Load Types, Normalized Load Types, and Input Torques

This topic:

Reviews Payload Types.
How we can normalize Payload Types with coefficients: Q, K, Cm
Reviews the effect on input-torque from different payloads types, and how we can normalize it as the coefficient, Cc

Notes on the Terms: Payload, Duty and Capacity.

The 'payload', also named 'load', is the total force, or torque,  referred to the cam-follower.

The 'load' imposed on a cam-mechanism is also known as the duty of the mechanism.

The capacity is the ability of the mechanism to perform the duty for a specified lifetime.

hmtoggle_folder1        Payload: Load Types

It is important to know the payload-type, or load-type, when we design a cam-mechanism.

The output-load is passed from the cam-follower and back to the cam and the cam-shaft. Thus, the input-load that is imposed on a cam-shaft is a function of the load-type at the cam-follower.

The different load-types result in different loads on the cam-shaft.

The nominal output loading, which will be a Force for linear motion, and a Torque for rotary motion, is derived from the following 'Payload-Types'.


A: Force or Torque: constant.

For example, friction, gravity, work loads.


B: Force or Torque: proportional to displacement.

For example, a spring.


C: Force or Torque: proportional to velocity.

For example, viscosity.


D: Force or Torque: proportional to acceleration.

For example, inertia.


E: Force or Torque: conforms to a special function.

For example, an engine cycle.

EXAMPLE 1A: Gravity, Spring and Inertia: Speed Dependence



The two images to the left show the same load types on a cam mechanism, at two different speeds.

The Payload-types are:

Spring, and

You can see that at 'high-speed' the inertia is greater. At the higher speed the load becomes negative at point3s, along the deceleration of the rise.



Example 1B : Gravity, Spring and Inertia: Different Pre-load of Spring

The image below shows the period of negative loading when the cam has a 'falling' motion.

In such a case, the cam-follower would lose contact with an open track cam and control of the payload would be lost.

To make sure the cam-follower remains in contact with the cam-profile:

Improve the motion design to reduce the maximum negative acceleration.
Use an enclosed track, a blade cam, or a conjugate cam

- or -

Increase the Constant Load(A) or Spring Load(B)


Virtually all indexing mechanisms, and many reciprocating and oscillating mechanisms, have a duty that combines a Constant (A) and an Acceleration (D) load, with less significant amounts from the other kinds of loads.

Constant Load - from friction forces (bearing seals), raising weights or gravitational force, and other work loads - can be resolved into a single force or torque resisting the output motion.

Acceleration Load - from the inertia of various masses - can be resolved into a single equivalent inertia connected to the output or the cam-follower.

Total load = inertia load + constant load.

The peak of the total load usually is at the same point as the maximum inertia load.

Other common Payload Types

Index mechanisms: Friction(A) + Inertia(D).
Spring-loaded reciprocating mechanisms: Friction + Spring Pre-Load(A), Spring-Rate(B) + Inertia(D).

See example above - same mechanism at two different machine speeds.

Very high-speed mechanism: possibly significant viscous loading (C), and, of course, Inertia(D).

The maximum value and proportion of each load type component (A, B, C, D and E), depends on the application. Thus, there is an infinite number of load patterns. It is possible to tabulate normalized values for the most common combinations.

Payload for Conjugate Cams

The idealised design of Conjugate Cams eliminates the need for a Spring to maintain the contact of the roller against the cam. Frequently, the cam-follower rollers are adjusted, or designed, to give an 'optimal' pre-load against the cam, so that the rollers do not slip.

This is an 'idealised design'. More frequently, manufacturing and machining tolerances, mean it is difficult to guarantee contact between the cam and the roller throughout the cam's rotation.

The roller will often lose contact during some part of the machine cycle.

Frequently, Conjugate Cams use a spring, air-cylinder or hydraulic device, to force one of the cam-follower rollers against the cam to eliminate backlash. The loading device only needs a short travel to compensate for manufacturing tolerances.

hmtoggle_folder1        Normalized Loads

Inertia Load

The maximum inertia load is: [Using these simple equations: F= M.a ; T=I.α













The Inertia Load Coefficients Fi or Mi are 'nominal', and must be modified by the application of the Torsion-Factor, Ct.

Friction Load

The constant load, such as friction, is:

FricF for linear motion
FricM for rotary motion

Referred to the mechanism output in both cases. Add the Friction Load to the Inertia Load.

