1. Field of the Invention
The present invention relates in general to speed changing apparatus and, in particular, to large-ratio speed changing apparatus. More particularly, the present invention relates to a large-ratio strain wave gearing speed changing apparatus for both speed reduction and speed increase applications with improved power capacity and service life.
2. Description of the Related Art
Speed changing is indispensable. Frequently a prime mover must work at high rotational speeds for optimized efficiency while the load it drives must run at tenths or even hundredths its speed. One way to obtain such large speed reduction ratio is to use a cascade of individual reducers of smaller ratio but each at its best efficiency.
However, this cascaded speed reduction suffers in overall speed-changing efficiency due to its nature of having the entire load passing successively through each and every reducer stage of the cascade. The arrangement is also bulky for the obvious reason that each stage in the cascade must be fully rated to handle one hundred percent of the total power delivered by the prime mover.
One type of “single-stage” reducers currently used widely is the cycloidal drive manufactured by Sumitomo Heavy Industries, Ltd. of Tokyo, Japan. Although relatively compact for speed-changing ratios ranging from tens to more than one hundred, the single-stage drive is, essentially, one cycloidal gearing half stage followed by an off-axis power extraction half stage.
For the off-axis power extraction stage, a disc 13 is fixed to the planet element 12 coaxially on their axis 19 and has a number of round holes 17 to allow for engagement by a corresponding number of roller pins 18 planted on the plate 14. In many occasions the holes 17 are formed directly in the element 12, sparing the use of disc 13. This round plate 14 is coupled to the output shaft 16 of the drive and is centered on the central axis 10 of the device. This “power extraction” arrangement allows the drive to deliver a speed-reduction ratio of −K/i, wherein K is the pitch diameter of the planet element 12 and i is the difference between the pitch diameters of elements 11 and 12. In a typical example wherein the ring gear 11 has 80 teeth and a gear version of the planet element 12 has 79 (K=80 mm and i=1 mm using module 1 metric gears), the ratio is −80 when mechanical power is transmitted by the device via the input at shaft 15.
This is obvious as the edge of the hole 17C of the driving disc 13 that is in contact with the pin roller 18C of the driven plate 14 must be behind the roller 18C along the direction of rotation. In this sense pin roller and hole pairs identified by rollers RB and RD are partially working to transmit power because of the location of their contact points relative to the direction of rotation of the disc 13 and plate 14. In the same sense, the pin-roller and hole pair 18G and 17G is not working at all because the pin roller 18G, the driven, travels behind its contact point with its hole 17G, the driver.
Conventional cycloidal drives rely on a synchronizing engagement between two elements (gears) of different pitch diameter with offset axes. But this is not an optimized mechanism due to low utilization: Of all eight pin/hole pairs shown in
Further, to achieve a speed reduction ratio of K, a cycloidal drive requires a fixed ring gear of K+1 teeth. For large ratio, the large ring gear number makes the drive bulky if the rated torque is substantial therefore the teeth must be sufficiently robust—in size. In other words, compactness of the cycloidal drive places a limitation on the torque and power rating of the drive.
Due to advantages such as no backlash, compactness and simple construction, another type of large-ratio reducer widely used in precision and aerospace applications is the harmonic drive manufactured by Harmonic Drive Systems Inc. of Tokyo, Japan. Operating the basic concept known as strain wave gearing, harmonic drive is relatively low in available power rating. The drive also delivers typically less than 60 percent efficiency under normal load because its spline element flexes all the time as the drive operates to transmit mechanical power.
Essentially the same as in the case of a cycloidal drive, for a strain wave gearing device to have large speed changing ratio, the two spline components must have an as-small-as-possible difference in their respective working tooth numbers. Although physically different in construction compared to cycloidal drives, conventional strain wave gearing speed changing devices suffer the same drawbacks in terms of characteristics such as power rating and power-to-weight ratio described above.
In addition to large-ratio speed reducers there are also the need to increase a slow input speed to an output up to tens, hundreds of times or more faster. Speed increasing is the opposite of reducing in terms of speed change ratio but is also important in many applications.
It is an object of the present invention to provide a strain wave gearing speed changing apparatus for large-ratio speed changing that has increased power density using two or more meshing engagements.
It is also an object of the present invention provide a strain wave gearing speed changing apparatus for large-ratio speed changing that has improved efficiency due to reduced flexing in the components.
It is also an object of the present invention provide a strain wave gearing speed changing apparatus for large-ratio speed changing that has improved service life due to reduced flexing in the components.
In order to achieve the above and other objects, the present invention a strain wave gearing speed changing apparatus for changing an input speed to an output either greatly slower or faster, the apparatus has a coaxial pair of circular splines that includes a first circular spline having a tooth number TA and a second circular spline having a tooth number TB. A coaxial pair of flex splines includes a first flex spline having a tooth number TB and a second flex spline having a tooth number TC. The first flex spline meshes with the first circular spline and the second flex spline meshes with the second circular spline at two, preferably more meshing engagements. A wave generator is connected to one of the input and output shafts of the apparatus. Two splines of one of the two coaxial pairs being fixed together to operate flexingly on the wave generator. One spline of the other of the two coaxial pairs being fixed to the frame of the apparatus and the other spline being connected to the other of the input and output shafts. In the apparatus, the four splines satisfy the dimensional relationship of TA=TK+Ti, TB=TK, TC=TK−Tj and TD=TK±Ti−Tj.
