Cylindrical cam stirling engine drive

Information

  • Patent Grant
  • 6701709
  • Patent Number
    6,701,709
  • Date Filed
    Friday, August 16, 2002
    21 years ago
  • Date Issued
    Tuesday, March 9, 2004
    20 years ago
Abstract
A Stirling engine includes a grooved cam drive mechanism with followers having a pair of longitudinally displaced bearings. One roller bearing is adapted to ride along an upper surface of the cam groove, while the other roller bearing is adapted to ride along a lower surface of the cam groove. Each follower includes an outer shaft on which a first bearing is mounted, and an inner shaft extending through the outer shaft on which a second bearing is mounted. A preferably annular space is provided between the inner and outer shafts when the follower is in an unloaded state. Then, when the follower is engaged within the grooved cam, the inner shaft is cantilevered relative to outer shaft within the annular space and results in pre-loading the first bearing against one inner surface of the groove cam and the second bearing against an opposite inner surface of the grooved cam.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




This invention relates broadly to a Stirling engine. More particularly, this invention relates to a cam drive system for a Stirling engine that converts linear mechanical motion of pistons into rotary motion at an output shaft and vice versa.




2. State of the Art




Stirling engines are heat engines that operate on a closed thermodynamic cycle to convert heat energy into mechanical energy by alternately compressing and expanding a confined working fluid (gas or liquid). As with any heat engine, the engine requires a hot sink and a cold sink and, in the Stirling engine, the confined working fluid is externally heated and cooled. Unlike a steam engine, the working fluid does not change phase at anytime during the thermodynamic cycle. The alternate heating and cooling of the working fluid produces an alternating pressure within the engine. The alternating pressure (or pressure wave) can be converted to mechanical power by several means. For example, the pressure wave can act on pistons, bellows, or diaphragms to convert the pressure wave into mechanical power. Pistons, bellows, and diaphragms produce linear motion that must be converted to rotary motion where rotary motion engine output is desired.




There are a number ways to accomplish the conversion of linear motion from the piston into rotary motion. Crankshafts, wobble-plates, swash-plates, cams, and various other means have been used in the past.




Theories claim Stirling engine performance can be improved by causing a displacer of the engine to dwell at top dead center and bottom dead center. By dwelling at these positions, the working fluid remains in a heat exchanger of the engine for a longer time resulting in greater energy transfer to or from the walls of the heat exchanger to or from the working fluid. Dwells in motion are relatively easy with cams as compared with other mechanisms such as cranks, wobble-plates, and swash-plates that inherently produce sinusoidal or nearly sinusoidal motion. The cam followers engaging the cams can either be sliding or rolling.




High-speed cam design requires attention to the first three derivatives of the displacement function: velocity, acceleration, and jerk. The displacement required is defined by the piston stroke. The shape of the cam curve with respect to rotation is made up of intervals of rise, fall, and dwell. During dwell, there is no piston motion as the cam rotates. The intervals are designed and pieced together so that there preferably are never infinite or excessively high values of acceleration and/or jerk. By controlling acceleration and jerk, the forces on a cam follower and associated moving components can be kept to acceptable levels. This also reduces wear, spalling, and friction on the followers and cam surface in contact with the follower.




Except at very low speeds, sliding cam followers require copious lubrication to maintain a hydrodynamic barrier between the follower and cam surface. Lubrication can be achieved by submersion or pump flooding the cam/follower contact area. The follower rides on a thin hydrodynamic layer of lubricant that reduces friction, prevents high speed contact, and carries away heat that may be generated. However, at high speeds, sliding cam followers require a crankcase containing a fluid lubricant such as oil or grease (wet sump).




Rolling followers can also be used, but have other problems. U.S. Pat. No. 4,996,953 to Buck describes a grooved cam system for a Stirling engine. When the direction of follower load reverses, as it will with double-acting Siemens-type Stirling pistons, the cam follower alternately contacts both sides of the cam groove as the cam rotates. Because the cam rotates in one direction continuously, the rolling follower must reverse direction instantly when switching contact from an upper surface to a lower surface. This reversing may be acceptable for small light weight follower bearings operating at low speeds but large heavy follower bearings rotating at high speeds have considerable inertia and attempting to instantly reverse direction when contacting the opposite surface results in skidding and destruction of the mating follower and cam surfaces.




