Keywords

1.1 Introduction

During the second half of the 20th century, Soviet scientists were among the world leaders in the gear geometry and applied theory, that are the theoretical fundamentals of designing gears and gear-cutting tools.

The authors of the current paper have considered works related to the development of the theory of gearing (TG) published in Russia from the mid-1930s to the present. Overall, the review covers more than 400 publications of nearly 200 authors (among more than 1000 studied works).

The first part of this review was published under name “Russian school of the theory and geometry of gearing: Its origin and golden period (1935–1975)” in J. Front. Mech. Eng. Higher Education Press and Springer-Verlag Berlin Heidelberg, 2016, 11(1), pp. 44–59. Having examined 165 publications of more than 70 researchers, the authors talked about the authoritative scientific schools that emerged and worked actively during this period in Leningrad, Moscow, Saratov, Novocherkassk, Gorky, Kurgan, Izhevsk. The main scientific and practical achievements of these schools were considered. Among them:

  • the kinematic, matrix and other methods of analysis and synthesis of gearing,

  • the technological synthesis of spiral bevel and hypoid gears.

  • the mastering of new types of gears, including the W-N gears, globoid and spiroid gears etc.

The present, second part relates on development of Russian school of the theory of gearing in 1976–2000 years. This period has a number of features provided by historical reasons. First, the USSR industry revealed the first obvious symptoms of stagnation at the late 1970s. Second, the number of post-graduates decreased, since universities generally solved the problem of teaching stuff that was urgent in the early 1960s because of the abrupt increase of the number of engineer students.

However, within these hard 15–20 years preceding the USSR breakup, certain old scientific schools continued functioning in the Soviet Union and new centers developing the theory and practice of gearing arose.

The list of publication involves the most profound works of the leading scientists and the most original works of less famous experts with the advanced ideas and results. To make this review interesting for a wide audience, it involves a certain number of works on designing tools, on gear strength and accuracy.

1.2 Review of Works Published in Russian in 1976–2000

By the mid 1970s the theory of gearing as an individual science has reached its completeness: basic and priority problems of gearing analysis and synthesis have been solved. The number of novel theoretical works has declined. The structure of scientific theses has been mainly unified: construction of design formulas for a specific gearing  algorithmization  computer-aided analysis  production  experiment  implementation certificates. Investigations came closer to the production; and the theory of gearing became, first of all, the tooling for solving specific engineering problems.

The main results of the review of works dated the last quarter of the 20th century [1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20,21,22,23,24,25,26,27,28,29,30,31,32,33,34,35,36,37,38,39,40,41,42,43,44,45,46,47,48,49,50,51,52,53,54,55,56,57,58,59,60,61,62,63,64,65,66,67,68,69,70,71,72,73,74,75,76,77,78,79,80,81,82,83,84,85,86,87,88,89,90,91,92,93,94,95,96,97,98,99,100,101,102,103,104,105,106,107,108,109,110,111,112,113,114,115,116,117,118,119,120,121,122,123,124,125,126,127,128,129,130,131,132,133,134,135,136,137,138,139,140,141,142,143,144,145,146,147,148,149,150,151,152,153,154,155,156,157,158,159,160,161,162,163,164,165,166,167,168,169,170,171,172,173,174,175,176,177,178,179,180,181,182,183,184,185,186,187,188,189,190,191,192,193,194,195,196,197,198,199,200,201,202,203,204,205,206,207,208,209,210,211,212,213,214,215,216,217,218,219,220,221,222,223,224,225,226,227] are introduced in two tables. The table in Fig. 1.1 represents 5 groups including 26 scientific problems that comprised the main results of theoretical investigations. The table in Fig. 1.2 enumerates 30 types of gears, mechanisms and their parts, and also 3 areas of activity that implement the practical results of works in 1976–2000.

Fig. 1.1
figure 1

Theoretical developments in the period 1976–2000

Fig. 1.2
figure 2

Practical results in the period 1976–2000

Each of the tables contains: (a) names of the solved problems (investigated objects, spheres of their application), (b) family names of main authors who solved these problems (with indication of the work number in the reference list and publication date), (c) connection lines that relate the authors and their solved problems. Family names of the authors who contributed most to the theory of gearing (to our opinion) and the most essential works are highlighted in bold in the tables. The tables allow for tracking:

  • themes that are considered to be the most popular and important at that time;

  • researchers working on the theme of your interest;

  • issues considered by the researchers and the scope of the subject matter for each of them.

