Rotary fluid mover

Information

  • Patent Grant
  • 6241498
  • Patent Number
    6,241,498
  • Date Filed
    Tuesday, February 15, 2000
    24 years ago
  • Date Issued
    Tuesday, June 5, 2001
    23 years ago
Abstract
A pump for moving a fluid has a housing with a internal chamber accommodating a pair of rotating pistons. Each piston has protrusions that register with pockets in the other piston in non-contact relation as the pistons rotate. A fluid accumulator in fluid communication with the pump holds a supply of fluid to prevent excessive pressure rise.
Description




FIELD OF THE INVENTION




The invention relates to fluid pumps, such as blowers and superchargers for internal combustion engines, and other processes requiring large volumes of fluid at relatively low pressure.




BACKGROUND OF THE INVENTION




In an internal combustion engine a boost in horsepower can be accomplished by forcing a more dense air/fuel charge into the cylinders with a supercharger. A supercharger can provide a dependable and affordable method of increasing horsepower and torque. A supercharger forces a more dense air/fuel mixture into an internal combustion engine's cylinders than the engine can draw in under normal conditions. This higher-energy mixture produces more power. Supercharging increases the engine's volumetric flow without increasing its displacement. Therefore, a supercharged small engine can produce the horsepower and torque of a relatively larger engine.




There are two basic blower systems used to force an air/fuel mixture into an internal combustion engine. These blowers are either a dynamic or a positive displacement equipment. Turbocharging, which is a dynamic process, places a turbine wheel in the exhaust flow of the engine. The turbine blades are directly connected to a centrifugal blower. One major disadvantage of a turbocharger is “turbo-lag.” This is the delay that occurs after calling for power with the throttle before the rotational speed of the system spools up to deliver that power. An improperly sized or designed turbo system can rapidly over-boost and damage a spark-ignited internal combustion engine. The sizing of the turbocharger to the engine and the matching of the turbine size and design to impeller size and design are very critical. Additionally, the exhaust turbine tends to cool the exhaust gases thereby delaying the catalyst light-off of modern automotive emissions systems.




Centrifugal impeller the supercharging is a system having an impeller rotated with a drive belt from the crankshaft. A speed-increaser, either geared or gearless, is required to multiply the speed of the impeller relative to that of the input shaft. The delivery of a centrifugal impeller device varies dramatically with its rotational speed, and is prone to under-boost at low speed and over-boost at high speed. An example of a centrifugal impeller supercharger is disclosed by M. Shirai in U.S. Pat. No. 5,158,427.




The most common positive displacement system is the “Roots blower”. In this system, a belt-driven shaft drives two close-clearance rotors which are geared together. Each full rotation sweeps out a specific fixed volume, unlike the fan-like characteristics of a turbine device.




SUMMARY OF THE INVENTION




The invention is a fluid pump used as a supercharger to provide an air/fuel mixture to an internal combustion engine in an efficient and reliable manner for sharply increasing the torque and corresponding horsepower of the engine across its entire operating speed range. The supercharger has simple geometric shaped structures which are easy to fabricate at a relatively low cost. The supercharger employs a pair of cooperating rotors that do not have complex curved surfaces which require relatively costly NC profile milling or dedicated machine tool operations. Conventional materials such as aluminum, cast iron or plastics and established fabrication procedures are used to manufacture the supercharger.




The supercharger rotors have clearances relative to their cooperating or mating surfaces and housing surfaces that accommodate deflection. The cylindrical shapes of the rotors and inside surfaces of the housing allow for predictable and repeatable clearances between noncontacting mating parts. This reduces leakage which improves efficiency while maintaining low cost manufacturing procedures. The cylindrical shapes of the supercharger rotors and associated surfaces are inherently rigid and not prone to flexing and twisting when subjected to pressures and inertial loads.




The supercharger has a housing with two generally cylindrical chambers open to each other and fluid inlet and outlet ports. A rotor assembly located in the chambers operates to draw fluid, such as an air/fuel mixture, into the chambers and discharge the fluid out the outlet port and into the intake of an internal combustion engine. The rotor assembly has a pair of rotors mounted on shafts rotatably supported on the housing. Each rotor has semi-cylindrical pockets and semi-cylindrical protrusions that cooperate with the pockets of the adjacent rotor to move fluid through the supercharger when the rotors are rotated. The protrusions on each rotor do not contact the inside cylindrical surfaces of the housing. Also, the protrusions on each rotor do not contact the cooperating rotor as they move into and out of the mating pockets. This allows for both high speed and oil free operation. Furthermore, the protrusions can be integral portions of the rotor or may alternatively be separately manufactured pieces that can then be assembled to the rotor body. The protrusions are located in the semi-cylindrical pockets of the adjacent rotor generally half of the time during rotation of the rotors. Therefore, the pressure fluctuations and associated noise and heat are reduced. There is minimal trapped volume of fluid in the pockets. This reduces one of the common sources of noise, heat, and vibrations among prior devices. Additionally, the fluid inlet has two passages. This improves volumetric efficiency and reduces churning of the fluid and heating of the inlet region of the rotor.




