Open access peer-reviewed chapter

# A Case Study of Modelling Concave Globoidal Cam

By Nguyen Van Tuong and Premysl Pokorny

Published: October 1st 2009

DOI: 10.5772/8226

## 1. Introduction

Globoidal cam mechanisms are widely used in industry. Compared to other cam-follower systems, the globoidal cam-follower mechanisms have many advantages, such as: compact structure, high loading capacity, low noise, low vibration, and high reliability. They are widely used in machine tools, automatic assembly lines, paper processing machines, packing machines, and many automated manufacturing devices.

In term of the shape, globoidal cam is one of the most complicated cams. The most important task when modelling the globoidal cams is to represent their working surfaces. The working surfaces of the globoidal cams are the surfaces that contact with the roller surfaces. These surfaces are very complex and it is very difficult to create them accurately.

Up to now, a number of works dealing with finding the way to describe accurately these surfaces have been proposed.

Some researchers derived mathematically expressions for the surface geometry of the globoidal cam with cylindrical, hyperboloid, or spherical rollers, based on coordinate transformation, differential geometry, and theory of conjugate surfaces (Yan & Chen, 1994& 1995; Yan-ming, 2000; Cheng, 2002; Lee & Lee, 2001& 2007; Chen & Hong, 2008). They developed their own programs, which were written in Visual Basic, C or C++ languages, to assist themselves in studying. Some programs can draw and display the draft of the cam contour, or create the solid model. Some can create the data of the cam curve profile which will be the input data for CAD/CAM software such as Unigraphics to build the CAD model (Chen & Hong, 2008). Some other researchers also described mathematicaly the cam surface, but they used computer to develop a package, which was a combination of AutoCAD R14, 3D Studio Max, and VBA, to generate the surfaces of the roller gear cam (En-hui et al., 2001). In addition, some researchers studied to create the globoidal cam with conical rollers from machining point of view (Tsay & Lin, 2006). They represented the surface geometry of the cam as the swept surfaces of the tool paths. In their study, the expression of a surface normal, a rule surface and its offset, meshing vectors and meshing angles were introduced to define the accurate swept surfaces generated by the roller follower, and a program in C++ language developed to generate the surface coordinates of the cam.

In general, the works mentioned above have used the mathematical expressions for the globoidal cam surfaces and various cam laws as the input data to generate the cam surfaces. From machining point of view, the globoidal cam surfaces can be determined by corresponding angular displacements of both the cam and the driven member (Koloc & Vaclavik, 1993). These angular displacements can be extracted from the NC program generated by some special sofwares that are specialized for cam mechanisms. They can also be obtained from the follower displacement equations. In this study, the concave globoidal cam with swinging roller follower is modeled from angular input and output displacements.

The objective of the chapter is to introduce some effective methods for modelling concave globoidal cam. These methods can be implemented by using commercial CAD/CAM sofwares. In the chapter, Pro/ENGINEER® Wildfire 2.0 is used to create the cams for the illustrative example that we have recently done for industry in Czech Republic. In this case study, the input data for modelling are the angular input and output displacements of the cam and the follower. Furthermore, besides modelling methods, some important techniques that are useful for designers to find out the most accurate model are also represented. In this chapter, the terms “globoidal cam surface(s)” and “cam surface(s)” refer the working surface(s) of the globoidal cam.

The outline of the chapter is as follows. Section 2 presents the theoretical background of concave globoidal cam. In section 3 we describe in detail some modelling methods that can be used to create the globoidal cam surfaces. An application example is presented in Section 4. Finally, conclusion remarks are given in Section 5.

## 2. Theoretical background of concave globoidal cam

There are two types of globoidal cams. The first one is the globoidal cam that has a groove on its surface and the roller follower oscillates when the cam rotates. This type has two subtypes which are convex and concave (Figure 1). These cams are used for small angles of follower oscillation. The second one has one or more ribs on a globoidal body. This type is also called roller gear cam or Ferguson drive (Rothbart, 2004). The two surfaces of the rib always contact with the rollers (cylindrical, spherical or conical) of the follower. This follower may oscillate about its axis or have an intermittent rotation. Figure 2 shows two subtypes of the concave globoidal cam: the concave globoidal cam with an oscillating follower and the concave globoidal cam with an indexing turret follower. The rib of these cams looks like a thread or a blade so that sometimes they can be called thread-type or blade-type globoidal cams. In this study, the single thread-type is the globoidal cam that we will deal with.