U.S. Pat. No. 3,385,051 to Kelly teaches a dual blade cam system in which each of two wave-shaped blade cams extends radially outward from the output shaft of the engine. Roller bearings are provided on first and second sides of each of the cams. Blade-type cylindrical cams do not have the problems associated with reversing follower direction of rotation, because for reversing follower loads there are two followers, one above the cam blade, and one below. Each follower is continuously in contact with the same cam surface moving in the same direction. Therefore, there is no skidding. However, these follower assemblies tend to be large, heavy, complex, and expensive. Moreover, unless preloaded, these assemblies can be particularly loud, especially when the load reverses directions and the follower in contact with a cam surface is changed.




Some Stirling engines, such as swash-plate drive engines, operate with wet sumps and require sealing at the piston drive rods to prevent oil from entering the working fluid space from the crankcase fluid space as well as containing the working fluid in the working space. Lubricant in the working fluid can contaminate heat exchanger surfaces or plug the fine pores in the regenerator. Contaminated heat exchangers can reduce performance or cause the engine to be inoperable. Contaminated heat exchangers are difficult or impossible to clean. Explosion in the heater can result if the working fluid is air containing oxygen and the contaminating lubricant is flammable. Because of potential contamination or explosion hazard, and the desire to be able to operate in any orientation, dry-sump Stirling engine designs are desirable.




SUMMARY OF THE INVENTION




It is therefore an object of the invention to provide an improved cam drive mechanism for the conversion of Stirling engine piston linear motion to output shaft rotary motion and vice-versa.




It is another object or the invention to provide for optional cam shapes to produce various cam follower (thus piston) motions (displacement, velocity, acceleration, and dwell) such that the Stirling thermodynamics may be exploited by using optimized piston motions.




It is also an object of the invention to provide a compact Stirling engine mechanical drive that has low volume and weight with respect to traditional Stirling engines.




It is a further object of the invention to provide a high efficiency (low friction) mechanical drive.




It is an additional object of the invention to provide a drive mechanism that is easily manufactured and thus less costly to produce.




It is yet another object of the invention to provide a drive mechanism that is reliable and has low maintenance requirements.




In accord with these objects, which will be discussed in detail below, a Stirling engine is provided having a grooved cam drive mechanism, with cam followers coupled to each piston of the engine and engaged within the grooved cam. Each follower includes a pair of longitudinally displaced bearings. One bearing is adapted to ride along an upper inner surface of the cam, while the other bearing is adapted to ride along a lower inner surface of the cam.




More particularly, each follower includes an outer shaft on which a first of the bearings is mounted, and an inner shaft on which a second of the bearings is mounted. A preferably annular space is provided between the inner and outer shafts when the follower is in an unloaded state. Then, when the follower is engaged within the grooved cam, the inner shaft is cantilevered relative to outer shaft within the annular space and results in pre-loading the first bearing against one inner surface of the groove cam and the second bearing against an opposite inner surface of the grooved cam. The pre-loading eliminates excessive noise and increased bearing wear that would otherwise result.




In accord with one embodiment of the invention, the axes of rotation for the bearings are offset by a first amount in the unloaded state, and a second lesser amount in the loaded state.




In accord with another embodiment, the cam groove has a stepped surface and the bearings of a cam follower have different diameters but a common rotational axis in the unloaded state. When the follower inserted into the groove, the axes of rotation for the bearings are offset, and the larger diameter bearing bears against a surface opposite the step and the smaller diameter bearing bears against a surface of the step.




The bearings are preferably crowned, i.e., have a preferably spherically curved surface. This permits line contact with the cam surface thus reduces the effect of the difference in cam surface velocity at different radial distances from the output shaft rotation centerline. Moreover, the tandem pair of bearings on each follower provide greater load carrying capacity. Furthermore, each bearing is dedicated to rotation in only a single direction.




The cam and followers of the invention provide an engine capable of operating at high speed and low noise. Furthermore, the cam drive mechanism operates with low wear. Moreover, the cam and followers are easily manufactured, and provide a compact, relatively inexpensive, and light weight assembly.




