US2046737A - Multiple stage blower - Google Patents
Multiple stage blower Download PDFInfo
- Publication number
- US2046737A US2046737A US750042A US75004234A US2046737A US 2046737 A US2046737 A US 2046737A US 750042 A US750042 A US 750042A US 75004234 A US75004234 A US 75004234A US 2046737 A US2046737 A US 2046737A
- Authority
- US
- United States
- Prior art keywords
- air
- fan
- blading
- blower
- pressure
- 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.)
- Expired - Lifetime
Links
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 230000002000 scavenging effect Effects 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
- F04D25/166—Combinations of two or more pumps ; Producing two or more separate gas flows using fans
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S415/00—Rotary kinetic fluid motors or pumps
- Y10S415/914—Device to control boundary layer
Definitions
- This invention relates to improvements in multiple stage blowers. It is necessary in many installations to supply a plurality of currents of air at different pres- 5 sures, for example currents of cooling air and scavenging air for internal combustion engines, and to simplify the blower installation, it has been proposed to construct blowersto produce two separate air currents of different pressures. With centrifugal blowers it has been customary to sub-divide the blading so that each subdivision thereof produces one of the air currents but it is found with such an arrangement that any marked alteration in consumption of air in one 15 of the currents reacts adversely on the pressure 1 conditions and quantity of air in the second current.
- blower in which the fan blading impels the air 20 current in the axial direction of the fan shaft and to provide two co-axial fan blade systems of different diameter on thesame shaft so that the two blade systems produce two air currents of different pressure, one in each system. Whilst 25 this form of blower is more satisfactory in operation than the centrifugal type, it is relatively expensive to manufacture.
- a blower of the type referred to for producing two distinct air currents of different pressures comprises at least two co-axially 40 mounted fans of different diameter, of which the larger is spaced axially from the smaller in the direction of the blower intake.
- the fans are each closely surrounded by one of two concentrically disposed cylindrical jackets or casings,
- FIG. 1 shows a multiple stage 5 blower in central sectional elevation constructed in accordance with the invention, only that portion of the blower being shown which is necessary for clear understanding of the invention.
- Fig. 2 shows in similar view a modification of 10 Fig. 1.
- the blower shown in the drawing is constructed for use with internal combustion engines and is arranged to supply two air currents of different pressure, one for. cooling the engine and the other for scavenging purposes, the engine, for example, being used as the driving motor of a vehicle or aircraft.
- the blower is arranged to' be driven fro-m the crank shaft of the engine, a portion of which is indicated at. I, the blower shaft 4 being geared to the shaft l by two sets of transmission gear wheels 2 and 3, this gear transmission being represented somewhat diagrammatically in the drawing.
- Two fans 5 and 6 are keyed upon the shaft 4, the fan 5 being of larger diameter than the fan v6 and displaced axially with respect thereto towards the air inlet of the. blower.
- the blower is mounted so that the air current produced by the travelling speed of the vehicle oraircraft enters the inlet of the blower in the direction of the arrows I thus producing an initial air pressure at the inlet.
- the blading8 of the fan 5 is of greater radial length than the blading I2 of the fan 6, but is of the same root diameter, the fans 5 and 6 being provided with hubs of equal diameter.
- a cylindrical spacer l5 of the same diameter as the hubs of the fans is interposed between the two fans as shown in the drawing and is likewise keyed to the shaft 4.
- a domed member I6 is provided and directed towards the incoming air stream and is of a stream line configuration adapted to conduct the airsmoothly into the fan blading, the domed member terminating adjacent to the fan 5 with a diameter equal to the diameter of the hub of the said fan.
- An outer cylindrical jacket or casing l4 surrounds the blading 8 of the fan 5 close to the periphery thereof andan inner cylindrical jacket or casing 9 is similarly arranged around the blading I! of the fan 6 and is concentrically disposed within the casing It so as to provide an outer annular. conduit Ill between the casings O and shaft 4.
- conduit I3 is formed by the provision of an inner cylindrical wall I! following more or less the contour of casing 9 as shown in the drawing.
- the casing 9 terminates at the inlet end ll of the inner conduit l3 adjacent to the delivery side of the blading 8 and acts as a partition which in the operation of the blower divides the air current delivered by the blading 8 into two annular streams, the outer one of which is conveyed by the conduit I 0 to an outlet, not shown in the drawing but is represented diagrammatically by a broken arrow, and is conducted therefrom to the cooling system of the internal combustion engine.
- the inner annular current of air delivered by the blading 8 is further compressed by the blading 12 of the fan 6, this blading being given a suitable pitch for this purpose.
