CA1224971A - Gear rotor fuel pump - Google Patents

Abstract

GEAR ROTOR FUEL PUMP

ABSTRACT OF THE DISCLOSURE
A rotary pump for pumping liquid which includes a rotor combination in the form of a vane pump or gear and rotor with pumping chambers disposed circumferentially around the rotor. The chambers progressively increase in the inlet area and ensmall in the outlet area. Resilient means are interposed between the ensmalling chambers and an outlet to block backflow of the pressurized outlet liquid into pumping chambers containing vaporized liquid instead of solid liquid, thus reducing the pump noise under conditions of vaporization termed "cavitation".

Description

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Title Gear Rotor Fuel Pump Eield of Invention Electric fuel pumps utilizing a rotary pump and electric drive housed together for mounting on a vehicle or in a vehicle fuel tank.

Background of the Invention Rotary fuel pumps driven by an electrical powering device have been utilized for some years in some vehicles either as original equipment or as appliances to supplement the original fuel supply system. The pump and power unit are frequently in a common housing as shown, for example, in United States Patent No. 4,35~,641, issued October 5, 1982 to Charles H. Tuckey.

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Since the pumps are frequently mounted in the fuel tanks of a vehicle, the noise factor is extremely important. A pump under load will normally produce more noise and this may be audible as a humming noise, to an S annoying degree, to passengers in the vehicle. Various pulse dampening devices have been tried with some success but since they usually involve material such as a closed cell foam material or a hollow pulse dampening chamber of a synthetic flexible material, the useful life. of these devices is limited by the vulnerability of the material in the presence of hydrocarbons.

Normally, during operation of these pumps, the media being pumped is in a liquid state and noise is at a minimum level. As the pumping cells are filled during the intake portion of the cycle, there are no voids, that is, no vapor in the pumping chamber when the exhaust ports are opened. If, however, a void or vapor is present (cavitation) in the pumping chamber when the exhaust port is opened, the pressure on the outlet side of the port can force fluid back through the exhaust port in a reverse direction into the pumping chamber to fill the void.

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Since fuel in ~he outlet side of the exhaust port is normally at an operating pressure of, for example, 15 to 80 pounds per square inch, any reversal of flow through the exhaust port would be a very high velocity causing an impact noise. With a relatively standard rotation pump, this sequence can occur five times per revolution of the pumping rotor and at high speed can become very audible.

It is an object of the present invention to provide a pump construction which will avoid the reverse flow impact during cavitation and consequently materially reduce the noise of the pump operation under these circumstances.

It will be appreciated that in the pumping cycle as one pumping cell is exhausting, another cell is taking in fluid at the same time. In other words, intake and exhaust pressure waves are timed with one another, and normally the quantity of fluid being exhausted from each cell is the same as that being taken in by another cell.

The principle of the present invention lies in the elirnination of the reversal of fluid 10w through the exhaust port.

Another object of the invention is the interposition of a flexing device over the exhaust port adjacent the rotor to al]ow the escape of fluid under pressure but to prevent fluid under pressure from impacting back into the pumping chamber under cavitation conditions, namely, vapor conditions.

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A further concept of the invention involves dividing the exhaust port area into several openings with a one-way valve at the discharge side of each port opening. This will allow liquid fuel under pressure to flow out and at the same time prevent any fluid pressure from backing up into the pumping chamber during a vapor or cavitation condition.

With respect to previously issued patents, Parsons U. S. patents 2,650,544 and 2,383,153 show sealing pla-tes for gear rotor pumps but these plates do not have the function of flexing for output fluid and serving as one-way relief plates for noise control. The Parsons patent 2,383,153 shows a stub shaft mount for an inner gear rotor, but the sealing disc does not rotate with the inner rotor. The U. S. patent to Dolan

2,787,963 illustrates a biased rigid plate bearing against a gear rotor assembly for start-up pressure, this plate being backed by pump outlet pressure after start up.

The concept of a flexible back-up plate for pumping elements which provides at least one side of the pumping chamber and which allows escape of pressure liguid to a pressure outlet system with a unidirectional function in the circumstance of vaporization (cavitation) is an important feature of the present disclosure.