Additional objects and advantages of the invention will become apparent to those skilled in the art upon reference to the detailed description taken in conjunction with the provided figures.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a partial cut-away view of a first embodiment of a Stirling engine according to the invention;





FIG. 2

is a partial section view of the pistons, cylinders, and heat exchange system of the Stirling engine of the invention;





FIG. 3

is a plan elevation of a first embodiment of a cam follower according to the invention;





FIG. 4

is a section view along line


4





4


in

FIG. 3

;





FIG. 5

is a broken section view of a portion of the cam drive system according to the invention;





FIG. 6

is a plan elevation of a second embodiment of a cam follower according to the invention;





FIG. 7

is a section view along line


7





7


in

FIG. 6

;





FIG. 8

is a broken section view of a portion of a second embodiment of the cam drive system according to the invention, shown having a stepped rectangular groove and the second embodiment of the cam follower;





FIG. 9

is a side elevation of an alternative inner shaft for the cam follower of the invention;





FIG. 10

is a section view across line


10





10


in

FIG. 9

;





FIG. 11

illustrates the dynamic balancing of the cam drive mechanism of the invention;





FIG. 12

is a partial cutaway of a second embodiment of a Stirling engine according to the invention; and





FIG. 13

is a partial cutaway perspective view of the Stirling engine of FIG.


12


.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




Turning now to

FIGS. 1 and 2

, a first embodiment of a Siemens-type Stirling engine


10


is shown. The engine


10


has four pistons


12


, each provided in a cylinder


14


, and preferably displaced ninety degrees apart. Each piston


12


has a piston seal


16


that prevents passage of a working fluid


17


between a compression space


18


and an expansion space


20


within the cylinder


14


. The pistons


12


are free to move axially in the cylinders


14


and control a cam drive mechanism, described below. While theoretically the engine


10


requires that the positions of the four pistons


12


be maintained in a ninety-degree phase relationship to each other with respect to a rotational axis A


r


of a cam


52


and an output shaft


24


, in practice, other phase relationships can be used.




In a Siemens-Stirling engine


10


, each cylinder


14


is connected to an adjacent cylinder by a heater


30


, a regenerator


32


, and a cooler


34


(FIG.


2


). As the pistons


12


translate back and forth in the cylinders


14


, the working fluid


17


is forced to flow in an oscillating fashion to and from the compression spaces


18


and expansion spaces


20


thru the heater


30


, regenerator


32


, cooler


34


and the connecting ducts


36


.




Piston rod seals


40


isolate the preferably gaseous working fluid


17


from a gas space


42


in a preferably dry-sump crankcase


46


. Linear piston rod bearings


44


support and locate the piston guide rods


22


.




The output shaft


24


is supported in the crankcase


46


by three bearings


48


. An output shaft seal


50


about the shaft


24


contains a preferably pressurized gaseous fluid


51


in the crankcase gas space


42


. A cam


52


is rigidly attached to the output shaft


24


. The cam


52


defines a preferably rectangular groove


54


, with upper and lower surfaces


56


,


58


.




For each piston


12


, a cam follower fitting assembly


60


is provided and includes a mount


68


supporting a cam follower


70


adapted to be inserted into the groove


54


. The mount


68


of the assembly is attached to the lower end of each piston guide rod


22


. A cam follower guide rod


72


is coupled to the bottom of the fitting assembly


60


coaxial with the piston rod


22


and rides in a linear bearing


73


, and a cam follower alignment pin


74


is provided parallel to the follower guide rod


72


. The follower guide rod


72


and alignment pin


74


reciprocate within mating bores


76


,


78


, respectively, as the piston


12


reciprocates. The follower alignment pin


74


maintains the correct position of the follower assembly


60


with respect to the cam


52


by preventing the follower assembly


60


from rotating about the common axis of the piston guide rod


22


and the follower guide rod


72


due to offset loads on the cam follower


70


which urges the follower


70


away from the cam


52


.




Referring to

FIGS. 3 and 4

, a first embodiment of the cam follower


70


includes first and second longitudinally displaced ball bearings


80


,


82


that are preferably of equal diameter. The bearings


80


,


82


are preferably slightly crowned, i.e., have a spherically curved surface. While difficult to see due to the relatively large radius of curvature, this crowning is shown in the figures at


81


and


83


. The crowning permits line contact between the bearings


80


,


82


and respective inner surfaces


56


,


58


of the cam groove


54


, and thus reduces the effect of the difference in cam surface velocity at different radial distances from the output shaft rotational axis A


r


. Moreover, the crowning prevents minor misalignments and deflections from causing binding.




