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Publication numberUS3324799 A
Publication typeGrant
Publication dateJun 13, 1967
Filing dateAug 5, 1965
Priority dateAug 5, 1965
Publication numberUS 3324799 A, US 3324799A, US-A-3324799, US3324799 A, US3324799A
InventorsTerrano Paul P
Original AssigneeTrw Inc
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Radial staging for reentry compressor
US 3324799 A
Abstract  available in
Images(2)
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Claims  available in
Description  (OCR text may contain errors)

June 13, 1967 P. P. TERRANO 3,324,799

RADIAL STAGING FOR REENTRY COMPRESSOR Filed Aug. 5, 1965 2 Sheets-$heet 1 INVENTOR. 814/4 P 72224A/0 m' Mf ATTORNEYS June 13, 1967 P. P. TERRANO 3,324,799

RADIAL STAGING FOR REENTRY COMPRESSOR Filed Aug. 5. 1965v 2 Sheets-Sheet 2 INVENTOR. P4114. Ewen/v0 ATTORNEYS United States Patent 3 324,799 RADIAL STAGING FdR REENTRY COMPRESSOR Paul P. Terrano, Cleveland, Ohio, assignor to TRW Inc, Cleveland, Ohio, a corporation of Ohio Filed Aug. 5, 1965, Ser. No. 477,480 3 Claims. (Cl. 103-96) This invention relates generally to reentry compressors and more particularly relates to a reentry compressor having a single sided rotor and wherein multiple staging is accomplished by interconnecting multiple concentric pumping channels in series flow relation, the multiple concentric channels being disposed in confronting registry with multiple concentric rows of blades havin an optimum number of blades and a predetermined diameter ratio.

Multiple staging of reentry compressors is frequently desirable as increased pressures may be required for particular applications. In accordance with the principles of the present invention, two or more stages can be obtained in a single sided rotor by disposing multiple concentric rows of blades and pumping passages in spaced relation relative to rotational axis. With such an arrangement, the inlet and outlet ports may be interchanged and the basic arrangement can either be repeated or combined in series or in parallel. Such a multistaging arrangement avoids most of the flow losses inherent in other designs and more nearly maintains the continuity of fluid flow from the inlet to the outlet.

It is an object of the present invention, therefore, to provide a means of multistagin" a reentry compressor of the type utilizing a single sided rotor.

Another object of the present invention is to provide a multistaging arrangement for a reentry compressor wherein the inlet and outlet ports may be selectively interchanged with no change in the basic principle.

Another object of the present invention is to provide a multistaging arrangement for a reentry compressor which can be repeated and combined in series or parallel.

A still further object of the present invention is to provide a multistaging arrangement for a reentry compressor wherein flow losses are minimized and wherein the continuity of fluid flow from the inlet and outlet is preserved.

Many other objects, features, advantages and additional objects of the present invention will become manifest to those versed in the art upon making reference to the detailed description which follows and the accompanying sheets of drawings in which an exemplary form of a reentry compressor is shown by way of illustrative example.

On the drawings.

FIGURE 1 is an elevational view with parts broken away and shown in cross-section illustrating an exemplary form of a reentry compressor embodying the principles of the present invention;

FIGURE 2 is a fragmentary cross-sectional view similar to FIGURE 1 but showing a covered interconnecting passageway between stages;

FIGURE 3 is a cross-sectional view taken generally n the plane of line IIIIII of FIGURE 2 and illustrates additional details of construction of the covering plate;

FIGURE 4 is an elevational view showing additional details of construction of the rotor; and

FIGURE 5 is an elevational view of the cover member provided in accordance with the principles of the present invention and showing at line II the plane of the crosssectional portions of FIGURE 1.

As shown on the drawings:

Fluid pumps which are commonly known as drag pumps. offer characteristics in a centrifugal compressor which fall somewhere between those of the positive displacement pump and the centrifugal pump. This means the single stage pump produces a medium pressure at the output when running at a medium speed, as compared with either of the other two types. Because of those characteristics and the fact that it is not a positive displacement pump, there are many applications where such a pump should do a good job and be economically feasible as compared to the other two types.