Other objects and features of the invention will be apparent in the following description and claims in which the principles of the invention are set forth together with details to enable a person skilled in the art to practice the invention, all in connection with the best mode presently contemplated for the invention.

Brief Description of the Drawings . _ DRAWINGS accompany the disclosure and the various views thereof may be briefly described as:
FIG. 1, a longitudinal section of a rotating, electrically driven pump.
FIG. 2, a transverse sectional view on line 2--2 of FIG. 1.
FIG. 3, a longitudinal section of a modified pump construction.
FIG. 4, an interior view of the inlet end of the pump and the pump assembly.
FIG. 5, a view of the pump inlet end from the outside.
FIG. 6, a view of the pump inlet end from the inside without the pump elements.
FIG. 7, an elevation of a ~pring.
FIG. 8, side view of the spring retainer.
FIG. 9, an eleva-tion view of the gear pump seal plate.
FIG. 10, a view of a finger plate for edge reinforcement of a seal plate.
FIG. 11, a view similar to FIG. 3 with a supplemental flexible plate on the gear rotor assembly.
FIG. 12, an elevation of the supplemental plate.
FIG. 13, an edge view of the supplemental plate.
FIG. 14, an inside end view of an end housing of the pump assembly, at arrow 14.
FIG~ 15, an outside end view of the end housing of the pump assembly, at arrow 15.
FIG. 16, a sectional view of the end housing at line 16--16 of FIG. 15.

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Detailed Description o~ the Invention and the Manner and Process of Usin~
With respect to a proper disclosure, reference is made to my copending application, U. S. Serial No.
403,097, filed July 29, 1932, now issued into U. S.
Patent No. 4,500,270, and U. S. Patent No. 4,352,641, issued October 5, 1982. In FIG. 1, the inlet end of a rotary pump is illustrated wherein an end cap 10 has a nippl~ inlet port 11 and an outwardly extending an-nular flange 12 with an annular rim 14 captured in a shell 16 with an inturned flange 18. A sealing O-ring 20 is interposed between flanges 14 and 18.

Inside of -the flange 14 is a retainer plate 22 for a pulse dampener diaphragm which carries a spring retainer cup 24. A pulse modulation diaphragm 30 lies inside the retainer plate 22, the annular edge being captured and retained between the periphery of plate 22 and the periphery of a pump end plate 40. Within a surface recess 41 in the plate 40 is a reed valve retainer disc 42 retained by a recessed screw 44. A
dampener spring 46 bears at one end against the end cap 10 in an annular groove and at the other end is lodged in the cup 24. The bottom of the cup bears against the central area of the diaphragm 30.

The reed valve retainer disc 42 has a flat surface which can serve as a stop for the central por-tion of the diaphragm 30 and the bot-tom of cup 24.

Adjacent the pump end plate 40 is a pump cam ring 50 which houses a pump rotor 52 mounted on a motor armature drive shaft 54 with a pin 56 providing the driving relationship.

The rotor 52 has radial slots to receive pump roller vanes 60. A bearing retainer housing and back-up plate 62 adjacent the pump cam ring 50 has a central open-ing to receive an armature shaft bearing 64 on the armature shaft 54 which extends from the armature assembly 70. The housing 62 has a rearwardly extending flange 72 with an annular recess to receive the end of a flu~ring 74. The discharge end of the pump is not shown but is described in the above-referenced application and patent. The back-up plate 62 bearings against the pump rotor combina-tion and çloses the pumping chambers on one side of that combination.

; With reference to the pump end plate 40, the recess 41 is illustrated in profile in FIG. 2. This re-cess is enlarged at the top of the figure in a recess 80.
At the bottom of the plate at the side opposite recess 41 there are two lobe-like spaced recesses 82 and 84 connected by an arcuate port 85 which extend downwardly and are open to ports 86 perforating the plate to the inlet end. These ports register with openin~s 88 in the inlet plate 22 and diaphragm 30. Openings 88 extend to an annular inlet chamber 90 open to the port 11.

In FIG.2, four exhaust ports 92, 94, 96 and 98 perforate the plate 40 into the recess 41. At the top of FIGS. 1 and 2, a port 100 connects the recess 80 to a through passaye 102 in plate 50 leading to a pass-age 103 in housing 62 opening to the armature chambersurrounding the armature assembly 70.

