Wave gear device having tapered flexible external gear
09534681 ยท 2017-01-03
Assignee
Inventors
Cpc classification
F16H2049/003
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y10T74/19647
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16H55/0833
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
With a wave gear device, the gears employ homothetic curve tooth profiles AD, BE. Furthermore, a transposition is applied to the external teeth along the tooth trace such that the movement loci M.sub.2, M.sub.3 of the external teeth in a section perpendicular to the axis, from the aperture end to the inner end, share the movement locus M.sub.1 of the aperture end and bottom portion thereof, and a continuous meshing of the teeth in the tooth trace direction is achieved. Furthermore, the tooth bottom rim thickness of the aperture end of the external teeth is optimized using a modified Goodman diagram, and a tooth bottom rim thickness which takes into account the relationship between the tooth profile and the transmitted torque from the aperture end to the inner end is employed for the flexible external gear.
Claims
1. A wave gear device, comprising: a rigid internal gear of annular shape; a flexible external gear disposed coaxially to an inside thereof; and a wave generator fitted to an inside thereof; the flexible external gear being provided with a flexible cylindrical barrel part, a diaphragm radially extending from a rear end of the cylindrical barrel part, and external teeth formed on an outside peripheral surface part at a front end opening side of the cylindrical barrel part; the external teeth of the flexible external gear being flexed into ellipsoidal shape by the wave generator, and meshing with internal teeth of the rigid internal gear at both ends in a major axis direction of an ellipsoidal curve thereof; the external teeth of the flexible external gear flexed into ellipsoidal shape having increasing amounts of flexure, substantially proportional to a distance from the diaphragm, from a diaphragm side towards a front end opening side along a tooth trace direction thereof; the external teeth of the flexible external gear and the internal teeth of the rigid internal gear both being spur gears of module m; a number of teeth of the flexible external gear being set to 2n fewer than a number of teeth of the rigid internal gear, where n is a positive integer; in an axis-perpendicular cross section at any location in the tooth trace direction of the external gear, an amount of flexure in a radial direction by the external teeth at a major axis location in an ellipsoidal rim neutral line, with respect to a rim neutral line prior to flexure of the external teeth into ellipsoidal shape, being 2 mn, where is a flexural coefficient; the flexural coefficient of an opening end cross section being =1 when, in the tooth trace direction of the external teeth of the flexible external gear, an axis-perpendicular cross section at an end on the front end opening side is designated as an opening end cross section, and an axis-perpendicular cross section at an end on the diaphragm side as an inner end cross section; an opening end tooth profile shape in the opening end cross section of the external teeth being defined by an external tooth addendum tooth profile section of convex curving shape, an external tooth linear tooth profile section continuous therewith, an external tooth deddendum tooth profile section of concave curving shape continuous therewith, and an external tooth root section continuous therewith; a tooth profile shape of a section of the external teeth extending from the opening end cross section to the inner end cross section being a shifted tooth profile shape in which minus tooth profile shifting is applied to the opening end tooth profile shape, in order to avoid interference with the internal teeth; a tooth profile shape of the internal teeth in an axis-perpendicular cross section being defined by an internal tooth addendum tooth profile section of convex curving shape, an internal tooth linear tooth profile section continuous therewith, an internal tooth deddendum tooth profile section of concave curving shape continuous therewith, and an internal tooth root section continuous therewith; meshing of the external teeth and the internal teeth being approximated by rack meshing, and movement loci of the external teeth of the flexible external gear with respect to the internal teeth of the rigid internal gear in association with rotation of the wave generator being derived in axis-perpendicular cross sections taken in the tooth trace direction of the external teeth; a first homothetic curve (BC) being derived by homothetic transformation by a ratio at a homothetic center at a point (B), the homothetic ratio being <1, of a curve segment (AB) extending from a point (A) of an apical portion in the movement locus (M.sub.1) obtained in the opening end cross section, to the point (B) in a next bottom portion; a second homothetic curve (CA) being derived through homothetic transformation, by a ratio (1)/ at a homothetic center at an end point (C), of a curve (BC) obtained by rotating the first homothetic curve (BC) by 180 degrees about the end point (C) of the first homothetic curve (BC); a straight line (L) being drawn to intersect the curve (CA) at a pressure angle , and a curve segment (AD) being derived between the end point (A) of the curve (CA) and an intersection point (D) with the straight line (L); the external tooth addendum tooth profile section being defined by the curve segment (AD); the external tooth linear tooth profile section being defined by a linear segment extending from the