To maximize performance in one or two cylinder engines, an accumulator is situated between the supercharger and the engine inlet. The accumulator moderates the pressure variations in the intermediate manifold when the engine cylinder is not in the intake phase. In the case where a liquid fuel is introduced up stream of the accumulator site, the accumulator employs a generally conic shape to avoid collection or pooling of liquid fuel in the accumulator chamber. When the engine equipped with the supercharger and accumulator is used to power a vehicle, such as a go-kart, the cone shaped accumulator allows vehicle acceleration and high speed cornering without fuel pooling in the accumulator. A preferred location for the accumulator is adjacent to and slightly above the engine inlet port. The supercharger may be employed in multi-cylinder engines of three cylinders or greater without the need for the accumulator.











DESCRIPTION OF THE DRAWING





FIG. 1

is a perspective view of a single cylinder internal combustion engine combined with a supercharger and accumulator of the invention;





FIG. 2

is a diagrammatic view of the engine, supercharger and accumulator of

FIG. 1

;





FIG. 3

is an enlarged top plan view of the supercharger of

FIG. 1

;





FIG. 4

is a sectional view taken along line


4





4


of

FIG. 3

;





FIG. 5

is a sectional view taken along line


5





5


of

FIG. 3

;





FIG. 6

is a sectional view taken along line


6





6


of

FIG. 3

;





FIG. 7

is an enlarged foreshortened plan view of a protrusion mounted on a rotor of the supercharger;





FIG. 8

is a sectional view taken along line


8





8


of

FIG. 7

;





FIG. 9

is an enlarged sectional view taken along line


9





9


of

FIG. 2

;





FIG. 10

is a sectional view taken along line


10





10


of

FIG. 9

;





FIG. 11

is a perspective view of the air/fuel accumulator;





FIG. 12

is a side elevational view of the accumulator of

FIG. 11

;





FIG. 13

is a top plan view of the accumulator of

FIG. 11

;





FIG. 14

is a bottom plan view of the accumulator of

FIG. 11

;





FIG. 15

is a diagrammatic view of an internal combustion engine operatively connected to a modification of the supercharger and accumulator of the invention;





FIG. 16

is a perspective view of the supercharger of

FIG. 15

;





FIG. 17

is a top plan view of the supercharger of

FIG. 16

;





FIG. 18

is an end elevational view of the drive end of the supercharger of

FIG. 16

;





FIG. 19

is an end elevational view of the left end of the supercharger of

FIG. 16

;





FIG. 20

is a front elevational view of the supercharger of

FIG. 16

;





FIG. 21

is a rear elevational view of the supercharger of

FIG. 16

;





FIG. 22

is a bottom plan view of the supercharger of

FIG. 16

;





FIG. 23

is an enlarged sectional view taken along the line


23





23


of

FIG. 17

;





FIG. 24

is an enlarged sectional view taken along the line


24





24


of

FIG. 17

; and





FIG. 25

is an enlarged sectional view taken along the line


25





25


of FIG.


17


.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




The supercharging system of the invention is used with an internal combustion engine


20


to increase the engine's volumetric efficiency and output horsepower. As shown in

FIGS. 1 and 2

, engine


20


has a crank case


21


rotatably supporting a power output shaft


22


. A head


23


mounted on top of case


21


is attached to a fuel intake pipe or manifold


24


and an exhaust pipe


26


. Engine


20


is a single cylinder four cycle conventional air cooled internal combustion engine. An example of engine


20


is a five horsepower, single cylinder, four cycle internal combustion engine. Other types of internal combustion engines including two cylinder models are adaptable to the supercharging pump and accumulator system of the invention. Additionally, the pump may be used without the accumulator on engines of three or more cylinders.




Engine


20


is supplied with an air/fuel mixture with a supercharger or fluid pump


27


. Supercharger


27


has a housing


28


rotatably supporting a drive shaft


29


. A power transmission comprising a first sprocket


31


on shaft


29


, a second sprocket


32


on shaft


22


, and an endless roller link chain


33


coupling sprockets


31


and


32


provides a direct drive between engine


20


and supercharger


27


. Sprockets


31


and


32


have a diameter whereby the RPM of engine


20


is the substantially the same as the operating speed of supercharger


27


. Sprockets


31


and


32


can have a sprocket ratio to provide desired air flow to a specific engine size. Supercharger


27


is a positive displacement fluid pump operable to deliver a supply of air/fuel mixture to engine


20


to increase its adiabatic efficiency and horsepower. The air/fuel mixture flows through a pipe or tubular member


34


connected to supercharger


27


and intake pipe


24


of engine


20


.