The tables cover both directions of development of the theory of gearing: “world-wide”—IGD, and “Russian”—theory of real gearing. Features of the “Russian” direction is mainly considered. As far as the “world-wide” direction is concerned, it comprises the following technique for solving the problems of analysis and synthesis for in Russia and abroad:

  • methods of the classical theory of gearing (at computer-aided design of geometry of any type of gears);

  • non-differential methods of analysis of gear generating processes when implementing both versatile and special applied software,

  • numerical methods of optimization (at synthesis of geometry of tooth operating flanks and transient surfaces);

  • the expanded list of quality features of gearing which includes the criteria for assessing the terms of oil wedge generation and other;

  • methods of boundary and finite elements at analysis of contact interaction of work surfaces and of the tooth deformation mode;

Let us consider the features of the “Russian” approach in four paragraphs:

  1. 2.1.

    new geometric concepts in the theory of gearing;

  2. 2.2.

    development of methods of optimization synthesis;

  3. 2.3.

    development of methods of generating process analysis;

  4. 2.4.

    software: features of development and implementation.

1.2.1 New Geometric and Geometry and Kinematic Concepts

The crucial contribution to the development of the theory of gearing after 1970s was the introduction and application of new concepts:

(1) covering surface (Sheveleva [180]); (2) fan, wedge, bunch of normal lines (Babichev [14]); (3) feeding-in acceleration [121]; (4) space of meshing (Lagutin [108]); Let us consider these innovations.

1.2.1.1 Enveloping and Covering Surfaces

In the theory of surface generation by moving solids two following types of the obtained surfaces should be distinguished: undulated covering line Σ1 and smooth enveloping line Σ2—see Fig. 1.3.

Fig. 1.3
figure 3

Covering Σ1 and enveloping surface Σ2 of the generating surface Σ0

The covering surface Σ1 is the set of a discrete family of fragments of basic tool surfaces (BTS); the enveloping surface Σ2 is the surface contacting all elements of this discrete set. The enveloping surface Σ2 is usually a smooth surface, while the covering surface Σ1 is always the faceted surface. The concept “covering” was proposed by G. I. Sheveleva and effectively applied at study of bevel and hypoid gears [180]. Note, that the term “covering” is not perfect when translated into English. In practice it means a real, wavy or rough surface.

The surface Σ2 is usually determined as the enveloping for one- or two-parametric family of generating surfaces. The covering surface Σ1 is determined by direct tracking of the position of points of the generating surface Σ0 with respect to the blank; it is the method of direct digital modeling (DDM) sometimes called the “method of direct enveloping”. Methods of DDM are more reliable than kinematic ones, so it is preferable to determine the covering surface Σ1 rather than the enveloping surface Σ2 in many CAD and CAE systems. Although, in order to determine Σ1 it is required to perform hundreds of calculations more than for Σ2.

Note, that covering surfaces Σ1can consist of stripes (bands), for instance, at line grinding of teeth—see Fig. 1.4, each of the “bands” is the surface obtained by enveloping process (line A is the contact line at one-parametric enveloping). Each stripe is contacting the two-parametric Σ2 enveloping surface along the line (this line passes along the stripe). When the feed is reduced, the “bands” become narrower. When the feed value tends to zero, the generated surface will be approaching the enveloping surface of a family of “bands”. It will be exactly the surface Σ2 generated by two-parametric enveloping by the surface Σ0.

Fig. 1.4
figure 4

The band type of roughnesses

The covering Σ1 can consist of individual “flakes”, for example, when cutting the gearwheels by module hobs or diagonal gear grinding. Figure 1.5 shows the deviations of the flake covering surface Σ1 from the enveloping Σ2. “Flakes” are contacting with Σ2 at the centre of the flake. The shape of “flakes” is in general case hexagonal that can degenerate into parallelogram.

Fig. 1.5
figure 5

The shape of roughness is hexagonal “flakes”

The curvature of band and flake covering surfaces Σ1 crucially and essentially differs from the curvature of the enveloping surface Σ2. Thus, the radius of curvature for the involute is smoothly increasing from its base circle. And the radius of curvature for the covering surface generated by the rectilinear rack is ρ = ∞ at all points (and at jogs it is ρ = 0), since the covering profile is the broken line contacting the involute by each of its rectilinear segments.

Using of the concept of the covering surface instead of the enveloping one creates a number of difficulties when solving the contact problem by numerical methods: errors of strains and contact stress analysis increase, boundaries of instant contact areas lose their smoothness. The common means of “approaching” the covering surface with the enveloping one is the issue of small feeds at computer-aided modeling of the generating process. It reduces the roughness of the surface obtained at modeling and decreases the errors at solving the contact problem. But it does not solve the problem of analysis of the enveloping curvature, since the curvature of the covering surface does not depend on the feed value.

1.2.1.2 Jogs on Tooth Profiles and Flanks

Jogs (lines of surface intersection or points of profile intersection) are present practically on all gear parts and tools. The concept of jogs as of specific features of generating surfaces comes from Rodin [161]. He wrote: «the surface of a part consisting of a number of adjacent areas can be considered as a single surface. The point of jog of the profile located at the boundary of adjacent areas can be considered as an arc of a circumference with the radius tending to zero». Figure 1.6 (left) shows three possible types of jogs which give rise to three types of normal lines families: a fan (at intersection of two profiles), a wedge (at intersection of two surfaces) and a bunch (at intersection of three surfaces). Figure 1.6 (right) specifies, why the point B at the jog of the rack is the contacting one, that is, it lies on the generated transient curve of the tooth fillet; and the point C does not belong to the transient curve. The reason is that one of the normals of the fan at the point B passes through the pitch point, while there is no such a normal line at the fan of the jog C. Note, that the classic theory of gearing does not answer the question why the point B is the contact one and the point C is not. Terms “fan, wedge, bunch” have been later replaced by terms “sector, prism, pyramid” – see chap. 6 by Babichev and Barmina in this book.