Figure 3 illustrates the geometrical relationships between a concave globoidal cam with an oscillating follower. According to the structure of the globoidal cam, as can be seen from Figure 2&3, the symmetrical plane of the follower contains the cam axis and the axes of the rollers intersect at a point that lies on the follower axis. In Figure 3, the development plane is the plane that is normal to the axis of the roller and located anywhere along the length of the roller. The intersection point between the development plane and the axis of the roller is the pitch point (P). Datum plane is the plane normal to the cam axis and contains the follower axis. The angular displacement of the roller is measured from this plane.

The following are some parameters related to a globoidal cam-follower system (Koloc & Vaclavik, 1993; Reeve, 1995).

1. - angular input displacement (the rotation angle of the cam).

2. - angular output displacement from datum plane (the rotation angle of the follower). has a relationship with and it can be expressed by function = f(), (En-hui et al., 2001).

3. 0 – angle from datum plane to start of follower motion, measured in direction of motion. If the start point is encountered after the datum plane then 0 is positive.

4. 1 – angle between the axis of the upper roller with the datum plane. At the beginning, when the upper roller is at the starting point then 0= 1.

5. 2 – angle between the axis of the lower roller with the datum plane.

6. t - distance between the axis of the follower to the end of the roller, measured along the roller axis.

7. e – clearance between the end of the roller and the cam body.

8. F - distance from the axis of the follower to the pitch point.

9. C - distance between the cam axis and the turret axis.

10. R - perpendicular distance from cam axis to the pitch point, expressed as

= C  F.cos(b1)E1

11. h – distance from the pitch point to the datum plane. It is the height of the point P and presented as

= F.sin (b1)E2

Obviously, the coordinates of the pitch points on the rollers can be calculated if the angular input and output displacements are known. From these coordinates and some other information, the pitch surfaces of the cam can be modeled.

## 3. Modelling methods

There are some methods used to model concave globoidal cams. The most important task in the modelling procedure is to create the working surfaces of the cam. Once these surfaces are created, other surfaces of the cam can be easily formed later. Here, we introduce two groups of methods that can be used to create the cam surfaces, namely Pitch surface-based methods and Standard cutter-based method.

### 3.1 Pitch surface-based methods

In a globoidal cam-follower system, when the follower rotates, the locus of the roller axis will generate a ruled surface (pitch curved surface) in space (Tsay & Lin, 2006). The two axes of two rollers in this case study will generate two pitch curved surfaces. The working surfaces of the cam can be obtained from the pitch surfaces by offsetting them a distance that is equal to the radius of the roller.

There are several methods to get the pitch surface. The followings are three methods that can be used to create the pitch surface.

#### 3.1.1 Graphs-based method (method 1)

Sweep a straight line with two constraints (Figure 4): (i) the angle between this line and the datum plane varies when the cam rotates and its value is i j; (ii) the coordinates of the pitch point P on this line, in the cylindrical coordinate system, corresponding with the input angular displacement j, satisfy the formulas below.

hji=F.sinβjiE3
Rji=CF.cosβjiE4

where i = 1, 2, corresponding with the upper and the lower pitch surfaces; j = 1,2,…,n, corresponding with the angular output displacements.

The relationship between pairs and , h and , R and can be expressed in graphs. These graphs are useful for modelling the cam in commercial CAD/CAM softwares.

#### 3.1.2 Open section-based method (method 2)

This method is similar to the previous method but here the two pitch surfaces are created at the same time. These surfaces are made by sweeping an “open section” which consists of three straight lines. Two of them are collinear with the axes of the two rollers. The last one connects them together.

