Engine balance refers to how the forces (resulting from combustion or rotating/reciprocating components) are balanced within an internal combustion engine or steam engine. The most commonly used terms are primary balance and secondary balance. Unbalanced forces within the engine can lead to vibrations.
Causes of imbalance
Although some components within the engine (such as the connecting rods) have complex motions, all motions can be separated into reciprocating and rotating components, which assists in the analysis of imbalances.
Using the example of an inline engine (where the pistons are vertical), the main reciprocating motions are:
- Pistons moving upwards/downwards
- Connecting rods moving upwards/downwards
- Connecting rods moving left/right as they rotate around the crankshaft, however the lateral vibrations caused by these movements are much smaller than the up–down vibrations caused by the pistons.
While the main rotating motions that may cause imbalance are:
- Connecting rods (rotating around the piston end as required by the varying horizontal offset between the piston and the crank throw)
The imbalances can be caused by either the static mass of individual components or the cylinder layout of the engine, as detailed in the following sections.
If the weight— or the weight distribution— of moving parts is not uniform, their movement can cause out-of-balance forces, leading to vibration. For example, if the weights of pistons or connecting rods are different between cylinders, the reciprocating motion can cause vertical forces. Similarly, the rotation of a crankshaft with uneven web weights or a flywheel with an uneven weight distribution can cause a rotating unbalance.
Even with a perfectly balanced weight distribution of the static masses, some cylinder layouts cause imbalance due to the forces from each cylinder not cancelling each other out at all times. For example, an inline-four engine has a vertical vibration (at twice the engine speed). These imbalances are inherent in the design and unable to be avoided, therefore the resulting vibration needs to be managed using balance shafts or other NVH-reduction techniques to minimise the vibration that enters the cabin.
Types of imbalance
A reciprocating imbalance is caused when the linear motion of a component (such as a piston) is not cancelled out by another component moving with equal momentum moving in the opposite direction in the same plane.
Types of reciprocating phase imbalance are:
- Mismatch in counter-moving pistons, such as in a single-cylinder engine or an inline-three engine.
- Unevenly spaced firing order, such as in a V6 engine without offset crankpins
Types of reciprocating plane imbalance are:
- The offset distance between crankpins causing a rocking couple on the crankshaft from the equal and opposite combustion forces, such as in a boxer-twin engine, a 120° inline-three engine, 90° V4 engine, an inline-five engine, a 60° V6 engine and a crossplane 90° V8 engine.
In engines without overlapping power strokes (such as engines with four or fewer cylinders), the pulsations in power delivery vibrate the engine rotationally on the X axis, similar to a reciprocating imbalance.
A rotating imbalance is caused by uneven mass distributions on rotating assemblies
Types of rotating phase imbalance are:
- Unbalanced eccentric masses on a rotating component, such as an unbalanced flywheel
Types of rotating plane imbalance are:
- Unbalanced masses along the axis of rotation of a rotating assembly causing a rocking couple, such as if the crankshaft of a boxer-twin engine did not include counterweights, the mass of the crank throws located 180° apart would cause a couple along the axis of the crankshaft.
- Lateral motion in counter-moving pairs of assemblies, such as a centre-of-mass height difference in a pair of piston–connecting-rod assemblies. In this case, a rocking couple is caused by one connecting rod swinging left (during the top half of its crank rotation) while the other is swinging right (during the bottom half), resulting in a force to the left at the top of the engine and a force to the right at the bottom of the engine.
Torsional vibration is caused when torque is applied at offset distances along a shaft.
This occurs along the axis of a crankshaft, since the connecting rods are usually located a different distances from the resistive torque (e.g. the clutch). This vibration is not transferred to outside of the engine, however fatigue from the vibration could cause crankshaft failure.
Radial engines do not experience torsional imbalance.
Cause of imbalance
A piston travels further during the top half of the crankshaft's rotation than during the bottom half, which results in non-sinusoidal vibrations called secondary vibration.
The difference in distance travelled is due to the movement of the connecting rod. At 90 degrees after top dead centre (TDC) the crankshaft end of the connecting rod is exactly at the halfway point of its stroke; however, the angle of the connecting rod (i.e. the left–right movement, when looking down the crankshaft) means that the piston end of the connecting rod must be lower than the halfway point, in order for the connecting rod to maintain a fixed length. The same also applies at 270 degrees after TDC, therefore the piston end travels a greater distance from 270 degrees to 90 after TDC than it does in the 'bottom half' of the crankshaft rotation cycle (90 degrees to 270 degrees after TDC). In order to travel this greater distance in the same amount of time, the piston end of the connecting rod must experience higher rates of acceleration during the top half of its movement than in the bottom half.