In some instances, it is desirable to have a discharge pressure in the same magnitude as the positive displacement pump while running in the same speed magnitude. In accordance with the principles of the present invention, such objective can be accomplished by placing additional stages on the drag pump without increasing the size and complexity of the pump by providing multiple concentric rows of blades and pumping passages which are interconnected or interrelated to afford a multistaging arrangement.

The pump of the present invention is shown generally at 10 and comprises a casing 11 having a flange 12 in which is formed a plurality of threaded apertures 13. A cover 14, similarly flanged as at 16, passes a plurality of fasteners 17 which together with lock washers 18 may be used to fasten the casing 11 and the cover 14 in firm assembly with one another.

The cover 14 is particularly characterized by an inner face 20 having formed therein a semi-toroidal circumferentially extending pumping duct 21 having an inner wall 22 and an outer wall 23, both of which are arranged in generally concentric relation to the axis of the pump, thereby to form a pumping duct which extends circumferentially from an end portion 24 to an end portion 26.

In accordance with the principles of the present invention, a second pumping duct is shown at 27 and is likewise of semi-toroidal configuration extending circumferential-1y and having an inner wall 28 and an outer wall 29 and extending from a portion shown at 30 to an end portion 31. The pumping channel or duct 21 is interconnected with the pumping channel or duct 27 by means of a passageway 32.

In the form of the invention illustrated, the cover 14 has a boss 33 in which is formed an inlet port 34 communicating with the inner pumping duct 27 near the end portion 31 thereof.

The cover 14 is further characterized by a boss 36 in which is formed an outlet port 37, which outlet port 37 intersects the outer pumping channel or duct 21 near the end portion 24 thereof. Accordingly, fluid entering the inlet port 31 will pass through the pumping channel or duct 27 and thence through the interconnecting passage 32 into the end portion 26 of the outer pumping channel or duct 21 and will then pass through the outlet port 37.

Referring now to FIGURES 1 and 4, it may be noted that a rotor is provided at 36 and includes a shaft 37 which is journaled in a bearing assembly shown in dotted outline generally at 38. The rotor 36 has a radial face 39 which is particularly characterized by having formed therein semi-toroidal circumferentially continuous vane ducts which are concentric with respect to one another and which are spaced to lie in confronting registry with the pumping channels or ducts 21 and 27. In this connection, note that the face 39 has an outer circumferentially extending recess formed therein which is identified at 40 including an inner wall 41 and an outer wall 42.

There is further provided an annular circumferentially extending recess 43 having an outer wall 44 and an inner Wall 46.

In the course of fabrication, the rotor 36 is provided with a plurality of slots which extend transversely of the corresponding recesses 40 and 43 and which slots are more specifically identified in FIGURE 4 at 47. Received within each slot 47 is a vane 48 for the outer recess or vane duct 40 and 49 for the inner recess or vane duct 43. Thus, a plurality of vanes 48 are disposed in an annular row in circumferentially spaced relation so that all of the vanes 48 and 49, in the respective recesses 40 and 43, form a plurality of impeller pockets 50 and 51 adapted to be moved upon rotation of the impeller 36 within the casing formed by the cover 14 and the casing 11.

As will be noted upon inspecting the structure shown in the drawings, the two concentric rows of blades 48 and 49 have an optimum number of blades and an appropriate diameter ratio. In the arrangement shown, the inlet port 34 is near the center and the outlet port 37 is near the outside diameter, however, it will be readily recognized by those versed in the art that the inlet and outlet ports may be interchanged with no change in the basic principle. An inlet at the outer diameter is desirable for certain combinations of flow, pressure and speed, while an inlet at the center is indicated for certain other combinations. Further, the basic arrangement of multiple concentric channels and blade rows can be repeated and can be combined either in series or in parallel. Further, three or more concentric channels could also be used rather than two, as shown in the exemplary structure, and it will be readily recognized that if desired, partial channels'could be used instead of circumferentially continuous channels.