As viewed in FIG. 2, a multi-fingered reed valve in the form of a thin flexible sheet has fingers 104, 106 and 108 overlying exhaust ports 94, 96 and 98. These fingers extend from a central palm portion 110 clamped to the pump end plate 40 by the flat retainer 42.
A tab 112 extends from the palm portion 110 in a direc-tion essentially oppos~te to the fingers to lodge in a recess and serve as a locator for the reed valve. It is not necessary tha-t port 92 be covered by a resilien-t fin-ger since by the time the compressive chambers reach this port, any vapor will be reduced to a liqud.

IN THE OPERATION of the pump when the armature is rotating and driving the pump rotor 52 within the cam ring 50, the roller vanes 60 create a sub-atmospheric condition in the inlet lobes 82, 84, and inlet fluid, for example, liquid gasoline, enters port 11 from a tank supply and flows into annular recess 90 and through open-ing 88 to passages 86 leading to the lobe-like recesses 82 and 84 and the connecting arcuate port 85 which is located at the periphery of the pump rotor 52. The ~24~

liquid enters the radial slots of the pump rotor and is carried around to the exhaust ports 92, 94, 96 and 98.
As the vane openings are ensmalled by the cam ring, the pressure of the fluid is increased and forced out of the exhaust ports into the recesses ~l and 80. Under normal circumstances, the fuel is forced past the reed valves or fingers 104, 106, 108 and will exit through the passages 100, 102 and 103 on the way to the outlet.

"Cavitation" is a term applied to a condition in pumping wherein the fluid being pumped turns -to a vapor. With volatile fuels, this is frequently a prob-lem especial~y in hot weather. As previously indicated, if an outlet pressure has developed in the outlet passage and a pumping chamber in the rotor reaches the outlet lexhaust) ports of the pump carrying, not solid fuel, but vapor, the liquid in the outlet passages tends to move back into the vacant pump chamber. This causes a reverse flow impact which creates noise in the pump.

To avoid this reverse flow impact, the reed valve fingers overlie the exhaust or outlet ports of the pump and block any tendency of the outlet pressure to move back into a vapor filled pump chamber. In this embodiment the exhaust ports have been divided from a single; arcuate port into individual ports which can be controlled individually.

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Another feature of the disclosed pump which contributes -to a steady even flow lies in the flexible diaphra~m 30 backed by the spring 46. Pressure in the outlet chamber 41 will ac-t against the diaphragm and spring and these resilient elemen~s will absorb pulses and smooth out the output flow.

A second embodiment of ~he invention is illus-trated in FIGS. 3 to 10. This embodiment is illustrated and described in my copending application, Serial No.
403,097, filed July 29, 1982, now issued into U. S.
Patent No. 4,500,270.

With reEerence first to FIG. 3, the general assembly of the gear rotor pump is shown in a longitu-dinal sec-tion. An inlet end shell or housing 120, which can be a die casting or molded part, butts against a cam ring 122 which has a reducsd flange 124 telescoping into one end of a flux ring 126. At the other end of the flux ring is an outlet end part 12~. The inlet end and the outlet end each have opposed shoulders against which sealing rings 130 are disposed, held in place by spun-in ends 132, 134 of an ou-ter metallic shell 136. The inlet housing 120 has a flat inner surface 137 which serves as one wall of a pump rotor housing.

In FIG. 3, an armature assembly 140 is illus-trated having a cylindrical drive projection 142 at oneend with slender projecting fingers 144 circumferentially spaced around projection 1~2. At the other end of assembly 140 is a commu-ta-tor disc 146.

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The armature shaft 160 at the commutator end is received in a central recess 162 in the end housing.
Reverting to FIG. 3, the outlet end housing 128 has an axially extending passage 164 which serves as a pump outlet in conjunction with a brass outlet fitting 166 carrying a one-way, spring-pressed outlet valve 168.
This fitting is molded into the outlet housing 128 formed of a glass reinforced plastic which has a high degree of resistance to hydrocarbons, as do the other plastlc parts of the assembly. A screw outlet bleed adjustment plug 170 is threaded into recess 172 in end housing 128 to control a passage 174 leading to the in-terior of the pump assembly. A filter disc 176 is posi-tioned in a port 178 connecting to passage 174.