This unequal acceleration results in higher inertia force created by the mass of a piston (in its acceleration and deceleration) during the top half of crankshaft rotation than during the bottom half. In the case of an inline-four engine (with a conventional 180-degree crankshaft), the upwards inertia of cylinders 1 and 4 is greater than the downwards inertia of cylinders 2 and 3. Therefore, despite an equal number of cylinders moving in opposite directions at any given time (creating perfect primary balance), the engine nonetheless has a non-sinusoidal imbalance. This is referred to as a secondary imbalance.
Mathematically, the non-sinusoidal motion of the crank–slider mechanism can be represented as a combination of two sinusoidal motions:
- a primary component with the frequency of the crank rotation (equivalent to what the piston motion would be with an infinitely long connecting rod)
- a secondary component which occurs at double the frequency and is equivalent to the effect of connecting-rod tilting angle that lowers the small-end position from when it is upright
Though the pistons do not move in exactly this fashion, it is still a useful representation for analyzing their motion. This analysis is also the origin of the terms primary balance and secondary balance, which are now also used outside of academia to describe engine characteristics.
Consider a single cylinder engine, with a piston, of mass , moving up and down along the -axis. The piston is connected to the crankshaft by a rod of length . If the crankshaft has a radius , and tends an angle theta, , to the -axis, then the position of the piston, , is given by:
The first part is the component of the crankshaft along the -axis. The second is the component of the connecting rod, as determined using Pythagoras' theorem, whose hypotenuse is length and whose -axis length is .
If the crankshaft is rotating at an angular speed , through an angle in time ,then
The linear speed of the piston along the -axis can be calculated as the rate of change of its -position with respect to time, i.e. , which can be written
- using the chain rule. For a constant angular speed, this becomes
The second derivative will yield the acceleration of the piston. Similarly this can be rewritten as
Consider the crankshaft is being driven around, say by the momentum of a flywheel. The acceleration of the piston corresponds to the force applied to the piston by the crankshaft, using Newton's second law . (The crankshaft in turn feels the inertia of the piston and the reaction force is transmitted through its bearings to the surroundings and felt as a vibration.)
Before differentiating, it helps to make a substitution.
Differentiating with respect to θ:
Nb chain rule:
This is quite unwieldy and does not simplify to anything terribly useful. But it can be simplified effectively using approximations. In a real engine, the connecting rod is longer than the radius of the crankshaft.
Suppose , then . So
Given that :
Similarly, , so if we ignore the smaller term:
Recall that: and So the reciprocating force felt at the axis due to the motion of the piston is
So there is a first component, with a magnitude , with a frequency equal to the rotational speed of the engine, and a second one, with a magnitude , at double the frequency. Smaller but of the same order of magnitude as the first component of magnitude . (The minus sign means that the force is downwards when the right hand side is positive, and vice versa. So when , and the piston is at top dead centre, the force pulling it is downwards and is the maximum value.)
We can see that the effect of the combined crankshaft and connecting rod is to produce a force upon the axis around which the camshaft turns, which has one component that vibrates at the frequency of the rotation of the crankshaft, and a second one of a similar magnitude that vibrates at twice the frequency.
The first component corresponds to the primary balance and the second component to the secondary balance.
In an inline engine, a second cylinder is added parallel to the first one. Suppose that the crankshaft is arranged such that the pistons are apart. When one piston is at TDC, the other is at BDC. The forces that act upon the axis of rotation of the crankshaft combine:
Assume that the weights of the pistons are equal:
So the primary balance component disappears - the engine is balanced according to its primary component forces - but the secondary balance components combine and the two cylinder engine suffers twice the vibration forces as the single one does.
If a four cylinder inline engine is constructed out of a pair of such a two cylinder engine in a back to back arrangement, then by symmetry it will experience the same vibration signature, albeit twice the magnitude.
It is not clear when considering a 4-cylinder engine from a symmetry point of view why it would suffer from any vibration, since it appears that the pistons cancel each other out and might balance. Mathematical analysis shows where the cause of the vibration arises.
Consider a 3-cylinder inline engine, in which each of the pistons are apart, i.e. at , and . For insight into how the angles cancel each other see e.g. List of trigonometric identities.
Consider a 5-cylinder inline engine in which the cylinders are all evenly spaced at apart. The angle are ,, , and . The derivation for the 5-cylinder engine is simplified using the same methods as in the previous case.