Further, although in FIGURE the interconnecting passage 32 is shown uncovered, it is also possible to provide a cover for such passage in order to cut down losses and in this regard a cover is shown in the arrangement of FIGURES 2 and 3 wherein like parts are designated by like numbers but with a suffix a. As shown in FIG- URES 2 and 3, the area adjacent the interconnecting passage 32a is recessed at its edges, thereby to receive and seat a sheet metal cover 60 having a narrow end 61 located adjacent the end portion a of the inner duct 27a to an end portion 62 which extends transversely as at 63 to overlie the end portion 26a at the end of the outer pumping duct 21a. The recess portion adjacent the edges of the interconnecting passage 32a are shown at 64.

By virtue of the provision made, continuity of fluid flow from the inlet port 34 to the outlet port 37 is afforded and multistaging is accomplished with a minimum of flow loss.

The number of blades, the diameter ratio and the cant angle may be difierent in each row of blades, depending on performance criteria. In such event, the blades may be assembled to the rotor by means other than the slotting procedure described by way of exemplification.

It may also be noted that it is desirable that the inlet port be located near the inner diameter of the corresponding channel while the outlet port should be located near the outer wall of the corresponding channel.

Although minor modifications might be suggested by those versed in the art, it should be understood that I wish to embody within the scope of the patent warranted hereon all such modifications as reasonably and properly come within the scope of my contribution to the art.

I claim as my invention:

1. A fluid pump of the drag type comprising a casing having an inlet opening for connection to a source of fluid to be pumped and an outlet opening for direction of the pumped fluid to a point of utilization,

said casing having a radial face formed internally thereof characterized by having formed therein inner and outer concentrically disposed annular pumping ducts communicating with said inlet and outlet ports, a rotor in said casing having a drive shaft connected thereto,

said rotor having a radial face including annular recesses disposed in concentric relation for registry with said pumping ducts,

said rotor having a plurality of circumferentially spaced slots each extending across said annular recesses,

and vane means in said slots to form with said recesses a plurality of impeller pockets in each respective recess,

and interconnecting passage means in said casing disposed between said pumping ducts to interconnect said pumping ducts in staged flow relation, said radial face of said casing being recessed adjacent said interconnecting passage means, and a thin cover member received and seated in said recessed portion of said casing face to overlie said interconnecting passage means and the adjacent end portions of said inner and outer ducts, thereby to insure continuity of fluid flow with minimum flow loss.

2. A reentry compressor comprising a single sided rotor having multiple concentric rows of blades,

a casing having a wall extending closely adjacent said rotor and having formed therein multiple concentric pumping channels confronting said rows of blades,

said wall having passage means formed therein extending radially and interconnecting said concentric pumping channels in flow relation,

and interchangeable inlet and outlet ports formed in said casing communicating with said respective ends of said concentric pumping channels to direct pumping fluid to and from the pump, and

means forming a cover for said passage means to reduce flow losses between the concentric pumping channels.

3. A two stage pump comprising a rotor having a radial face,

two concentric blade channels of substantially semi-toroidal cross-section in said face,

a plurality of circumferentially spaced pumping blades in said channel forming a plurality of pumping pockets,

and a casing having two concentric pumping ducts of substantially semi-toroidal cross-section confronting said pumping blades,

one end of each of said concentric pumping ducts having a port formed therein comprising respectively an inlet and an outlet for the pump,

the opposite end of each said concentric pumping ducts being interconnected by a crossover passageway to stage said pumping ducts in interconnected flow relation, and

a cover for said crossover passageway and overlying the adjacent ends of said pumping ducts to reduce flow losses between the pumping ducts.