intersection point (D) in the straight line (L); the external tooth deddendum tooth profile section being defined by a concave curve connecting the external tooth linear tooth profile section and the external tooth root section which is defined by a predetermined external tooth root curve, so as to ensure a predetermined radial clearance of the external tooth linear tooth profile section with respect to the internal teeth; a straight line (L) being drawn to intersect the first homothetic curve (BC) at the pressure angle , and a curve segment (BE) being derived between the end point (B) in the first homothetic curve (BC) and an intersection point (E) with the straight line (L); the internal tooth addendum tooth profile being defined by the curve segment (BE); the internal tooth linear tooth profile section being defined by a linear segment extending from the intersection point (C) in the straight line (L); on a same plane, a straight line being drawn to connect a point (A) at which a fatigue limit of alternating stress of steel constituting a material of the flexible external gear is plotted on a vertical axis, and a point (B) at which a central value of yield stress and tensile strength of the steel is plotted on a horizontal axis, to create a modified Goodman diagram; root rim thickness t.sub.m of the opening end cross section of the flexible external gear being determined in such a way that the location of the coordinate points obtained by plotting, on the vertical axis, of stress amplitude expressed as the sum of bending stress produced by flexure on the major axis appearing on the surface of the root rim at the opening end of the flexible external gear in association with ellipsoidal deformation thereof and of the tensile stress arising at the root rim due to load torque, and plotting, on the horizontal axis, of the average stress of of the tensile stress, lies on the midpoint (M) of the line segment (AC) obtained by designating as (C) the intersection point of the straight line (AB) and the straight line passing through the origin at 45 degree angle to the horizontal axis in the modified Goodman diagram; and at individual locations from the opening end to the inner end of the external teeth, root rim thickness in each axis-perpendicular cross section being determined in such a way that the location of coordinate points obtained by plotting, on the vertical axis, of stress amplitude expressed as the sum of bending stress produced by flexure and the tensile stress arising at the root rim at the location in question due to transmission load torque, and plotting, on the horizontal axis, of the average stress of of the tensile stress in question, lies to the right side of the midpoint (M) on the modified Goodman diagram.
2. The wave gear device according to claim 1, wherein the root rim thickness t in axis-perpendicular cross sections taken at locations from the opening end to the inner end of the external teeth is t=t.sub.m.
3. The wave gear device according to claim 1, wherein the shifted tooth profile shape of the section from the opening end cross section to the inner end cross section in the external teeth is one to which minus tooth profile shifting is applied to the opening end tooth profile shape, in such a way that the movement locus obtained in individual axis-perpendicular cross sections from the opening end cross section to the inner end cross section contacts the movement locus obtained in the opening end cross section, at a point in bottom portions thereof.
4. The wave gear device according to claim 2, wherein the shifted tooth profile shape of the section from the opening end cross section to the inner end cross section in the external teeth is one to which minus tooth profile shifting is applied to the opening end tooth profile shape, in such a way that the movement locus obtained in individual axis-perpendicular cross sections from the opening end cross section to the inner end cross section contacts the movement locus obtained in the opening end cross section, at a point in bottom portions thereof.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
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MODE FOR CARRYING OUT THE INVENTION
(12) A wave gear device in which the present invention is applied will be described below, making reference to the drawings.
(13) (Constitution of Wave Gear Device)
(14)
(15) As shown in these drawings, the wave gear device 1 has a ring-shaped rigid internal gear 2, a flexible external gear 3 disposed to the inside thereof, and a wave generator 4 of ellipsoidal contours fitting inside thereof. The rigid internal gear 2 and the flexible external gear 3 are both spur gears of module m. The difference in number of teeth between the two gears is 2n (n is a positive integer), with the rigid internal gear 2 having the greater number. The flexible external gear 3 is flexed into ellipsoidal shape by the wave generator 4 of ellipsoidal contours, and meshes with the rigid internal gear 2 in sections at either end of the ellipsoidal shape in the major axis L1 direction. As the wave generator 4 rotates, the locations at which the two gears 2, 3 mesh move in a circumferential direction, generating between the two gears 2, 3 relative rotation according to the difference in number of teeth between the two gears. The flexible external gear 3 is provided with a flexible cylindrical barrel part 31, a diaphragm 32 continuing on from the rear end 31b thereof and spreading out in a radial direction, a boss 33 continuing on from the diaphragm 32, and external teeth 34 formed on an outside peripheral surface section at an opening 31a side of the cylindrical barrel part 31.