Fig. 1.6
figure 6

Types of jogs and contact at the point B

Figure 1.7 shows that the jog and its adjacent segments of surfaces are the single surface with the continuous curvilinear coordinate v. In this figure: 1 is v-line; 2 are brushes of normal lines; 3 is fan of normal lines; nA, nB are main unit vectors. Publications [12,13,14,15,16,17,18,19] are devoted to the development of the kinematic method for investigation of generating processes with higher reliability as compared to the classic method. It applies both jogs and curvilinear coordinates that are single for the whole tooth or the gear rim (and even along the whole BTS for all edge tools: hobs, mills, broaches, shavers [13]—see Fig. 1.8).

Fig. 1.7
figure 7

Parameters of the edge jog: 1—v-line; 2—brushes of normal lines;

3—fan of normal lines;

nA, nB—main unit vectors of the fan of normal lines

Fig. 1.8
figure 8

Curvilinear coordinates on the real BTS for hobs and broaches

Figure 1.8 shows several neighboring teeth of the edge tool with pointing the curvilinear coordinates u (along the cutting edge) and v (across it). The coordinate v is related here with the tooth number i.

From physical point of view, the real BTS is the set of cutting edges with adjoining front and back planes (surfaces). From mathematical point of view, the real BTS is the smooth surface with two continuous curvilinear coordinates on it.

For the real BTS we should know all information related to the geometry that influences the generating and cutting processes. Computational models for such tools are to be found in [17].

Summary: jogs are the useful means when analyzing the generation processes.

1.2.1.3 Feeding-in Parameters of the Generating Surface to the Solid of the Generated Part: Velocities and Acceleration of Feeding-in, etc.

One of the main issues of the theory of gearing is to determine the tooth surface Σ2 of the second element when knowing the tooth surface Σ1 of the first element. When solving this problem one should consider the motion of the surface of the first element solid in the coordinate system of the second one, that is, in the three-dimensional space of the second element (Cartesian). It is logical to assume that the motion parameters of the solid 1 surface in the space of the solid 2 should be used. However, in classical theory of gearing there is no common system of concepts and characteristics specifying the interaction of the solid surface with the space. And in order to describe this interaction the parameters are used that specify the spatial motion of only the solid as the set of points rather than the solid limited by the surface. In order to eliminate the misunderstanding of the essence of the said above, let us explain the difference of any point A of the solid from the point K lying on surface Σ1 of this solid. At the point K there is the normal line to the solid surface Σ1 (and the tangent surface and curvature parameters), while at the point A (inside the solid) there is nothing similar to it. For the generation process of the solid surface Σ2 of the second element it is important to know the motion in space of the second element of points of the surface Σ1 projected on its normal N at these points. V. A. Shishkov paid attention on it at the end of 1940s, proposed the local parameter of interaction of the solid surface with the space and called it the “velocity of feeding-in”. It is obtained as the scalar product:

$$ V_{\text{N}} = {\mathbf{V}}_{12}^{{}} \cdot {\mathbf{n}} = V_{12x}^{{}} \cdot n_{x} + V_{12y}^{{}} \cdot n_{y} + V_{12z}^{{}} \cdot n_{z} $$
(1.1)

where n is the unit vector of the normal N directed outwards from the solid 1, V12 is the vector of the relative velocity at this point: V12= V1–V2.

Velocity VN is also called the velocity of mutual approach (for VN > 0) and removal (for VN < 0). If VN = 0, surfaces Σ1 and Σ2 are contacting at this time instant and at this point. VN is the important but not the only parameter of feeding-in motion. Other parameters should be considered: acceleration of feeding-in aN, as the first time derivative of the velocity VN; and its higher time derivatives.

Applying VN and aN, it became possible to develop the generalized method of study of load for cutting edges of a wide range of enveloping gear cutting tools (hobs and grinding wheels) for rough and final machining. It also became possible to implement this method by the software that allowed for investigating the operation of a large group of different types of tools [120,121,122].

Let us show examples of investigations carried out by means of this software.

Figure 1.9 shows the example of investigating the cutting process for arch teeth of cylindrical gears by spiral disk mills proposed by M. L. Erikhov. On the left in this figure the cutting scheme is shown; on the right the boundaries of the cutting zone and thickness of the layers to be cut (in mm when the mill is fed along its axis S = 1 mm/rev) are shown. Parameters of the machine-tool meshing are: z = 20, m = 5, mill radius rm = 100 mm, the number of racks (chaser) k = 8, the ratio of angular velocities of the mill ω1 and the blank ω2 is equal to i12 = ω12 = z.