An air/fuel mixing device


36


, known as a carburetor, mounted on housing


28


operates to introduce fuel, such as gasoline and alcohol, into air flowing through device


36


to provide an air/fuel mixture for engine


20


. A fuel line


37


connected to device


36


carries liquid fuel from a tank (not shown) to device


36


.




An air/fuel mixture accumulator


38


is in fluid communication with pipe


34


to hold a supply of an air/fuel mixture between the engine intake strokes without excessive pressure rise. For example, for a single cylinder engine the volume of accumulator


38


is about twelve times the engine displacement. As shown in

FIGS. 1

,


9


and


11


, accumulator


38


has a funnel or cone shape which allows a vehicle driven with engine


20


to accelerate and corner without pooling of fuel in accumulator


38


. Further, it must be emphasized that supercharger


27


may be employed in multi-cylinder engines of three cylinders or greater without the need for accumulator


38


.




Supercharger housing


28


, shown in

FIGS. 3 and 4

, has a central body


39


located between end members


41


and


42


. A first cover plate


43


is located adjacent to the outside of end member


41


. A plurality of bolts


46


attach end member


41


and cover plate


43


to body


39


. A second cover plate


44


closes the outside of end member


42


. A plurality of bolts


47


secure end member


42


and cover plate


44


to body


39


. An annular boss


48


secured to body


39


with bolts


49


has a passage


51


open to a pair of passages


52


and


53


in body


39


to carry the air/fuel mixture from device


36


to the interior of body


39


.




Body


39


has a first arcuate inside wall


54


surrounding a first chamber


56


and a second arcuate inside wall


57


surrounding chamber


58


. Passage


52


is open to chamber


56


to allow the air/fuel mixture to flow in a tangential direction into chamber


56


. Passage


53


is open to chamber


58


so that the air/fuel mixture flows in a tangential direction into chamber


58


. Walls


54


and


57


have cylindrical surfaces which are machined with conventional machine tools. Body


39


has a central portion


59


separating passages


52


and


53


. Opposite portion


59


is an air/fuel discharge port


60


for carrying the air/fuel mixture from chambers


56


and


58


to pipe


34


leading to engine intake and accumulator


38


.




As shown in

FIG. 5

, a first rotor or rotating piston


61


mounted on shaft


29


is located in chamber


58


. Rotor


61


has a pair of pockets or recesses


62


and


63


open to its cylindrical outer surface


64


. Body surface


57


is concentric with rotor external surface


64


. Surface


64


concentric with shaft


29


comprise segments of a cylinder pitch circle. Pockets


62


and


63


have semi-circular cross sections and semi-cylindrical surfaces. Pockets


62


and


63


are on opposite sides of rotor


61


and ninety degrees or normal to key slots


66


and


67


in opposite portions of rotor


61


. A first protrusion


68


extended into key slot


66


is wedged into a tight-fit relationship with rotor


61


. A second protrusion


69


is anchored in key slot


67


. The outer apex portions of protrusions


68


and


69


are located in close non-contacting relationship with body surface


57


. The details of the anchor structure to retain protrusions


68


and


69


on rotor


61


are shown in FIG.


8


.




A second rotor or rotary piston


73


is mounted on a shaft


74


. Opposite ends of shaft


74


are rotatably mounted on end members


41


and


42


with bearings


76


and


77


. A sleeve


78


secured to shaft


74


with a bolt


79


supports shaft


74


on bearing


76


. A second sleeve


81


surrounding the opposite end of shaft


74


is keyed to rotor body


82


with a tongue and groove coupling


83


. Sleeve


81


extends through bearing


77


whereby bearing


77


supports shaft


74


on end member


42


.




Shaft


29


extends through sleeves


84


and


86


located adjacent opposite ends of body


61


. Sleeve


84


extends through bearing


71


to support shaft


29


on end member


41


. Sleeve


86


extends through bearing


72


to support shaft


29


on end member


42


. A tongue and groove connection


87


drivably joins sleeve


86


to body


61


so that body


61


rotates with shaft


29


.