The same applies to any number of odd cylinders in an inline engine, the primary and secondary forces will always cancel out to give a balanced engine.
Effects and reduction measures
The vibration caused by secondary imbalance is relatively small at lower engine speeds, but it is proportional to the square of the engine speed, potentially causing excessive vibration at high engine speeds. To reduce these vibrations, some engines use balance shafts. A balance shaft system most commonly consists of two shafts with an identical eccentric weight on each shaft. The shafts rotate at twice the engine speed and in opposite directions to each other, thus producing a vertical force which is designed to cancel out the force caused by the engine's secondary imbalance. The most common use of balance shafts is in V6 engines and large displacement inline-four engines.
Effect of cylinder layout
For engines with more than one cylinder, factors such as the number of pistons in each bank, the V angle and the firing interval usually determine whether reciprocating phase imbalances or torsional imbalances are present.
Straight-twin engines most commonly use the following configurations:
- 360° crankshaft: This configuration creates the highest levels of primary and secondary imbalance, equivalent to that of a single cylinder engine.; but the even firing order provides smoother power delivery (albeit without the overlapping power strokes of engines with more than four cylinders).
- 180° crankshaft: This configuration has primary balance but an uneven firing order and a rocking couple; also, the secondary imbalances are half as strong (and at twice the frequency) compared with a 360° straight-twin engine.
- 270° crankshaft: This configuration minimises secondary imbalances; however, a primary-rotating-plane imbalance is present and the firing order is uneven. The exhaust note and power delivery resemble those of a 90° V-twin engine.
Straight-three engines most commonly use a 120° crankshaft design and have the following characteristics:
- Firing interval is perfectly regular (although the power strokes are not overlapping).
- Primary and secondary reciprocating-plane balance is perfect.
- Primary and secondary rotating-plane imbalances are present.
Straight-four engines (also called inline-four engines) typically use an up–down–down–up 180° crankshaft design and have the following characteristics:
- Firing interval is perfectly regular (although the power strokes are not overlapping).
- Primary and secondary reciprocating-plane imbalances are present.
- Secondary reciprocating forces are high, due to all four pistons being in phase at twice the rotating frequency.
- Counterweights have been used on passenger car engines since the mid-1930s, either as full counterweight or semi-counterweight (also known as half-counterweight) designs.
Straight-five engines typically use a 72° crankshaft design and have the following characteristics:
- A perfectly regular firing interval with overlapping power strokes, resulting in a smoother idle than engines with fewer cylinders.
- Primary and secondary reciprocating-plane balance is perfect.
- Primary and secondary rotating-plane imbalances are present.
Straight-six engines typically use a 120° crankshaft design, a firing order of 1–5–3–6–2–4 cylinders and have the following characteristics:
- A perfectly regular firing interval with overlapping power strokes. The use of two simple three-into-one exhaust manifolds can provide uniform scavenging, since the engine is effectively behaving like two separate straight-three engines in this regard.
- Primary and secondary reciprocating-plane balance is perfect.
- Primary and secondary rotating-plane balance is perfect.
V-twin engines have the following characteristics:
- With a V angle of 90 degrees and offset crank pins, a V-twin engine can have perfect primary balance.
- If a shared crank pin is used (such as in a Ducati V-twin engine), the 360° crankshaft results in an uneven firing interval. These engines also have primary reciprocating-plane and rotating-plane imbalances. Where the connecting rods are at different locations along the crankshaft (which is the case unless fork-and-blade connecting rods are used), this offset creates a rocking couple within the engine.
V4 engines come in many different configurations in terms of the 'V' angle and crankshaft configurations. Some examples are:
- The Lancia Fulvia V4 engines with narrow V angle have crank pin offsets corresponding to the V angles, so the firing interval matches that of a straight-four engine.
- Some V4 engines have irregular firing spacing, and each design needs to be considered separately in terms of all the balancing items. The Honda RC36 engine has a 90° V angle and a 180° crankshaft with firing intervals of 180°–270°–180°–90°, which results in uneven firing intervals within 360 degrees and within 720 degrees of crankshaft rotation. On the other hand, the Honda VFR1200F engine has a 76° V angle and a 360° crankshaft with shared crank pins that have a 28° offset, resulting in 256°–104°–256°–104° firing interval. This engine also has an unusual connecting rod orientation of front–rear–rear–front, with a much wider distance between cylinders ('bore spacing') on the front cylinder bank than on the rear, resulting in reduced rocking couples (at the expense of wider engine width).