The present invention also provides a strain wave gearing speed changing apparatus for changing an input speed to an output either greatly slower or faster, the apparatus has a coaxial pair of circular splines that includes a first circular spline having a tooth number TA and a second circular spline having a tooth number TD. A coaxial pair of flex splines includes a first flex spline having a tooth number TB and a second flex spline having a tooth number TC. The first flex spline meshes with the first circular spline and the second flex spline meshes with the second circular spline. A wave generator is connected to one of the input and output shafts of the apparatus. Two splines of one of the two coaxial pairs being fixed together to operate flexingly on the wave generator that may have equal spline tooth engagement pitch circle circumference lengths. One spline of the other of the two coaxial pairs being fixed to the frame of the apparatus and the other spline being connected to the other of the input and output shafts. In the apparatus, the four splines satisfy the dimensional relationship of TA=TK+Ti, TB=TK, TC=TK−Tj and TD=TK+Ti−Tj.
The present invention further provides a strain wave gearing speed changing apparatus for changing an input speed to an output either greatly slower or faster, the apparatus has a coaxial pair of circular splines that includes a first circular spline having a tooth number TA and a second circular spline having a tooth number TD. A coaxial pair of flex splines includes a first flex spline having a tooth number TB and a second flex spline having a tooth number TC. The first flex spline meshes with the first circular spline and the second flex spline meshes with the second circular spline at one single meshing engagement. A wave generator is connected to one of the input and output shafts of the apparatus. Two splines of one of the two coaxial pairs being fixed together to operate flexingly on the wave generator that may have equal spline tooth engagement pitch circle circumference lengths. One spline of the other of the two coaxial pairs being fixed to the frame of the apparatus and the other spline being connected to the other of the input and output shafts. In the apparatus, the four splines satisfy the dimensional relationship of TA=TK+Ti, TB=TK, TC=TK−Tj and TD=TK+Ti−Tj.
As is illustrated, while the planet gear 32 moves epicyclically inside the frame ring gear 31 as a first ring-spur gear pair, another planet gear 33 that is fixed coaxially with gear 32 also moves epicyclically inside its ring gear 34, a second pair of ring-spur gears. As the gear 33 spins and moves epicyclically inside gear 34, its outer most edge (of its pitch circle) 33P plots a trace 33T. This trace 33T is made to exactly coincide with the pitch circle of the ring gear 34. Essentially, ring gear 34 of the second pair, together with its meshing spur gear 33, serves a similar function as the off-axis power extraction means of a conventional cycloidal drive but allows the present inventive apparatus to produce a speed change ratio that is much larger, as is described hereinafter.
Further, the two coaxial spur gears 42 and 43 are fixed together to each other to operate epicyclically on the carrier 45E. The large ring gear 41, in this depicted example of
In this gear train system, the four gears 41, 42, 43 and 44 satisfy the dimensional relationship of A=K+i, B=K, C=K−j and D=K+i−j wherein K is pitch diameter of the large spur gear 42, i is the difference of pitch diameters between the large ring gear 41 and large spur gear 42 (and also the difference of pitch diameters between the small ring gear 44 and small spur gear 43), and j is the difference of pitch diameters between the large ring gear 41 and small ring gear 44 (and also the difference of pitch diameters between the large spur gear 42 and small spur gear 43).
The speed changing apparatus of
By contrast, a conventional cycloidal drive (of
Further, the two coaxial flex splines 142 and 143 are fixed together to each other to operate flexingly on the wave generator 145E. The large circular spline 141, in this depicted example of
In this spline-based gear train system, the four splines 141, 142, 143 and 144 satisfy the tooth number relationship of TA=TK+Ti, TB=TK, TC=TK−Tj and TD=TK+Ti−Tj wherein TK is tooth number of the large flex spline 142, i is the difference between tooth numbers of large circular spline 141 and large flex spline 142 (and also the difference between tooth numbers of small circular spline 144 and small flex spline 143), and Tj is the difference between tooth numbers of large circular spline 141 and small circular spline 144 (and also the difference between tooth numbers of large flex spline 142 and small flex spline 143).
The strain wave gearing speed changing apparatus of
A speed changing apparatus of the present invention can be used in different configurations of input, output and reaction member assignments among its constituent gear and carrier members. Essentially, a general-purpose speed changing apparatus of the present invention—used either as a speed reducer or an increaser having either a fixed ring gear or a fixed spur gear—can be constructed to have a coaxial pair of ring gears that includes a large ring gear having a pitch diameter A and a small ring gear having a pitch diameter D. Such an apparatus also has a coaxial pair of spur gears that includes a large spur gear having a pitch diameter B and a small spur gear having a pitch diameter C. The large spur gear meshes with the large ring gear and the small spur gear meshes with the small ring gear, forming two meshing pairs. A carrier member is connected to one of the input and output shafts of the apparatus. Two gears of one of the two coaxial pairs are fixed together to operate epicyclically on the carrier. One gear of the other of the two coaxial pairs is fixed to the frame of the apparatus and the other gear is connected to the other of the input and output shafts. In such a system, the four gears satisfy the dimensional relationship of A=K+i, B=K, C=K−j and D=K+i−j.