Fig. 1.9
figure 9

Scheme for cutting arch teeth and boundaries of the cut layer on the developed view of the cutting edge trace

Results of computer-aided modeling of spiral disk mills operation show that:

  1. (1)

    two teeth of each three-teeth chaser are constantly participating in cutting;

  2. (2)

    the most loaded teeth are the middle teeth of all chasers;

  3. (3)

    outer cutting edges of all chasers practically do not participate in operation;

  4. (4)

    the maximum thickness of the cut is at the top edge of the fifth rack, it is Smax = 0.35 mm since the cutting start;

  5. (5)

    the maximum thickness Smax of the cut layers in the course of the tool cutting-in is transmitted from the top and the transient segments to the lateral ones;

  6. (6)

    the double increase in the radius rm of the tool widens the cutting layer by 8%, but it practically does not influence the value of Smax;

  7. (7)

    the decrease in the number of chasers doubles the value of Smax;

  8. (8)

    the double decrease in the radial feed decreases the value of Smax in two times with simultaneous narrowing the cut by 30%.

Figure 1.10 shows the cutting scheme and cutting zone for face bevel teeth which applied as half-couplings in systems of control and as gearwheels in wave gears.

Fig. 1.10
figure 10

Scheme for cutting the face bevel teeth and boundaries of cutting zones: dotted line—computer-aided analysis; solid lines—wax model experiment

Flanks of face bevel teeth are the enveloping lines of a two-parametric family of lines (cutting edges of the disk hob in Fig. 1.10). These surfaces were investigated by Ya. S. Davydov, V. I. Bezrukov, L. Ya. Liburkin; their works are described in the first part of our review. But only in [158, 159] the problem was solved for determining the curvature radii of surfaces generated by two-parametric motion of the generating line. The difficulty of this problem solution is that the surface circumscribed by the cutting edge when running-in 1 (Fig. 1.10) is the “spiral surface on the bagel”. And the spiral pitch is decreased when the tool is approaching the axis of the blank rotation due to the feed motion. That is, the tooth surface on the item is the envelope of the single-parametric family of a “spiral surface on the bagel” deformed at motion (due to feed 2).

Further in Figs. 1.11, 1.12, and 1.13 the investigation results for cutting the spur involute gears by shaping cutters are shown. Note, that Figs. 1.11 and 1.12 are based on the concept of the feeding-in velocity (as by V. A. Shishkov). The role of the feeding-in acceleration aN is lower: to increase the computational accuracy for thicknesses of cuts and the boundaries of cutting zones (including the zones of secondary cutting) when analyzing the finishing passes of the tool.

Fig. 1.11
figure 11

Thicknesses of layers cut by the involute shaper with z0 = 20, x0 = 0.5 when cutting the gearwheels with z1 = 20 and x1 = 0

Fig. 1.12
figure 12

Cutting zones at machining of the gearwheel with internal teeth with z1 = 30 and x1 = 0.5 by the shaper with z0 = 20 and x0 = 0.5

Fig. 1.13
figure 13

Cutting zone and lines of equal thicknesses of cut layers for the finishing pass of the involute shaper

In planar meshing the following theorem allows for assessing the load of the tool:

Theorem

If the point of the tool profile is in the machining allowance, then the tool load is proportional to the moment developed by the normal line to the profile with respect to the pitch point (Fig. 1.13).

Figure 1.13 shows the example of the finishing gear shaping of the involute gearwheel. The cutting zone with the variable width is stretched along the meshing line (as the “oasis” along one river bank). When the direction of running-in is changed, the cutting zone (“oasis”) is transmitted to the other side of the meshing line (“river”) scarcely changing its width.

The velocity V of the material removal by abrasives and the thickness S of the cut layer are:

$$ V = \left( {\omega_{0} - \omega_{1} } \right) \cdot R_{\varSigma } $$
$$ {\text{S}} = S_{0} \cdot R_{\varSigma } \cdot \left| {\frac{{\omega_{0} - \omega_{1} }}{{V_{P} }}} \right| $$

where ω0 and ω1 are angular velocities of running-in motion for the tool and blank (ω > 0 when rotating counterclockwise); R is the arm of the normal line to the tool profile with respect to the pitch point P; VP is the circumferential velocity at centroids; S0 is the circumferential feed per lead.

Note: The point at the tool is work loaded if the profile normal line coming out of the tool solid creates the moment directed along the relative angular velocity ω0–ω1 with respect to pitch point P.

In accordance with the theorem, it is seen in Fig. 1.13 that the maximum thickness of the cut is S = 0.15·S0 (at the beginning of the tool operation).

When determining the thickness of the cut layers, it is rather difficult to find the boundaries of cutting zones, especially at finish gear machining. Acceleration of the cutting-in allowed for solving this problem (though approximately) even for such a complex process as gear hobbing by generating method. These issues are studied in details in the thesis by Langofer [120].

