Phased rotary displacement device

Information

  • Patent Grant
  • 6213744
  • Patent Number
    6,213,744
  • Date Filed
    Tuesday, November 16, 1999
    25 years ago
  • Date Issued
    Tuesday, April 10, 2001
    23 years ago
Abstract
A rotary device containing a housing with two side plates, a shaft, an eccentric connected to the shaft, a rotor mounted on the shaft, a first gear, and a second gear. The rotor contains at least 3 sides, the housing has an interior surface defined by at least a first lobe and a second lobe, the first gear is an internal gear which is connected to the rotor, the second gear is an external gear connected to the housing, the difference between the pitch diameter of the first gear and the pitch diameter of the second gear is is equal to twice said eccentricity of the eccentric, and the ratio between the pitch diameter of the first gear and the pitch diameter of the second gear is equal to the ratio between the number of said sides in said rotor divided by the number of lobes in the interior surface of said housing.
Description




FIELD OF THE INVENTION




A phased trochoidal rotary chamber device which can be used for compression and expansion of fluid, pumping of liquid, or as a hydraulic motor.




BACKGROUND OF THE INVENTION




In U.S. Pat. No. 5,769,619, applicants described and claimed a rotary device comprised of a housing comprising a curved inner surface in the shape of a trochoid and an interior wall, an eccentric mounted on a shaft disposed within said housing, a first rotor mounted on said eccentric shaft which is comprised of a first side and a second side, a first pin attached to said rotor and extending from said rotor to said interior wall of said housing, and a second pin attached to said rotor and extending from said rotor to said interior wall of such housing, and a third pin attached to said rotor and extending from said rotor to said interior wall of said housing. This rotary device also contains the following features: (1) a continuously arcuate track is disposed within said interior wall of said housing, wherein said continuously arcuate track is in the shape of an envoluted trochoid, (2) said first pin has a distal end which is disposed within said continuously arcuate track, (3) said second pin has a distal end which is disposed within said continuously arcuate track, (4) said third pin has a distal end which is disposed within said continuously arcuate track, (5) said distal end of said first pin is comprised of a shaft disposed within a first rotatable sleeve, (6) said distal end of said second pin is comprised of a shaft disposed within a second rotatable sleeve, said distal end of said third sleeve is comprised of a shaft disposed within a third rotatable sleeve, (7) said rotor is comprised of a multiplicity of apices, wherein each such apex forms a compliant seal with said curved inner surface, and wherein each such apex is comprised of a separate curved surface which is formed from a strip of material pressed into a recess, (8) said curved inner surface of said housing is generated from an ideal epictrochoidal curve and is outwardly recessed from said ideal epitrochoidal curve by a distance of from about 0.05 to about 5 times as great as the eccentricity of said eccentric, (9) the diameter of the distal end of each of said first pin and said second pin is from about 2 to about 4 times as great as said eccentricity of said eccentric, and (10) each of said first pin, said second pin, and said third pin extends from beyond said interior wall of said housing by from about 1 to about 2 times the diameter of each of said pins. The entire disclosure of this U.S. Pat. No. 5,769,619 is hereby incorporated by reference into this specification.




It is an object of this invention to provide a trochoidal rotary chamber device which is more durable, more reliable, and more efficient than the trochoidal rotary chamber device described and claimed in U.S. Pat. No. 5,769,619.




SUMMARY OF THE INVENTION




In accordance with this invention, there is provided a rotary device comprised of a housing with a side plate, a shaft disposed within said housing, a rotor mounted on said shaft, and a set of meshing gears, one with internal teeth attached to the rotor, and the other with external teeth attached to the side plate of the housing, both of such gears being concentric to the element they are attached to.











BRIEF DESCRIPTION OF THE DRAWINGS




The invention will be described by reference to the specification and the enclosed drawings, in which like elements are identified by like numerals, and in which:





FIG. 1

is an exploded view of one preferred rotary mechanism of the invention;





FIG. 2

is partial sectional view of the mechanism of

FIG. 1

, illustrating the interaction between the rotor and external gear on the side plate of the housing;





FIG. 3

is a schematic representation of a trochoidal surface and an envoluted trochoidal surface produced by the device of this invention;





FIGS. 4

,


5


,


6


,


7


, and


8


are schematic representations of a rotor with a solid curved surface, a strip seal, a spring-loaded seal, and a and a strip of material, as well as all of these structures, disposed at one or more of its apices sealing purposes.











DESCRIPTION OF THE PREFERRED EMBODIMENTS




The instant invention is comprised of an improvement on the structure disclosed in U.S. Pat. No. 5,769,619.