References Cited UNITED STATES PATENTS 1,635,846 7/1927 Holmes 1031 10 1,811,651 6/1931 Schlachter 10396 2,256,741 9/1941 Gurley 10396 3,139,232 6/1964 Peterson 230-131 FOREIGN PATENTS 731,085 2/ 1943 Germany.

752,398 10/ 1952 Germany.

874,503 4/ 1953 Germany.

DONLEY I. STOCKING, Primary Examiner.

HENRY F. RADUAZO, Examiner.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US1635846 *Feb 11, 1925Jul 12, 1927Westco Chippewa Pump CompanyPump
US1811651 *Jul 5, 1929Jun 23, 1931Dempster Mill Mfg CompanyPrimer for impulse pumps
US2256741 *Dec 3, 1938Sep 23, 1941Gurley John WRotary pump
US3139232 *Aug 24, 1959Jun 30, 1964Orville N PetersonRefrigeration pump
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DE752398C *Jul 18, 1941Oct 13, 1952Siemens AgSelbstansaugende Umlaufpumpe
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Referenced by
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US4412781 *Jul 21, 1981Nov 1, 1983Hitachi Ltd.Vortex blower
US4556363 *Jun 20, 1983Dec 3, 1985Nippondenso Co., Ltd.Pumping apparatus
US4662659 *Apr 21, 1986May 5, 1987Hydril CompanyTubular joint with trapped mid-joint metal-to-metal seal having unequal tapers
US5248223 *Jun 9, 1992Sep 28, 1993Walbro CorporationFuel pump with anti-reversion inlet
US5295784 *Aug 17, 1992Mar 22, 1994Durr Dental Gmbh & Co. KgSuction device, especially for use in dentistry
US5310308 *Oct 4, 1993May 10, 1994Ford Motor CompanyAutomotive fuel pump housing with rotary pumping element
US5580213 *Dec 13, 1995Dec 3, 1996General Motors CorporationElectric fuel pump for motor vehicle
US5596970 *Mar 28, 1996Jan 28, 1997Ford Motor CompanyFuel pump for an automotive fuel delivery system
US5966927 *Mar 31, 1997Oct 19, 1999Wilson; Michael A.Efficiency enhanced turbine engine
US6071071 *Jul 2, 1997Jun 6, 2000J. Eberspacher Gmbh & Co.Side-channel fan, in particular for supplying combustion air in an independent heater of a motor vehicle
US6105359 *Jul 15, 1999Aug 22, 2000Wilson; Michael A.Efficiency enhanced turbine engine
US6394748Aug 21, 1998May 28, 2002Werner Rietschle Gmbh + Co. KgMulti-stage side channel pump
US6877511Jun 10, 2003Apr 12, 2005Bird Products CorporationPortable drag compressor powered mechanical ventilator
US7090460Sep 28, 2001Aug 15, 2006Leybold Vakuum GmbhPump embodied as a side channel pump
US7222623Dec 29, 2004May 29, 2007Birds Products CorporationPortable drag compressor powered mechanical ventilator
US7849854Sep 7, 2004Dec 14, 2010Bird Products CorporationPortable drag compressor powered mechanical ventilator
WO1998002663A1 *Jul 2, 1997Jan 22, 1998Eberspaecher J Gmbh & CoSide channel fan, in particular for supplying combustion air in an independent heater of a motor vehicle
WO1999010656A1 *Aug 21, 1998Mar 4, 1999Rietschle Werner Gmbh & Co KgMulti-stage side channel pump
WO2001006102A1 *Jul 19, 1999Jan 25, 2001Michael A WilsonEfficiency enhanced turbine engine
WO2002031360A1 *Sep 28, 2001Apr 18, 2002Englaender HeinrichPump embodied as a side channel pump
WO2004005724A1 *Jul 4, 2003Jan 15, 2004Boc Group PlcRegenerative fluid pump and stator for the same
Classifications
U.S. Classification415/55.6, 415/55.4
International ClassificationF04D23/00
Cooperative ClassificationF04D23/008
European ClassificationF04D23/00R