Returning to

FIG. 5

, rotor body


82


has a pair of semi-cylindrical pockets


88


and


89


open to the outer cylindrical surface


91


. Surface


91


is concentric with body surface


59


. Surface


91


concentric with shaft


29


comprise segments of a cylinder pitch circle. The adjacent portions of surfaces


64


and


91


move in contiguous relationship as there is a small clearance between the adjacent surfaces. An example of this clearance is 0.005 to 0.007 inch. The rotor-to-rotor clearance reduces noise, wear of the rotors, and reduces heat generation. Pockets


88


and


89


are on opposite portions of body


82


and ninety degrees from key slots


92


and


93


. Protrusions


94


and


96


are anchored in slots


92


and


93


. The outer apex portions of protrusions


94


and


96


are in close non-contacting relation with body surfaces


54


. Other insert-type protrusion attachment shapes may be used with the supercharging system of the invention. Alternatively, protrusions


94


and


96


can be integral portions of a monolithic rotor body. The number and locations of pockets and protrusions can vary to maintain dynamic balance of rotors


61


and


73


.




As shown in

FIGS. 7 and 8

, body


82


has a longitudinal recess


97


and outwardly directed lips


98


and


99


at opposite sides of recess


97


. The bottom of recess


97


is formed of flat surfaces of body projections or members


101


and


102


. Projections


101


and


102


are spaced from each other providing a longitudinal opening


103


to slot


93


and recess


97


. Protrusion


96


has a generally semi-cylindrical body


104


joined to neck


106


connected to a head


107


. Body


104


has a semicylindrical outer surface


108


and a flat inside surface or base


109


. Surface


108


has a radius smaller than the radius of pocket


62


to minimize trapping of air between protrusion


96


and rotor pocket


62


. Opposite portions of surface


108


are located against lips


98


and


99


with inside surface


109


bearing against adjacent projection surfaces. Neck


106


extends through opening


103


locating head


107


in recess


93


. Head


107


extends adjacent the tapered inside faces of projections


101


and


102


. Protrusion


96


has a cylindrical hole


111


in body


104


, a cylindrical hole


112


in head


107


and a slot


113


in neck


106


connecting holes


111


and


112


. A pin


114


located in hole


112


expands neck


106


and head


107


to firmly retain protrusion


96


on projections


101


and


102


. Lips


98


and


99


prevent circumferential movements of protrusion


96


on body


82


. Projections


101


and


102


prevent rocking of protrusion


96


on body


82


. Protrusion


96


is an extruded metal part which is assembled longitudinally into recess


97


, opening


103


, and slot


93


. Protrusion


96


can also be an integral portion of rotor body


82


. Pin


114


is moved into hole


112


to retain protrusion


96


in a fixed position on rotor body


82


. Protrusions


68


,


69


and


94


are retained on rotors


61


and


73


in the same manner as shown in FIG.


8


.




As shown in

FIGS. 4 and 6

, shafts


29


and


74


are drivably connected with spur gears


116


and


117


located within end cover


44


. Gear


116


is fixed to shaft


29


with a key


118


and bolt


119


. Gear


116


is located between thrust bearing washers


141


and


142


. Washer


141


fits around an annular head


143


accommodating the head of bolt


119


. Washer


142


surrounds sleeve


86


. Washers


141


and


142


engage opposite sides of gear


116


. An annular spring


144


, such as a wavetype spring, located in a shallow recess in cover plate


44


engages washer


141


and biases the thrust bearing washers axially to retain washer


142


against end member


42


. This locates the axial positions of the gear


116


and rotor


61


. As shown in

FIG. 4

, the flat ends of rotor


61


are spaced a small distance from adjacent inside surfaces of end members


41


and


42


. The small clearance between rotor


61


and end members


41


and


42


reduces wear, friction and heat generation during rotation of rotor


61


. A bolt


121


threaded into an end of shaft


74


secures gear


117


to shaft


74


. A key


120


interconnects gear


117


with shaft


74


whereby gear


117


rotates shaft


74


and rotor


73


. Bolt


121


retains gear


117


between thrust bearing washers


146


and


147


. Washer


146


fits on a head


148


accommodating bolt


121


. Washer


147


surrounds sleeve


81


. A spring


149


, such as an annular wave-like spring, located in a recess in cover plate


44


biases washer


146


to retain washer


147


against end member


42


to maintain the axial location of shaft


74


, gear


117


and rotor


73


. Rotor


73


has flat ends spaced a small distance from adjacent surfaces of end plates


41


and


42


. The small clearance, seen in

FIG. 4

, between rotor body


82


and inside surfaces of end plates


41


and


42


reduces wear, friction and heat generation during rotation of rotor


73


. Gears


116


and


117


have the same pitch diameters whereby shafts


29


and


74


rotate at the same speed. The pitch diameters of gears


116


and


117


are the same as the diameters of rotors


61


and


73


. Rotors


61


and


73


turn in opposite directions at the same speed so that protrusions


68


and


69


register with pockets


88


and


89


in non-contact relation and protrusions


94


and


96


register with pockets


62


and


63


in non-contact relation during concurrent rotation of rotors


61


and


73


. This reduces wear of the protrusions and rotor pockets and minimizes noise.