(16) Due to the wave generator 4 of ellipsoidal contours fitting within an inside peripheral surface section of the external tooth formation section of the cylindrical barrel part 31, the cylindrical barrel part 31 experiences a progressively increasing amount of flexure towards the outside or towards the inside in a radial direction, towards the opening end 31a from a rear end 31b on the diaphragm side. As shown in
(17) (Tooth Profile Shape of Both Gears)
(18)
(19) As shown in
(20) (Method of Forming Tooth Profiles of Both Gears)
(21) Next, the method of forming the tooth profiles of the external teeth 34 and the internal teeth 24 will be described making reference to
(22) (Movement Loci of Teeth Through Rack Approximation)
(23)
x=0.5 mn( sin )
y=mn cos
(24) Assuming, for simplicity of description, that m=1 and n=1 (the tooth count differential is 2), the movement locus is as described by the following equation.
x=0.5( sin )
y= cos
(25) The origin of the y axis in
(26) (Method of Forming Tooth Profile in Principal Cross Section)
(27)
(28) The first homothetic curve BC is then rotated by 180 degrees about the end point C of the first homothetic curve BC, to obtain a curve BC. A second homothetic curve AC is obtained through transformation of this curve BC at a ratio (1)/ at a homothetic center at the end point C. The second homothetic curve AC is adopted as the tooth profile curve employed for defining the addendum tooth profile of the flexible external gear 3.
(29) The tooth profile curves for defining these addendum tooth profiles are expressed by the following equations.
(30) Basic equation for addendum tooth profile of rigid internal gear:
x.sub.Ca=0.5{(1)+(sin )}
y.sub.Ca=(1+cos )} (0)
(31) Basic equation for addendum tooth profile of flexible external gear:
x.sub.Fa=0.5(1)(+sin )}
y.sub.Fa=(1)(1+cos )} (0)
(Tooth Profile Shape of Principal Cross Section of External Teeth)
(32) The tooth profile curve AC for defining the addendum tooth profile, derived in the aforedescribed manner, is employed in forming an external tooth tooth profile in the principal cross section (an axis-perpendicular cross section of the opening end 34a) of the external teeth 34 in the following manner. To describe with reference to
(33) (Tooth Profile Shape of Internal Teeth)
(34) Likewise, the tooth profile curve BC employed for defining the addendum tooth profile is employed to form the tooth profile of the internal teeth 24. To describe with reference to
(35) The tooth profile sections 43, 44, 53, 54 of the deddendums of the two gears do not participate in meshing. Consequently, these dedendum tooth profile sections 43, 44, 53, 54 can be designed freely, provided that there is no interference with the respective corresponding addendum tooth profile sections 51, 52, 41, 42.
(36) In this way, tooth profile shapes are formed at locations of principal cross sections (axis-perpendicular cross sections of the opening end 34a of the external teeth 34) in both of the gears 2, 3 shown in
(37) (Tooth Profile Shape at Locations Other than Principal Cross Section in External Teeth)
(38) With regard to meshing of the tooth profiles of the principal cross section established in the aforedescribed manner, during intermeshing of the addendum tooth profiles of the two gears 2, 3, when the flexible external gear 3 moves along the standard deflecting movement locus M.sub.1 shown in
(39) Accordingly, a shifted tooth profile in which a tooth profile shifting is applied to the tooth profile of the principal cross section (the axis-perpendicular cross section of the opening end 34a) is adopted as the external tooth tooth profile of axis-perpendicular cross sections in a section extending from the opening end 34a to the inner end 34b in the external teeth 34. Specifically, the shifted tooth profile shapes are obtained by applying minus tooth profile shifting to the external-tooth tooth profile of the opening end 34a, doing in such a way that movement loci obtained through rack approximation of the external teeth 34 with respect to the internal teeth 24 in axis-perpendicular cross sections from the opening end 34a to the inner end 34b contact the bottom portion B of the movement locus M.sub.1 obtained at the opening end 34a constituting the principal cross section location. In so doing, proper meshing in at least localized fashion can be ensured on all cross sections in the tooth trace direction of the external teeth 34.