Spring Load

When there is an output force component that is proportional to displacement, such as a spring force, it is convenient to add the maximum value spring force to the Friction-Force, Ff , or Friction-Moment, Mf as if it were a constant load.

In that case, the total output-load calculation is conservative. You can take these as safe values for preliminary designs.

Load Mix: Inertia; Friction; Spring

Instead of adding the 'Maximum Spring-Rate Force' to the 'Constant Load', we can take all three load patterns into account. When appropriate, the total maximum load can be adjusted downwards by a load-mix coefficient, Cm.




Cm depends on the relative values of constant load to spring load and also inertia load.

hmtoggle_folder1        Pre-load Coefficient (K); Inertia Ratio (Q).

Pre-load Coefficient, K


The Spring Rate Effect is defined by a 'pre-load coefficient', K.

It is applicable to all cam systems.

K is the ratio of minimum non-inertia loading : maximum non-inertia loading.

Fp, Mp = minimum non-inertia load (p = pre-load)

Ff, Mf  = maximum non-inertia load (f = full-load)

Linear System


Rotary System


Example Loads to the left.


When there is no spring load component (see top image to the left), Mf = Mp

Thus,   K-nospring

Inertia Ratio, Q

The other coefficient we need to evaluate Cm, is the ratio of Peak Inertia : Maximum Non-Inertia loading.

The Inertia Ratio, Q:

InertiaRatioQ-L   or   InertiaRatioQ-R

The instantaneous output load for linear and rotary motions are:



It follows that the maximum value of these is where:


for both Linear and Rotary loading.

Cm can be evaluated for a range of values of Q [range of 0 to 1] and K [range of 0 to 1].

normaloutdis [Correction: instantaneous normalised displacement coefficient]

wdd [Correction: instantaneous normalised acceleration coefficient]

hmtoggle_folder1        Input Torque Coefficient

The input torque [drive torque] varies throughout the motion. The variation is a function of the output load pattern and the motion-law.

Since the output load pattern varies with the mix of inertia load, spring load, and constant load, so too does the input torque.

For all cases, the mix is defined with the factors Q and K , as defined above.

For each motion-law, the instantaneous input torque can be expressed as a function of the instantaneous output load:


for linear motion


for rotary motion

Where: :









The instantaneous output load, fo or mo, is a function of the normalized motion-law factors, the load mix, and the payload.

Thus, the above equations can also be expressed as:


- or -


The maximum value of mc occurs during the acceleration phase.

It can be simply expressed by introducing a normalized Input-Torque Coefficient, Cc.

Input Torque Coefficient (No Spring Loading, K =1)



for linear motion


for a rotary motion.


= Peak Input Torque

Cc = the maximum of:


The value of Cc, the Input Torque Coefficient, can be evaluated for any motion-law and a range of load mix factors. The input torque patterns for some standard motion-laws are shown (below) for different values of Q and when K=1 [no spring loading]. From these patterns it can be seen that there is a wide disparity between the input torques of different motion-laws, for all values of Q.

Input Torque Coefficient, Cc [K= 1, and Q= 0 – 1]


Drive Torque Fluctuations with each Motion-Law.

It is common to use the maximum value of the Input Torque Coefficient, Cc, when the inertia ratio, Q=1

Simple Harmonic Motion varies smoothly and gradually from a low positive peak to a moderate negative: this is a good characteristic.

However, if this motion-law is preceded or followed by a dwell, then there will be a discontinuity of acceleration at the start and end of the motion, and the dynamic response may be unacceptable.


When the Inertia Ratio is 1, the input torque of the Mod-Trap varies quite suddenly from a high positive to a low negative: this is a bad characteristic.

It can cause severe overrun if the input transmission has low inertia and low rigidity.


When the Inertia Ratio is 1, the input torque of the Cycloidal varies gradually from a fairly high positive to a fairly low negative


When the Inertia Ratio is 1, the input torque of the Mod-Sine varies gradually from positive to negative.
It varies more gradually than, and is better than, Cycloidal.

This makes the Mod-Sine very tolerant of a bad input transmission which, combined with its good dynamic response properties, is the reason for its popularity.


This image shows the:

Peak Values of Input-Torque Coefficient Cc against Q , Inertia Ratio, for each motion-law for constant loading (K=1).

Input Torque Coefficient, Cc [K= 0–1 & Q = 0–1]

The more complex loading pattern that includes a spring load component (0<K<1) we can find that both peak output load represented by Cm and the peak input torque, represented by Cc, are considerably reduced with low pre-load ratios.





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