#### 3.1.3 Curves- based method (method 3)

Sweep a straight line that is collinear with the roller axis. The two end points of this line must lie on two curves (Figure 6). One of these curves is a circle in the datum plane. This circle goes through the intersection point of the roller axes and its center is in the cam axis and it is also called the origin trajectory. The other curve is a three-dimensional (3D) curve. This 3D curve is the locus of a point, which located on the roller axis (it can be the pitch point), when the follower rotating. The coordinates of that point satisfy formulas (3) and (4) above.

#### 3.1.4 Standard cutter-based method (method 4)

An end mill cutter can generate the surfaces of a globoidal cam. If the diameters of the cutter and the roller are equal, the motion of the cutter will be similar to that of the roller in the machining process, and of course, the cutter must rotate about its axis (roller axis). The sweep surface of the tool path can represent the working surface of the cam. The following is one way that can be used to get the cam surface.

Cut a bank by sweeping a rectangular section (Figure 7) to form the cam surfaces if the following constrains are performed:

1. The width of the section is equal to the diameter of the roller. The length of the section satisfies the following formula.

= t + eE5

2. where, L is the length of the rectangular section, t and e are two geometrical parameters of the cam which mentioned in section 2.

3. Two points on the section, which are intersection points between the symmetry axis of the section and its edges, must follow two 3D curves. These curves are loci of two points, which are on the roller axis, when the follower rotates. One of these curves is the origin trajectory. The curves which are used in the curves- based method can be applied here.

4. This section plane always contains the cam axis.

The globoidal cam can be modeled by using CAD/CAM softwares such as CATIA, Unigraphics NX, Pro/Engineer.... The four methods above can be implemented in Pro/Engineer. In theory, geometric errors may exist on every model. These errors may be so very high that the model cannot be acceptable. Hence, after modelling, models must be checked to find out the best one among them. In this study, Pro/Engineer Wildfire 2.0 is used to create the globoidal cam. The implementation of those methods is presented in a form of an illustrated example in the next section. Besides, some other important tasks to check the model are included as well.

## 4. Application example

### 4.1. Input data and calculations

Given a concave globoidal cam with an oscillating follower that has two cylindrical rollers. The angle between two axes of the rollers is 600. The increment of the input angle of the cam is 0.20, starts from 0 and ends at 3600. The angular input and output displacements are given in a table that consists of 1800 pairs of corresponding angles. Some of them are presented in Table I in the appendix. To observe easily, the relationship between the angular input and output displacements is showed in Figure 8. The following are some other parameters of the system, which are showed in Figure 2: d = 25.5 mm, l = 16 mm, C= 107.8 mm, t = 58.7 mm, 0 = 7.490, e = 2.3 mm.

There are some calculations that must be done before making the models as follows:

1. Calculating the angular outputs included 0.

2. Calculating the angle

βj1

and

βj2E6

βj1=βj+β0E7

βj2=60βj1E8

### 4.2. Modelling procedures and results

The following are the main steps to create the globoidal cam by using four methods described above in Pro/Engineer Wildfire 2.0. The accuracy of the system is set to 0.0005 to get high accurate models.

The graphs-based method

1. Create a revolution surface of the globoidal body of the cam (Figure 9a).

2. Create 3 graphs for the angle between the sweeping line and the datum plane (Figure 9b), the height of the pitch point on the sweeping line, and the distance (radius) from the pitch point to the cam axis. These graphs show the dependence of the three above parameters on the angular output displacement of the cam.

3. Create the upper pitch surface by using the Variable Section Sweep command (Figure 9c). The origin trajectory in this case is the circle which is the intersection between datum plane and the cam body. Constrains for this command are formulas that have the form as

sd#= evalgraph("graph_name",trajpar*360)E9

where

- sd# is the dimension which will vary. It can be R or h or (Figure 3a).

- graph_name is the name of the graph which created in step 2, corresponding with the dimension sd#.

Refer (Tuong & Pokorny, 2008b) to get some more useful infomation about these graphs.

4. (4) Repeat steps 2 and 3 for the lower pitch surface (Figure 9c), using other three graphs.

5. (5) Offset the two pitch surfaces to get the working surfaces of the cam (Figure 9d).