The issues considered above in p. 2.1.3 and shown in Figs. 1.9, 1.10, 1.11, 1.12, and 1.13 reveal only one of possible direction of applying the concepts of cutting-in parameters (velocity, acceleration and higher derivatives) for analysis of tool loading. But application of the concept “acceleration of cutting-in” simplifies the solution of other important problems of gear geometry. For instance, when aN> 0, the envelope is formed inside the solid of the generating element which is physically impossible. When determining Σ2, the value aN allows for simultaneously determining the radii of curvature and micro-roughness height along the whole surface formed by generating for the band-type and flaky shapes of roughnesses—see Fig. 1.4 above.

By means of the concept of the feeding-in acceleration the new formula has been obtained to analyze the reduced curvature at any normal section at the point of contact of two moving solids that are contacting along the line:

$$ \frac{1}{{R_{\varSigma } }} = - \frac{{\omega_{W}^{2} }}{{a_{N} }} $$

where ωW is the angular velocity of solids rolling on the plane of the section where the curvature is analyzed; The fundamental nature of this formula means that according to its generality it is commensurate with the known in geometry Rodrigues and Frenet formulas, but it is intended for surfaces developed in the process of their forming by generating methods.

1.2.1.4 Space of Meshing

This concept was introduced to the scientific circulation by Lagutin [108]. The term implies the physical space obtained at axes of gearwheels of the synthesized gear, each point of the space possessing its set of beams of the screw of relative motion (Fig. 1.14). By considering each of these beams as the probable contact normal and relating it to velocities of elements by vector equations, different isosurfaces can be singled out of this space, that is, the geometric loci for points at which the gear will possess specific properties: the assigned pressure angle, specific sliding etc. S. A. Lagutin proposed to apply such isosurfaces as boundaries of the area of gear existence and as potential surfaces of meshing.

Fig. 1.14
figure 14

Point and plane of contact normal lines in the space of meshing

Publication [108] enriches and makes more profound the investigation results on synthesis of gears with helical motion of elements [91], on determining analogs of meshing axes in general-type worm gears [89], on gear synthesis by method of loci [90] that were obtained together with L. V. Korostelev and his followers.

Later, the author performed the synthesis of general-type worm gears by means of the meshing space [110, 119] and was looking for equivalent settings for cutting bevel gears with circular teeth. We suppose that the significance of the analysis of meshing space at gear synthesis will be increased in time.

1.2.2 Development of Methods for Synthesis and Optimization of Gearing

The priority practical problem of gear design is to determine tooth profiles or surfaces that provide the maximum load carrying capacity of a gear. Figure 1.15 presents the basic methods for increasing the load carrying capacity of gearing (by example of spur and helical gears). This figure systemizes the methods based on advancement of tooth geometry. The left column (blocks 1–4) represents the ways of increasing the tooth bending strength, that is, procedures of changing the tooth shape aimed at decreasing the stresses inside teeth and, first of all, at the tooth dedendum.

Fig. 1.15
figure 15

Ways of increasing the gear load-carrying capacity

The central column in Fig. 1.15 (blocks 5–8) presents the methods for synthesis of tooth flanks that provide the least contact stresses and thereby the increased lifetime of teeth.

The right column (blocks 9–12) includes the ways of correction and modification of profiles (both for the synthesized and the existing gears, first of all, for the involute ones). Here the word “correction” means the agreed variation of conjugate segments on the pinion and gearwheel at once (block 9), for example, in order to decrease the contact stresses by increasing the reduced radii of curvature in the danger zone.

“Modification” is the deviation of one of the conjugate segments of profiles (usually on the addendum) from mutual enveloping in order to redistribute the forces at multi-pair contact or within the areas of reconjugation (with account of tooth deformation under load). Modification also decreases the forces of tooth impact at the initial moment of tooth contact, thus decreasing the vibration activity of the meshing which is vital for heavy-loaded high-speed gears. The following procedures are distinguished at modification: simple flanking (block 10), when the curve is assigned (segment of the straight line, circumference arc, etc.) on the profile of the generating rack or on the tooth; and complex flanking (block 11), when the profile is synthesized on the modified segment. Such flanking simultaneously eliminates the edge tooth contact at the initial (final) stage of their contact; and it gives the smooth load increase on teeth coming into contact (and the smooth load decrease for teeth coming out of the contact) etc.

The complexity of the problem in blocks 7–9 is that tooth deformations depend on the value of the torque T, that is why, optimal values and the shape of modification lines and flanking are various for different T. The gear should be designed so that it could operate properly at all its loading modes. The situation is worsened by the tendency of heavy-loaded gears to trochoidal interference, that is, untimely coming of teeth into the edge contact at tooth deformation.