FIG. 1

is an exploded perspective view of one preferred rotary mechanism


10


. Referring to

FIG. 1

, it will be seen that rotary mechanism


10


is comprised of housing


12


, shaft


14


, rotor


16


, external gear


18


, internal gear


20


, eccentric


22


, bearing


24


, and side plate


26


.




Referring again to

FIG. 1

, it will be seen that housing


12


is preferably an integral structure. However, housing


12


may comprise two or more segments joined together by conventional means such as, e.g., bolts.




In one embodiment, housing


12


consists essentially of steel. As is known to those skilled in the art, steel is an alloy of iron and from about 0.02 to about 1.5 weight percent of carbon; it is made from molten pig iron by oxidizing out the excess carbon and other impurities (see, e.g., pages 23-14 to 23-56 of Robert H. Perry et al.'s “Chemical Engineer's Handbook,” Fifth Edition (McGraw-Hill Book Company, New York, New York, 1973).




In another embodiment, housing


12


consists essentially of aluminum. In yet another embodiment, housing


12


consists essentially of plastic. These and other suitable materials are described in George S. Brady et al.'s “Materials Handbook,” Thirteenth Edition (McGraw-Hill, Inc., New York, New York, 1991).




In another embodiment, housing


12


consists essentially of ceramic material such as, e.g., silicon carbide, silicon nitride, etc.




In one embodiment, housing


12


is coated with a wear-resistant coating such as, e.g., a coating of alumina formed electrolytically, electroless nickel, tungsten carbide, etc.




One advantage of applicant's rotary mechanism


10


is that the housing need not be constructed of expensive alloys which are resistant to wear; and the inner surface of the housing need not be treated with one or more special coatings to minimize such wear. Thus, applicants' device is substantially less expensive to produce than prior art devices.




Housing


12


may be produced from steel stock (such as, e.g., C1040 steel stock) by conventional milling techniques. Thus, by way of illustration, one may use a computer numerical controlled milling machine which is adapted to cut a housing


12


with the desired curved surface.




Similarly, the rotor


16


may be made of any material(s) from which the housing


12


is made.




Referring again to

FIG. 1

, and in the preferred embodiment depicted therein it will be seen that housing


12


is comprised of an external gear


18


mounted on an inner wall


26


of such housing


12


. The external gear


18


is so disposed that, when drive shaft


14


is disposed therein, the gear


18


is concentric to the drive shaft


14


.




The external gear


18


preferably has a substantially circular cross-sectional shape.




In order for the external gear


18


and the internal gear


20


to phase properly the rotor


16


in the housing


12


, they have to meet two different conditions. In the first place, the difference between the two pitch diameters of the internal and external gears must be exactly twice the eccentricity of the shaft


22


. In the second place, the ratio between the pitch diameters of the internal and external gears must be the same as the ratio between the numbers of sides in rotor


16


divided by the number of lobes in housing


12


. These criteria will be discussed in more detail later in this specification.




The eccentricity of eccentric


22


generally will be from about 0.05 to about 10 inches. It is preferred that the eccentricity be from about 0.15 to about 1.5 inches.




Referring again to

FIG. 1

, and in the preferred embodiment depicted therein, it will be seen that bearing


24


can either be a sleeve bearing and/or a rolling element bearing.




Referring to

FIG. 2

, it will be seen that rotor


16


is comprised of a bore


28


with a center line


34


and an internal diameter


42


. The internal diameter


42


of bore


28


is smaller than the pitch diameter


30


of internal gear


20


.




As is known to those skilled in the art, the term pitch diameter refers to the diameter of an imaginary circle, which commonly is referred to as the “pitch circle,” concentric with the gear axis


34


, which rolls without slippage with a pitch circle of a mating gear. Reference may be had, e.g., to U.S. Pat. Nos. 5,816,788, 5,813,488, 5,704,865, 5,685,269, 5,474,503, 5,454,175, 5,387,000, and the like. The disclosure of each of these U.S. patents is hereby incorporated by reference into this specification.




Referring again to

FIG. 2

, it will be seen internal diameter


42


is also smaller than diameter


32


of the addendum circle of internal gear


20


. As is known to those skilled in the art, the addendum circle is a circle on a gear passing through the tops of the gear teeth. See, e.g., U.S. Pat. Nos. 5,438,732, 5,154,475, 5,090,771, 4,864,893, 4,813,853, 4,780,070, and the like. The entire disclosure of each of these U.S. patents is hereby incorporated by reference into this specification.