V6 engines are commonly produced in the following configurations:
- 60° V angle: This design results in a compact engine size, and the short crankshaft length reduces the torsional vibrations. Rotating plane imbalances. The staggering of the left and right cylinder banks (due to the thickness of the connecting rod and the crank web) makes the reciprocating plane imbalance more difficult to be reduced using crankshaft counterweights.
- 90° V angle: This design historically derives from chopping two cylinders off a 90° V8 engine, in order to reduce design and construction costs. An early example is the General Motors 90° V6 engine, which has an 18° offset crankshaft, resulting in an uneven firing interval. Newer examples, such as the Honda C engine, use 30° offset crank pins, resulting in an even firing interval. As per V6 engines with 60° V angles, these engines have primary reciprocating plane and rotating plane imbalances, staggered cylinder banks and smaller secondary imbalances.
[Precision: A 'flat' engine is not necessarily a 'boxer' engine. A 'flat' engine may either be a 180-degree V engine or a 'boxer' engine. A 180-degree V engine as used in the Ferrari 512BB has opposed cylinder pairs whose connecting rods use the same crank throw. Contrary to this, in a 'boxer' engine, as applied in BMW motorcycles, each connecting rod has its own crank throw which is positioned 180 degrees from the crank throw of the opposed cylinder.]
Flat-twin engines typically use 180° crankshafts and separate crank throws and have the following characteristics:
- Primary and secondary reciprocating plane balance is perfect.
- Primary and secondary rotating plane imbalance is present.
Flat-four engines typically use a left–right–right–left crankshaft configuration and have the following characteristics:
- Primary imbalances are caused by the rocking couples of the opposing pistons being staggered (offset front to back). The intensity of this rocking couple is less than a straight-four engine, since the pairs of connecting rods swinging up and down move at different centre of gravity heights.
- Secondary imbalances are minimal.
Flat six engines typically use a boxer configuration and have the following characteristics:
- An evenly spaced firing interval with overlapping power strokes. A simple three-into-one exhaust for each cylinder bank provides uniform scavenging, since the engine is effectively behaving like two separate straight-three engines in this regard.
- Primary reciprocating plane and rotating plane imbalances, due to the distance along the crankshaft between opposing cylinders. A flat-six engine would have perfect primary balance if fork-and-blade connecting rods were used.
- Secondary imbalances are minimal, because there are no pairs of cylinders moving in phase, and the imbalance is mostly cancelled out by the opposing cylinder.
- Torsional imbalances are lower than straight-six engines, due to the shorter length of a flat-six engine.
This section is an introduction to the balancing of two steam engines connected by driving wheels and axles as assembled in a railway locomotive.
The effects of unbalanced inertias in a locomotive are briefly shown by describing measurements of locomotive motions as well as deflections in steel bridges. These measurements show the need for various balancing methods as well as other design features to reduce vibration amplitudes and damage to the locomotive itself as well as to the rails and bridges. The example locomotive is a simple, non-compound, type with two outside cylinders and valve gear, coupled driving wheels and a separate tender. Only basic balancing is covered with no mention of the effects of different cylinder arrangements, crank angles, etc. since balancing methods for three- and four-cylinder locomotives can be complicated and diverse. Mathematical treatments can be found in 'further reading'. For example, Dalby's "The Balancing of Engines" covers the treatment of unbalanced forces and couples using polygons. Johnson and Fry both use algebraic calculations.
At speed the locomotive will tend to surge fore-and-aft and nose, or sway, from side to side. It will also tend to pitch and rock. This article looks at these motions that originate from unbalanced inertia forces and couples in the two steam engines and their coupled wheels (some similar motions may be caused by irregularities in the track running surface and stiffness). The first two motions are caused by the reciprocating masses and the last two by the oblique action of the con-rods, or piston thrust, on the guide bars.
There are three degrees to which balancing may be pursued. The most basic is static balancing of the off-center features on a driving wheel, i.e. the crankpin and its attached parts. In addition, balancing a proportion of the reciprocating parts can be done with additional revolving weight. This weight is combined with that required for the off-center parts on the wheel and this extra weight causes the wheel to be overbalanced resulting in hammer blow. Lastly, because the above balance weights are in the plane of the wheel and not in the plane of the originating unbalance, the wheel/axle assembly is not dynamically balanced. Dynamic balancing on steam locomotives is known as cross-balancing and is two-plane balancing with the second plane being in the opposite wheel.