- the air delivered by blading I2 is conveyed by the conduit I3 to an outlet I8, shown at the bottom right-hand portion of the drawing, from which it is conducted to the scanvenging ports of the engine cylinders.
- blower shown in Fig.1 is modified as illustrated in Fig. 2. In all of its essential elements and arrangements this blower is similar to that shown in Fig. 1, and corresponding elements are denoted with similar reference numerals.
- , smaller in diameter than blading I2 is fixed on the blower shaft 4 and spaced, in the direction of air flow, from blading l2 by spacing cylinder 22 which, the same as cylinder l5,"is also keyed to Blading 2
- annular duct 24 is formed, which is concentric with duct l3, and into which the inner portion of blading I2 delivers air of the second pressure stage, and the pressure of which is further increased to a third pressure stage by blading 2
- Air of the second pressure stage for scavenging Purposesas in Fig. 1-- is delivered directly through duct I3 into exhaust port IS.
- the exhaust port for the first pressure stage is indicated in Fig. 2 only by a dotted arrow.
- a multi-stage blower comprising in combination a plurality of axially spaced rotatable fans having blading of progressively different radial 5 length, and pitched to impel air in the direction of their rotary axis, and concentric cylindrical casings, each closely surrounding one of the fans to form between the casings delivery chambers for separate air currents, each casing for a smaller diameter fan extending beyond that fan and closely to the blading of the next preceding larger diameter fan, whereby the air stream deivered by the larger fan is divided into two individual concentric streams, of which the inner stream constitutes the air supply for the next smaller diameter fan, and the outer stream is directy discharged into the chamber surrounding the inner stream, and means for separately discharging the air from each chamber to obtain a plurality 20 of separate air streams of difierent pressure stages.
- a multi-stage blower comprising in combination a plurality of axiallyspaced rotatable fans having blading of progressively different 25 radial length, and pitched to impel air in the direction of their rotary axis, and concentric cylindrical casings, each closely surrounding one of the fans to form between the casings delivery chambers for separate air currents, each casing 30 for a smaller diameter fan extending beyond that fan and closely'to the blading of the next preceding larger diameter fan, whereby the air stream delivered by the larger fan is divided into two individual concentric streams, of which the 35 inner stream constitutes the air supply for the next smaller diameter fan, the blade pitch of each smaller diameter fan being suitaby dimensioned with respect to the pitch of the blading portion of the next preceding larger fan which 40 supplies the air to'the smaller fan, whereby the pressure of the air delivered to it by the preceding fan is increased, and each fan delivers into its larger appertaining chamber directly an air "current of different pressure, and means for separately discharging the different pressure currents from said
- a multi-stage blower comprising in combination a plurality of axially spaced rotatable fans having blading of progressively different radial length, and pitched to impel air in the direction of their rotary axis, and concentric cylindrical casings, each closely surrounding one of chambers for separate air currents, each casing 55 for a smaller diameter fan extending beyond that fan and closely to the blading of the next pre-
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
July 7, 1936. GOSSLAU I 2,Q46,737
MULTIPLE STAGE BLOWER Filed Oct. 26, 1934 /4 9 6 r2 p I 77 X 7 f 3 w17 l6 r M Mil, 014w Patented July 7, 1936 UNITED STATES I 2,046,737 -MULTIPLE STAGE nLowEa Fritz Gosslau, Berlin-Charlottenburg, Germany, assignor, by mesne assignments, to Sie'mens Apparate und Maschinen Gesellschaft mit beschrankter Haftung, Berlin, Germany, a corporation of Germany Application October 26, 1934, Serial No. 30,042
In Germany October 30, 1933 3 Claims. (01. 230-122) This invention relates to improvements in multiple stage blowers. It is necessary in many installations to supply a plurality of currents of air at different pres- 5 sures, for example currents of cooling air and scavenging air for internal combustion engines, and to simplify the blower installation, it has been proposed to construct blowersto produce two separate air currents of different pressures. With centrifugal blowers it has been customary to sub-divide the blading so that each subdivision thereof produces one of the air currents but it is found with such an arrangement that any marked alteration in consumption of air in one 15 of the currents reacts adversely on the pressure 1 conditions and quantity of air in the second current.
It has therefore been proposed to'construct a blower in which the fan blading impels the air 20 current in the axial direction of the fan shaft and to provide two co-axial fan blade systems of different diameter on thesame shaft so that the two blade systems produce two air currents of different pressure, one in each system. Whilst 25 this form of blower is more satisfactory in operation than the centrifugal type, it is relatively expensive to manufacture.