The apparatus of
Note that the examples of
In summary, a speed changing apparatus of the present invention outlined in
As is comprehensible for those skilled in the art, the speed-reducing configurations in Table 1 can be easily changed into speed-increasing simply by swapping the I and O role assignment of each.
Speed reduction ratios listed in Tables 1 and 2 show that with gears having tooth numbers centered at a value of K (with i and j values reduced to 1), a speed reducer of a ratio of, at the optimized case, K2 can be constructed. This compares to the conventional cycloidal drive's reduction ratio of K.
Note, as is comprehensible, that a spur gear meshed inside a ring gear usually must have a tooth number sufficiently smaller than that of the ring. For example, with the popular 20-degree pressure angle gears, a minimum of 8-tooth difference is necessary. One typical approach to avoid gear interference for small tooth number difference is to employ profile shifting for the gears. Alternatively, with larger gear pressure angle, smaller tooth number difference without gear interference is possible.
Also, since the epicyclic elements of one coaxial pair of the speed-changing apparatus of the present invention is normally so large in size comparable to the other coaxial pair that only one pair is possible. A counterweight is therefore necessary in practical implementations of this inventive speed-changing apparatus, as is schematically illustrated as counterweight 65W in the embodiment depicted in
A speed changing apparatus of the present invention outlined in
The strain wave gearing-based speed-reducing configurations in Table 3 can be easily changed into speed-increasing simply by swapping the I and O role assignment of each.
An optimized version of the apparatus of FIG. 4A—though not illustrated in the drawings but based on the same principle as that of the gearing version described in
Essentially similar to the case in the embodiment of
Further, the two coaxial flex splines 182 and 183 are fixed together to each other to operate flexingly on the wave generator 185E. The first circular spline 181, in this depicted example of
In this spline-based gear train system, the four splines 181, 182, 183 and 184 satisfy the tooth number relationship of TA=TK+Ti, TB=TK, TC=TK−Tj and TD=TK+Ti−Tj wherein TK is tooth number of the first flex spline 182, Ti is the difference between tooth numbers of first circular spline 181 and first flex spline 182 (and also the difference between tooth numbers of second circular spline 184 and second flex spline 183), and Tj is the difference between tooth numbers of first circular spline 181 and second circular spline 184 (and also the difference between tooth numbers of first flex spline 182 and second flex spline 183).
Compared to the conventional gearing implementations, dimensional configuration of the strain wave gearing implementation of the speed changing apparatus of the present invention, as described above, is required to satisfied a relationship among its four spline elements expressed in terms of spline tooth numbers. Pitch diameters are not used as in the case of the conventional gearing implementation because, while the two circular splines have definite pitch diameters, the two flex splines do not—their mechanical force transmitting engagement circle flexes all the time when operating. Though, regardless of whether it is the convention gearing or strain wave gearing implementation, the dimensional discrepancy parameters, i and j in the case of conventional gearing and Ti and Tj for strain wave gearing, must be made as small as possible if large speed changing ratio is desired.
The strain wave gearing speed changing apparatus of
Also note that the double flex spline construction 188 of
Note that to allow the two flex splines to have equal spline tooth engagement pitch circle circumference length, their “effective module,” the equivalent to the module number for conventional gears, must be different from each other due to their different spline tooth numbers. This does not cause problem in practical implementations because splines are much easier to make than gears.
As an example, take the exemplified 400-to-1 reduction ratio apparatus of
For the second engagement pair shown in
For this example the meshing distribution can be arranged in perfect symmetry that the rotary component, namely, the two flex splines 182 and 183 shaped by the wave generator 185E can be well balanced all the time as the system operates. There is no issue of center of mass.
As another example, assume the apparatus of
For the second engagement pair in
For this example the meshing distribution can not be arranged in perfect symmetry that the rotary component, namely, the two flex splines 182 and 183 shaped by the wave generator 185E can be well balanced all the time as the system operates. However, the center of mass of the wave generator can be easily corrected as the deviation is small.
Note, however, that while more meshing points allow for increase capacity, yet if only one single meshing is used, the flexing of the flexing splines can, substantially, be avoided. In this extreme case of configuration, the service life of the speed changing apparatus can be optimized, with the sacrifice of power capacity of course.
While the above is a full description of the specific embodiments, various modifications, alternative constructions and equivalents may be used. Therefore, the above description and illustrations should not be taken as limiting the scope of the present invention.
This application is a Continuation-in-Part of U.S. patent application Ser. No. 13/289,477 filed Nov. 4, 2011, which claims benefit of U.S. Provisional Application Ser. No. 61/410,245 filed Nov. 4, 2010, the disclosure which is hereby incorporated by reference in its entirety.
Number | Date | Country | |
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61410245 | Nov 2010 | US |
Number | Date | Country | |
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Parent | 13289477 | Nov 2011 | US |
Child | 14457523 | US |