r.j. gayler - bg tuning manual
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tuninng manualTRANSCRIPT
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The BG Tuning Manual
Page 1
CHAPTER ONE
POWER!
Horsepower.... What exactly is it?
Wherever people gather to talk motoring, motorcycling or motor sport of any kind it is only a matter
of time before the word power comes into the conversation.
But very few people really understand what horsepower is.
The dictionary definition is....
A unit to measure the rate of doing work...
Not a lot of help for someone trying to make crucial
decisions on how to tune an engine!
Yet every rider and driver knows the feel of power...
The surge of acceleration as the throttle is opened, the
clutch dropped, and suddenly the wheels are spinning -
thats the feel of high power.
Even as you wind back the twist grip of your 50cc
moped, its power that gets you moving, even though not
quite so sexy.
In fact, nothing moves without power - clockwork toys,
elastic band propelled pellets, human beings on bicycles,
Harrier jump jets... all need power, large or small, to
move at all.
A simple falling stone uses motive power from the
kinetic energy imparted when someone or something lifts
it against the pull of gravity.
So power can also be defined as the result of converting
work into movement.
And the internal combustion engine happens to be one of
the most convenient ways of producing movement.
All you need to do is pour the fuel in at one end, pull the
right knobs and levers... and instant power comes out the
other end.
The engine thus converts fuel into movement.
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But what exactly, is fuel?
Fuel is neatly packaged heat...
Anything that burns when a match is applied is potentially capable of producing power, in this case
petrol/gasoline or methanol.
So the engine is a heat converter and of course this is why, when this subject is studied in college, it
is entitled heat engines.
Two stroke or four stroke, one cylinder or sixteen, the conversion process is always carried out in
the same way - by drawing in a mixture of fuel and air, compressing it, igniting it and using the
resultant combustion to drive a piston or turbine down or round, and rotate a crank.
When the engine converts fuel into power, the process is rather inefficient and only about a quarter
of the potential energy in the fuel is released as power at the flywheel. The rest is wasted as heat
going down the exhaust and into the air or water.
This ratio of actual to potential power is called the THERMAL EFFICIENCY, of the engine.
The machine we use to measure engine performance is a dynamometer and the way in which it
works is closely tied to the explanation of power.
MEASURING POWER
The term Horsepower, was evolved during the 19th century to describe the capability of engines to
carry out a measure of work related to the conversion of energy into motion by the horse.
At that time it was a realistic way of comparing mechanical power to horse power.
The unit of engine horsepower, which used to be called B.H.P, the abbreviation of Brake Horse
Power, is now being replaced with the Watt, hitherto used to quantify the power of electric
motors and other appliances.
One B.H.P is the equivalent of 746 Watts.
Both of them are a measurement that describes the power that is actually measured at the flywheel.
A dynamometer is not actually capable of showing power as a direct reading, but measures torque
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and R.P.M, from which power is calculated.
Engine Data Acquisition Systems are electronic measuring system that captures information from
an engine or chassis dynamometer, then automatically calculates the power.
Torque is the amount of work that an engine is actually doing at any given moment, that is, the
turning force being exerted at the crankshaft, and is measured in Foot Pounds, or Newton
Metres, depending on whether you are using the British Imperial or the International Metric
System.
Imagine an engine sited at the top of a deep well turning a drum,
which is four feet in diameter, i.e. 2 feet radius.
A rope attached to the drum is hanging down the well with a weight
of 100 lbs. on the end.
As the engine turns the drum it will lift the weight. The drum is
four foot in diameter and the rope is being pulled in at two foot
from the centre of rotation; therefore the work being done or torque
is measured as 2ft x 100lbs = 200 foot pounds
The speed at which the drum is rotating is measured as Revolutions
Per Minute (R.P.M).
B.H.P is calculated as follows
TORQUE X R.P.M
B.H.P = -------------------
CONSTANT
The constant depends on the units of torque, which are being
measured. As we are using ft.lbs it will be 5250, so if we say that
the engine is turning at 1000 R.P.M then:
200 x 1000
B.H.P = ------------------- = 38
5250
Because we cannot calculate B.H.P without knowing the R.P.M, it means that B.H.P is a measure of
the speed at which work is done as previously mentioned, a unit to measure the rate of doing work.
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To understand the way in which the
dynamometer works, imagine anchoring a
spring balance to the ground, with a rope
attached to the top eye and wrapped around a
drum with a slipknot is tightened as the drum
is rotating, the rope will be tensioned and the
balance will extend to indicate this tension as a
weight. As the knot is further tightened,
friction between rope and drum will slow the
drum and its driving engine until, at 1000
R.P.M, the spring balance reads 100 lbs.
The weight being lifted is 100 lbs and the
speed of the drum or engine will then be used
in the formula to calculate the horsepower.
If the speed of the engine/drum were 1000 R.P.M the B.H.P being exerted would be 38. If the speed
were 1500 R.P.M this would mean the engine was lifting the weight faster and exerting more power
to do it. The calculation would then be:
200 x 1500
-------------- = 57 B.H.P
5250
THE DYNAMOMETER
So a piece of rope, a spring balance, a rev counter and an engine fitted with a flywheel or drum to
take the rope is all you need to make a dynamometer
Well, yes but! if the throttle is wide open and nothing is moving where is all the power going?
The answer is, that its turning back into heat again.
Where?
Youve guessed it! Between the drum and the rope - as friction.
So although the idea of a cheap dyno sounds good, in fact the power being used, turning into
friction heat, would set fire to the whole lot.
Unless, of course, we cool it by pouring water over it, and thats just what the modern dynamometer
does.
It uses a device like the torque - converter of an
automatic transmission to do the job of the rope
and drum and is running in a continuous flow
of cooled water to absorb the heat.
The engine turns the inner part of the torque -
converter and the water drag thus created tries
to turn the outer casing, which is coupled to a
big accurate weighing machine reading torque.
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Now that we understand the meaning of power and how to measure it just how important is it?
Does an increase in power automatically mean higher speeds?
Not necessarily power is only of value when applied with suitable engineering skill. Smooth,
controllable power will often return better results than ultimate B.H.P peaking over a narrow rev
band. This is often the secret behind the out-performance of many smaller racing machines over
their more powerful contemporaries.
WHAT CONTROLS POWER?
HOW CAN IT BE IMPROVED?
An engine very much like a human being. It takes in air and fuel(food).
It burns the fuel (digestion). It converts the energy released into power (muscles).
Discharge of exhaust (bowels). Oil pump and circulation (heart).
Cooling system (pores). Pistons and cylinders (lungs).
The camshaft (brain) coordinates of the whole sequence of operations in the same way as the brain.
The efficiency of these individual functions effects engine performance in the same way they would
affect a human.
Poor or contaminated fuel will have low energy content.
Bad ignition or combustion chamber shapes will reduce the ability to digest the fuel fully, resulting
in an unpleasant and dirty exhaust.
Clogged or inadequate oil filters or a worn oil pump will result in component failure.
A dirty cooling system with clogged radiator pores will result in overheating.
A poorly designed camshaft will result in erratic breathing.
They all work together to produce the final flywheel muscle power, however good or bad.
To understand the process well start with the breathing cycle.
If we think of the engine as an air pump then theoretically it should draw in and exhaust its own
volume of air each time it cycles - that is, once every revolution if its a two stroke and once every
two revolutions if its a four stroke. In fact, ordinary production engines dont achieve this and only
manage to shift about 80% of their volume.
This ratio of possible air pumped to actual air pumped is called Volumetric Efficiency and this is
what we have to improve to get more power. The difference in appearance between two engines of
similar type, one of which is in standard road trim and one in full race trim can be seen on the left.
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Fig.11 is a standard street Honda 750 four and Fig.12 is a
full race version of the same model. The noticeable
external differences in the engine preparations are to
increase the VOLUMETRIC EFFICIENCY.