It is an object of this invention to provide a multiple stage blower of the type in which the 30 fan blading impels the air in the axial direction of the fan shaft, which is relatively simplein construction and cheap to manufacture whilst ensuring complete segregation of the several air currents of different pressure produced by the 35 blower. g
In a preferred construction according to the invention, a blower of the type referred to for producing two distinct air currents of different pressures, comprises at least two co-axially 40 mounted fans of different diameter, of which the larger is spaced axially from the smaller in the direction of the blower intake. The fans are each closely surrounded by one of two concentrically disposed cylindrical jackets or casings,
65 fan from which that air supply is delivered, to
produce an increase in pressure of the air so delivered.
In order that the invention may be fully understood, reference is directed to the accompanying drawing, which in Fig. 1 shows a multiple stage 5 blower in central sectional elevation constructed in accordance with the invention, only that portion of the blower being shown which is necessary for clear understanding of the invention.
Fig. 2 shows in similar view a modification of 10 Fig. 1.
The blower shown in the drawing, is constructed for use with internal combustion engines and is arranged to supply two air currents of different pressure, one for. cooling the engine and the other for scavenging purposes, the engine, for example, being used as the driving motor of a vehicle or aircraft.
Referring to Fig. l, the blower is arranged to' be driven fro-m the crank shaft of the engine, a portion of which is indicated at. I, the blower shaft 4 being geared to the shaft l by two sets of transmission gear wheels 2 and 3, this gear transmission being represented somewhat diagrammatically in the drawing. Two fans 5 and 6 are keyed upon the shaft 4, the fan 5 being of larger diameter than the fan v6 and displaced axially with respect thereto towards the air inlet of the. blower. Preferably the blower is mounted so that the air current produced by the travelling speed of the vehicle oraircraft enters the inlet of the blower in the direction of the arrows I thus producing an initial air pressure at the inlet. The blading8 of the fan 5 is of greater radial length than the blading I2 of the fan 6, but is of the same root diameter, the fans 5 and 6 being provided with hubs of equal diameter. A cylindrical spacer l5 of the same diameter as the hubs of the fans is interposed between the two fans as shown in the drawing and is likewise keyed to the shaft 4. At the intake side of the fan a domed member I6 is provided and directed towards the incoming air stream and is of a stream line configuration adapted to conduct the airsmoothly into the fan blading, the domed member terminating adjacent to the fan 5 with a diameter equal to the diameter of the hub of the said fan.
' An outer cylindrical jacket or casing l4 surrounds the blading 8 of the fan 5 close to the periphery thereof andan inner cylindrical jacket or casing 9 is similarly arranged around the blading I! of the fan 6 and is concentrically disposed within the casing It so as to provide an outer annular. conduit Ill between the casings O and shaft 4.
l4 and an inner annular conduit l3 between the casing 9 and the peripheries of spacer l5 and the hub of the fan 6; the forwardly Continuing portion of the conduit I3 is formed by the provision of an inner cylindrical wall I! following more or less the contour of casing 9 as shown in the drawing. The casing 9 terminates at the inlet end ll of the inner conduit l3 adjacent to the delivery side of the blading 8 and acts as a partition which in the operation of the blower divides the air current delivered by the blading 8 into two annular streams, the outer one of which is conveyed by the conduit I 0 to an outlet, not shown in the drawing but is represented diagrammatically by a broken arrow, and is conducted therefrom to the cooling system of the internal combustion engine. The inner annular current of air delivered by the blading 8 is further compressed by the blading 12 of the fan 6, this blading being given a suitable pitch for this purpose. The air delivered by blading I2 is conveyed by the conduit I3 to an outlet I8, shown at the bottom right-hand portion of the drawing, from which it is conducted to the scanvenging ports of the engine cylinders.