As shown in

FIG. 4

, cover plate


43


closes the open side of end member


41


and bearings


71


and


76


. A flat disk


122


located between cover plate


43


and end member


41


is mounted on shaft


29


. Disk


122


on rotation of shaft


29


moves a lubricant, such as oil, upward to lubricate bearings


71


and


76


.




As shown in

FIGS. 9 and 10

, a T-connector


123


is mounted on intake pipe


24


. Hose


34


is joined to the side of connector


123


to direct the air/fuel mixture into a passage


124


of connector


123


. The air/fuel mixture only flows into the combustion chamber of the engine on the intake cycle. The air/fuel mixture flows into the accumulator


38


during the remaining cycle of the engine. Accumulator


38


has a cone or funnel shaped side wall


126


and a dome top wall


129


surrounding a chamber


128


. As seen in

FIG. 9

, side wall


126


extends downwardly from the outer edge of dome


129


at an angle of


40


degrees from the vertical axis of accumulator


38


. Accumulator


38


moderates the pressure variations in the air/fuel intake manifold or passage to engine


20


. The cone shape of wall


126


avoids collection or pooling of liquid fuel in accumulator chamber


128


as the fuel flows down wall


126


to passage


133


. The ratio of air/fuel mixture is maintained as liquid fuel is not collected in accumulator chamber


128


. Side wall


126


is joined to a downwardly directed neck or cylindrical end


129


. A clamp


131


secures end


129


to a sleeve


132


having a passage


133


open to passage


124


and chambers


128


. Screen


134


extends across passage


133


to reduce burning of the air/fuel mixture in chamber


128


in the event that the engine backfires.




Excessive pressure in passage


124


and chamber


128


is relieved with a check valve comprising a ball


136


biased with a spring


137


against an annular shoulder


138


. When ball


136


is moved away from shoulder


138


, the air/fuel mixture flows to atmosphere through a side port


139


in connector


123


or is piped back to the inlet of supercharger


27


. Other types of pressure relief valves can be used to vent excessive pressure of the air/fuel mixture in accumulator chamber


128


.




A modification of the supercharging system of the invention, shown in

FIGS. 15

to


25


, is used with an internal combustion engine


220


to increase the engine's volumetric efficiency and output horsepower. As shown in

FIG. 15

, engine


220


has a crank case


221


rotatably supporting a power output shaft


222


. A fuel intake pipe or manifold


224


directs an air/fuel mixture to engine


220


. An exhaust pipe


226


carries exhaust gas away from engine


220


. Engine


220


is a single cylinder four cycle conventional air cooled internal combustion engine. An example of engine


220


is a five horsepower, single cylinder, four cycle internal combustion engine. Other types of internal combustion engines including two cylinder models are adaptable to the supercharging pump and accumulator system of the invention. Additionally, the pump may be used without the accumulator on engines of three or more cylinders.




Engine


220


is supplied with an air/fuel mixture with a supercharger or fluid pump


227


. Supercharger


227


has a housing


228


rotatably supporting a drive shaft


229


. A power transmission comprising a first sprocket


231


on shaft


229


, a second sprocket


232


on shaft


222


, and an endless roller link chain


233


coupling sprockets


231


and


232


provides a direct drive between engine


220


and supercharger


227


. Sprockets


231


and


232


have the same diameters whereby the RPM of engine


220


is the substantially the same as the operating speed of supercharger


227


. Sprockets


231


and


232


can have a sprocket ratio to provide desired air flow to a specific engine size. Supercharger


227


is a positive displacement fluid pump operable to deliver a supply of air/fuel mixture to engine


220


to increase its adiabatic efficiency and horsepower. The air/fuel mixture flows through a pipe or tubular member


234


connected to supercharger


227


and intake pipe


224


of engine


220


.




An air/fuel mixing device


236


, known as a carburetor, mounted on housing


228


operates to introduce fuel, such as gasoline and alcohol, into air flowing through device


236


to provide an air/fuel mixture for engine


220


. A fuel line


237


connected to device


236


carries liquid fuel from tank


235


to device


236


.




An air/fuel mixture accumulator


238


is in fluid communication with pipe


234


to hold a supply of an air/fuel mixture between the engine intake strokes without excessive pressure rise. For example, for a single cylinder engine the volume of accumulator


238


is about twelve times the engine displacement. Accumulator


238


has a funnel or cone shape which allows a vehicle driven with engine


220


to accelerate and corner without pooling of fuel in accumulator


238


. Accumulator


238


has the same structure as accumulator


38


shown in FIG.


9


. The accumulator


238


is mounted on a check valve assembly, as shown in

FIGS. 9 and 10

, which directs the air/fuel mixture to the intake port of engine


220


. Supercharger


227


may be employed in multi-cylinder engines of three cylinders or greater without the need for accumulator


238


.