Referring again to

FIG. 2

, it will be seen that two internal gears


20


and


21


are depicted, one of which is disposed at end


46


of the rotor


16


, and the other which is disposed at end


48


of rotor


16


. In the preferred embodiment depicted, each of gears


20


and


21


is disposed within a counterbore (


50


and


52


, respectively). In another embodiment, not shown, only one gear


20


or


21


is disposed on one side of rotor


16


.




The gears


20


,


21


may be attached to rotor


16


by conventional means such as, e.g., by mechanical means (using fasteners such as bolts, internal retaining rings, etc.), by interference fit, by electron beam welding, etc.




In the embodiment depicted in

FIG. 1

, the rotor


16


contains four sides and has a substantially square shape. As will be apparent to those skilled in the art, one may use rotors with 3 sides (not shown), 5 sides, 6 sides, etc. In general, it is preferred the rotor contain at least 3 sides and no more 6 sides.




Referring again to

FIG. 2

, it will be seen that an external gear


18


is disposed within side plate


26


and, more precisely, within counterbore


54


of side plate


26


. In the embodiment depicted, only one such external gear


18


is shown disposed on one side plate. In another embodiment, not shown, two such external gears are used and are disposed on both sides of rotor


16


. It will be apparent that, although only one side plate


26


is shown in

FIGS. 1 and 2

for the sake of simplicity of representation, at least two such side plates generally are required for each housing, one for each side of the housing.




Referring again to

FIG. 2

, it will be seen that side plate


26


is comprised of a bore


50


with a centerline


40


and an internal diameter


44


. The internal diameter


44


of bore


50


is smaller than the pitch diameter


36


of external gear


18


.




It will be seen that internal diameter


44


is also smaller than the diameter


38


of the external gear


18


, which is the inner bore of external gear


18


.




The gear(s)


18


may be attached to side plate


26


by conventional means such as, e.g., by mechanical means (using fasteners such as bolts, internal retaining rings, etc.), by interference fit, by electron beam welding, etc.




As mentioned elsewhere in this specification, in order for the external gear


18


and the internal gear


20


to phase properly the rotor


16


in the housing


12


, two different conditions must be met. In the first place, the difference between the two pitch diameters of the internal and external gears (viz., pitch diameters


30


, and


36


) must be exactly twice the eccentricity of the shaft


22


. In the second place, the ratio between the pitch diameters


30


and


36


of the internal and external gears must be the same as the ratio between the numbers of sides in rotor


16


divided by the number of lobes in housing


12


.





FIG. 3

is a schematic representation of trochoidal surface


82


and envoluted trochoidal surface


60


referred to in this specification. Referring to

FIG. 3

, and in the preferred embodiment depicted therein, it will be seen that surface


60


defines a multiplicity of lobes


62


,


64


, and


66


which, in combination, define an inner surface


60


which has a continuously changing curvature.




Referring again to

FIG. 3

, it will be seen that, with regard to lobe


62


, the distance from the centerpoint


68


to any one point on lobe


62


will preferably differ from the distance from the centerpoint to an adjacent point on lobe


62


; both the curvature and the distance from the centerpoint


68


is preferably continuously varying in this lobe (and the other lobes). Thus, for example, the distance


70


between point


68


and


72


is preferably substantially less than the distance


74


between points


68


and


76


; as one progresses from point


72


to point


76


around surface


60


, such distance preferably continuously increases as the curvature of lobe


62


continuously changes. Thereafter, as one progresses from point


76


to point


78


, the distance


80


between point


68


and point


78


preferably continuously decreases.




Referring again to

FIG. 3

, it will be apparent to those skilled in the art that, in this preferred embodiment, the same situation also applies with lobes


66


and


64


. Each of such lobes is preferably defined by a continuously changing curved surface; and the distance from the centerpoint


68


is preferably continuously changing between adjacent points.




In the preferred embodiment illustrated in

FIG. 3

, it is preferred to have at least two of such lobes


62


,


64


, and


66


. It is more preferred to have at least three of such lobes. In another embodiment, at least four of such lobes arc present.




It is preferred that each lobe present in the inner surface


60


have substantially the same curvature and shape as each of the other lobes present in inner surface


60


. Thus, referring to

FIG. 3

, lobes


62


,


64


, and


66


are displaced equidistantly around centerpoint


68


and have substantially the same curvature as each other.