Based on Figs. 1.1, 1.2, and 1.15, let us enumerate the works on analysis and optimization of geometry for tooth profiles and flanks for plane and spatial gearings in order to increase the load-carrying capacity of gears:

Block 1 (Fig. 1.15): optimization of the shape of the transient curve in order to decrease the stress at tooth root: works by Vulgakov [220, 221] specifying bending strength of heavy-loaded aviation gears. Investigations of tooth mode of deformation are also presented in works by Airapetov and Genkin [4,5,6,7], Reshetov and Bragin [34], Syzrantsev [196], Goldfarb with his followers [61, 64], Dorofeyev [40]—see Fig. 1.1.

Block 2 (Fig. 1.15): application of asymmetric tooth profiles: Kapelevich [79] and Vulgakov [221]. They are efficient in many gear drives, in which the tooth load on one flank is significantly higher and is applied for longer periods of time than for the opposite one.

Block 3 (Fig. 1.15): arch tooth shape that increases the tooth bending strength. In spur and helical gears there are works by Erikhov [46, 48] and Syzrantsev [48, 196]; Belyaev and Siritsyn [25]; Reshetov [122]. In bevel and hypoid gears there are up to 20 authors and dozens of publications—see “gears”–>“bevel” and “hypoid” in Fig. 1.2.

Block 4 (Fig. 1.15): synthesis of tooth profiles and flanks for the big reduced radius of curvature RΣ at tooth contact thus reducing the Hertz contact stresses. There are different methods for such a synthesis:

Method 1. For the assigned type of conjugated profiles (or flanks) it is necessary to determine the segments where RΣ → max. It is the method for designing involute gears by determining the optimal shift coefficient x1 and x2 (for instance, applying the blocking contours): Bolotovsky et al. [29, 30].

Method 2. It is necessary to search for new types of gearing and (or) optimize the geometry of new and existing types of gears. Such gears involve the following types (see Fig. 1.2):

Method 3. It is necessary to apply numerical methods at optimization synthesis of gearing. It can be used both at local synthesis and global one. The global approach is more complex but it gives more reliable results. The versatile method of the global synthesis by criterion of location and dimensions of the bearing pattern is developed and implemented for bevel and hypoid gears by M. G. Segal in the early 1970s. The certain contribution to the development of the global method of synthesis at the same period was made by B. A. Cherny and K. I. Gulyaev. These works were considered in our previously published first part of the review. Note, that from mathematical point of view the optimization synthesis is reduced in general case either to the problem of non-linear programming or to the variation problem. In the first case the values of the set of parameters (vector x) are determined for which the target function F(x) reaches its extreme point (under the set of limitations). In the second case the control function f(u,v) (the profile or flank of a tooth with curvilinear coordinates u and v) is determined for which the target function F(f(u,v)) reaches its extreme point. Such approaches started producing the results only after 2000, that is why, we do not consider them in this second part of the review.

Block 5 (Fig. 1.15): application of gears with multi-pair engagement. They are:

  1. (1)

    Spur gears with the overlap ratio more than 2 (ε > 2); teeth of such gears are shown in Block 5 in Fig. 1.15. The minimum pinion tooth number in these gears is about 30. At any instant of meshing at least two pairs of teeth are interacting; and the force transmitted by the tooth is reduced almost in two times, thus decreasing contact and bending stresses. Gears require high production accuracy: the error of pitch and profile should be an order less than tooth deformations under load.

    These gears were first applied in aviation in 1980 abroad and only in the 21st century in Russia. It became common to replace classical gears with 1 < ε < 2 by gears with ε > 2 (for instance, in gearboxes of lorries “Belarus”: the casing geometry, shafts and bearings, mounting surfaces are left the same; gearwheel tooth number are increased in 1.5 times with decreasing the module by 1.5 times (with correcting the shift coefficients if necessary); parameters of the basic rack profile are taken to be as follows: α = 20°, ha* = 1.25, hl* = 2.5, c0* = (0.2–0.25). It provides the increase in the transmitted power up to 30…50%.

  2. (2)

    Wave gears (Fig. 1.16) are also related to gears with multi-pair meshing: up to 30…40% of the whole tooth number are in the simultaneous contact, thus providing high load carrying capacity, kinematic accuracy and smoothness of operation. In these gears one of the meshing gearwheels is flexible (3 in Fig. 1.16). It is used to transmit the deformation wave from the element 1 which is called the generator. Gearwheels are always spur and helical, but sometimes there are gears with face bevel teeth. The gear ratio of all wave gears is usually i= 40…300 and it is determined by the expression:

    Fig. 1.16
    figure 16

    Example of wave gear: 1—driving element (generator); 2—driven element (rigid gearwheel); 3—column (thin-wall elastic barrel with teeth of the flexible gearwheel cut on the outside)

    $$ i = \frac{{z_{driven} }}{{z_{driven} - z_{stationary} }} $$

    The tangible contribution to the design and implementation of wave gears was made by Ginzburg [56]; Emelyanov and Popov [44], Kraynev [218] et al.

