 1 and 2,
reference 5 generically indicates a multistage motor-compressor for the compression of a fluid, for motor vehicles for example. In particular, the motor-compressor 5 is of the type with twostages - The low-
pressure stage 6 comprises a low-pressure impeller, which henceforth will be called the primary impeller 8 (Figure 3). The primary impeller 8 rotates around an axis A and is preceded by afixed ogival portion 9, placed inside a low-pressure scroll, which henceforth will be called theprimary scroll 10. The primary impeller 8 is fixed on one end 15' of a shaft of anelectric motor 15. The primary impeller 8 also comprises a series of substantially radial,shaped blades 11, of known type. - The
primary scroll 10 is composed of ashaped casing 12, connected in a removable manner, via bolts and at least one half-ring 13, to afixed plate 20 carried on anexternal casing 32 of themotor 15, which has a substantially cylindrical shape. Theshaped casing 12 has a central air-inlet opening 14 to the low-pressure stage 6. Theprimary scroll 10 also has at least one curved, fluid-delivery duct 16, which has a substantially spiral shape placed substantially on plane P perpendicular to axis A. - According to the variant in Figures 1-8, the
primary scroll 10 is equipped with threecurved ducts 16 arranged at 120° to each other, for the purpose of having a balanced load on theprimary scroll 10. Thefixed plate 20 of themotor 15, together with theshaped casing 12 of theprimary scroll 10, form anannular chamber 17 in communication with thecurved ducts 16. On one side, theannular chamber 17 is in communication with thecentral opening 14, through an annular inlet opening 18 facing towards axis A, while on the other side it is in communication with thecurved ducts 16 throughcorresponding outlet openings 19, facing towards the outside of theannular chamber 17. - The
shaped blades 11 of the impeller 8 are suitable for conveying incoming air from thecentral opening 14 to thecurved ducts 16. The axial direction of the airflow to be compressed is optimized by theogival portion 9. In order to convey compressed air from the impeller 8, eachcurved duct 16 has an increasing section from the outlet opening 19 of theannular chamber 17 to the outlet opening 25, which is defined by the terminal radial section of thecurved duct 16. The spiral shape of thecurved duct 16 induces a fluid flow that turns in the same direction of rotation as the impeller 8. - The high-
pressure stage 7 of the motor-compressor 5 comprises a high-pressure impeller, which henceforth will be called the secondary impeller 21 (Figure 3), rotating around its axis. This axis can advantageously coincide with axis A of the primary impeller 8. Thesecondary impeller 21 is fixed on theend 15" of the shaft of themotor 15 opposite from that of the primary impeller 8, thereby providing a balanced load on the shaft of themotor 15 such that the group ofimpellers 8 and 21 can be spun at high speed. - The
secondary impeller 21 is equipped with itsown ogival portion 22, suitable for optimizing the direction of the axial flow. Theogival portion 22 is placed inside a high-pressure scroll, which henceforth will be called thesecondary scroll 23. Thesecondary impeller 21 also comprises a series of substantially radial,shaped blades 24. - The
secondary scroll 23 is composed of a shaped casing 26 connected in a removable manner, via bolts and at least one half-ring 27, to anotherfixed plate 33, carried on theexternal casing 32 of themotor 15. The shaped casing 26 of thesecondary scroll 23 has asleeve 31 with a central air-inlet opening 28 to the high-pressure stage 7. - In addition, the
secondary scroll 23 has at least onecurved duct 29, substantially placed on another plane R perpendicular to axis A. The secondary scroll 23 (see also Figure 7) advantageously has just onecurved duct 29, which also has a substantially spiral course and terminates with astraight section 30. The spiral of thecurved duct 29 is such as to generate a fluid flow that also turns in the same direction as thesecondary impeller 21. - The
fixed plate 33 together with the shaped casing 26 forms anannular chamber 34, one side of which is in communication with thecentral opening 28, through an annular inlet opening 36 facing towards axis A. On the other side, theannular chamber 34 is in communication with thecurved duct 29, through an opening 37 facing towards the outside, which forms the inlet opening of thecurved duct 29. Theshaped blades 24 of theimpeller 21 are suitable for conveying incoming air from thecentral opening 28 to theannular chamber 34. - In order to convey compressed air entering through the