The first bearing


80


is mounted on a cylindrical mount


84


of an outer shaft


86


, and the second bearing


82


is mounted on a cylindrical mount


88


of an inner shaft


90


extending through the outer shaft


86


. A centerline of the outer shaft


86


is concentric with a coupling end


92


of the inner shaft


90


. An annular clearance gap


100


, preferably equal all around, is provided between a raised section


102


of the inner shaft


90


and the inner surface of the outer shaft


86


. The cylindrical mount


88


defines a rotational axis A


m


that is parallel to but offset by a distance d


1


from a centerline C


1


of the remainder of the inner shaft


90


. Thus, the bearings


80


,


82


are not rotationally concentric and the outer diameter of bearing


82


is offset from the outer diameter of bearing


80


by a distance d


2


that is equal to distance d


1


.




The outer surface of the coupling end


92


the inner shaft


90


includes an outer key slot


93


, and the inner surface of a coupling end


94


of the outer shaft


86


includes an inner key slot


96


. An inner key


98


extends into the slots


93


,


96


and rotationally locks the inner shaft


90


relative to the outer shaft


86


.




Referring to

FIG. 5

, the follower


70


is coupled within a bore


106


of the mount


68


of the follower assembly


60


. The outer surface of the coupling end


94


of the outer shaft


86


includes a outer key slot


108


, and the mount bore


106


includes an inner key slot


110


. An outer key


112


extends into the key slots


108


,


110


and rotationally locks the outer shaft


86


within the bore


106


. The coupling end


92


of the inner shaft


90


extends through the bore


106


. The coupling end


92


is provided with threads (not shown), and a washer


114


and nut


116


are secured thereon to lock the follower


70


to the mount


68


. The keys


98


,


112


ensure that the follower is properly oriented in the mount


68


for the desired orientation of bearing offset d


2


.




When the follower


70


is coupled to the mount


68


, it is positioned for insertion into the cam groove


54


. Once in the cam groove


54


, the inner shaft


90


is cantilevered along a resilient beam portion


118


relative to outer shaft


86


. That is, because the centerline C


1


of the follower


70


(

FIG. 4

) is held perpendicular to the rotational axis A


r


of the cam (

FIG. 1

) and by proper choice of the radial clearance gap


100


and the offset d


2


, offset bearing


82


is forced against lower cam surface


58


and bearing


80


is forced against the upper cam surface


56


. A portion of the distance d


2


and gap


100


is used up in bending the resilient portion


118


of inner shaft


90


. This bending of the resilient portion beam


118


produces a preload that appears as a couple acting at contact points on the cam groove surfaces


56


,


58


. The couple is counteracted by an opposite couple created by forces from the piston guide rod


22


and cam follower guide rod


72


acting on linear bearings


44


and


73


, respectively. The preloading eliminates excessive noise that would otherwise result and provides for extended bearing life, and more efficient operation.




In addition, the pistons


12


, piston guide rods


22


, cam follower mount


68


, cam follower


70


, cam follower guide rod


72


, and cam follower alignment pin


74


comprise a rigid assembly that has a centerline C


2


passing through the center of the contact area of the cam follower


70


; i.e., between the two bearings


80


,


82


. By locating the piston rod centerline C


2


through the center of the contact area of the cam follower


70


, the moment about the piston rod centerline C


2


is reduced by providing the shortest moment arm from the piston rod centerline to any point of contact between the cam bearings


80


,


82


and the cam surfaces


56


,


58


.




Referring to

FIGS. 1 and 5

, in operation, as each piston


12


is forced up and down by alternating pressure in the cylinder


14


(FIG.


2


), the engagement of the bearings


80


,


82


of the cam follower


70


with the cam surfaces


56


and


58


force the cam


52


and consequently the output shaft


24


to rotate about rotational axis A


r


. The cam follower alignment pin


74


slides in its bore


78


in the crankcase


46


and prevents the cam follower assembly


60


from rotating about the axis defined by rods


22


and


72


.




In view of the above arrangement for the cam drive mechanism, and assuming a preferred set of parameters in which:




i) the spring rate of the cantilevered beam portion


118


of the inner shaft


90


measured at the bearing-to-cam contact point equals 10,000 lbs/inch,




ii) the cam groove width=bearing diameter+0.020 inch, and




iii) the annular gap


100


between the raised section


102


of the inner shaft


90


and the outer shaft


86


=0.020 inch, Table 1 sets forth various preferred exemplar contact forces created and gaps defined between identified elements during operation and otherwise.