Volumetric Efficiency = Breathing Ability = Power
A chain of parts controls the breathing cycle, each one of
which depends on the others to work at its best.
The process starts right back at the air cleaner which
varies from being a large box containing a large paper
filtration and silencing element, necessary for silent
operation and engine protection under a variety of dusty
and sandy conditions, through to the light and minimal
filters of rally cars and speedway bikes, to the completely
open bell mouths of full circuit drag machines.
The next link in the chain is carburetion. The process of mixing the fuel and air and feeding them to
the engine in balanced doses, that is about fifteen times as much air as fuel.
Fifteen to one - air fuel/ratio - another important controller in a final power output!
Although we call it carburetion, here it can also include fuel- injection, just another method of
delivering fuel to the engine.
So, via inlet manifolds or stubs we move to the next link and here it is where the two stroke and
four stroke engines divide.
11
12
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FOUR STROKE TWO STROKE
AIR BOX OR CLEANER
RAM - PIPE
CARBURETTOR
FUEL - INJECTION
INLET MANIFOLD
CYLINDER HEAD CRANK CASE
PORTING PISTON VALVE
INLET VALVE PISTON SUPERCHARGER
CAMSHAFT TRANSFER TIMING
COMBUSTION
EXHAUST VALVE EXHAUST PORT TIMING
SIMPLE PARALLEL COMPLEX MULTI-
PIPE EXHAUST SYSTEM TAPER SYSTEM ONLY
COUPLED WITH MULTI COUPLED WITH 3
CYLINDER ENGINES CYLINDERS
POSSIBILY A EXPANSION CHAMBER,
SIMPLE REVERSE CONE
MEGAPHONE RESTRICTIVE TAIL PIPE
150+ BHP / LITRE 200 BHP / LITRE
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The four-stroke chain of power
The mixture
enters the cylinder
head and is
induced through
the inlet valve into
the combustion
chamber. The way
in which it enters
the chamber is
controlled by the
port shape and finish inlet valve timing, which
in turn is controlled by the camshaft.
The camshaft is probably the most important single component in the four stroke engine, as far as
power production is concerned, and it is certainly the most complicated piece to design and produce
(P.17).
Compression takes place followed by ignition and combustion - the point at which four- and two-
stroke reunite in a common process.
Exhaust in a four-stroke engine is again first controlled by the camshaft operating the exhaust valve,
and then by the design of the port and the exhaust system, which in turn, has a considerable effect
on exhaust efficiency (P.18).
The two-stroke chain of power.
There are several ways in which the two-stroke engine will
work but we will consider the modern loop-scavenge design,
which is the most commonly used production version.
(Fig.19)
As the piston rises, a depression is created in the crankcase
and the mixture is drawn in at the point where the piston
skirt starts to uncover the inlet point. As the piston comes
down, the inlet port is closed and the charge is compressed
and driven up the transfer port into the combustion chamber.
Because the mixture is being forced into the chamber under
pressure, this is really a form of supercharging and is one of
the reasons that this type of engine can produce so much
power relative to its size.
19
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As the piston rises again, compression takes place, followed by ignition and combustion, driving the
piston down which opens the exhaust port and drives a new charge into the combustion chamber at
the same time. Because these two happen together, the design of the transfer port and the exhaust
system must be just right in order to clear the foul gases and ensure a full charge of new mixture
without wasting any down the exhaust port.
Although the two designs appear to be very different, the overall function of both is the same - fuel
into power, the level of which is governed by volumetric efficiency.
The significant part of the power train chart is the point where the two engines coincide at
combustion. The key to high power output is fast, controlled, near total burning of the compressed
mixture. This key is common to all types of internal combustion engine and is dependant on all the
parts around it.
Next well start to look at those parts in detail.
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CHAPTER 2. BREATHING - THE INDUCTION SYSTEM.
AIR BOXES AND CLEANERS.
The need to use an air box at all must be judged by the environment surrounding the engine and in
which the vehicle is going to be used.
For example, while it is unlikely that a motorcycle needs any additional cold air fed into the carbs,
the engine compartment of a car is often very hot and poorly ventilated, so the argument for an air
box here is to get cold air from the front of the car, under the bonnet to the carbs.
On the other hand, if the bike or car is going to be used in excessively dusty or sandy conditions,
then an air box and filter are essential.
General rule of thumb is that vehicles used for pure circuit work or fast roadwork, including
dragsters, in Europe, can do without any air box at all, except during the occasional long hot
summer when the dust level is high.
This all supposes that you are prepared to put up with the induction roar of unsilenced intakes.
It goes without saying that autocross, rally, dirt and grass track vehicles all need cleaners. The
important thing is to apply the air box in the right way.
In order to avoid upstream restrictions, it should be sited at the
point at which the induction pulse can expand in the same way as
if there were no box there at all, i.e. the bell mouths should be
allowed to protrude into the box with adequate clearances and the
measurement "A" should be at least as great as the carburettor
bore size.
Tubular couplings as seen here will effectively increase the
tuned ram length to an RPM level that will probably be too
low.
RAM LENGTH is effectively the tuned length from the
inlet valve head or piston port face, to the end of the intake
trumpet.
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At the moment that the valve or port first starts to open, a pressure wave starts to travel back and
forth through the inlet tract, changing from plus pressure to minus pressure, or effective suction.
If the wave front is caught at the right moment, it can be used to help ram mixture into the engine,
thus inducing a form of mild supercharging. You can calculate approximate correct ram length
using the formula below, where L = length.
For a four-stroke:
228 x T 5791 x T
L in ins = --------------- in mms = -------------------
N N
Where T = Total intake valve duration in degrees
N = The estimated RPM at which max. power is required, minus five hundred
And for a two-stroke:
1150 x T 29210 x T
L in ins = --------------- in mms = --------------------
N N
Where T = Inlet port opening in degrees
N = The estimated RPM at which max. power will be achieved.
The two-stroke calculation will result in a length that is too great to be practical and may be divided
by 3 or 5 to fit installation requirements.
Ram pipes or trumpets should have fully round ends.
Contrary to general belief, much of the intake air is drawn in around
the edges of the mouth and, if there are sharp edges in this area, flow
will be interrupted and turbulence will cause restriction in the bell
mouth.
This is also the reason why bell mouths should be allowed to protrude
into the air box rather than finish flush with the wall.
The position of the air entry to the box is not critical provided it is not
within 50mms or so, of the bell mouths.
CARBURETTORS.
In order to increase power the process of improving volumetric efficiency is invariably tied up with
an increase in the operating RPM. However, if we increase RPM, then we will inevitably be
increasing the air speed in the inlet tract, which includes the carburettor.
The size of carburettor that is normally suitable for the standard engine is rarely large enough for
any appreciable increase in the state of tune other than stage 1.
Stage 1 modifications can vary from one engine to another but generally comprise a mild increase
in cam profile on a four-stroke or lengthening of inlet and exhaust timings by about 5 degrees on a
two- stroke, raising compression by about one ratio, smoothing out porting and possibly fitting a
high performance exhaust system.
Even at this level the engine can easily be strangled by its standard carburetion. So any further
increase means that we are inevitably faced with the need to up rate the carburetion.
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To evaluate the European options available, we will first divide them into two types depending on
their principles of operation:
Fixed choke, butterfly air control.
Weber and Dellorto
Other fixed choke carburettors are available but are impractical due to lack of adjustable features.
Variable choke, butterfly air control, constant depression (CD) S.U., Stromberg C.D., Mikuni.
Variable choke, manual slide control of air and fuel. Amal, Bing, Keihin, Mikuni, Dellorto.
Suitability and convenience of application:
1. Weber D.C.O.E. series side draught
I.D.A. and D.C.N series downdraught
Size range from 38mm to 48mm.
Without doubt the best high performance carburettor available in the world for application in cars.
Wide range chokes and jets readily available for applying
to any engine.