6. (6) Merge all surfaces to become one and convert the united surface to solid (Figure 9e).

7. (7) Perform some extra cuts to get the desired cam, model 1 (Figure 9f).

The open section-based method

1. Create a revolution surface and 3 graphs like the first two steps in the first method.

2. (Create the two pitch surfaces at the same time by using the Variable Section Sweep command (Figure 10a) with the same constrains in step 3 in the first method.

3. Perform steps 5, 6 & 7 as in the first method to get the solid model (Figure 10b) and the desired cam, model 2 (Figure 10c).

The curves-based method

1. Create a revolution surface of the globoidal body of the cam (Figure 11a).

2. Create the origin trajectory and two 3D curves (Figure 11b).

3. Create the two pitch surfaces by using the Variable Section Sweep command (Figure 11c).

4. Perform steps 5, 6 & 7 as in the first method to get the offset surfaces (Figure 11d), the solid model (Figure 11e) and the desired cam, model 3 (Figure 11f).

The standard cutter-based method

1. Create a revolution blank of the cam body (Figure 12a).

2. Create the origin trajectory and two 3D curves (Figure 12b).

3. Perform two cuts with rectangular section by using the Variable Section Sweep command (Figure 12c).

4. Perform some extra cuts to get the desired cam, model 4 (Figure 12d).

Among the four methods, the two first methods need more steps than the others but the modelling time is much shorter than that of the two last methods. This is because when creating the pitch surfaces in the methods which need 3D curves, the system has to interpolate the swept surface through 1800 physical points on this curve.

To see the cam easily, the pitch surfaces on four final models in figures 9 to 12 are hidden. In general, these models look great and similar. In order to choose the best one among them, the interference between the cam and its rollers must be checked. If there is no interference and the clearance between the components is small enough, then the result is acceptable.

### 4.3 Making animation and checking interference

In order to make animation and verify the interference between components in the globoidal cam mechanism, first, an assembly of the cam and the follower is made. After that, use the Mechanism Design module to define the geometrical relationships of the system, make it move and analyze its motion also. Last, use a kinematics analysis to obtain information on interference between components. The following is the procedure to make animation and check interference.

1. Creating the assembly model.

2. Modifying Joint Axis Settings.

3. Creating a slot-follower.

4. Checking the assembly model.

5. Creating servo motor.

6. Creating and Running Analyses.

7. Viewing results and taking measurements.

When the globoidal cam rotates, the follower will stay or rotate depending on the location of the rollers on the cam surfaces. The follower will not move when the rollers still contact with the cam surfaces in the dwell periods. To get a motion for the follower, a point on one roller axis has to trace along a 3D curve on the pitch surface. The pitch point now can be used for this purpose (point PNT0 in Figure 13). This 3D curve is available on the model 3 and model 4. This curve can be drawn on model 1 and model 2 for the purpose of checking interference. The servo motor is always applied on the cam axis so that the cam can move about its axis. Servo motor can also be applied for the follower. In this case, the slot-follower connection is omitted. Figure 13 shows the cam-follower system in the Mechanism application with the slot-follower connection.

During the animation, the motions of the cam and the follower are simulated, and if there is any interference between the two components, Pro/Engineer will highlight the interfered positions. Figure 14 presents the result of the animation of model 1.

In the assembly of model 1 and model 3 and their followers, there is no interference between the cam and its rollers when the cam rotates one revolution, while interferences occur in the assembly of model 2 and model 4. There are 10 positions of interference in the assembly of former, while there are a lot of positions of interferences for the latter. These interferences appear on both sides of the rib on the rise and return periods, where the curvature of working surfaces changes strongly, and can be seen in the graphic window (Figure 15). There are totally 1800 positions checked for a full revolution of the cam. The angle between two positions (called frames in Mechanism Design module) is 0.20. This value is similar to the increment of the input angle of the cam. In comparison with model 2 and model 4, the latter has bigger interference volumes. The result is that model 1 and model 3 can be accepted.