The end housing 128 has axially extending split fingers 180 carrying spreading springs 182. See FIG. 3.
These fingers hold semi-circular permanent magnets which surround the armature outside an air gap and form the motor field.

The inlet end 120 of the pump at the left end of FIG. 3 has a cylindrical entrance collar 190. Viewed from the outer end, as in FIG. 5, this collar has an in-ternal bulge 192 toward the center. The bulge has an axial recess 194 splined on its inner surface and leads to a ~assage 196 ensmalled to form a valve seat for a ball valve 198 backed by a spring 200 retained by a press-fit button 202. Passage 196 communicates with a pump outlet passage 204 so that the ball valve may serve as a relief valve.

Inwardly of the collar 190, and rising from bulge 192, is a further bulge 206 integral with the end housing which has a central recess 210 to receive a pump rotor mount in the form of a stub shaft 220-. A
view of the inside of the inlet end 120 is found in FIG. 6. Outside the pin recess 210 is an arcuate inlet port 222 open, as shown in FIG. 3, to the interior of inlet collar 190. Two diametrically opposed threaded holes 224 are formed-on the inner face of housing 20 ~FIG. 6). On the opposite side of center from the ar-cuate inlet opening is an outlet port 230 (FIG. 6) con-nec-ted to previously referenced short passage 204.
Relief valve passage 196 described in connection with FIG. 3 shows also in FIG. 6. A shallow circular recess 234 surrounds pin shaft recess 210. Outlet port 230 has a short circumferential span as shown in FIG. 6 and this is positioned near the end of the compression area of the pump. Thus, any vapor in the pump will have been com-pressed into liquid state at this stage.

Cam ring 122, previously identified in FIGS.

3 and 4; has partial ring portions 124 which interfit with flux ring 126. This cam ring also has openings for headed retainer screws 240. These screw openings 242 are preferably laryer than the screws to allow diam-etrical adjustment of the cam ring relative -to the axis of the assembly. FIG. 4 shows cam ring 122. Triangular washer plates 244 underlie the heads of bolts 240 to ap-ply retention pressure on the cam ring and hold it secure-ly against the end housing 120. These plates also retainthe outer gear rotor during assembly.

The cam ring 122 has a large circular open-ing 250 which is positioned off center from the basic axis of rotation and this opening receives the outer gear rotor 252 of a year rotor pump. This par-ticular outer gear rotor has, as an example eleven tooth re-; cesses. The inner gear 254 of the gear rotor assembly is mounted on stub shaft 220 and has ten gear teeth formed thereon. The gear 254 has axial holes 255 spaced around the center shaft pin 220 to receive thefinger projections 144 on drive projection 142. Some small clearance isprovided between the finger projec-tions 144 and the holes 255 in rotor 254 to provide for slight misalignment.

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Pressed against the gear rotor assembly is a circular flat plate 260 preferably formed oE flexible material. This pla-te is most effective if it is flex-ible. A thickness range of .005 to .020", depending upon material used, has proved satisfactory. The material from whichthe plate 260 is formed is preferably thin metal and more particularly stainless steel, but some dense plastics or glass fiber fabrics may perform success-fully. A Teflon or similar friction reducing coating onthe plate significantly reduces friction. The circular plate is held firmly against and rotates with the rotor assembly, thereby forming a good seal and eliminating any ¦ axial clearance and at the same time causing very little friction. Behind this plate 260 is a multi-legged spider spring 262 (FIGS. 7 and 8) having five legs 264 bent, as shown in FIG. 8, in an axial direction from a center ring~
portion 263. The ends of the legs 264 are bent into a plane substantially parallel to the body portion 263 to form pressure pads 266. As shown in FIG. 3, the legs of ; the star or spider spring 262 interfit with the projec-tions 144 and are pressed against the plate 260 when the parts are brought into assembly. There is a slight clear-ance between the diameter of the stub shaft pin and the inside diameter of the plastic drive sleeve 142 to allow some angularity to exist between the armature shaft and stationary rotor pin to eevent binding if there is slight misalignment.