The curved surface


60


may be generated by conventional machining procedures. Thus, as is disclosed in U.S. Pat. No. 4,395,206, the designations “epitrochoid” and “hypotrochoid” surfaces refer to the manner in which a trochoid machine's profile curves are generated; see, e.g., U.S. Pat. No. 3,117,561, the entire disclosure of which is hereby incorporated by reference into this specification.




An epitrochoidal curve is formed by first selecting a base circle and a generating circle having a diameter greater than that of the base circle. The base circle is placed within the generating circle so that the generating circle is able to roll along the circumference of the base circle. The epitrochoidal curve is defined by the locus of points traced by the tip of the radially extending generating or drawing arm, fixed to the generating circle having its inner end pinned to the generating circle center, as the generating circle is rolled about the circumference of the base circle (which is fixed).




In one embodiment, the epitrochoidal curve is generated in accordance with the procedure illustrated in FIG. 29 of U.S. Pat. No. 5,431,551, the entire disclosure of which is hereby incorporated by reference into this specification.




As is disclosed on lines 36 to 55 of column 5 of U.S. Pat. No. 4,395,206, it is common practice to recess or carve out the corresponding profile of the epitrochoid member a distance “x” equal to the outward offset of the apex seal radius (see FIG. 4 of such patent). As is stated on lines 48 et seq. in such patent, in “. . . the case of an inner envelope type device 20′, as shown in FIG. 4, such carving out requires that the actual peripheral wall surface profile 33 which defines the cavity 34 of the housing 35 be everywhere radially outwardly recessed from the ideal epitrochoid profile 36. In the case of an outer envelope device 21′, as illustrated in FIG. 5, such carving out requires that the actual peripheral face profile of the epitrochoid working member, rotor 38, be everywhere inwardly radially recessed from the ideal epitrochoid profile 39.”




Referring again to

FIG. 3

, it will be seen that applicants' inner housing surface profile


60


is generated from ideal epitrochoid curve


82


and is outwardly recessed from ideal curve


82


by a uniform distance


84


. In one preferred embodiment, uniform distance


84


is a function of the eccentricity of the eccentric


22


used in device


10


(see FIG.


1


).




Referring again to

FIG. 1

, it will be seen that rotary mechanism


10


is comprised of a shaft


14


on which the eccentric


22


is mounted. Shaft


14


preferably has a circular cross-section and is cylindrical in shape. Shaft


14


is connected to eccentric


22


. In one embodiment, illustrated in

FIG. 1

, shaft


14


and eccentric


22


are integrally formed and connected.




In one preferred embodiment, both shaft


14


and eccentric


22


consist essentially of steel such as, e.g., carbon steel which contains from about 0.4 to about 0.6 weight percent of carbon.




FIG. 4 of U.S. Pat. No. 5,431,551 is a front view of the shaft/eccentric assembly of this patent, and discussion is presented in such patent of the eccentricity of such assembly. As is known to those skilled in the art, eccentricity is the distance of the geometric center of a revolving body (eccentric


22


) from the axis of rotation.




Referring again to

FIG. 3

, and in the preferred embodiment illustrated therein, it is preferred that the distance


84


be from about 0.5 to about 5.0 times as great as the eccentricity of eccentric


22


(see FIG.


1


). In a more preferred embodiment, the distance


84


is from about 1.0 to about 2.0 times as great as the eccentricity. In one embodiment, distance


84


is about 0 times as great as the eccentricity.





FIG. 6

is a perspective view of a rotor assembly


10


in which the apices


86


,


88


,


90


, and


92


are not directly contiguous with the inner surface


56


of housing


12


. In this embodiment, inner surface


56


defines a theoretical trochoidal shape


82


(see FIG.


5


).




The apparatus


10


may comprise one or more of apex seals disclosed in FIG. 6 of U.S. Pat. No. 5,769,619, the entire disclosure of which is hereby incorporated by reference into this specification. Thus,

FIGS. 4

,


5


,


6


,


7


, and


8


depict rotor(s)


16


with different types of scaling surfaces on each of its apices. In these Figures, for the sake of simplicity of representation, the external gear(s)


18


has been omitted.




Referring to

FIG. 5

, it will be seen that apex


118


is preferably a solid curved surface which is made from the same material as is rotor


16


. In this embodiment, the apex


118


is non-compliant, it provides close-clearance sealing at a distance of from about 0.0001 to about 0.002 inches from the inner surface of the housing (not shown), and it will describe an envoluted trochoidal geometry during its operation.




Referring to

FIG. 6

, apex


120


is connected to an apex seal


121


. In the embodiment depicted, apex seal


121


is a linear strip seal which is disposed within rotor


16


. Linear strip seal


121


can be metallic or non-metallic.