A tendency to instability will vary with the design of a particular locomotive class. Relevant factors include its weight and length, the way it is supported on springs and equalizers and how the value of an unbalanced moving mass compares to the unsprung mass and total mass of the locomotive. The way the tender is attached to the locomotive can also modify its behaviour. The resilience of the track in terms of the weight of the rail as well as the stiffness of the roadbed can affect the vibration behaviour of the locomotive.
As well as giving poor human ride quality the rough riding incurs maintenance costs for wear and fractures in both locomotive and track components.
Sources of unbalance
All the driving wheels have an out-of-balance which is caused by their off-center crank pins and attached components. The main driving wheels have the greatest unbalance since they have the biggest crankpin as well as the revolving portion of the main rod. They also have the valve gear eccentric crank and the back end of the eccentric rod. In common with the linked driving wheels they also have their own portion of the side rod weight. The part of the main rod assigned a revolving motion was originally measured by weighing it supported at each end. A more accurate method became necessary which split the revolving and reciprocating parts based on the position of the center of percussion. This position was measured by swinging the rod as a pendulum. The unbalance in the remaining driving wheels is caused by a crankpin and side rod weight. The side rod weights assigned to each crankpin are measured by suspending the rod on as many scales as there are crankpins or by calculation.
The reciprocating piston–crosshead–main-rod–valve-motion link is unbalanced and causes a fore-and-aft surging. Their 90-degree separation causes a swaying couple.
Measuring the effects of unbalance
The whole locomotive tends to move under the influence of unbalanced inertia forces. The horizontal motions for unbalanced locomotives were quantified by M. Le Chatelier in France, around 1850, by suspending them on ropes from the roof of a building. They were run up to equivalent road speeds of up to 40 MPH and the horizontal motion was traced out by a pencil, mounted on the buffer beam. The trace was an elliptical shape formed by the combined action of the fore-and-aft and swaying motions. The shape could be enclosed in a 5⁄8-inch square for one of the unbalanced locomotives and was reduced to a point when weights were added to counter revolving and reciprocating masses.
The effect of vertical out-of-balance, or varying wheel load on the rail, was quantified by Professor Robinson in the U.S. in 1895. He measured bridge deflections, or strains, and attributed a 28% increase over the static value to unbalanced drivers.
The residual unbalance in locomotives was assessed in three ways on the Pennsylvania Railroad testing plant. In particular, eight locomotives were tested at the Louisiana Purchase Exposition in 1904. The three measurements were:
- The critical speed. This was defined as the speed at which the unbalanced reciprocating parts reversed the pull of the locomotive. At higher speeds this motion was damped by throttling oil flow in dashpots. The critical speed varied from 95 RPM for a Baldwin tandem compound to over 310 RPM for a Cole compound Atlantic.
- the horizontal motion at the pilot. As an example, the Baldwin compound Atlantic moved about 0.80 inch at 65 MPH compared with 0.10 inch for the Cole compound Atlantic.
- A qualitative assessment of the load on the plant supporting wheels. A 0.060-inch diameter wire was run under the wheels. Measuring the deformed wire gave an indication of the vertical load on the wheel. For example, a Cole compound Atlantic showed little variation from a 0.020-inch thickness for all speeds up to 75 MPH. In contrast, a Baldwin compound Atlantic at 75 MPH showed no deformation, which indicated complete lifting of the wheel, for wheel rotation of 30 degrees with a rapid return impact, over rotation of only 20 degrees, to a no-hammer blow deformation of 0.020 inch.
Qualitative assessments may be done on a road trip in terms of the riding qualities in the cab. They may not be a reliable indicator of a requirement for better balance as unrelated factors may cause rough riding, such as stuck wedges, fouled equalizers and slack between the engine and tender. Also the position of an out-of-balance axle relative to the locomotive center of gravity may determine the extent of motion at the cab. A. H. Fetters related that on a 4–8–2 the effects of 26,000 lb dynamic augment under the cg did not show up in the cab but the same augment in any other axle would have.
Static balancing of wheels
Balance weights are installed opposite the parts causing the out-of-balance. The only available plane for these weights is in the wheel itself which results in an out-of-balance couple on the wheel/axle assembly. The wheel is statically balanced only.
Static balancing of reciprocating weight
A proportion of the reciprocating weight is balanced with the addition of an extra revolving weight in the wheel, i.e. still only balanced statically. The overbalance causes what is known as hammer blow or dynamic augment, both terms having the same definition as given in the following references. Hammer blow varies about the static mean, alternately adding to and subtracting from it with each wheel revolution. In the United States it is known as dynamic augment, a vertical force caused by a designer's attempt to balance reciprocating parts by incorporating counterbalance in wheels.