The sealed throttle spindles make them particularly
suitable for up- stream supercharging.
Usable for motorcycles but rather big and bulky for
average application, also needs special fuel delivery
requirements, i.e. pump delivery or modified needle
valves.
2. Dellorto D.H.L.A. series sidedraught
F.Z.D. series sidedraught
Size range from 20mm to 48mm
D.H.L.A. series similar to Weber D.C.O.E. but not quite as efficient in terms of air flow.
Not quite the same range of variables available.
Other series are readily adaptable to motorcycle applications.
3. S.U. - Size range from one and a quarter to two inch .
The most widely used performance carburettor up to the late 70s.
Very popular for road conversions. Very adaptable with wide range of tuning needles available.
Tend to suffer fuel surge on high cornering G-forces.
4. STROMBERG C.D. - Size and range from one and a quarter to one and three quarters of an
inch.
Similar in operation to S.U. Not such a wide range of needles, application not quite so simple.
5. MIKUNI & KEIHIN - Both make C.D. carburettors for use on road bikes and also make manual
slide control versions for use on racing bikes.
They are available as kits for some production models but generally, they are difficult to apply to
other models due to the lack of non-standard jets and needles.
Properly set up, they make efficient and reliable racing carburetion.
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6. AMAL - size range 25mm - 42mm
The most popular and successful motorcycle carburettor over many years.
Very adaptable to almost any engine and very forgiving to slight errors in tuning.
All carburettors, whatever the make, suffer, to a degree, from two major faults...
Fuel frothing due to vibration and float chamber fuel surge due to cornering G-forces.
In many cases these can be minimised by careful attention to flexible mountings, float levels,
needle valves and springs where applicable.
CARBURETTOR SELECTION
Refer to the Staging table in the camshaft section of the manual for Stage descriptions.
Stage 1. There is no real point in modifying even slightly if the standard engine is not of the GT
type, which is really the manufacturer's first mild production tuning step from his basic engine.
Carburetion at this stage will generally be two small C.D.'s or a single progressive twin-choke
which will only require needle or jet changes for Stage 1.
Stage 2. Increase in volumetric efficiency at this point will call for an increase in size of C.D.
carbs. e.g. 1300cc engine running on 2 x 1.25 inch S.U.s will need to move up to 1.5 inch units. Or
will need a large choke version of twin-choke DD carb.). Also will need a change of air cleaners to
free-flow type. At this stage single choke injection systems can be considered as a possible
alternative.
Stage 3. Further volumetric efficiency improvements now create a "grey area" in which well-
engineered twin carbs, or single choke injection, will still do the required job, but the move toward
one choke per cylinder must be seriously considered. Cylinder sizes up to 400 cc will require a
40mm carburettor with 30 to 34 mm chokes fitted e.g. Ford 2000cc four cylinder will need 2 x
48DCOE Weber or DHLA Dellorto.
Stage 4. One choke per cylinder is now essential to fully justify other engine modifications.
Available choices are Weber DCOE, Dellorto DHLA, Amal, Keihin or Mikuni smooth bores.
Carburettor sizes will need to be as follows for various cylinder sizes:
250cc 40mm with 32-34mm choke or injection bore.
400cc 45mm with 36-40mm choke or injection bore.
500cc 48-52 with 40-46mm choke or injection bore.
Stage 5/6 As above except that we now move into the area where individual engine build
specifications will dictate precise intake breathing requirements, and it is no longer possible to
predict general sizes.
Only dynamometer testing of the engine build combinations will produce the most effective results
from carburetion or injection variants.
At best, initial carburetion choice can only be a compromise generally suited to the user's overall
requirements and will eventually have to be adjusted accordingly.
Genuine designers and suppliers of good high performance equipment will be able to advise you on
jet settings for your individual needs.
Beware of buying cheap unrelated tuning parts; nobody will be prepared to advise you on the
tuning details needed to complete a satisfactory job.
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FUEL INJECTION, THE ALTERNATIVE
The term "fuel-injection" should really only describe the process of injection directly into the
combustion chamber, in the same way that a diesel engine functions.
The last petrol engine of any note to do this, was the Mercedes 300SL and generally, the design
was discarded due to impracticality and high cost. That engine also used desmodromic valve gear,
but more of that later.
However, direct injection has recently been introduced in a small range of modern cars.
Generally, present day injection systems squirt fuel into the inlet manifold or cylinder head close to
the inlet valve. They are really just another form of carburetion, classified under the expression
"pressurised fuel metering systems", and of course, are now all controlled by microprocessor
engine management systems.
All injection systems work on the same basic principle. A series of signals from the engine are
monitored and used to produce a squirt of fuel of the correct size at the correct time. The important
signals that need to be measured are:
1. Engine speed - sensed electronically by a transducer on the crankshaft.
2. Throttle position - measured electronically and indicating the driver's power call-off from the
engine at any time, e.g. the sudden change from one eighth open to full open indicates driver
requirement for sudden acceleration and therefore mixture richness is fed in accordingly.
3. Engine air consumption or volumetric efficiency. A big thorn in the side of injection equipment
designers. Measured electronically now, but on earlier systems, measured mechanically by use of
manifold pressure sensing devices or by a 'floating' air bell in the induction tract. This is very
sensitive but can be subject to problems of dirt deposits causing 'sticky' operation. It is also
difficult to modify when the engine is up rated because it is critical in design and in itself offers an
obstruction to clean airflow.
Various other controls are introduced depending on the sophistication of the system or the
individual requirements of the manufacturer. Such devices as atmospheric pressure, temperature
and exhaust gas analysis sensors, feed signals to a microprocessor, which in turn, digitally instructs
the metering system to correct the fuel flow accordingly.
But, regardless of the level of the additional sophistication, all systems have to work around the
three basic control parameters listed above.
Most injection systems are purpose-designed for the vehicle to which they are fitted and are
difficult to re-adapt for other engines.
Systems used on formula 1 and 2 cars are available in component form to be used on any engine,
but the responsibility for adapting and fitting, include determination of the computer control
software to suit fuel requirements lies with the customer, a formidable task for anyone who does
not have expensive test equipment.
Bosch were far and away the world leaders in supply of electronic fuel injection systems or
technology licensing, but an increasing number of other manufacturers are now offering
alternatives, many based on the Bosch technology.
Although their then "state of the art" systems, fitted to high performance market leaders like
B.M.W. and Mercedes were based on the fully electronic "L" system, other then current models
like the 4/4 Ford Sierra, still used the out of date mechanical "K" system, though at the expense of
poor fuel consumption and high emission levels and maintenance costs.
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Carburettor manufacturers Weber, started to offer retro-fit fuel injection system, programmably
adjustable with a PC desktop computer, and incorporating an electronic ignition system controlled
from the same processor.
A low-cost alternative system designed to be fitted at manufacturing stage, was developed in the
Piper workshops over a period of a few years, and was made available as an electronic multi-point
carburetion system for high volume production vehicles.
The table below lists the variations of driving conditions and the resulting demands put on any fuel
metering system, whether carburetion or injection.
Driving Throttle Engine Volumetric Fuel
Condition Position Speed Efficiency Requirement
Cold start Closed to Low Poor Rich
15%
Hot start 15% Low Poor Weak
Cruise at 70
motorway flat 20% Med/high Poor Weak
or downhill
Flat out flat
road 100% High Good Med.
Accelerate on
steep hill 50 - 100% Low Poor Med.
Dragster start
from lights 100% Low Poor Rich
Cruise at 70
slight uphill 60% Med Med Med.
Shut throttle
suddenly from Closed High Poor Near zero
150 mph
The difficulty of meeting all these possible combinations makes the carburettor look good value for
money and it is.
However the requirements of greater economy, together with reduced exhaust emission levels, were
necessitating the change to a much greater level of sophistication in carburettor design and were
inevitably leading us into the era of electronic carburetion.