In one embodiment, where apex seal


121


is a fixed strip of material, it provides close-clearance sealing at a distance of from about 0.001 to about 0.002 inches away from the inner surface of the housing and describes an ideal trochoidal geometry during its operation. In another embodiment, where the seal


121


is made compliant by conventional means, it provides substantially zero clearance sealing and also describes an ideal trochoidal geometry during its operation.




Referring to

FIG. 7

, apex


122


is comprised of a separate curved surface


123


affixed to apex


122


and made complaint by virtue of the presence of spring


125


. In this embodiment, the apex


122


provides substantially 0 clearance sealing and describes an envoluted trochoidal geometry during its operation. The surface


123


may consist of an ultra-high molecular weight plastic.




Referring to

FIG. 8

, apex


124


is comprised of a separate curved surface


127


which is formed from a strip of material pressed into a recess (not shown) in rotor


16


. If this curved surface


127


is made from compliant material, apex


124


will also be compliant during operation, thereby providing substantially zero clearance, and will describe an envoluted trochoidal geometry during its operation. A port (not shown) communicating with the pressurized portion of a pressurized volume (not shown) may be employed to pressurize the back the curved surface


127


, such that improved clearance control is achieved at higher pressures. In a similar manner, an equalizing pressure can also be applied to linear strip seal


121


(see

FIG. 6

) and/or surface


123


(see FIG.


7


).





FIG. 4

illustrates an embodiment in which each of the different apex sealing means described above exist with reference to one particular rotor


16


. It will be apparent that other combinations of sealing means besides the ones depicted also may be used.




It is to be understood that the aforementioned description is illustrative only and that changes can be made in the apparatus, in the ingredients and their proportions, and in the sequence of combinations and process steps, as well as in other aspects of the invention discussed herein, without departing from the scope of the invention as defined in the following claims.



Claims
  • 1. A rotary device comprised of a housing with a first side plate, a second side plate, a shaft disposed within said housing, an eccentric connected to said shaft with an eccentricity of from about 0.05 to about 10 inches, a rotor mounted on said shaft, a first gear, and a second gear, wherein:(a) said rotor has at least about 3 sides, (b) said housing is comprised of an interior surface defined by at least a first lobe and a second lobe, (c) said first gear is an internal gear which is connected to said rotor, wherein said first internal gear has a first pitch diameter, (d) said second gear is an external gear connected to said housing, wherein said second gear has a second pitch diameter, (e) the difference between said first pitch diameter and said second pitch diameter is equal to twice said eccentricity of said eccentric, and (f) the ratio between said first pitch diameter and said second pitch diameter is equal to the ratio between the number of said sides in said rotor divided by the number of said lobes in said interior surface of said housing.
  • 2. The rotary device as recited in claim 1, wherein said housing has a curved inner surface which is in the shape of an envoluted trochoid.
  • 3. The rotary device as recited in claim 2, wherein said rotor is comprised of a first side, a second side, a third side, and a fourth side.
  • 4. The rotary device as recited in claim 3, wherein said housing is comprised of a first lobe, a second lobe, and a third lobe.
  • 5. The rotary device as recited in claim 4, wherein said eccentricity of said eccentric is from about 0.15 to about 1.5 inches.
  • 6. The rotary device as recited in claim 5, wherein said eccentric is disposed within a bearing.
  • 7. The rotary device as recited in claim 6, wherein said rotor is connected to a third gear which is an internal gear.
  • 8. The rotary device as recited in claim 7, wherein said housing is a fourth gear which is an external gear.
  • 9. The rotary device as recited in claim 4, wherein each of said first lobe, said second lobe, and said third lobe have substantially the same curvature.
  • 10. The rotary device as recited in claim 1, wherein said housing has a curved inner surface which is in the shape of an ideal trochoid.
  • 11. The rotary device as recited in claim 1, wherein said housing consists essentially of silicon carbide.
  • 12. The rotary device as recited in claim 1, wherein said first lobe has substantially the same curvature as said second lobe.
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Number Name Date Kind
3173406 Campos Mar 1965
3226013 Toyoda et al. Dec 1965
3242912 Huber Mar 1966
3400604 Jones Sep 1968
3465729 Jones Sep 1969
3764239 Huf Oct 1973
3799706 Bilobran Mar 1974
5431551 Aquino et al. Jul 1995
5769619 Crvelin et al. Jun 1998
5947709 Koyama et al. Sep 1999
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Number Date Country
1137899 Oct 1962 DE
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2077357 Dec 1981 GB