Supercharger housing


228


, shown in

FIGS. 16

to


22


, has a central body


239


located between end members


241


and


242


. A first cover plate


243


is located adjacent to the outside of end member


241


. A plurality of bolts


246


attach end member


241


and cover plate


243


to body


239


. A second cover plate


244


closes the outside of end member


242


. A plurality of bolts


247


secure end member


242


and cover plate


244


to body


239


. As shown in

FIGS. 18

,


19


and


22


, end member


243


has a pair of downwardly directed legs


249


. End members


244


has a pair of downwardly directed legs


250


laterally aligned with legs


249


. Each leg


249


,


250


has a threaded bottom hole for accommodating a bolt to secure housing


228


to a fixed support. Body


239


has a side passage


251


open to a pair of passages


252


and


253


to carry the air/fuel mixture from device


236


to the interior chamber of body


239


.




Body


239


has a first arcuate inside wall


254


surrounding a first chamber


256


and a second arcuate inside wall


257


surrounding chamber


258


. Passage


252


is open to chamber


256


to allow the air/fuel mixture to flow in a tangential direction into chamber


256


. Passage


253


is open to chamber


258


so that the air/fuel mixture flows in a tangential direction into chamber


258


. Walls


254


and


257


have cylindrical surfaces which are machined with conventional machine tools. Body


239


has a central portion


259


separating passages


252


and


253


. Opposite portion


259


is an air/fuel discharge port


260


for carrying the air/fuel mixture from chambers


256


and


258


to pipe


234


leading to engine intake and accumulator


238


.




As shown in

FIG. 24

, a first rotor or rotating piston


261


mounted on shaft


229


is located in chamber


258


. Rotor


261


has a pair of semi cylindrical pockets or recesses


262


and


263


open to its cylindrical outer surface


264


. Body outer surface


257


is concentric with arcuate rotor surface


264


. Surface


264


concentric with shaft


229


comprise segments of a cylinder pitch circle. Pockets


262


and


263


have semi-circular cross sections and semi-cylindrical surfaces. Pockets


262


and


263


are located in opposite sides of rotor


261


. Rotor


261


has a pair of protrusions


268


and


269


. The number and locations of pockets and protrusions can vary to maintain dynamic balance of rotor


261


. Each protrusion


268


,


269


has a generally semi-cylindrical shape located


90


degrees or normal to pockets


262


and


263


. Protrusions


268


and


269


project outwardly in opposite directions from surface


264


to dynamically balance rotor


261


. The outer apex portions of protrusions


268


and


269


are located in close non-contacting relationship with body surface


257


. There is a small space between protrusions


268


and


269


and surface


257


to prevent wear and friction between adjacent surfaces of the protrusions and body


239


and generation of heat and noise.




A second rotor or rotary piston


273


is mounted on a shaft


274


. Opposite ends of shaft


274


are rotatably mounted on end members


241


and


242


with bearings


276


and


277


, as seen in

FIG. 23. A

sleeve


278


secured to shaft


274


with a bolt


279


supports shaft


274


on bearing


276


. A second sleeve


281


surrounding the opposite end of shaft


274


is keyed to rotor body


282


with a tongue and groove coupling


283


. Sleeve


281


extends through bearing


277


whereby bearing


277


supports shaft


274


on end member


241


.




Shaft


229


extends through sleeves


284


and


286


located adjacent opposite ends of body


261


. Sleeve


284


extends through bearing


271


to support shaft


229


on end member


242


. Sleeve


286


extends through bearing


272


to support shaft


229


on end member


241


. A tongue and groove connection


287


drivably joins sleeve


286


to body


261


so that body


261


rotates with shaft


229


.




Returning to

FIG. 24

, rotor body


282


has a pair of semi-cylindrical pockets


288


and


289


open to the outer cylindrical surface


291


. Surface


291


is concentric with body surface


259


. Surface


291


concentric with shaft


229


comprise segments of a cylinder pitch circle. The adjacent portions of surfaces


264


and


291


move in contiguous relationship as there is a small clearance between the adjacent surfaces. An example of this clearance is 0.005 to 0.007 inch. The rotor-to-rotor clearance reduces noise, wear of the rotors, and reduces heat generation. Pockets


288


and


289


are on opposite portions of body


282


and ninety degrees from a pair of protrusions


294


and


296


. Each protrusion


294


,


296


has a semi-cylindrical outer surface having the shape and configuration of pockets


262


and


263


of rotor


261


. The outer apex portions of protrusions


294


and


296


are in close non-contacting relation with body surfaces


254


. Protrusions


294


and


296


are integral portions of the monolithic rotor body


282


. The rotors


261


and


273


and their protrusions


268


,


269


,


294


and


296


are one-piece structures. Rotors


261


and


273


are identical in size and shape. They can be made by an extrusion process and externally broached or shaved to finished size. Profile milling procedures can also be used to make the one-piece rotors


261


and


273


. Large rotors can be hollow to reduce weight.