central opening 28 in theannular chamber 34, thecurved duct 29 has an increasing section from the portion adjacent to its inlet opening 37 to a corresponding outlet opening 38 (Figure 5) defined by the terminal radial section of thecurved duct 29, which is equal to that of thestraight section 30. - The motor-
compressor 5 also comprises aconveyor 39 with anouter wall 40 and a central opening 41 (Figure 3), in which thesleeve 31 of thesecondary scroll 23 engages in a sealed manner. Theconveyor 39 is also provided with threeinlet openings 42 associated with the threeoutlet openings 25 of thecurved ducts 16 of theprimary scroll 10. The threeinlet openings 42 are also arranged at 120° to each other. A corresponding transfer duct, generically indicated byreference 44, is placed between each outlet opening 25 of theprimary scroll 10 and the corresponding inlet opening 42 of theconveyor 39. - According to the invention, each
transfer duct 44 is shaped so as to create a flow entering theconveyor 39 with a substantially helical course and a direction of rotation opposite to the direction of rotation of thesecondary impeller 21. In particular, eachtransfer duct 44 comprises a first section 52 (Figures 1, 4 and 6) connected to the correspondingcurved duct 16 and substantially tangential to the primary impeller 8, a second section 56 (Figures 2, 5 and 8) connected to thecorresponding opening 42 of theconveyor 39 and substantially tangential to thesecondary impeller 21, and a longitudinalintermediate section - The second
tangential section 56 of thetransfer duct 44 and thecorresponding opening 42 of theconveyor 39 are positioned in a manner to generate the said helical course of the flow, with an opposite direction of rotation to that of theimpeller 21. Furthermore, eachtransfer duct 44 comprises afirst connector section 53, substantially helical in form and placed between the firsttangential section 52 and theintermediate section curved connector section 58 placed between the secondtangential section 56 and theintermediate section - The
transfer ducts 44 are advantageously placed on the outside of thecasing 32 and are each formed by twosegments 46 and 47 (Figures 1 and 2), connected in a removable manner to theprimary scroll 10 and theconveyor 39 respectively. The twosegments corresponding flanges bolts 51. - The
segment 46 of eachtransfer duct 44 comprises the saidfirst section 52, the corresponding substantiallyhelical connection section 53, and astraight portion 54, which forms aportion 54 of theintermediate section segment 47 of eachtransfer duct 44 comprises the saidsecond section 56, thecurved connection section 58 and anotherstraight portion 57 of theintermediate section - All of the
ducts compressor 5 are outwardly sealed to support the pressurized fluid, via toroidal gaskets for example, pastes or in any other known manner. The shapedcasing 12 of theprimary scroll 10 is provided with a series of cooling ribs orfins 59. Similarly, the shaped casing 26 of thesecondary scroll 23 and theconveyor 39 are provided with corresponding series of cooling ribs orfins fins compressor 5. Thetransfer ducts 44 have an elliptic section to contain the radial bulk of the motor-compressor 5. - In the illustrated embodiment, the two
impellers 8 and 21 are coaxial and are driven by a singleelectric motor 15. In Figures 4 and 5, thearrows 63 and 64 represent the direction of rotation of themotor 15, while the black arrows on thetransfer ducts 44 represent the flow of fluid. Figure 4 clearly shows that the direction of rotation of the flow in thesegments 46 is consistent with that of the motor 15 (arrow 63), while Figure 5 shows that the direction of rotation of the flow in thesections 57 of thesegments 47 is opposite to that of the motor 15 (arrow 64). - According to the variant in Figure 9, the motor-
compressor 5 comprises just onedelivery duct 16 and just onetransfer duct 44 to theconveyor 39. According to the variant in Figure 10, the motor-compressor 5 comprises twodelivery ducts 16 and twotransfer ducts 44, placed diametrically opposite each other. Thus, the two variants have a number ofoutlets 25 for thescroll 10 andinlets 42 to theconveyor 39 equal to the number oftransfer ducts 44. The shape of thetransfer ducts 44 in Figures 9 and 10 is identical to that of thetransfer ducts 44 in Figure 2. In Figures 9 and 10 parts that are the same or similar to those in Figure 2 are indicated with the same reference numbers, and so the two variants will not be described any further. - Figure 11 shows a