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A reinforcing plate 270 shown in FIG. 10 has a central hole 272 with spaced holes 274 to accommodate the projections 144. The periphery of plate 270 has ten radial fingers 276. This plate lies between disc 260 and the spider spring 262 so the fingers reinforce the edge of disc 260.

The shaft pin 220 is placed in recess 210 per-pendicular to the surface 137 of the end housing against which.the outer gear rotor 252 and the inner gear rotor 254 are pressed by the spider spring 262. Thus, in essence, there is a cantilever mount on shaft 220 for the inner gear rotor 254. The outer gear rotor 252 is supported by and rotatable in the cam ring 122.

The cylindrical drive projection 142, previously referenced as mounted on the armature assembly, has a central bore 145 which receives and is supported on the distal end of the stub shaft 220. There is some diam-etrical clearance between the bore 145 and the shaft 220 so that the drive projection 142 is rotatably piloted on the shaft but allows some play. This, coupled with the clearance between drive pins 144 and drive holes in rotor 254, compensate for any misalignment of the armature assembly relative to the stub shaft. As previously indi-cated, some clearance is provided between the drive fingers 144 and the holes 255 to allow for any slight misalignment.

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The seal plate 260, which may be made of a thin non-corrosive metal or a dense plastic, is sufficiently flex-ible that it will provide an ade~uate seal on the parts and this avoids the necessity for a very accurately machined and positioned housing plate at this side of the rotor. It also eliminates difficult tolerances on the cam ring 122 and gear rotors. The operating clear-ance needed between rigid parts is also eliminated and this reduces leakage and cost of manufacturing.

The seal plate 260 is illustrated in elevation in FIG. g. This plate has a central opening 261 to accommodate the shaft 220 surrounded by openings 270 to accommodate the finger projections 144.

IN OPERATION, fluid supply through collar 190 enters the inlet port 222 and moves into gear recesses between the inner and outer gear rotors 252 and 254.
As gear rotor parts 252 and 254 rotate, driven by the ¦ armature 140, the drive element 142, and fingers 144, liquid is placed under a pressure as the teeth of the rotor 254 move into the gear recesses of the gear rotor 252. Fluid, such as gasoline, is forced into the outlet ¦ ports 230 (FIGS. 3 and 6) and passes around the outer gear ¦ rotor;252 into the armature chamber and to the outlet hous-ing port 164.

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There is some outside clearance between carn ring 122 and shell 136 so the ring can be shifted rela-tive to the headed screws 240 before they are tightened.
There must be some clearance between the teeth of the inner rotor gear and those of the outer rotor gear at a point directly across from the area where the -teeth are in mesh. This clearance would normally be in a range of .0005 to .003. The clearance can be adjusted by movement of the cam ring which pilots the outer rotor gear. The object is to keep the teeth tip clearance to a minimum to prevent pressurized fluid from leaking across from the pressure side to the inlet side of the pumping unit. Once this is established, the screws 240 are tightened and the parts will maintain the proper relationship.

In this embodiment in FIGS. 3 to 10, the same function of noise reduction is accomplished by the flex-ible disc 260 as by the fingers 104, 106 and 108 in FIGS.
1 and 2. Should there be cavitation (vapor) in the pump at the outlet side, the flexible disc 260 would prevent outlet pressure from shooting back into the pump cavi-ties. When solid fuel is being pumped, the periphery of disc 260 flexes -to egress the fuel to the outlet ports.
However, the disc 260 forms a barrier, as do the reed valves;of FIGS. 1 and 2, preventing the outlet pressure from reaching pump chambers which may contain vapor rather than solid fuel. Thus, there is a significant reduction in noise as the pump operates particularly in warm weather.

'7~1 If desired, a flexing disc 2~0 could be utilized on the gear rotor pump assembly of FIG. 3 on the other side of the inner and outer gear rotors, but this disc would not rotate with the rotors. In this case, the recessed area 230 would be extended as shown in dotted lines in FIG. 6.