As shown in

FIGS. 23 and 25

, shafts


229


and


274


are drivably connected with spur gears


316


and


317


located within end cover


243


. Gear


316


is fixed to shaft


229


with a key


318


and bolt


319


. Gear


316


is located between thrust bearing washers


341


and


342


. Washer


341


fits around an annular head


343


accommodating the head of bolt


219


. Washer


342


surrounds sleeve


286


. Washers


341


and


342


engage opposite sides of gear


316


. An annular spring


344


, such as a wave-type spring, located in a shallow recess in cover plate


243


engages washer


341


and biases the thrust bearing washers axially to retain washer


342


against end member


242


. This locates the axial positions of the gear


316


and rotor


261


. As shown in

FIG. 23

, the flat ends of rotor


261


are spaced a small distance from adjacent inside surfaces of end members


241


and


242


. The small clearance between rotor


261


and end members


241


and


242


reduces wear, friction and heat generation during rotation of rotor


261


. A bolt


321


secures gear


317


to shaft


274


. A key


320


interconnects gear


317


with shaft


274


whereby gear


317


rotates shaft


274


and rotor


273


. Bolt


321


retains gear


317


between thrust bearing washers


346


and


347


. Washer


346


fits on a head


348


accommodating bolt


321


. Washer


347


surrounds sleeve


281


. A spring


349


, such as an annular wave-like spring, located in a recess in cover plate


243


biases washer


346


to retain washer


347


against end member


242


to maintain the axial location of shaft


274


, gear


317


and rotor


273


. Rotor


273


has flat ends spaced a small distance from adjacent surfaces of end plates


241


and


242


. The small clearance, seen in

FIG. 23

, between rotor body


282


and inside surfaces of end plates


241


and


242


reduces wear, friction and heat generation during rotation of rotor


273


. Gears


316


and


317


have the same pitch diameters whereby shafts


229


and


274


rotate at the same speed. The pitch diameters of gears


316


and


317


are the same as the diameters of rotors


261


and


273


. Rotors


261


and


273


turn in opposite directions at the same speed so that protrusions


268


and


269


register with pockets


288


and


289


in non-contact relation and protrusions


294


and


296


register with pockets


262


and


263


in non-contact relation during concurrent rotation of rotors


261


and


273


. This reduces wear of the protrusions and rotor pockets and minimizes noise.




As shown in

FIG. 23

, cover plate


243


closes the open side of end member


242


and bearings


271


and


276


. A flat disk


322


located between cover plate


243


and end member


241


is mounted on shaft


229


. Disk


322


on rotation of shaft


229


moves a lubricant, such as oil, upward to lubricate bearings


271


and


276


.




The present disclosure is preferred embodiments of the supercharger and accumulator for an internal combustion engine. It is understood that the supercharger and accumulator are not to be limited to the specific constructions and arrangements shown and described. It is understood that changes in parts, materials, arrangement and locations of structures may be made without.