curve 66 of the compression ratio β as a function of flow Q of the motor-compressor 5. In the case oftransfer ducts 44 able to generate a helical flow that is totally consistent with the rotation of themotor 15, apredetermined compression curve 66 is obtained. If instead thesecond section 56 of eachtransfer duct 44 provokes an opposite helical flow to that of themotor 15, the outcome is a displacement of thecurve 66 to the right in Figure 11, which indicates that a greater compression ratio is achieved at high flow-rates. - The functioning of the motor-
compressor 5 is as follows. - By making the two
impellers 8 and 21 rotate in the direction of the arrows 63 and 64 (Figures 4 and 5), the fluid entering from thecentral opening 14 of the casing 12 (see also Figure 3) is propelled by theblades 11 into thecurved ducts 16 of thescroll 10, undergoing a first compression. Exiting from theoutlet openings 25 of thecurved ducts 16, the fluid flow, indicated in Figures 3-5 by black arrows on the various ducts, is channelled into thetransfer ducts 44 and is introduced, through theinlet openings 42, into theconveyor 39 with a helical motion that turns in the opposite direction to the direction of rotation of themotor 15. Theconveyor 39 then channels the fluid flow, via thecentral opening 28 of thesleeve 31, to the inlet opening 37 of thesecondary scroll 23, where it undergoes a second compression imparted by thesecondary impeller 21 and then passes into thecurved duct 29 of thesecondary scroll 23. Finally, the pressurized fluid is conveyed to where utilized by thestraight section 30. - From what has been seen above, the advantages of the motor-
compressor 5 according to the invention with respect to motor-compressors of known art are evident. In particular, thetransfer ducts 44 avoid energy loss in the flow and improve the efficiency of the motor-compressor 5. Furthermore, the fixing of the twoimpellers 8 and 21 on the two ends 15' and 15" of the shaft of thecommon motor 15 renders operation of theimpellers 8 and 21 well balanced, avoiding the generation of vibration and thereby allowing an increase in the speed of rotation. - It is intended that various modifications and refinements can be made to the above-described motor-
compressor 5 without departing from the scope of the claims. For example, eachtransfer duct 44 could be in a single piece, and be connected to thescroll 10 and to theconveyor 39 in a removable manner, via a bolted flange for example. In addition, the twoimpellers 8 and 21 could be spun by independent electric motors and the respective axes A could be parallel, oblique or coplanar, but with a predetermined angle formed between them. In this case as well, the twoimpellers 8 and 21 are preferably rotated by a common electric motor, possibly via at least one drive transmission group, of known type.
Claims (14)
- Multistage motor-compressor for the compression of a fluid, comprising a first compression stage (6) having a primary impeller (8) and at least one delivery duct (16), a second compression stage (7) having a secondary impeller (21) spinning in a predetermined direction of rotation, and at least one transfer duct (44) placed so as to put said delivery duct (16) in communication with a fluid conveyor (39) of said second stage (7), characterized in that said transfer duct (44) is shaped in a way to create a fluid flow entering said conveyor (39) with a substantially helical course and with a direction of rotation opposite to the direction of rotation of said secondary impeller (21).
- Motor-compressor according to claim 1, characterized in that said second stage (7) is fitted with at least one axial inlet duct (28) for said flow, said conveyor (39) including its own inlet opening (42) for said flow in communication with said transfer duct (44) and with the inlet opening (28) of said second stage (7).
- Motor-compressor according to claim 2, characterized in that said first stage (6) comprises a pair of diametrically opposite delivery ducts (16), said conveyor (39) comprising a corresponding pair of inlet openings (42), also diametrically opposed, said inlet openings (42) being in communication with said delivery ducts (16) through a corresponding pair of mutually-alike transfer ducts (44).
- Motor-compressor according to claim 2, characterized in that said first stage (6) comprises three delivery ducts (16) set at 120° to each other, said conveyor (39) comprising three corresponding inlet openings (42), also set at 120° to each other, said inlet openings (42) being in communication with said delivery ducts (16) via three mutually-alike transfer ducts (44).