Thus, in each of the embodiments shown in FIGS.l and 3, a pump rotor combination operates with expanding and ensmalling pumping chambers. In each, there is a circumferential inlet area and a circumferen-tial outlet area spaced circumferentially from each other.
The ensmalling chambers in the outlet area are blocked on onel side of the rotor combination, and, at the other side of the rotor, are closed by biased means which will flex to allow liquid egress in the outlet area. This biased means prevents backflow of the outlet pressure into a pumping chamber which may be vapor filled rather than liquid filled. This has been found to significantly reduce the noise of an operating pump. Since, when these pumps are used for fuel in a passenger vehicle, they are frequently mounted within a fuel tank, the noise factor is important to the comfort of passengers. In areas where the ambient heat is high, the vaporization of vola-tile fuel will cause what is termed as "cavitation" in the pump. Te present invention is directed to minimi~-- ing th;e noise normally caused by cavitation.

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As described above in the description of FIGS. 3 to 10, a flexible disc may also be used on the side of ~he gear and rotor assembly opposite to that on which the flexible disc 260 is located in FIG. 3. This is illustrated in FIG. 11 where like parts carry the same reference characters as those in FIG. 3.

In FIG. 11, the entrance collar 290 has an axial fuel entry passage 292 which, as in FIG. 3, has a bulge 192 with a relief passage 194 opening to passage 196 communicating with a pump outlet passage 296. A check valve ball 198 seats at the juncture of passages 194 and 196 backed by a spring 200 held in by a press-fit retainer 202. Centrally of the collar 290 is a bore 210 mounting a stub shaft 220 which carries the gear rotor assembly 252, 254.

Between the inlet collar 290 and the cam ring 122 i5 a thin flexible plate 300 shown in elevation in FIG. 12 and in an edge view in FIG. 13. This plate is preferably of the same material as described in connection with flexible plate 260.
The plate has a friction reducing function and is preferably formed with a Teflon coating to accomplish this~ It has other functions which will be described. Plate 300 has two diametrically opposed holes 302 to accommodate retaining bolts and an edge notch 304 to register with an outlet passage 204 in the collar 290. A relatively long arcuate inlet port 310 is disposed outside the center of the plate 300 ensmalling slightly from one end 312 to the other end 314. This port lies radially in the intake area of the gear rotor assembly 252-254. Opposed to the port 310 is a circumferentially short outlet port 316.

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Yiewing the inlet collar 290 from the outer end, as shown in FIG~ 15, an arcuate inlet port 320 is shown which will register with the port 310 of plate 300 and also with the intake area of the gear rotor assembly. The collar 290 has an arcuate recess 322 leading to port 320 radially about twice the dimension of port 320 and which extends circumferentially from one end of port 320 substantially past the other end of port 320 so that it is almost twice as long as ports 310 and 320.

Viewing the inlet collar from the inner pump end in FIG. 14, the arcuate inlet port 320 again appears. Spaced from the smaller end of the inlet port is the outlet port 296 extending radially outward through passage 204 to reach the armature chamber where pump outlet flow ultimately reaches the pump outlet passage 164.

Embossed in the pump face surface of the collar 290 and lying flat against the plate 300 is a shallow recess which has a circumferential boundary 330 terminating at a radial line 332 which joins a central circular line 334 which in turn ; terminates at port 196 and passage 296.

IN THE OPRRATIO~, the flexible plate 260 in the operating pump rotates with the pump rotors in a sealing relationship. However r on the pressure side of the pumping elements opposite the inlet po~t 310l as the pressure develops within the pumping elemen-ts 252, 254, the fuel will force the flexible plate 260 away from the outer rotor 252 and enter into ~2~
the motor armature chamber. Port 316 relieves the pressure within the pumping elements near the end of the pressure zone thereby allowing the flexible plate to reseat against the rotating elements and thus prevent the fuel in the motor chamber from reaching the inlet area of port 310.

It will be understood that pressure in the armature chamber against the seal plate 260 in the outlet zone area will balance the pressure on both sides of the rotating seal ~60 to allow the seal to seat against the rotors. The back-up element 270 urges the seal toward the rotors.

The plate 260 also has another ~unction in that, if vapor appears in the pressure side of the pump (cavitation), the pressure in the armature chamber will force the flexing plate back to the rotors and prevent fuel backflow into the pumping chambers. In this manner, it acts as a one-way valve and thus eliminates the noise that otherwise would occur during cavitation.