In racing, this had been the case since the early seventies.
Further discussion of electronic fuel systems may be found in the section on electronic engine
management.
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INLET PORTS AND VALVES
The transition of the manifold from the
carburettor or injection air control body
to the port and valve should be as a
gradually reducing cross-sectional area
from the bell mouth at the atmospheric
end of the tract, right through to the
intake valve head (Fig. 43), in order to
ensure that efficient maximum gas
velocity is achieved.
This is around 400ft/sec. (122
metres/sec.) and should be achieved as
close to the valve as possible.
In the case of the four-stroke, this will be just upstream of the valve guide boss where the port must
start opening out to reduce velocities in the throat and around the valve head.
For the two-stroke, maximum velocity can occur at the piston skirt face.
Having calculated the correct minimum throat diameter, the intake tract should progressively
converge to that size from the bell mouth, at a rate of approximately 4mms in 100, (4%) or an
included angle of 2-3 degs.
This taper in the intake tract is to compensate for the gas drag that occurs in any flow system, and
that would otherwise tend to restrict the effective cross-sectional area.
Minimum intake throat diameter, related to cylinder capacity and RPM.
Sq Mms/Litre/Cylinder
1 sq. in. = 645 sq. mms
So if you have a 500cc
cylinder capacity and the
engine is tuned to produce
max. power at
7000 rpm, then the
minimum port
section at
the throat should be
1800/2 = 900 sq. mms.
= 1.39 sq. ins.
1.4 sq. ins. area = 1.33 ins. dia.
43
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When we refer to the valve, we mean of course the poppet valve in the four-stroke engine as
opposed to the sleeve valve, long ago discarded in four-stroke engines, but still retained by the two-
stroke in the form of the piston skirt opening and closing the cylinder ports.
It is a great pity that the efficient flow characteristics of the poppet valve are denied the two-stroke,
due to the difficulty of driving them at crankshaft speed.
Nevertheless, the facts are
unavoidable: a well
designed inlet port and
valve (Fig. 45) achieves a
discharge coefficient
approaching 100%, whilst
the sleeve valve of the
two-stroke (Fig. 46) only
reaches about 80% at its
most efficient.
The discharge coefficient is the ratio of the amount of gas that will pass, compared to its size.
There are many publications illustrating the detailed cylinder head modifications that should be
carried out on specific models of engine, so I do not intend to waste time and space by re - covering
old ground here.
However, there are some vital signs and rules that should be observed, regardless of the hardware
that is being worked on.
Gas flow within the intake system, particularly around
the valve head and stem, is highly complex and almost
impossible to visually depict other than in an animated
diagram.
Every irregularity in the flow path causes vortex
shedding to occur (Fig. 47), which effectively reduces
the efficiency of the system.
Vortex shedding is the effect of tiny swirls of gas being
generated at every sudden change of direction or size.
When re-working an intake system, the simplest
approach is to imagine yourself as the slug of intake gas,
moving along the tract.
Each obstruction or change of section that would upset
or irritate your path will be equally disturbing to the
inlet charge flow.
All inlet tract joints should be accurately matched, i.e. carb to manifold and manifold to port,
including gaskets.
Every stepped joint will cause turbulence in the stream and will sap valuable energy from the
ingoing charge.
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46
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All corners should be radiussed to remove
potential flow interruption, but not at the cost
of removing too much metal and losing the
correct shape for example, in (Fig. 48)
careless removal of metal at "A" will result
in a port flow that is so bad it would have
been better left as standard.
The black area shows the correct
modification.
Inlet valve guide bosses can be smoothed
and streamlined but the valve stem is
unalterably round and will eventually control
the turbulent pattern in the throat.
In some ports there is a case for removing the inlet guide and boss right back to the port wall,
providing there is sufficient guide length left to fully support the valve and hold it square on the
seat.
Areas adjacent to the inlet valve seat should be radiussed to create a smooth blend from port wall to
valve seat and from seat to combustion chamber roof. Careful attention in this area alone can raise
the flow coefficient by over 10%.
Similarly, the shape of the valve head is of great importance and, although true individual valve
head shape can only be determined by knowing the characteristic of the port, as a general rule of
thumb, "flat" approach ports, as used in Mini A-series engines work best with "penny on a stick"
valve heads, while downdraught ports give best flow with a "tulip" or spherically backed valve
head.
Highly developed racing engines invariably have steeply down-draughted intake ports to assist the
inlet flow across the valve head.
Although the general design for these engines is the pent-roofed, four valve layout, the Yamaha
FZ750 used 5 valves per cylinder and had even experimented with seven valves, in the interests of
improving the intake flow process.
Two-stroke inlet valves.
Two-stroke piston skirts can be re-worked to ensure that they fully clear the top of the port and, if it
has any downdraughting, should be chamfered to match.
Although the sharp edges can be broken to assist flow at small openings, radiussing should not be
carried out because this will make the port timing unstable.
Inlet valve timing.
Four-stroke.
Average production engine timing duration is from 240 to 260 degrees, with opening points
varying from 5 degrees to 25 degrees before T.D.C. and closing from 40 degrees to 55 degrees after
B.D.C.
Valve lifts range from 8.0mm for a 250cc cylinder to 10.0mm for a 500cc cylinder. These engines
will be giving about 60 Bhp/L and produce maximum power between 5200 and 5800 rpm.
A
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If we increase the level of tune in "stages", then these characteristics will alter as indicated in the
chart below.
Stage Application Inlet V Timing Valve lift (mms) Potential
BTDC ATDC 250cyl 500cyl Bhp/L
Std. Std. Saloon 20 50 7.0 10.0 50
St 1 Improved std. 30 60 9.0 10.5 62
St 2 Rally M/cross
Grasstrack 40 70 9.5 11.0 80
St 3 Race 1 50 80 10.0 11.5 95
Race 2 58 88 10.0 11.5 105
SPL Super/ch Drag 62 92 10.0 12.0 150
SPL Turbo/ch Race 45 85 10.0 12.5 150
Specially developed racing four-strokes running high boost pressures, and ultra-high revving two-
strokes will develop in excess of 200 Bhp/L.
TWO - STROKE PORT TIMING
Because the piston uncovers the ports equally on its up and down strokes, it has symmetrical
timing unless disc or other forms of rotary valve timing control are added.
These methods of control invariably increase the cost and complexity of the engine, which is a pity
because the two-stroke does respond to asymmetric changes in inlet timing.
Whilst, in general, slight changes in inlet opening do not give power improvements, the same
changes in inlet closing certainly do. Therefore, while it is necessary to lengthen inlet timing to
increase power and rpm, the low speed power losses are enormous, hence the need for a lot of gear
ratios.
This effect can be offset slightly by the use of reed valves in a piston ported engine, but, whilst they
increase low and mid-range power, they lose a certain amount of top end power due to the flow
restriction and the fact that, even though the reed is very light, it still has inertia which has to be
overcome by the inlet stream. This in turn means that the small amount of energy required to move
the reeds must be taken from the inlet stream which therefore loses some of it's high speed ram
effect.
Previous reference has been made to the fact that the loop/scavenge or conventional crankcase
induction two-stroke is really a supercharged engine because it sucks the gas into the crankcase and
then blows it into the combustion chamber.
Why, therefore, doesn't it produce as much power as an externally supercharged engine?
The reason is that the petrol/air mixture is fouled, either by its own intrinsic oil content or by being
exposed to injected hot oil being sprayed around the crankcase.
It is also pre-heated by thermal transfer, from the surrounding hot components, further heated by
compression through the transfer ports before being subjected to combustion.
All this means that the combustion process is not as efficient as a four-stroke but, because it
happens twice as often, it can still produce good power.
Approximate changes in staged tuning of the inlet are shown in this table.