- Motor-compressor according to claims 3 or 4, characterized in that said impellers (8 and 21) are driven by drive means (15) placed inside a casing (32), said transfer ducts (44) being placed on the outside of said casing (15).
- Motor-compressor according to any of the previous claims, characterized in that each of said transfer ducts (44) comprises a first section (52) connected to said delivery duct (16) and substantially tangential to said primary impeller (8), a second section (56) connected to said conveyor (39) and substantially tangential to said secondary impeller (21), and a longitudinal intermediate section (54 and 57).
- Motor-compressor according to claim 6, characterized in that each of said transfer ducts (44) also comprises a substantially helical section (53) placed between said first tangential section (52) and said intermediate section (54 and 57), and a curved section (58) placed between said second tangential section (56) and said intermediate section (54 and 57).
- Motor-compressor according to claim 7, characterized in that each of said transfer ducts (44) is subdivided into two segments (46 and 47), each comprising a portion (54 and 57) of said intermediate section, each of said segments (46 and 47) being fitted with a flange (48 and 49) for connection with the other segment (46 and 47).
- Motor-compressor according to one of the claims 3 to 8, characterized in that said transfer ducts (44) are shaped in a way to create a fluid flow exiting from said delivery ducts 16 with a substantially helical course and with a direction of rotation concordant with the direction of rotation of the primary impeller (8).
- Motor-compressor according to one of the previous claims, characterized in that said drive means (15) comprise two distinct electric motors for driving said two impellers (8 and 21).
- Motor-compressor according to one of the claims 1 to 9, characterized in that said drive means (15) comprise a common electric motor for said two impellers (8 and 21).
- Motor-compressor according to claim 11, characterized in that said impellers (8 and 21) are coaxial and are fixed on two opposite ends (15' and 15") of a shaft of said electric motor (15).
- Motor-compressor according to claim 11, characterized in that said impellers (8 and 21) are coaxial or spin around two axes that are coplanar and which form a predetermined angle.
- Motor-compressor according to one of the claims 11 to 13, characterized in that a drive transmission group is placed between said electric motor (15) and at least one of said impellers (8 and 21).
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/499,265 US20070036662A1 (en) | 2005-08-05 | 2006-08-04 | Multistage motor-compressor for the compression of a fluid |
JP2006214157A JP2007046610A (en) | 2005-08-05 | 2006-08-07 | Multistage motor-compressor for compression of fluid for automobile |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT000558A ITTO20050558A1 (en) | 2005-08-05 | 2005-08-05 | MOTORCOMPRESSOR WITH MORE STAGES FOR THE COMPRESSION OF FLUIDS, FOR EXAMPLE FOR MOTOR VEHICLES |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1749992A1 true EP1749992A1 (en) | 2007-02-07 |
EP1749992B1 EP1749992B1 (en) | 2010-02-10 |
Family
ID=36480888
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP06101557A Not-in-force EP1749992B1 (en) | 2005-08-05 | 2006-02-10 | Multistage motor-compressor for the compression of a fluid, for motor vehicles for example |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1749992B1 (en) |
AT (1) | ATE457417T1 (en) |
DE (1) | DE602006012139D1 (en) |
IT (1) | ITTO20050558A1 (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010065681A (en) * | 2008-09-10 | 2010-03-25 | Borgwarner Inc | Coupling turbochargers for passive pre-swirl counter-rotation |
GB2490563A (en) * | 2011-05-03 | 2012-11-07 | Peter John Bayram | Pre-rotating or de-rotating fluid flow with a volute |
EP3112686A4 (en) * | 2014-02-25 | 2017-01-04 | Mitsubishi Heavy Industries, Ltd. | Multistage electric centrifugal compressor and supercharging system of internal combustion engine |