(40) To discuss in more specific terms, in each of axis-perpendicular cross sections taken towards the location of the inner end 34b on the diaphragm side from the opening end 34a of the external teeth 34, an amount of addendum modification mnh is established according to the flexural coefficient at each of the axis-perpendicular cross section locations, doing so in such a way that the movement locus in each axis-perpendicular cross section contacts the bottom part B of the movement locus M.sub.1 at the opening end 34a. In a case in which m=1 and n=1, the amount of addendum modification (tooth profile shifting) is h, and assumes a negative value represented by the following expression.
h=1
(41) Through application of tooth profile shifting in this manner, the root rim thickness t in each axis-perpendicular cross section in the tooth trace direction of the external teeth 34 is
t=t.sub.1
(42) Here, t.sub.1: root rim thickness in principal cross section (axis-perpendicular cross section at the opening end).
(43) (Method of Establishing Root Rim Thickness of External Teeth and Amount of Addendum Modification of Teeth)
(44)
.sub.b=3Et/(RD)
(45) Here, E: Young's modulus t: root rim thickness R: reduction ratio D: diameter of rim neutral circle prior to deformation
(46) Additionally, where .sub.n is the tensile stress arising on the major axis due to output torque T, the surface area of the root receiving the load is DL, and therefore .sub.n is defined by the following expression.
.sub.n=T/(DLt)
(47) Here, L: tooth width of flexible external gear
(48) Consequently, the stress arising on the major axis of the flexible external gear 3 is the sum of .sub.b and .sub.n, and the stress arising at the root rim surface on the minor axis of the flexible external gear 3 is compressive stress .sub.b. Thus, stress amplitude of the flexible external gear 3 arising due to rotation of the wave generator 4 is:
((.sub.b+.sub.n)(.sub.b))/2=.sub.b+.sub.n/2
(49) and average stress is:
((.sub.b+.sub.n)+(.sub.b))/2=.sub.n/2,
(50) On the same plane, a straight line is drawn connecting a point A (the vertical coordinate of which is .sub.A) at which the substantial fatigue limit of alternating stress of the steel constituting the material of the flexible external gear 3 is plotted on the vertical axis, and a point B (the horizontal coordinate of which is .sub.B) at which the center of yield stress and tensile strength of the steel is plotted on the horizontal axis, to create a so-called modified Goodman diagram. The triangular area bounded by this straight line, the horizontal axis, and the vertical axis is the permissible range of points produced by plotting the average stress of the root rim surface of the flexible external gear 3 on the horizontal axis, and the stress amplitude thereof on the vertical axis.
(51) Here, in a case in which an ellipsoidal rim neutral curve of the flexible external gear 3 is given, a point P is derived by plotting, on the vertical axis, of the stress amplitude (.sub.b+.sub.n/2) appearing at the root rim surface in the principal cross section (the axis-perpendicular cross section at the opening end 34a) arising due to rotation of the wave generator 4, and plotting, on the horizontal axis, of the average stress .sub.n/2. In the first instance, it is necessary for this point P to be included within the aforedescribed triangular area.
(52) At this time, the transmission load torque T transmitted by the flexible external gear 3 is proportional to the product of the root rim thickness t and the tensile stress .sub.n. The root rim thickness t is proportional to the tensile stress .sub.b in association with bending. Consequently, the torque T of the flexible external gear is proportional to the product of the tensile stress .sub.b and the tensile stress .sub.n. Here, .sub.b is represented by a line segment PQ, where Q designates the intersection point of a straight line parallel to the vertical axis and passing through point P, and a straight line forming a 45 degree angle to the horizontal axis and passing through the origin. From the above, the torque T is proportional to the area of an oblong shape bounded by straight lines parallel to the horizontal axis and passing respectively through point P and point Q to the vertical axis, and the line segment PQ.