Application Inlet duration RPM Potential
Open Close at BHP/L
BTDC ATDC max.
power
Std Street 70 70 7000 80-90
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Stage 1 78 78 8500 100-120
Stage 2 90 90 12000 150-250
The choice between piston-valved and disc-valved
two-stroke racing engines is still argued out and
successful machinery is divided into both categories.
The successful Yamaha's (Fig. 51) retained piston
valves as did most of the motocross bikes (Fig. 52),
but tended to combine reed valves as well.
On the other hand the RG 500 Suzuki and KH250
Kawasaki (Fig. 53), got their results using rotary disc
valves.
51
52
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CHAPTER 3.
COMBUSTION - THE POWER STROKE.
Four-stroke and two-stroke characteristics re-unite during the process of combustion.
In both cases, a fast efficient burn is THE major key to high power output, and the factors that
control it are common to both.
As the piston rises, the mixture is compressed and consequently undergoes a rise in temperature.
As the cylinder pressure rises to about 13.6 bar (13.6 x Standard Atmospheric Pressure), which will
occur somewhere between 20 and 40 degs. before T.D.C., the plug fires and the combustion
process starts.
Once again, it must be stressed.....
IT IS A PROCESS OF BURNING! - IT IS NOT AN EXPLOSION!
An explosion is the result of uncontrollable detonation, which does occur in the internal
combustion engine occasionally and, if allowed to continue unchecked, produces disastrous results.
As combustion continues, the cylinder pressure rises to between 54 to 68 bar (Fig. 54), to create the
driving force on the piston crown.
This maximum pressure varies with engine design, but a good thumb rule is that it will be about
one hundred times the compression ratio.
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The efficiency with which combustion takes place is controlled by a number of important factors
that readily respond to adjustment or modification and are equally applicable in both two- and four-
stroke engines.
They are as follows :
Swirl - Control of movement of the inlet mixture as it enters the combustion chamber, as a result of
the correct shaping or reshaping of the inlet port and valve, or the transfer port.
This results in a turbulent pattern within the inlet charge, which in turn creates a pre-mixing effect
on the richer and weaker portions of the charge and assists even burning.
Fig. 55 shows an example of perfect swirl control imprinted in the light carbon on the piston crown
of a well-modified engine.
Fig 55a shows a graphical example of the same effect, as it would be created by the correct shaping
of a two-stroke port layout.
In engines with two valves per cylinder, swirl will take place around a vertical axis, forming
layered pancakes or doughnuts of mixing gas.
In engines with four valves, the swirl is created around a horizontal axis forming wave-like rolls of
mixing gas.
In either case, the object is to induce a gas movement that holds the fuel vapour in suspension with
the air and packs it evenly into the cylinder space, ready for compression.
55 55a
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Combustion chamber shape and finish - A neat, minimum combustion chamber area, ensures that
flame-spread is rapid and progressive, permitting the ignition process to be delayed as long as
possible, i.e. a minimum of spark advance. (See section on ignition control)
This is one area in which the two-stroke engine really scores, because
its' lack of valve head intrusion in the combustion chamber means
that the chamber can be of near perfect, small part spherical design,
with the plug in the centre. (Fig. 57)
In all cases combustion chamber surface finish should be smooth and
highly polished to reflect heat back into the chamber and to retard the
build-up of carbon related deposits that can cause detonation or run-
on.
Having selected the desired compression ratio, chamber volumes should be balanced to within half
a c.c. between all cylinders.
Squish - The final compressive shock received by the charge, immediately before the start of
combustion.
Created by close proximity of certain areas of the piston
crown to the cylinder face at T.D.C. (Fig. 58), squish is
used to drive the compressing charge into the most suitable
area for start of combustion.
The squish gap should be as small as is practically
possible, and can be as little as 0.5 mm or less, depending
on crank and con-rod stretch at high R.P.M.
Remember that the "inertia weight"... that is the effective
weight of the piston and connecting rod small end at high
engine RPM, is enough to stretch the upper limit of piston
crown travel by more than 0.3mm at high speed.
Good squish
control allows
mixture that
otherwise may
be trapped in the
"dead areas" of
the combustion
chamber, to be
driven towards
the combustion
chamber centre,
and closer to the
ignition point.
57
58
59
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Compression ratio - The ratio of the swept volume of the cylinder to the compressed volume of the
cylinder.
Calculated as follows:
Swept volume + Clearance volume
Compression ratio = ------------------------------------------
Clearance volume
Compression ratios vary from 8 to 1, used for standard engines, up to 12 to 1 for petrol burning
race engines and 15 to 1 for alcohol burning race engines.
Compression ratios for two-stroke engines are often calculated using trapped volume above the
exhaust port, instead of true swept volume. This means that C.R. varies with exhaust timing and,
calculated on this basis, the results are much lower and vary from 7 to 1 up to 9.5 to 1.
Measuring Compression Ratio.
This apparently simple task is often carried out incorrectly, to the considerable detriment of the
maximum power output.
If the engine is a twin cam 2 or 4 valve layout, the combustion chamber will usually finish up as a
part spherical or pent-roof shape. (Fig. 59)
The piston may have a slight rise on the crown and may also have valve clearance pockets, and the
flat area above the top ring land, will probably not reach the top of the bore at TDC.
Cylinder head gaskets will vary in thickness and valve heads will protrude into the chamber.
This complexity of layout often means that the simplest way to check the compression ratio, is to
set one cylinder to TDC, smear a thin seal of grease around the top ring land, then build the
cylinder head into place in the normal manner and torque it down.
Then, if the spark plug is not upright, tilt the engine until the plug axis is vertical and, using a
pipette or measuring cylinder, fill the chamber with water until it is half way up the plug thread.
Remember, when using water as the measuring liquid, to allow for the meniscus curve caused by
the surface tension.
That is always measure to the top or bottom of the curve. It doesn't matter which as long as you
are consistent.
This should have then fully filled the combustion
chamber and allowed for the plug body volume, but just
to be sure, use a piece of thin wire to agitate the liquid
through the plug hole, to help shift or burst any air
bubbles that may still be trapped. (Fig. 60)
This method should give you a fairly accurate measure
of the true clearance volume, and of course, the swept
volume is the bore area times the stroke.
If you decide to measure the head and block volumes
separately, then make sure you allow for the volume of
the compressed head gasket as well.
This can typically represent one complete ratio on a
"square" bore/stroke ratio 400 c.c. cylinder.
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FUELS.
The type of fuel in use obviously heavily influences the combustion process.
As previously mentioned, power is derived from the conversion of heat, and fuel is merely neatly
packaged heat.
The amount of heat (and consequently power energy) in a particular type of fuel, is quantified as its'
"calorific value".
Just as consumed calories from food, release body heat, so consumed calories from fuel release
combustion heat.
One calorie is the amount of heat required to raise one gram of water one degree centigrade.
Straight petrol (gasoline), regardless of octane level, has a calorific value of around 44
KiloJoules/Kg or 19000 British Thermal Units/Lb.
However, in order for a fuel to give out its' maximum energy potential, it must also be resistant to
knock.
Knock or detonation is the uncontrolled process of combustion that occurs due to the presence of
trapped gas in hotspots.
So although fuel additives don't actually increase a fuels' calorific value, they do enable it to deliver
more of its' potential by holding off the onset of knock, thus allowing suitable amounts of spark
advance to be used for maximum power.
In effect therefore, the fuel additive is giving an energy or heat conversion boost.
As well as boosting effective heat content by reducing spark advance knock, fuel additives can also
enhance the power output of a particular fuel by allowing the use of higher compression ratios.
Table of fuel properties :
Effective Octane
Energy Value Rating
2 - star pump petrol 80 92
4 - star pump petrol 100 97
Unleaded petrol 95 94
Avgas aviation petrol 110 104
4 - star with fuel booster 108 102
Methanol 118 110
4 - star/Nitromethane 120 100
4 - star/Nitrous Oxide 120 97
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CHAPTER 4.