Although the interference does not occur between the cam surfaces of the acceptable models with their rollers, but there may have clearances between them. Thus, these clearances must be checked to ensure that they are small enough. If they are large, the errors of output angular displacements will be large and the model in this case may have to be eliminated. These clearances can be manually measured in assembly standard mode or in mechanism mode. The measuring result is that in one revolution of the cam the biggest clearances are on the rise and return periods and they are less than 0.2 micrometer for both models (Tuong & Pokorny, 2008). Obviously, these gaps also cause errors in the output angular displacements but these errors are very small and can be accepted.

In this study, the four models above were created on a notebook with 1.86 GHz Core 2 Duo processor, 2GB RAM. It took only few minutes to create the pitch surface, the most time-consuming task, for the model of the first method (graphs-based method). Meanwhile, it took quite long with the methods that used 3D curves (method 3 and 4). The similar problem happened when performing the analysis running for checking interference. Therefore, the first method is the best choice when considering the modelling methods.

In our research, besides the example above, another example for modelling concave globoidal cam with indexing turret follower has also been done (Tuong & Pokorny, 2009). In that case study, the pitch surface-based modelling method was successfully used to create the cam. Some techniques which introduced above can be used for that case. However, the modelling procedure is much more complicated than the case of the concave globoidal cam with swinging roller follower. Figure 16 shows the animation playback of the concave globoidal cam with indexing turret follower.

## 5. Conclusion

In this study, four modelling methods are developed to create the concave globoidal cam. These methods are implemented in Pro/Engineer® Wildfire 2.0 using the same input data of a concave globoidal cam with an oscillating follower. After verifying the four models corresponding with the four methods, it can be said that the model which is created from the graphs-based method is the best one because it meets the required accuracy and the modelling time is short. This method is easy to conduct in Pro/Engineer, which is one of the most powerful CAD/CAM packages in industry. This is also a great potential for industry application. The case study presented here is a concrete example but the modelling methods and techniques can be applied for other spatial cams with cylindrical rollers when the angular input/output are known. The result of this study is very useful in terms of modelling and manufacturing globoidal cam.

## Appendix

 0.00 0.00000000 179.60 44.99616011 0.20 0.00000000 179.80 44.99904001 0.40 0.00000000 180.00 45.00000000 0. 8 0 0.00000000 180.20 44.99904001 0. 8 0 0.00000000 180.40 44.99616011 1 . 0 0 0.00000000 … … …. … 213.00 23.59739548 10 4 . 6 0 0.00000000 213.20 23.39136475 10 4 . 8 0 0.00000000 213.40 23.18530279 105.00 0.00000000 213.60 22.97922791 105.20 0.00000680 213.80 22.77315844 105.40 0.00005418 214.00 22.56711268 105.60 0.00018212 214.20 22.36110896 105.80 0.00042995 214.40 22.15516558 106.00 0.00083638 214.60 21.94930085 106.20 0.00143945 … … 106.40 0.00227659 253.60 0.00227659 106.60 0.00338459 253.80 0.00143945 106.80 0.00479962 254.00 0.00083638 … … 254.20 0.00042995 146.40 22.97922791 254.40 0.00018212 146.60 23.18530279 254.60 0.00005418 146.80 23.39136475 254.80 0.00000680 147.00 23.59739548 255.00 0.00000000 147.20 23.80337666 … … 147.40 24.00928999 359. 0 0 0.00000000 147.60 24.21511717 359. 2 0 0.00000000 147.80 24.42083990 3 59 . 4 0 0.00000000 148.00 24.62643991 359.60 0.00000000 148.20 24.83189893 359.80 0.00000000 … … 360.00 0.00000000

### Table 1.

Table 1. Example of some selected angular input/output displacements, unit: degree

## Acknowledgments

The work upon which this paper is based is a part of MSM-4674788501 research program, grant from the Technical University of Liberec, Czech Republic.

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Nguyen Van Tuong and Premysl Pokorny (October 1st 2009). A Case Study of Modelling Concave Globoidal Cam, Advanced Technologies, Kankesu Jayanthakumaran, IntechOpen, DOI: 10.5772/8226. Available from:

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