DE102017205704A1 (en) * | 2017-04-04 | 2018-10-04 | Robert Bosch Gmbh | Turbocompressor, in particular for a fuel cell system |
WO2018197622A1 (en) * | 2017-04-29 | 2018-11-01 | Daimler Ag | Internal combustion engine for a motor vehicle, in particular for a car |
WO2019001911A1 (en) * | 2017-06-27 | 2019-01-03 | Ebm-Papst Mulfingen Gmbh & Co. Kg | Turbo compressor with integrated flow channels |
WO2022029386A1 (en) | 2020-08-05 | 2022-02-10 | Enogia | Multi-stage centrifugal compressor |
EP2821652B1 (en) * | 2012-02-29 | 2022-08-31 | Mitsubishi Heavy Industries, Ltd. | Centrifugal fluid machine with air intake pipe structure |
WO2022214852A1 (en) * | 2021-04-09 | 2022-10-13 | Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. | Supplying a mixture of air and exhaust gas to a compressor wheel of a compressor |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114857043B (en) * | 2022-04-21 | 2023-10-24 | 珠海格力电器股份有限公司 | Air compressor, fuel cell and new energy vehicle |
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2005
- 2005-08-05 IT IT000558A patent/ITTO20050558A1/en unknown
-
2006
- 2006-02-10 DE DE602006012139T patent/DE602006012139D1/en active Active
- 2006-02-10 AT AT06101557T patent/ATE457417T1/en not_active IP Right Cessation
- 2006-02-10 EP EP06101557A patent/EP1749992B1/en not_active Not-in-force
Patent Citations (5)
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US3171353A (en) * | 1962-02-27 | 1965-03-02 | Kenton D Mcmahan | Centrifugal fluid pump |
US4969803A (en) * | 1987-09-03 | 1990-11-13 | Man Gutehoffnungshutte Gmbh | Compressor unit |
EP1041289A2 (en) * | 1999-03-31 | 2000-10-04 | Cooper Cameron Corporation | Direct drive compressor assembly |
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Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010065681A (en) * | 2008-09-10 | 2010-03-25 | Borgwarner Inc | Coupling turbochargers for passive pre-swirl counter-rotation |
EP2163746A3 (en) * | 2008-09-10 | 2010-04-21 | BorgWarner Inc. | Coupling turbochargers for passive pre-swirl counter-rotation |
US8388302B2 (en) | 2008-09-10 | 2013-03-05 | Borgwarner Inc. | Coupling turbochargers for passive pre-swirl counter-rotation |
GB2490563A (en) * | 2011-05-03 | 2012-11-07 | Peter John Bayram | Pre-rotating or de-rotating fluid flow with a volute |
GB2490563B (en) * | 2011-05-03 | 2015-07-22 | Peter John Bayram | Spiral energy recovery and flow pre-rotation for turbochargers, turbo-expansion valves, turbojets and marine propellers, etc |
EP2821652B1 (en) * | 2012-02-29 | 2022-08-31 | Mitsubishi Heavy Industries, Ltd. | Centrifugal fluid machine with air intake pipe structure |
US10174670B2 (en) | 2014-02-25 | 2019-01-08 | Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. | Multi-stage electric centrifugal compressor and supercharging system for internal combustion engine |
EP3112686A4 (en) * | 2014-02-25 | 2017-01-04 | Mitsubishi Heavy Industries, Ltd. | Multistage electric centrifugal compressor and supercharging system of internal combustion engine |
DE102017205704A1 (en) * | 2017-04-04 | 2018-10-04 | Robert Bosch Gmbh | Turbocompressor, in particular for a fuel cell system |
WO2018197622A1 (en) * | 2017-04-29 | 2018-11-01 | Daimler Ag | Internal combustion engine for a motor vehicle, in particular for a car |
WO2019001911A1 (en) * | 2017-06-27 | 2019-01-03 | Ebm-Papst Mulfingen Gmbh & Co. Kg | Turbo compressor with integrated flow channels |
WO2022029386A1 (en) | 2020-08-05 | 2022-02-10 | Enogia | Multi-stage centrifugal compressor |
FR3113303A1 (en) | 2020-08-05 | 2022-02-11 | Enogia | Multi-stage centrifugal compressor |
WO2022214852A1 (en) * | 2021-04-09 | 2022-10-13 | Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. | Supplying a mixture of air and exhaust gas to a compressor wheel of a compressor |
Also Published As
Publication number | Publication date |
---|---|
EP1749992B1 (en) | 2010-02-10 |
DE602006012139D1 (en) | 2010-03-25 |
ATE457417T1 (en) | 2010-02-15 |
ITTO20050558A1 (en) | 2007-02-06 |
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