THE EXHAUST SYSTEM.
Four stroke engines.
The four-stroke exhaust system consists of considerably more than the visible external manifold
and pipe, and starts at the exhaust valve.
The valve itself needs to be much heavier in design at the back of the head than the inlet valve, in
order to cope with the hot and scouring exhaust blast.
Do not be tempted to remove any of the protruding valve guide.
The valve is continuously struggling to shed its heat, and relies on contact with the guide and seat
for this process.
For the same reason, the seat width must always be greater than for inlet valves and should be
between 2.0 and 2.5 mm, depending on cylinder and valve size.
Modifications to the exhaust port should consist of increasing the bowl area around the stem and
guide, and then a smooth blend to the chosen pipe size.
As far as shape is concerned, a short straight section blended into an updraughted port gives the
best flow/diameter ratio. (Fig. 61)
Just as with the inlet port, radiussing sharp corners will also improve flow.
Effect of the exhaust cam.
When fitting a full-race cam, the valve lift at T.D.C. is considerably increased.
A 400cc cylinder, in standard trim, will have about 1.0mm of lift at overlap T.D.C.
When a full-race cam is fitted, this will increase to around 5.0mm. This happens to both inlet and
exhaust valves, so valve to piston clearance and valve to valve clearance is reduced considerably.
One way to alleviate this problem is to pocket the exhaust valve head. (Fig. 62).
Unlike the inlet, the flow capability of the exhaust actually improves with partial masking.
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This phenomenon presents us with the convenient option of recessing the exhaust valve to improve
valve-to-valve clearance.
However this procedure also results in the exhaust valve stem being too long for the valve spring
fitted length, or too close to the cam lobe to allow suitable clearance adjustment.
This problem is dealt with further in Chapter 8.
Exhaust pipe length and size.
As the exhaust valve opens, a positive or pressure wave front is created which travels down the
exhaust pipe at the speed of sound.
As this pressure wave reaches the end
of the pipe, it expands and a negative
or suction pulse travels back up the
pipe towards the engine. As the
negative wave front in turn reaches the
cylinder, it reverses again and moves
back towards the end of the pipe.
This fluctuating pressure pulse effect
can be used to great advantage in
tuning the engine.
If the system is designed in such a way
that the negative or suction pulses return to the cylinder at overlap T.D.C., then they will assist in
clearing the combustion chamber of exhaust gases.
In turn, this will cause a depression at the inlet valve, which will help draw in the inlet charge.
Coupling the pipes of multi-cylinder engines will also mean that the pulse effects from one cylinder
can be used to assist the breathing of another.
The following formula can be used to calculate the ideal length for a given application:
129540 x E.T.
L = ----------------
R.P.M. x 6
Where:
L = Primary pipe length in mms measured from the exhaust valve head.
E.T. = Exhaust valve duration in degrees from point of valve opening before B.D.C plus the full
180 degree stroke up to T.D.C.
R.P.M. = The estimated revs, at which max. power will be achieved minus five hundred.
Example:
Exhaust timing = 80 B.B.D.C. to 50 A.T.D.C. Estimated maximum power R.P.M. = 7200
E.T. = 80 + 180 = 260
R.P.M. will be 7200 - 500 = 6700
Therefore :
129540 x 260
Primary pipe length = --------------- = 837 mms. or 32 ins.
6700 x 6
Having calculated the primary pipe length, we must now calculate the diameter as follows :
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Divide "L" by 10 to bring it to cms. Call this "L2". (83.7)
Take the cylinder capacity in ccs and double it. (Say 400 x 2 = 800)
Divide by "L2" as previously calculated. (800 / 83.7 = 9.56)
Divide by 3.4 (9.56 / 3.4 = 2.8)
Find the square root (2.8 = 1.67) Multiply by two and add 0.3 ((1.67 x 2) + 0.3 = 3.64)
Multiply by 10 to bring it back to mms. (10 x 3.64 = 36.4) 36.4mms = 1.43ins
This will give the O.D. of the tube in which at first sight will appear rather small.
This is because it assumes the use of a perfectly smooth straight pipe, which is impractical to use,
so the following allowances must be made.
To allow for the viscous drag created in the bends used in an "average" primary pipe and also to
allow for the slight pipe flattening that takes place at the bends, increase the internal cross-
sectional area by 10-15%, depending on how tortuous the system is.
This will probably finish up as a pipe size that is non-standard, so go for the nearest available stock
diameter above this figure.
Remember that "L" is from the exhaust valve head, so the exhaust port length will have to be
deducted to get the actual manufacturing length.
This will then give the joining point of the primary pipes.
From this point, the secondary or tailpipe length can be "L" or any multiple of "L" and its diameter
can be calculated using the method above, but by starting off with four times the cylinder capacity
for a four cylinder engine, or three times for a "six".
For maximum power development, "fours" should always finish up in a single tailpipe (Fig 64),
while "sixes" should finish up with twin pipes, one of which couples cylinder numbers 1,2 and 3,
the other coupling numbers 4, 5 and 6.
For street use, fours can also be designed with a secondary pipe set (Fig. 65) which, although not
giving quite the same maximum power, gives a much broader spread of power.
The secondary pipes need to equal or be a multiple of L, with the next stock diameter up on the
primary.
64 65
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Production V8s with 90 degree cranks should ideally have a crossover system (Fig. 66), but this is
usually impractical, in which case they can be treated as two "fours", but will need a balance pipe
linking the tailpipes at a tuned length, calculated as above.
Racing V8s with 180 degree cranks can be correctly treated as two "fours" with no balance pipe
necessary (Fig. 67).
If a silencer is used, expansion will take place at this point, so the start of the chamber should occur
at a "tuned" tailpipe length, with additional tailpipe added to clear exhaust gas as necessary.
Dragsters, using only wide-open throttle, requiring
little or no progression, will typically use open
stubs to give the highest, shortest band of power.
(Fig 68)
The following chart is only intended as a guide to typical characteristics and requirements.
Individual engine applications will vary with engine characteristics and slight changes will be
needed to achieve maximum performance.
Exhaust valve timings for turbocharged and supercharged engines are dealt with in the relevant
section, later in the manual.
Exhaust timing selection chart
Exhaust Exhaust Av.max.
Application opens closes power E.T.
B.B.D.C. A.T.D.C. R.P.M.
Standard Engine 50 20 5500 230
Stage 1 Street 65 30 6200 245
66 67
68
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Stage 2 Rally, M/Cross 75-80 40-50 6800 260
Stage 3 Advanced Rally
and Motor Cross 82 54 7400 262
Stage 4 Full Circuit Race 88 56 8000 268
Dragster 90+ 60+ 8000+ 270+
Two-stroke engines.
The pressure pulse reversal as described earlier also takes place in the two-stroke exhaust system
and can be used to much greater effect if correctly manipulated.
This is due to the fact that the whole breathing process is dependant on a transfer of pressure from
one area to another and is not positively valve controlled as it is in the four stroke.
The rules of good design are not nearly as easy to define, and best results are ultimately only
achieved by exhaustive dynamometer testing.
Even then the results obtained will not apply to another engine if there is any slight variation in
timing.
Multi-cylinder coupling is not mathematically feasible except with three cylinder configurations
and even then, the improvement comes only in the mid-range, often very useful to spread the torque
of highly tuned engines.
In order to obtain ultimate power from multi-cylinder two-stroke engines, it is necessary that they
be treated as a group of single cylinders.
This often creates great difficulty in
accommodating the mass of snake-like
hardware. (Fig. 70)
The separate geometric components of the exhaust system are laid out in Fig. 71 and function in the
following manner :
(A) Primary Pipe.
Often a parallel tube, particularly in cheaper production road machines, but ideally a tapered
primary pipe should be used to control the expansion rate of the high speed gas slug ejected
from the port and to convert its kinetic energy into pressure energy.