TABLE 1











Contact Forces and Gaps for Various Cam and Follower






Configurations






















ID




Configuration




F80a




F82a




F80b




F82b




G80b




G82b




G82a




G80a




G100a




G100b









1




Prior to




0




0




0




0
























0.020




0.020







Insertion







into Groove






2




Inserted into




100




100




0




0




0.020




0.020




0.000




0.000




0.010




0.030







Groove






3




Piston Force




200




100




0




0




0.020




0.020




0.000




0.000




0.010




0.030







Up = 100






4




Piston Force




1,100




100




0




0




0.020




0.020




0.000




0.000




0.010




0.030







up = 1,000






5




Piston Force




0




200




0




0




0.010




0.020




0.000




0.010




0.000




0.040







Down = 100






6




Piston Force




0




1,100




0




0




0.010




0.020




0.000




0.010




0.000




0.040







Down = 1,000














In Table 1, F


80




a


and F


82




a


refer to forces at the surfaces of respective bearings


80


,


82


which are in contact with respective cam surfaces


56


,


58


, and F


80




b


, F


82




b


refer to forces at a diametric location on bearings


80


,


82


, respectively. Referring to Table 1 and

FIG. 5

, G


80




a


refers to the gap or space between bearing


80


and the upper cam surface


56


, and G


80




b


refers to the gap between bearing


80


and the lower cam surface


58


. Likewise, G


82




a


refers to the gap or space between bearing


82


and the lower cam surface


58


, and G


82




b


refers to the gap between bearing


82


and the upper cam surface


56


. Finally, Referring to Table 1 and

FIGS. 4 and 5

, G


100




a


refers to the gap space


100


between an upper side of the raised section


102


of the inner shaft


90


and the outer shaft


86


, and G


100




b


refers to the gap between a lower side of the raised section of the inner shaft and the outer shaft.




Therefore, as indicated at row ID


1


of Table 1, prior to installation of the follower bearings


80


,


82


into the groove


54


, all contact forces equal 0 lbs. Moreover, gaps G


80




a


,


80




b


,


82




a


, and


82




b


are undefined as there is no mating cam surface relative to which a measurement can be made. In addition, there is a uniform annular gap space at 100 between the inner and outer shafts, thereby making gaps G


100




a


and G


100




b


equal.




Once the follower is inserted into the groove (row ID


2


), the contact surfaces of each of the bearings


80


,


82


is subject to a preloading force F


80




a


, F


82




a


of 100 lbs, while gaps G


80




b


and G


82




b


are 0.020 inch, as the cam groove is 0.020 inch wider than the bearing diameters. Gaps G


80




a


and G


82




a


are 0.000 inch, as these are now contact points. Gap G


100




a


is reduced to 0.010 inch, while gap G


100




b


is increased to 0.030 inch because the beam


118


is deflected upward by bearing


82


contacting cam surface


58


.




Then, at row ID


3


, when an upward piston force of 100 lbs is added to the follower


70


, forces F


80




b


and F


82




b


are 0, as there is no contact with the cam surfaces at the respective bearing surfaces. Force F


82




a


remains at 100 lbs because the beam


118


has not deflected any more or less, while force F


80




a


equals 200 lbs (the preload of 100 lbs plus the upward piston force of 100 lbs). Gaps G


80




b


and G


82




b


equal 0.020 inch because the bearings


80


and


82


both remain in contact with their respective bearing surfaces, and gaps G


80




a


and G


80




b


consequently remain at 0.000 inch. Gap G


100




a


remains at 0.010 inch and G


100




b


remains at 0.030 inch because there is no relative movement between the inner and outer shafts


86


,


90


.




At row ID


4


, the upward piston force is increased to 1000 lbs. The forces F


80




b


, F


82




b


remain at 0. Force F


82




a


remains at 100 lbs because the deflection of the beam is not altered. Force F


80




a


is now at 1100 lbs (the sum of the preload and the upward piston force). The gaps are all as discussed above in row ID


3


.




At row ID


5


, a 100 lbs downward force is applied to the piston


12


, and hence the follower


70


. Forces F


80




b


and F


82




b


remain at 0. Force F


82




a


is 200 lbs (the sum of the preload and the piston force), while F


80




a


is 0 because the beam


118


has been deflected by the added 100 lbs force. Gap G


82




b


is 0.020 inch and gap G


82




a


is 0.000 inch because bearing


82


is still in contact with the lower cam surface


56


. Gaps G


80




a


and G


80




b


are each 0.010 inch because the beam has been deflected to a maximum extent. In addition, due to beam deflection, the annular space


100


is converted into a space that is not continuous about the inner shaft, as the inner shaft contacts the outer shaft (FIG.