  3. (3)

    Spiroid gears (Fig. 1.17) can also have multi-pair contact (up to 10 tooth pairs in simultaneous contact). By the end of the 20th century the leader in investigation, design and implementation of spiroid gears in Russia (and in fact in the world) was acknowledged to be Izhevsk Mechanical Institute (now Kalashnikov Izhevsk State Technical University). It was presented by two active groups of scientists headed by A. K. Georgiev and V. I. Goldfarb. Great contribution to development of theoretical investigations and implementation of spiroid gears was made by their followers: D. V. Glavatskikh, A. S. Kuniver, O. V. Malina, I. P. Nesmelov, V. N. Anferov, E. S. Trubachev, V. N. Abramenko, S. V. Ezerskaya, A. M. Fefer, V. A. Modzelevsky et al. The most important works published in 1976–2000 by these experts are presented in tables in Figs. 1.1 and 1.2.

    Fig. 1.17
    figure 17

    Example of spiroid gear

  4. (4)

    Planetary type precession gears with small tooth number difference. It is common that internal spur and helical gears can have small difference of gearwheel tooth numbers (up to z2-z1 = 1). The advantage of such gears is low contact stresses because of a high reduced radius of curvature and big number of teeth that are in simultaneous contact. The drawback is the gear ratio i = z2/z1 close to 1. Similar properties are also specific for bevel gears at the shaft angle Σ close to 180°. The main drawback (closeness of i to 1) can be overcome by making precession planetary gears. Definite layout features are also revealed by bevel gears with the shaft angle Σ close to 0° (Fig. 1.18a). Figure 1.18b–d presents the schemes of precession gears studied thoroughly in Zlatoust by Bezrukov, Lopatin and their followers [26, 27, 52, 126,127,128]); in Kishinev by Bostan [32, 33]), in Volgograd and Saint-Petersburg by Kislov, Tesker, Timofeev [88]); in Snezhinsk by Nechaev [136, 137]), and lately in Tyumen by Syzrantsev.

    Fig. 1.18
    figure 18

    Bevel and precession gears: a bevel gear for the boat; bd precession gears with bevel gearwheels

Block 6 (Fig. 1.15): gearing with closed lines of contact (CLC). Investigations of worm gears with CLC were carried out in the late 1960s in the USSR. Later similar investigations were made in Germany, Czech Republic and Japan. In gears with CLC the closed space is developed between contacting teeth, where the lubrication is blocked—see Fig. 1.19. The force from the driving tooth to the driven one is transmitted here not only by their CLC, but through the blocked oil. The volume of the space with oil is decreased at rotation of the gear elements and the pressed out oil provides good lubrication conditions for teeth. It reduces the wear and power losses in gearing and increases the transmitted force. In the late 1980s the issue of organizing a serial production of worm gearboxes with CLC was discussed, though it required high accuracy of meshing (5th–6th degrees of accuracy), the increased rigidity of the whole layout and precise bearings. Investigation results for worm gears with CLC in 1976–2000 are presented in works by Lagutin and Verkhovsky [117,118,119, 211,212,213].

Fig. 1.19
figure 19

Worm gear with closed lines of contact: a section by the mid plane of the gearwheel; b projections of contact lines on the plane perpendicular to the worm axis

Blocks 79 (Fig. 1.15): these issues are not considered in this part of the review, since works on these methods of increasing the load carrying capacity were only at the primary stage before 2000 both in Russia and CIS countries. Works according to blocks 10–12 are also not described here since the approaches considered there are of auxiliary importance.

Finishing the p. 2.2 “Development of synthesis methods…”, we refer the reader to the Table in Fig. 1.2. It can be used in order to:

Step (1) choose the interesting gear, mechanism, gear part or theme of investigations;

Step (2) follow the lines coming from the right and left to your chosen theme, family name of authors and number of publications;

Step (3) look through the title of publications in the list of reference and decide the priority of their studying.

1.2.3 Development of Methods for Analysis of Generating Processes and Theory of Gearing

In order to obtain information on this theoretical theme, refer to the Table in Fig. 1.1. By performing all steps described above, get the necessary information.

1.2.4 Software: Development and Application

Software applied at gear design and performance of other engineering analysis can be divided into 4 categories:

Category 1. Commercial software focused on solving the wide range of typical problems. They are CAD/CAM/CAE—systems with English interface, for instance, Pro/ENGINEER, ANSYS, CATIA, Solid Works and oth. The special software is intended for gear design: KISSsoft (Switzerland); LTCA (Gleason, USA); Kimos (Klingelnberg, Germany); PCM (USA); PCD (Japan) and oth.

Category 2. Russian software that tends to be commercial but usually solves a less number of problems. It involves the following systems for design of gears and their elements: (1) WinMachine by NTC, Korolev; (2) CAD KOMPAS by “Askon” supplemented by software “Compas#Gears” on gear analysis.