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(B) Primary Divergent Cone.
Controls initial expansion of the pressure pulse and is often combined with :
(C) Secondary Divergent Cone.
Which finally controls the pressure pulse expansion to
induce the negative pulse, which travels back to the port
to help scavenge the cylinder.
(D) Expansion Chamber.
Length acts as a time control before throttling of the gas
slug which starts at :
(E) Convergent Cone.
Which throttles down the slug to the :
(F) Tail Pipe.
The size of which controls the high back pressure reverse
"plug", which in turn pushes the overspill of intake charge
back into the cylinder before the piston shuts the door.
The whole sequence, using correctly designed
components, will result in a cylinder filling efficiency of
more than 100% at the "tuned" engine speed.
True design formulae for these systems are highly
complex and still not quite fully understood, but outlined
below is a simplified starting point for those who want to
have a go themselves :
41910 x TD
Length "G" in mms = ----------
R.P.M.
Where TD is transfer port duration in degrees.
R.P.M. is desired "on pipe" R.P.M.
41910 x ED
Length "H" in mms = ----------
R.P.M.
Where "ED" is exhaust port duration in degrees.
41910 x (TD + C)
Length "J" in mms = ---------------
R.P.M.
Where "C" will control the length of the parallel section
and lengthen time before reverse plug starts.
Find this empirically by starting at 0 and increasing in intervals of 5.
"De" will be around 2.25 x Piston diameter for high revs and 2.0 x Piston diameter for torque.
"Dt" will be around 0.45 x Piston diameter for high revs and 0.5 x Piston diameter for torque.
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Exhaust emissions.
Although not an important consideration in Europe when tuning for performance, exhaust
emission control is becoming a major factor of engine design consideration.
When the air/fuel mixture burns in the combustion chamber, a number of chemical changes
take place that result in the pungent and easily recognised exhaust fumes emitted from the tail
pipe.
These consist of harmless gases like oxygen and carbon dioxide, and the deadly gases like
nitrous oxides, carbon monoxide and hydrocarbons.
Nitrous oxides are usually the result of high combustion chamber temperatures, so these will
often rise when tuning takes place.
Hydrocarbons are formed when small, trapped pockets of gas are left partially unburnt or
mixtures are run too rich.
Well-tuned engines usually have low hydrocarbon outputs.
It is almost inevitable that, as Californian law already decrees, European exhaust emission
legislation will eventually mean that tuning kits may not be sold unless they conform to the
clean air laws.
Hopefully though, it will not apply to motor sport events.
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CHAPTER 5.
THE CAMSHAFT.
CAMSHAFT CHOICE.
The camshaft is undoubtedly the most important single component to be selected when tuning the
four-stroke engine.
The correct choice is often difficult to make and this chapter is principally concerned in setting out
the problems and facts, in order that the correct decision can be made for an individual application.
Recognition of the profile.
The cam lobe is made up of four essential elements (Fig.
79). The base circle or clearance circle, often called the
heel, together with the ramp - the flank - and the nose.
The BASE CIRCLE is the area of the cam in which little
or no contact takes place with the cam follower.
The centre of the base circle duration lies at
approximately 180 degrees from the nose centre line and
is the point at which valve clearances are normally set.
The RAMP is the area joining the base circle to flank, and
is designed to take up valve clearance in a controlled manner, immediately prior to the start of
valve lift.
The FLANK lifts the valve train with the spring in compression and accelerates to its maximum
speed.
The NOSE takes over at this point and controls the valve train deceleration until it momentarily
comes to rest at full lift, when the process reverses itself to the lower valve back to its seat, where
the ramp will re-open the clearance.
The whole procedure exerts an enormous strain on the components
involved, sometimes stacking-up contact stresses over the cam
nose as high as 1300 Meganewtons/sq.m. (200 lbs/sq.in.), calling
for a high degree of accuracy in design and manufacture, together
with the need for great care and attention when fitting.
The cam nose stress stack-up is the result of a number of
unavoidable design constrictions.
No matter how tight the engine manufacturing tolerances, there
will always be a small amount of mis-alignment or out-of-square
mating between components, sometimes causing hairline or
pressure point contact. (Fig. 80)
In order to minimise the effects of this possibility, cam lobes are often purposely machined with a
taper to mate with a spherically ground tappet face (Fig. 81), creating an intentional but calculable
high pressure footprint, slightly offset from the tappet centre-line to promote rotation of the tappet,
thus improving overall service life.
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This design feature means that individual cam lobes and
tappets bed together after an initial running period, and
should therefore never be allowed to re-mate with other
components during later re-assembly procedures.
Camshafts are made from either cast-iron or steel with the
latter usually recognisable by their smooth forged or turned
finish between the lobes as opposed to the rougher finish of
the former which are left as cast in this area.
In some cases they are also turned between the lobes to
reduce the core size, usually done when an increase in lift
dictates a smaller base circle diameter.
Cast iron shafts made of proferal or K iron, have the
lobes and gears heat treated by flame or induction hardening processes, whereas chill cast
components are hardened in the vital areas during the casting process.
Whatever production method is used, cast-iron cam lobes
finish up with a hardness pattern as in (Fig. 82), that is,
about a quarter of an inch depth of hardness over the nose,
tapering in depth down each flank.
This means that the base circle is usually relatively soft,
which is acceptable because there is little or no load at this
point. Because of this hardness pattern, these cams are
particularly suitable for regrinding; only requiring final
refinishing with a black, oil retaining, phosphate coating.
Steel cams, on the other hand, are case hardened, which means that they finish up with a thin
hardened layer, usually about 1.0mm thick, which is penetrated when the cam is reground.
This necessitates heat treatment or hard facing to regain acceptable hardness after a regrind.
Lobe hardness over the nose should be 50-53 Rockwell C on cast iron and 54-58 Rockwell C on
steel.
CAMSHAFT REGRINDING HOW DOES IT WORK?
A few years ago, by far the majority of European high performance camshafts were produced by
the process of re-profiling the standard cam.
Contrary to commonly held misconceptions, this procedure, if properly engineered, results in a
product that is equal, both in reliability and performance, to the same component made from raw
billet.
Although it would be ideal to make all camshafts from new billets to avoid the transportation
problems of exchange units, this is just not practical in Europe, due to the vast variety of makes and
models, often coupled with the non-availability of unmachined castings from the original
manufacturers and the obvious poor economics of producing special casting to meet the small
demands for one particular model.
This situation doesn't apply in the United States where a relatively small number of billets cover a
very wide range of vehicle.
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82
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To many people the process of regrinding a camshaft is a black art, resulting in the inevitable
question :
How can you machine metal away from a cam, yet have it finish up with more duration and lift?
It works like this
In (Fig. 83), the outer contour represents the
original lobe shape and the cam lift is represented
as dimension A, the difference between the base
circle radius and the nose.
The duration of the lift is shown as 120 degrees at
the cam, which would be 240 degrees at the
crankshaft, because the camshaft rotates at half
crank speed.
The inner contour line shows the cam shape after it
has been reground and it can be clearly seen that
the lift has now been increased to the dimension
B, this time the difference between the new basic circle radius and the nose.
At the same time the duration has been increased to 160 degrees at the cam, that is 320 degrees at
the camshaft.
From this diagram it is also now possible to see why the cast iron cam lends itself so readily to
regrinding. The deep hardness pattern over the nose is still fully effective.
As contemporary high efficiency engines are being evolved, the process of regrinding will no
longer be acceptable for a number of reasons.
The increasing use of hydraulic tappets, fitted to automatically adjust running valve clearances to
compensate for changes in engine dimensions due to heating and cooling effects, means that
nominal base circle sizes may not be altered.
In this case, the replacement camshaft will need to be produced from a new billet or casting.
However, restrictions such as slide-in camshaft bearing diameters will often control the overall
height of the cam lobe and thus mean that the new billet cam will have lobes no larger than those of
a re-ground shaft.