5


), making gap G


100




a


equal to 0.000 and gap G


100




b


equal to 0.040 inch.




Finally, at row ID


6


, the downward force is increased to 1000 lbs. The forces F


80




b


and F


82




b


remain at 0. Force F


82




a


is at 1100 lbs, while force F


80




a


remains at 0 lbs due to beam deflection. The gaps are all as discussed above with respect to row ID


5


.




As such, Table 1 shows that whenever the follower assembly


70


is installed into the groove


54


, there is always a clearance gap at G


80




b


and G


82




b


, and forces F


80




b


and F


82




b


are always 0 lbs. Gap G


82




a


is always 0.00 inch, and force F


82




a


is always greater than 0; thus, bearing


82


is always preloaded. There is a condition when the piston force is downward that force F


80




a


equals 0 lb and gap G


80




b


equals 0.010 inch. At this time bearing


80


is not preloaded, but this is only for a portion of the cam revolution. Importantly, both bearings


80


,


82


revolve in the same direction continuously.




The inner shaft


90


, outer shaft


86


, and mating components are easily manufactured, comprise a more compact, light-weight assembly, and should be less expensive than the followers required for bladed cam mechanisms. Moreover, the forces on the follower and associated moving components can be kept to acceptable levels, reducing wear, spalling, and friction on the followers and cam surfaces in contact with the followers.




Turning now to

FIGS. 6 and 7

, a second embodiment of a cam follower


270


, substantially similar to the first embodiment, (with like elements having reference numerals incremented by


200


relative to cam follower


70


) is shown. The cam follower


270


includes two inline bearings


280


,


282


. Bearing


280


is mounting on a bearing mount


284


at an end of outer shaft


286


, while bearing


282


is mounted on a bearing mount


288


at an end of inner shaft


290


. Bearing


282


is smaller in diameter than bearing


280


. Unlike inner shaft


90


, all cylindrical surfaces on inner shaft


290


are concentric and thus the bearings


280


and


282


are concentric about centerline C


3


in the free unloaded state. As such, annular gap


100


is equal all around.




Referring to

FIG. 8

, the cam groove


254


includes a step


259


, e.g., on the lower cam surface


258


. The distance between cam surfaces


256


,


258


, the height of step


259


, and the diameters of bearings


280


and


282


determine the preload when installed. More particularly, step


259


forces bearing


282


out of concentricity with bearing


280


. The cantilever beam section


318


(

FIG. 7

) of inner shaft


290


is thereby bent, thus producing a preload.




Turning now to

FIG. 9

, an alternate inner shaft


390


is shown which may be substituted for inner shafts


90


and


290


where a lower spring rate of a cantilever beam section


418


may be desired. Portions of the cantilever beam section


418


are removed to reduce the cross-sectional area of the section (FIG.


10


). This results in a beam that is relatively stiffer in one direction than the other so that deflections in different directions can be controlled.




Referring now to

FIG. 11

, the dynamic balancing of the cam drive mechanism is shown. The rotating cam with its asymmetric mass distribution creates a couple D


y


×F


x


about the origin O of the x-y coordinate system shown. The moving piston/follower masses create the opposite couple D


y


×F


y


. By correct choice of masses and separation distances, the opposite couples can be made equal and to cancel each other thus dynamically balancing the mechanism.




Turning now to

FIGS. 12 and 13

, a second embodiment of a Stirling engine


410


, substantially similar to the first embodiment (with like elements having reference numerals incremented by


400


), is shown. The engine


410


includes a dual guide rod design for the cam follower assembly. More particularly, first and second guide rods


476


,


477


are spaced apart and rigidly attached to the upper and lower portions


447


,


449


of the crankcase


446


. The guide rods


476


,


477


extend parallel to the piston rod


422


. The mount


468


of the cam follower assembly


460


includes upper ears


520


,


521


and lower ears


522


,


523


, each defining a bore provided with a bearing


524


. Guide rod


476


extends through bearings


524


in ears


520


,


522


, and guide rod


477


extends through bearings


524


in ears


521


,


523


. This design provides more rigid guidance to the follower assembly


460


(relative to the single guide rod


76


of the first embodiment). Moreover, this cam follower assembly is significantly shorter than the first embodiment, thereby permitting the overall height of the crankcase


446


to be reduced. Compare the height of crankcase


46


(

FIG. 1

) with the height of crankcase


446


. Thus, weight and size reduction result.