If it is desired to supply supercharging air to the engine the blower shown in Fig.1 is modified as illustrated in Fig. 2. In all of its essential elements and arrangements this blower is similar to that shown in Fig. 1, and corresponding elements are denoted with similar reference numerals. It will be noted, however, that in addition to bladings 8 and I2, a third fan 28 with blading 2|, smaller in diameter than blading I2, is fixed on the blower shaft 4 and spaced, in the direction of air flow, from blading l2 by spacing cylinder 22 which, the same as cylinder l5,"is also keyed to Blading 2| is closely surrounded by a cylindrical wall H which follows in substance the contour of wall 9 and extends closely to the delivery side of blading l2. Further, an inner cylindrical wall 23 is provided which at its left hand end approaches closely hub 20, and has the same diameter as this hub. It flares toward the delivery end of the blower, following in substance the contour of wall l1. Thereby, an' innermost annular duct 24 is formed, which is concentric with duct l3, and into which the inner portion of blading I2 delivers air of the second pressure stage, and the pressure of which is further increased to a third pressure stage by blading 2|. Thus the total amount of air delivered by blading I2 is divided into two parts. Air of the second pressure stage for scavenging Purposesas in Fig. 1--is delivered directly through duct I3 into exhaust port IS. The air for the third stagefor supercharging purposes above-mentioned-is delivered by blading I2 directly into duct 24, and after its pressure is increased by blading2l, passes through the remainder of this duct into exhaust port IS. The same is in Fig. 1, the exhaust port for the first pressure stage is indicated in Fig. 2 only by a dotted arrow.
The invention is not limited to the specific examples above described, but may be modified to suit particular requirements within the terms of the appended claims.
the fans to form between the casings delivery What I claim and desire to secure by Letters Patent of the United States is:
1. A multi-stage blower comprising in combination a plurality of axially spaced rotatable fans having blading of progressively different radial 5 length, and pitched to impel air in the direction of their rotary axis, and concentric cylindrical casings, each closely surrounding one of the fans to form between the casings delivery chambers for separate air currents, each casing for a smaller diameter fan extending beyond that fan and closely to the blading of the next preceding larger diameter fan, whereby the air stream deivered by the larger fan is divided into two individual concentric streams, of which the inner stream constitutes the air supply for the next smaller diameter fan, and the outer stream is directy discharged into the chamber surrounding the inner stream, and means for separately discharging the air from each chamber to obtain a plurality 20 of separate air streams of difierent pressure stages.
2. A multi-stage blower comprising in combination a plurality of axiallyspaced rotatable fans having blading of progressively different 25 radial length, and pitched to impel air in the direction of their rotary axis, and concentric cylindrical casings, each closely surrounding one of the fans to form between the casings delivery chambers for separate air currents, each casing 30 for a smaller diameter fan extending beyond that fan and closely'to the blading of the next preceding larger diameter fan, whereby the air stream delivered by the larger fan is divided into two individual concentric streams, of which the 35 inner stream constitutes the air supply for the next smaller diameter fan, the blade pitch of each smaller diameter fan being suitaby dimensioned with respect to the pitch of the blading portion of the next preceding larger fan which 40 supplies the air to'the smaller fan, whereby the pressure of the air delivered to it by the preceding fan is increased, and each fan delivers into its larger appertaining chamber directly an air "current of different pressure, and means for separately discharging the different pressure currents from said chambers.
3. A multi-stage blower comprising in combination a plurality of axially spaced rotatable fans having blading of progressively different radial length, and pitched to impel air in the direction of their rotary axis, and concentric cylindrical casings, each closely surrounding one of chambers for separate air currents, each casing 55 for a smaller diameter fan extending beyond that fan and closely to the blading of the next pre-
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2046737X | 1933-10-30 |
Publications (1)
Publication Number | Publication Date |
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US2046737A true US2046737A (en) | 1936-07-07 |
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ID=7982455
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US750042A Expired - Lifetime US2046737A (en) | 1933-10-30 | 1934-10-26 | Multiple stage blower |
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US (1) | US2046737A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2698129A (en) * | 1949-05-12 | 1954-12-28 | Joy Mfg Co | Multistage axial fan with boundary layer control |
US2739756A (en) * | 1952-03-07 | 1956-03-27 | Worthington Corp | Turbo-compressor |
US2937805A (en) * | 1952-12-15 | 1960-05-24 | Studebaker Packard Corp | Stator blade assembly and method and machine for making same |
US3283995A (en) * | 1965-04-28 | 1966-11-08 | United Aircraft Corp | Splitter vane construction for turbofan engine |
-
1934
- 1934-10-26 US US750042A patent/US2046737A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2698129A (en) * | 1949-05-12 | 1954-12-28 | Joy Mfg Co | Multistage axial fan with boundary layer control |
US2739756A (en) * | 1952-03-07 | 1956-03-27 | Worthington Corp | Turbo-compressor |
US2937805A (en) * | 1952-12-15 | 1960-05-24 | Studebaker Packard Corp | Stator blade assembly and method and machine for making same |
US3283995A (en) * | 1965-04-28 | 1966-11-08 | United Aircraft Corp | Splitter vane construction for turbofan engine |
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