The term hammer blow does not describe what takes place very well since the force varies continuously and only in extreme cases when the wheel lifts from the rail for an instant is there a true blow when it comes back down.
Up until about 1923 American locomotives were balanced for static conditions only with as much as 20,000 lb variation in main axle load above and below the mean per revolution from the unbalanced couple. The rough riding and damage led to recommendations for dynamic balancing including defining the proportion of reciprocating weight to be balanced as a proportion of the total locomotive weight, or with Franklin buffer, locomotive plus tender weight.
A different source of varying wheel/rail load, piston thrust, is sometimes incorrectly referred to as hammer blow or dynamic augment although it does not appear in the standard definitions of those terms. It also has a different form per wheel revolution as described later.
As an alternative to adding weights to driving wheels the tender could be attached using a tight coupling that would increase the effective mass and wheelbase of the locomotive. The Prussian State Railways built two-cylinder engines with no reciprocating balance but with a rigid tender coupling. The equivalent coupling for late American locomotives was the friction-damped radial buffer.
Dynamic balancing of wheel/axle assembly
The crankpin-and-rods weight on the wheels is in a plane outside the wheel plane location for the static balance weight. Two-plane, or dynamic, balancing is necessary if the out-of-balance couple at speed needs to be balanced. The second plane used is in the opposite wheel.
Two-plane, or dynamic, balancing of a locomotive wheel set is known as cross-balancing. Cross-balancing was not recommended by the American Railway Association until 1931. Up to that time only static balancing was done in America, although builders included cross-balancing for export locomotives when specified. Builders in Europe adopted cross-balancing after Le Chatelier published his theory in 1849.
Determination of acceptable hammer blow
Maximum wheel and axle loads are specified for a particular bridge design so the required fatigue life of steel bridges may be achieved. The axle load will not usually be the sum of the two wheel loads because the line of action of the cross-balancing will be different in each wheel. With the locomotive's static weight known the amount of overbalance which may be put into each wheel to partially balance the reciprocating parts is calculated. Strains measured in a bridge under a passing locomotive also contain a component from piston thrust. This is neglected in the above calculations for allowable overbalance in each wheel. It may need to be taken into account.
Response of wheel to hammer blow
Since the rotating force alternately reduces the wheel load as well as augmenting it every revolution the sustainable tractive effort at the contact patch drops off once per wheel revolution and the wheels may slip. Whether slipping occurs depends on how the hammer blow compares on all the coupled wheels at the same time.
Excessive hammer blow from high slipping speeds was a cause of kinked rails with new North American 4–6–4s and 4–8–4s that followed the 1934 A.A.R. recommendation to balance 40% of the reciprocating weight.
Out-of-balance inertia forces in the wheel can cause different vertical oscillations depending on the track stiffness. Slipping tests done over greased sections of track showed, in one case, slight marking of the rail at a slipping speed of 165 mph but on softer track severe rail damage at 105 mph.
Piston thrust from connecting rod angularity
The steam engine cross-head sliding surface provides the reaction to the connecting rod force on the crank-pin and varies between zero and a maximum twice during each revolution of the crankshaft.
Unlike hammer blow, which alternately adds and subtracts for each revolution of the wheel, piston thrust only adds to the static mean or subtracts from it, twice per revolution, depending on the direction of motion and whether the locomotive is coasting, or drifting.
In a double-acting steam engine, as used in a railway locomotive, the direction of the vertical thrust on the slide bar is always upwards when running forward. It varies from nothing at the end of stroke to a maximum at half stroke when the angle between the con-rod and crank are greatest. When the crank-pin drives the piston, as when coasting, the piston thrust is downwards. The position of maximum thrust is shown by the increased wear at the middle of the slide bars.
The tendency of the variable force on the upper slide is to lift the machine off its lead springs at half-stroke and ease it down at the ends of stroke. This causes a pitching and, because the maximum up force is not simultaneous for the two cylinders it will also tend to roll on the springs.
Similarities with balancing other machinery
The dynamic balancing of locomotive wheels, using the wheels as the balancing planes for out-of-balance existing in other planes, is similar to the dynamic balancing of other rotors such as jet engine compressor/turbine assemblies. Residual out-of-balance in the assembled rotor is corrected by installing balance weights in two planes that are accessible with the engine installed in the aircraft. One plane is at the front of the fan and the other at the last turbine stage.
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