There have been described and illustrated herein several embodiments of a Stirling engine and cam drive mechanism suitable for a Stirling engine. While particular embodiments of the invention have been described, it is not intended that the invention be limited thereto, as it is intended that the invention be as broad in scope as the art will allow and that the specification be read likewise. Thus, while ball bearings have been disclosed for use with the follower, it will be appreciated that other bearings, such as roller and needle bearings, can be used as well. In addition, while a preload of approximately 100 lbs (e.g., 75 lbs to 125 lbs) is preferred, it is recognized that the system can be designed to subject the bearings to other preload forces. Also, where particular gap dimensions have been provided, it is understood that other gap dimensions can be used. Furthermore, while a Siemens-type engine with four pistons/cylinders has been shown, it is understood that other types of Stirling engines with other numbers of pistons and cylinders can be used. Moreover, additional piston sets can be added by adding more grooves displaced axially along the output shaft. Additional piston sets can also operate in the same groove and face axially in the same direction as the original pistons or face in the opposite direction. For example, eight pistons can operate in one groove and maintain a ninety degree phase relationship by using a groove with two cycles per revolution instead of one cycle as shown in FIG.


1


. Also, it is appreciated that the engine can be used as a refrigerator or heat pump, in which rotation of the shaft


54


with attached cam


52


causes the followers


70


to move in the cam groove


54


in a manner that causes the pistons


12


to translate within their respective cylinders


14


. Furthermore, while the preferred description has included pistons within the cylinders, it is understood that bellows, diaphragms, and other mechanisms can be used, and for purposes of simplicity, the term ‘piston’ should be read to include bellows, diaphragms, and such other mechanisms, particularly with respect to the claims. It will therefore be appreciated by those skilled in the art that yet other modifications could be made to the provided invention without deviating from its spirit and scope as claimed.