The fact that the seal plate 260 rotates with the pumping rotors reduces the friction. The plate actually rotates with the inner rotor and only the differential action of the outer rotor is occurring between the outer rotor and the seal plate. This reduces the power needed in the motor and is significant because of the limited dimensions in the rather small pumping element. The power is thus better utilized in the actual pumping of the fuel.

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The above arrangement allows the circumferential lengthening o~ inlet ports 3]0 and 320 back to the end 312. This is due to the fact that there is a relatively short normally open exhaust port spaced well away from end 312 of the inlet port. Thus, there is no cross-flow between the inlet port and the outlet port. This lengthening of port 310 is very desirable in that it allows the intake function to continue for a longer time duration, thereby reducing cavitation tendencies in the pump.

10The function of the wear and seal plate 300 described above can complement the function of the plate 260. This plate 300 is thin and flexible and will move in response to Euel pressure in the outlet area of the pump rotors. To describe this function, reference is first made to the shallow embossed 15area shown in FIG. 14 defined by lines 330, 332 and 334 and the encompassed area 196 and 296. This area is shown in dotted lines in FIG. 12.

During the operation of the pump, fuel pressure in the arcuate pressure zone of the pumping elements will act against the flexible plate 300 to move it away from the pumping elements in the dotted area shown in FIG. 122. This flexing can take place because of the shallow recess bounded by 330, 332, 344, 196, 296, etc. in the face plate of the collar 290 and may be very slight in range of a few thousandths.

This flexing allows fuel under pressure to reach the normal outlet port 316 in plate 300. This supplements the action of plate 260 because the fuel flowing to the outlet past plate 300 decreases the amount of flexing required by the plate 260. Thus, the two plates 260 and 300 complement each other in providing outlet flow from the arcuate pressure zone of the pump and, at the same time, act as one way valving for this zone, thus minimizing the backflow in the event of cavitation and serving substantially to reduce the noise of the pump in a passenger vehicle.

Claims

THE EMBODIMENTS OF THE INVENTION IN WHICH AN
EXCLUSIVE PROPERTY OR PRIVILEGE IS CLAIMED AS DEFINED AS FOLLOWS:

1.
In a rotary pump for pumping a volatile liquid, (a) a rotor combination utilizing circumferentially disposed expanding and ensmalling, positive-displacement pumping chambers, (b) a first circumferential reduced pressure inlet area on said rotor combination, (c) a second circumferential increased pressure outlet area on said rotor combination spaced circumferentially from said first area, (d) a first means on one side of said rotor combination comprising an inlet housing having an inlet opening at one portion and a face plate at another portion, said face plate lying directly adjacent one side of said rotor combination, said face plate having a passage and connected ports communicating with said inlet opening and with said first circumferential reduced pressure inlet area of said rotor combination, said face plate having also an outlet port at the trailing end of said second circumferential increased pressure outlet area and having a shallow recess open at one side to said outlet port and axially overlying substantially all of said increased pressure area, (e) outlet housing means forming an outlet chamber on the side of said rotors opposite said inlet housing and in communication with said outlet port of said inlet housing, (f) second means closing said pumping chambers on the other side of said rotor combination, (g) power means to rotate said rotors, and (h) a thin flexible resilient plate member interposed between said one side of said rotor combination and said face plate of said inlet housing having a first aperture to register with said inlet opening and said first circumferential inlet area and second aperture in substantial registry with said outlet port in said inlet housing and a closed portion overlying said shallow recess, whereby liquid pressure developing in pumping chambers in said second circumferential area will move the portion of said resilient plate overlying said shallow recess into said recess away from said rotors to allow fluid under pressure to reach said outlet port while preventing backflow of liquid under pressure from said outlet port to the upstream portion or said second circumferential area, (i) said second means closing said pumping chambers on the other side of said rotor combination comprising a flexible, resilient sealing disc having one surface lying directly against said rotors and the opposite surface exposed to pressure in said outlet housing and having a flexible peripheral margin terminating radially outwardly of said pumping chambers, said margin being free to move away from said rotors against pressure in said outlet housing in response to higher pressure in said second circumferential area but acting also to prevent backflow of liquid under pressure from said outlet housing.