Claims
  • 1. A fluid mover comprising: a housing having an inside wall surrounding an internal chamber, a first shaft extended through the chamber, means rotatably mounting the first shaft on the housing, a first piston located in the chamber secured to the first shaft, said first piston having an outer surface having a plurality of pockets open to the outer surface, a second shaft extended through the chamber, means rotatably mounting the second shaft on the housing, power transmission means for concurrently rotating the first and second shafts, and a second piston located in the chamber secured to the second shaft, said second piston having an outer surface having a plurality of pockets open to the outer surface, protrusion means connected to the first and second pistons having outer portions located in non-contact relation with the inside wall of the housing and the pockets of first and second pistons during concurrent rotation of the pistons in the chamber, each of said first and second pistons having a body having key hole shaped grooves, said protrusion means includes T-shaped heads located in said key hole shaped grooves, and means to hold the heads in fixed relationship relative to said body, said housing having a fluid intake passage and a fluid exhaust passage open to the chamber whereby the turning pistons moves fluid from the fluid intake passage, through the chamber, and forces fluid out of the chamber through the fluid exhaust passage.
  • 2. The fluid mover of claim 1 wherein: said pockets of each piston are a pair of semi-cylindrical pockets located on opposite portions of the piston and normal to said protrusion means.
  • 3. The fluid mover of claim 1 wherein: the fluid intake passage is bifurcated and open to the chamber to allow fluid to flow in tangential directions into the chamber.
  • 4. The fluid mover of claim 1 wherein: each protrusion means has a semi-cylindrical outer surface having a radius smaller than the radius of each pocket.
  • 5. The fluid mover of claim 4 wherein: the pockets are semi-cylindrical pockets located on opposite portions of the pistons.
  • 6. The fluid mover of claim 1 wherein: the housing has first and second side walls on opposite sides of the internal chamber, and means operatively associated with the first and second shafts to maintain the first and second pistons in axial spaced relation relative to the first and second side walls of the housing.
  • 7. The fluid mover of claim 1 wherein: the power transmission comprises a first spur gear mounted on the first shaft and a second spur gear mounted on the second shaft, said spur gears having engaging teeth whereby the spur gears concurrently rotor the first an second positions.
  • 8. The fluid mover of claim 7 wherein: the housing has first and second side walls on opposite sides of the internal chamber, each piston has opposite end walls, and means to maintain the end walls of the piston in axial spaced relation relative to the first and second side walls of the housing comprising bearing washers located adjacent opposite sides of the spur gears and biasing means engageable with the bearing washers to maintain the axial locations of the end walls of the first and second pistons relative to the first and second side walls of the housing.
  • 9. The apparatus of claim 1 wherein: each outer surface of the first and second pistons is a cylindrical surface, the cylindrical surfaces of the first and second pistons have the same diameters, said power transmission means comprises a first spur gear mounted on the first shaft and a second spur gear mounted on the second shaft, said spur gears having engaging teeth whereby the first and second spur gears concurrently rotate the first and second pistons, said first and second spur gears having pitch diameters that are the same as the diameters of the first and second pistons.
  • 10. A fluid mover comprising: a housing having a first chamber and a second chamber open to the first chamber, each chamber having an inside surface, said housing having a fluid intake passage, a fluid exhaust passage open to the chambers, and side walls on opposite sides of the chambers, rotor means located in the chambers to draw fluid through the intake passage, into the chambers, and force fluid out of the chambers through the fluid exhaust passage, a pair of parallel shafts rotatably mounted on the housing, said rotor means having a pair of rotors mounted on the shafts rotatably supported on the housing, means to concurrently rotate the shafts and rotors, means operatively associated with the shafts to maintain the rotors in axial spaced relation relative to the side walls of the housing, each rotor having a plurality of pockets and protrusions, each rotor having a body having key hole shaped grooves, said protrusions including T-shaped heads located in the key hole shaped grooves, and means to hold the heads in fixed relationship relative to said body, the protrusions cooperating with the pockets of the adjacent rotor to move fluid through the chambers when the rotors are rotated, each pocket has a generally semi-circular cross section, each protrusion having a generally semi-cylindrical shaped outer surface with a radius smaller than the radius of the pocket.
  • 11. The fluid mover of claim 10 wherein: the protrusions have a non-contact relation with the inside surfaces of the chambers.
  • 12. The fluid mover of claim 10 wherein: the protrusions have a non-contact relation with the pockets of the adjacent rotor when the rotors are rotated.
  • 13. The fluid mover of claim 10 wherein: the fluid intake passage includes a fluid inlet having two passages open to the chambers to allow fluid to flow in tangential directions into the chambers.
  • 14. The fluid mover of claim 10 wherein: each rotor has opposite end walls, said means to maintain the rotors in axial spaced relation relative to the housing being operative to maintain the end walls of the rotors in spaced relation to the side walls of the housing.
  • 15. The apparatus of claim 10 wherein: each rotor has an outer cylindrical surface, the cylindrical surfaces of the rotors have the same diameters, said means to concurrently rotate the shaft means comprising first and second shafts, and rotors comprise a first spur gear mounted on the first shaft and a second spur gear mounted on the second shaft, said spur gears having engaging teeth whereby the first and second spur gears concurrently rotate said shafts and rotors, said first and second spur gears having pitch diameters that are the same as the diameters of the rotors.
CROSS REFERENCE TO RELATED APPLICATION

This application is a division of U.S. application Ser. No. 09/118,625 filed Jul. 17, 1998 now, U.S. Pat. No. 6,138,646. Application Ser. No. 09/118,625 claims the priority date of U.S. Provisional Application Ser. No. 60/053,148 filed Jul. 18, 1997.

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30157 Roots Sep 1860
137055 Chapman Mar 1873
337551 Berrenberg Mar 1886
380764 Pearson Apr 1888
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1325266 Smith Dec 1919
1846656 Rayfield Feb 1932
1923268 Jensen Aug 1933
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2201693 Heess et al. May 1940
3020901 Cook Feb 1962
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3602617 Takahashi Aug 1971
3799713 Cloots et al. Mar 1974
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Number Date Country
193063 Nov 1957 AT
619576 Jan 1927 FR
644016 May 1928 FR
Provisional Applications (1)
Number Date Country
60/053148 Jul 1997 US