Claims
  • 1. A Stirling engine, comprising:a) a pressure vessel containing a working fluid; b) a first heat exchanger means for heating said working fluid; c) a second heat exchanger means for cooling said working fluid; d) a regenerator for storing heat energy released by the working fluid; and e) a piston movable within the pressure vessel; f) a cam follower coupled to said piston, said cam follower including first and second longitudinally displaced bearings; and g) a rotatable shaft having a cam groove circumferentially thereabout, said cam groove includes first and second inner surfaces, wherein said first bearing contacts one of said first and second inner surfaces and a first clearance space is provided between said first bearing and said other of said first and second inner surfaces, and said second bearing contacts the other of said first and second inner surfaces and a second clearance space is provided between said second bearing and said one of said first and second inner surfaces.
  • 2. A Stirling engine according to claim 1, wherein:said first and second bearings each have a crowned bearing surface.
  • 3. A Stirling engine according to claim 1, wherein:said follower includes an outer shaft having a first mount on which said first bearing is mounted, and an inner shaft extending through said first shaft and having a second mount on which said second bearing is mounting.
  • 4. A Stirling engine according to claim 3, wherein:a space is defined between a portion of said inner shaft and said outer shaft, said inner shaft being sufficiently resilient to bend within said space relative to said outer shaft when subject to a predetermined load.
  • 5. A Stirling engine according to claim 3, wherein:in an unloaded state, said first and second mounts are offset by a first distance such that said first and second bearings have non-concentric rotational axes.
  • 6. A Stirling engine according to claim 5, wherein:when said first and second bearings are subject to a load, said first and second mounts are offset by a second distance smaller than said first distance.
  • 7. A Stirling engine according to claim 2, wherein:said first bearing is larger in diameter than said second bearing, and in an unloaded state, said first and second bearings have axes of rotation which are concentric.
  • 8. A Stirling engine according to claim 7, wherein:when said first and second bearings are subject to a load, said first and second mounts are offset such that said axes of rotation are non-concentric.
  • 9. A Stirling engine according to claim 8, wherein:one of said first and second inner surfaces of said cam groove is stepped.
  • 10. A Stirling engine according to claim 1, wherein:said first and second bearings are preloaded against the inner surfaces of said cam groove with which each is in contact.
  • 11. A Stirling engine according to claim 10, wherein:said preload is 75 to 125 lbs.
  • 12. A Stirling engine according to claim 10, wherein:said preload is at least 100 lbs.
  • 13. A Stirling engine according to claim 1, wherein:when said cam follower is moved relative to said cam groove, said first bearing rotates in a first direction only, and said second bearing rotates in a second direction only, opposite said first direction.
  • 14. A Stirling engine, comprising:a) a pressure vessel containing a working fluid; b) a first heat exchanger means for heating said working fluid; c) a second heat exchanger means for cooling said working fluid; d) a regenerator for storing heat energy released by the working fluid; e) a rotatable shaft having a cam groove circumferentially thereabout and defining first and second inner surfaces; f) a piston movable within the pressure vessel; and g) a cam follower coupled to said piston, said cam follower preloaded against both said first and second inner surfaces of said cam groove.
  • 15. A Stirling engine according to claim 14, wherein:said follower includes first and second longitudinally displaced bearings.
  • 16. A Stirling engine according to claim 14, wherein:said first and second bearings have non-concentric rotational axes under said preload.
  • 17. A Stirling engine according to claim 1, further comprising:h) a crankcase; i) a piston rod having first and second ends, said first end coupled to said piston and said second end extending into said crankcase; j) a follower mount within said crankcase and coupled to said piston rod, wherein said cam follower is rigidly coupled to said follower mount; and k) a pair of guide rods coupled within said crankcase and extending through said follower mount, said follower mount slidable relative to said guide rods.
  • 18. A Stirling engine, comprising:a) a pressure vessel containing a working fluid; b) a first heat exchanger means for heating said working fluid; c) a second heat exchanger means for cooling said working fluid; d) a regenerator for storing heat energy released by the working fluid; e) a rotatable shaft having a cam groove circumferentially thereabout and defining first and second inner surfaces; f) a piston movable within the pressure vessel along an axis; and g) a cam follower coupled to said piston, said cam follower including first and second longitudinally displaced bearings defining a center line therebetween, said center line aligned along said axis.
  • 19. A Stirling engine, comprising:a) a pressure vessel containing a working fluid; b) a first heat exchanger means for heating said working fluid; c) a second heat exchanger means for cooling said working fluid; d) a regenerator for storing heat energy released by the working fluid; e) a rotatable shaft having a cam groove circumferentially thereabout and defining first and second inner surfaces; f) a piston movable within the pressure vessel; and g) a cam follower coupled to said piston, said cam follower including i) an outer shaft having a first mount at an end, ii) an inner shaft extending through said first shaft and having a second mount at an end, iii) a first bearing mounted on said first mount, and iv) a second bearing mounted on said second mount, said inner and outer shafts defining a space between a portion of said inner shaft and said outer shaft, said inner shaft having a beam portion being sufficiently resilient to bend within said space relative to said outer shaft when subject to a predetermined load.
  • 20. A Stirling engine according to claim 19, wherein:said beam portion of said inner shaft has a non-circular cross-sectional shape.
  • 21. A cam follower for use against at least one camming surface, said cam follower comprising:a) an outer shaft having a first mount at an end; b) an inner shaft extending through said first shaft and having a second mount at an end, a space being defined between a portion of said inner shaft and said outer shaft, said inner shaft having a beam portion sufficiently resilient to bend within said space relative to said outer shaft when subject to a predetermined load; c) a first bearing mounted on said first mount; and d) a second bearing mounted on said second mount.
  • 22. A cam follower according to claim 21, wherein:said first and second bearings have respective axes of rotation which are concentric in an unloaded state, and non-concentric in a loaded state in which said first bearing is contacted against a first camming surface and said second bearing is contact against a second camming surface opposite said first camming surface.
  • 23. A cam follower according to claim 21, wherein:said first and second bearings have respective axes of rotation which are non-concentric and offset by a first distance in an unloaded state, and non-concentric and offset by a second distance smaller than said first distance in a loaded state in which said first bearing is contacted against a first camming surface and said second bearing is contact against a second camming surface opposite said first camming surface.
  • 24. A cam follower according to claim 21, wherein:said beam portion has a non-circular cross-sectional shape.
Parent Case Info

This application claims the benefit of U.S. Provisional Application No. 60/313,309, filed Aug. 18, 2001, which is hereby incorporated by reference herein in its entirety.

US Referenced Citations (9)
Number Name Date Kind
2475770 Wijsman Jul 1949 A
3385051 Kelly May 1968 A
4057040 Wax Nov 1977 A
4413474 Moscrip Nov 1983 A
4455825 Pinto Jun 1984 A
4996953 Buck Mar 1991 A
5095700 Bolger Mar 1992 A
5442913 Cho et al. Aug 1995 A
5533335 Shin Jul 1996 A
Provisional Applications (1)
Number Date Country
60/313309 Aug 2001 US