Category 3. Russian software developed in the leading scientific schools on gears and tools for “internal use”. They are:

  1. (1)

    Software Reduk 43 for analysis of geometry and strength of involute spur and helical gears with internal and external meshing, planetary gears, bevel gears with straight and circular teeth. The software was developed in 1990s by Department of gear technology of TsNIITMASH (D. E. Goller, A. A. Birbrayer and S. L. Berlin). It implements the techniques of analysis stated in the corresponding standards (GOSTs 16532-70, 1643-81, 21354-87, 19326-74, 1758-81 and other) that were developed at the same Department. This software allows for analyzing the load carrying capacity and durability of both individual gears and multi-stage gearboxes with account of tooth heat treatment, loading cyclogram, efficiency, power flow, etc. The software is actively applied at heavy engineering plants.

  2. (2)

    CAM/CAE “Volga 5” for geometric and manufacturing analysis of bevel gears with circular teeth developed in 1980s at Saratov SKBZS headed by M. G. Segal.

  3. (3)

    Software “SPDIAL+” for design, optimization and preproduction of spiroid and worm gears (Izhevsk, ISTU, Institute of Mechanics, headed by V. I. Goldfarb, leading developers are E. S. Trubachev, O. V. Malina et al.).

  4. (4)

    Software “Expert” for analysis and synthesis of bevel gearwheels with circular teeth (Moscow, “Mosstankin”, headed by G. I. Sheveleva, leading developers are A. E. Volkov and V. I. Medvedev).

Category 4. “Personal” software for solving the problems of analysis and synthesis of gears and tools developed for and gear design at enterprises. Majority of high-skilled experts have such programs. Basics of these programs are standard calculations plus own developments. Let us name only several such software:

  1. (1)

    Analysis and optimization design of aviation gears (V. L. Dorofeev, Moscow).

  2. (2)

    Synthesis and optimization of bevel gears (V. N. Syzrantsev, Tyumen).

  3. (3)

    Design and optimization of parameters of spur and helical, worm and double-enveloping gears (S. A. Lagutin, Electrostal).

Note that during the last third part of the 20th century there were works in the USSR on development of convenient and rational interfaces of programs on analysis and synthesis of gears (Saratov, Izhevsk, Khabarovsk, Leningrad, Tyumen, Minsk and oth.). In particular, an intensive work on development of task-oriented programming language was done in Tyumen [18, 19]. The dialog support system for IBM compatible computer was also worked out. The language involved the means for description of: (1) systems of coordinates and motions; (2) geometrical objects; (3) deviations and deformations; (4) the problem to be solved; (5) types of output data; (6) processing and cataloguing of results; (7) operation with regulating information (tables and formulas). Operations with interval arithmetic were thought out, that is, information (and results) could be represented not only by number, but also by range of numbers (for example, of allowable stresses). Syntax of the developed language was described by Backus-Naur method, since the formal grammar was made to be context-free. Moreover, it was LL(1) grammar which assumed, as known, the efficient methods of syntax analysis and translation by push-down automatons (PDA). When applying PDAs, semantics of the language was implemented by semantic sub-programs. Unfortunately, events of 1990s and rapid development of computer technologies along with the lack of experience and means put an end to that work that seemed to be future-oriented.

1.3 Achievements and Problems of Development of the Theory of Gearing in 1975–2000

1.3.1 Development of the Theory of Gearing

  • New concepts were introduced and applied: (a) the space of meshing (S. A. Lagutin); (b) the covering surface (G. I. Sheveleva); (c) the fan, wedge and bunch of normal lines, acceleration of feeding-in (D. T. Babichev).

  • Non-differential and kinematic methods for analysis of working and manufacturing meshing gained their development.

  • Having applied “the acceleration of feeding-in”, new techniques for solving a number of problems were developed: analysis of radii of curvature in meshing, determination of cutting zones and thicknesses of layers removed by cutting edges of tools; analysis of faceting values and other.

1.3.2 Main Theoretical Results on Development of the Theory of Real Gearing

  • Methods of gear synthesis were developed with account of many quality characteristics and factors of gear operation: terms of reconjugation, accuracy of production, deformations, vibration activity and other.

  • Techniques for investigation of tooth contact interaction and deformation mode of the whole tooth (including multi-pair tooth contact) were developed and implemented. It became possible to control the contact pattern.

  • The system of assigning the real ITS (initial tool surfaces) was developed and mathematical models for ITS were created.

1.3.3 The Important Practical Results—A Great Number of Very Adverse Types of Gearing Was Investigated (and Often Implemented: In Gears, in Hydraulic and Pneumatic Machines, in Machine-Tool Gearing)

  • Traditional gears and gearing: (a) spur and helical: involute (small module, big module, high-speed heavy loaded), with Novikov gearing and other; (b) bevel and hypoid; (c) spiroid, worm, double-enveloping, screw; (d) face gears; and other (Fig. 1.2).

  • Non-traditional gears and gearing: (a) gears with intermediate rolling bodies; (b) devices with closed systems of rolling bodies; (c) precessing bevel gears with shaft angles close to 0° and 180°; (d) hydraulic and pneumatic machines: helical (two- and three-rotor) common and planetary type; (e) hydraulic and pneumatic machines with non-circular gearwheels; and other.