(53) Consequently, the point at which the torque transmitted by the flexible external gear 3 of given specifications reaches maximum is the midpoint M of a line segment AC, where C is the intersection point of the modified Goodman diagram and a straight line passing through the origin and forming a 45 angle to the horizontal axis, and the root rim thickness corresponding to the midpoint M is the optimal value. Consequently, in this case, from the geometric relationships in the diagram:
.sub.b=.sub.A/2
.sub.n=.sub.A.sub.B/(.sub.A+.sub.B)
(54) The optimal value t.sub.m of root rim thickness t.sub.1 in the principal cross section (location of the opening end 34a) of the external teeth is given by the following expression.
t.sub.1=t.sub.m=.sub.ARD/(6E)
(55) As stated above, when minus tooth profile shifting is applied to the external teeth 34, and the root rim thickness thereof is designated as the root rim thickness t.sub.1 at the location of the opening end 34a in the tooth trace direction of the external teeth 34, the root rim thickness at locations other than the opening end 34a is t.sub.1. Consequently, when the root rim thickness t.sub.1 at the opening end 34a is set to the optimal rim thickness t.sub.m in the aforedescribed manner, the root rim thickness t in each of axis-perpendicular cross sections taken from the opening end 34a to the inner end 34b of the external teeth 34 is set to t.sub.m.
(56) In other words, the rim thickness of the flexible external gear is determined in such a fashion as to take progressively smaller values, in such a way that points corresponding to root rim thickness of axis-perpendicular cross sections lying in the tooth trace direction from the opening end 34a to the inner end 34b of the external teeth 34 are plotted to the right side of the midpoint M in the modified Goodman diagram. During this process, it is necessary for the coordinate points representing stress amplitude and average stress on the modified Goodman diagram to lie within the permissible range mentioned earlier.
(57) In the present invention, as shown below, the condition in question is met, and the coordinate points of the modified Goodman diagram representing the stress state of the flexible external gear 3 lie in the triangular area constituting the permissible range in the diagram in question.
(58) Specifically, with regard to the root rim thickness of axis-perpendicular cross sections from the opening end 34a to the inner end 34b, when the root rim thickness of the opening end 34a of the flexible external gear has been assigned the optimal value t.sub.m, in order to sustain meshing of the tooth profiles along the tooth trace, the root rim thickness is set to t.sub.m, which is equivalent to applying tooth profile shifting of a coefficient 1 (<1) to the teeth, doing so in such a way that the bottom portions of the movement loci of the external teeth 34 of the flexible external gear 3 to the internal teeth 24 of the rigid internal gear 2 in each of the axis-perpendicular cross sections are made congruent. At this time, according to the decrease in the rim thickness, the tensile stress of the rim at any location increases in the manner .sub.nm/, with respect to the tensile stress .sub.nm of the opening end 34a due to torque.
(59) Meanwhile, bending stress .sub.b arising on the major axis in any cross section of the flexible external gear is proportional to the product of the rim thickness t.sub.m and the amount of flexure w. Where the value of bending stress with respect to t.sub.m is designated as .sub.bm,
.sub.b=.sup.2.sub.bm=.sup.2.sub.A/2.
From the equation for a straight line, the vertical coordinate corresponding to the horizontal coordinate of average stress .sub.nm//2 on the modified Goodman diagram is:
(.sub.A/.sub.B)/.sub.nm/2/+.sub.A
Here, employing the relationship .sub.bm=.sub.A/2, in the axis-perpendicular cross section of the opening end 34a, from the relationship:
(.sub.B.sub.nm/2)(.sub.A/.sub.B)=.sub.bm+.sub.nm/2=.sub.A/2+.sub.nm/2
the following result is obtained.
.sub.nm=.sub.A.sub.B/(.sub.A+.sub.B)
(60) Consequently, the vertical coordinate of a modified Goodman straight line corresponding to the average stress .sub.nm//2 of a cross section of coordinate is given by the following expression.
(61)
(62) In contrast to this, the stress amplitude of a cross section of coordinate is:
(63)
(64) The difference of the two is:
(65)
and this value is positive with respect to the range of actual values of (in the present example, from 1 to 0.7), thereby showing that the coordinate values with respect to the rim thickness t lie within the permissible range.
(State of Meshing of Teeth)
(66)
(67) Next,