This in turn means that the hydraulic followers will have to be
replaced with solid followers and a method of valve clearance
adjustment introduced.
In any circumstances, it is desirable to switch to solid lifter
operation wherever possible for efficient high performance engine
conversion.
For the same reasons, the use of various types of overhead cam
operating systems will have layout geometries that will not allow
significant changes in cam dimensions. (Fig. 84)
The high performance replacements for these will, not only need to
be manufactured from new billets, but will also need to use state of
the art profile design techniques to give the best results.
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84
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It is a general, but mistaken impression that it is possible to look at a cam shape and say whether it
is for road or track.
This is clearly illustrated in (Fig. 85), which shows a
selection of racing cam shapes from a variety of
engines.
A is a standard Fiat, B is a racing XK140 Jaguar,
C is a racing Hillman Imp.
D, which most experts would define as a very mild
cam, was the profile used in the contemporary Golf
1.8 GTI racing engines.
E is a standard Triumph Bonneville, F is a
standard Ford 2.0 OHC, G is a racing Honda.
The shape of the lobe is entirely dependent on the
design of the components that work with it and will
vary hugely from engine to engine.
The technical requirements of successful high performance cam design require attention to a
number of simple but vital engine component functions.
The vast majority of production engines have valve train mechanisms that generate symmetrical
motion at the valve. (Figs. 86 & 87)
This is achieved by either directly moving the valve with conventional direct operating cam
technique (Fig. 86a), in which case a symmetrical cam profile imparts a symmetrical valve motion,
or by moving the valve via a rocker mechanism, which imparts symmetrical valve motion by
compensating for the constantly varying rocker ratio by using an asymmetrical cam profile.
However, modern computer design and analysis techniques allow for the development of cams that
impart asymmetrical motion to the valve, thus taking advantage of part of the generous safety
margins that are built into standard engine valve train dynamics.
86
85
87
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If we study the movement of a valve
during its' opening and closing cycle as
a graph (Fig. 88), then the actual valve
lift is shown as a single smooth curve
on the upper, or positive side of the zero
line.
The velocity is seen as two sharper
positive curves, representing the speed of
the valve as it lifts to full lift, pauses
momentarily, then speeds up once more
as it starts to close. (Fig. 89)
Finally, the acceleration is shown as
positive as the valve accelerates to
maximum velocity, then negative as it
decelerates to rest at full lift, followed by
a reverse cycle of acceleration and
deceleration as it closes.
The design of this acceleration pattern is the point at which all cam profile design starts.
Normally this pattern is symmetrical and is controlled by the maximum deceleration that occurs at
full lift, from which the valve spring dimensions are calculated, the speed at which the valve is
lowered back onto the valve seat in order to avoid valve bounce, and the amount of wind-up that
occurs in the valve train due to flexibility of the components.
This last factor is of course the reason why overhead direct acting valve trains can be made to
operate at far higher speeds than systems using rockers or push-rods, hence the evolution of the
twin OHC engine.
Using computerised design techniques and high precision manufacturing methods, the valve
dynamics can be modified by distorting the symmetry of the acceleration, velocity and lift curves,
to give a greater proportion of valve open, or breathing time, within any given valve duration.
The result of this strategy is that, for any given valve duration (i.e. time of valve leaving then
returning to its' seat), the actual open area through which gases can move is increased.
This means that a relatively short duration cam, giving good low-end performance, can also allow
enough breathing area for high speed volumetric efficiency and consequently increase power.
These poly-dynamic cam profiles represent a significant step towards the all-purpose high
performance camshafts, but it should be remembered that the high valve opening accelerations
impose stresses that are eroding the normal standard production safety limit margins.
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CAMSHAFT POSITION AND DRIVE
Referring again to Figs. 86&87, the camshaft and associated valve train component layouts
covering 95% of modern engine designs are shown, together with their applications, virtues and
disadvantages as listed below :
KEY USED BY VIRTUES DISADVANTAGES
(A)
Rover Gp. Single Camshaft Valve size
S.O.H.C. V.W. Audi Simple Drive Restriction due
Direct SAAB Honda Belt or Chain to in-line layout.
Operating many others. Bore size controls sum
of inlet and exhaust
seat diameters.
Ports often too
long.
(B) B.M.W.,Mazda Allows better Spark plug position
S.O.H.C. Colt,Moskvich, valve placing, is restricted due
with BL,Peugeot, still simple to rockers and shafts.
Rockers Porsche, Toyota drive.
Honda, Yamaha,
(C) Mostly Ease of Flexibility and
OHV servicing. weight of a long
industrial train of components.
Pushrod manufacturers.
(D) Datsun (Nissan), Ease of Flexible by normal
SOHC Fiat,Ford, Lada, servicing. OHC standards.
Loose Vauxhall. Choice of valve Excessive overall
follower position. height.
finger.
(E) AlfaRomeo, The only true Costly to manufacture.
Twin Cam.
Aston Martin, racing layout. Difficult to service,
Direct Ferrari, Honda, Allows freedom of but becoming easier
operating. Lancia, Lotus, valve and plug with hydraulically
Maserati, position. adjusting bucket
Jaguar, Toyota, followers.
Suzuki, Kawasaki
Many others.
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CAMSHAFT INSTALLATION.
As stated earlier, the camshaft is the most highly stressed component in the engine and therefore
requires particular care when being fitted.
The majority of cast-iron cams have a black phosphate coating.
The purpose of this is not, as many people think, a surface hardening process but it is for oil
retention during the early life of the cam. It carries out this function admirably but unfortunately
also retains any dirt that is brought into contact.
Even just handling a camshaft with grubby hands while fitting, can implant enough tiny particles of
grit to seriously shorten its life.
THE RULES OF SUCCESSFUL CAMSHAFT INSTALLATION.
Research indicates that the majority of cams that wear out, start to fail during the first few moments
of operation.
Many cams are irreparably damaged, even before the engine is started, because the basic rules of
camshaft break-in have not been followed.
The cause of premature cam and tappet failure is metal-to-metal contact between the tappet and
cam lobe. Should this contact occur due to lack of proper lubrication, or excessively high pressure
due to valve train interference shearing the oil film, then 'galling' will take place.
When this happens, metal is transferred from the tappet to the cam or vice versa in a process
comparable to welding. Microscopic high spots, which are present on all machined parts, become
overheated due to friction and pressure bond together, tearing sections loose from the tappet or
lobe. These pieces of metal remain attached to the mating part, creating further local overheating
during the following revolutions of the camshaft, leading to ultimate failure of the affected
components.
Listed below are the mistakes that lead to premature failure:
1.Inadequate lubrication during the initial rotation of the camshaft with full spring load applied.
2.Interference in the valve train due to improper installation and failure to check for interference.
Valve spring coil boxing, spring collar to guide contact, valve to valve contact and valve to piston
contact are the main problems.
3.Installation of used tappets with a new camshaft.
No matter how good tappets look, new tappets must be used with a new camshaft!!!
Beware of reclaimed tappets; they are usually ground flat whereas geometric relationships between
cam and follower, often involve the use of a tapered cam lobe working with a spherically radiussed
tappet foot.
Fig. 81 (above), shows an exaggerated view of this condition, which essentially comprises a cam
lobe taper of around 6-10 minutes! That's about 0.025mm over 13mm and a spherical radius on the
tappet foot of 1500-2500mm!
The centreline of the tappet is also offset from the lobe centreline by about 1.0mm.
4. Water, petrol or other contaminant in the oil that can lower film strength, or create abrasion.
5.Excessively long cranking on the starter. Oil will not reach cam lobes until engine is running.
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6.Low idle speeds during break-in. Cam lobes in pushrod engines usually depend on all thrown
from con-rods for lubrication. Oil delivery will not be sufficient at idle.
A word of warning !
Cam profiles, particularly high performance profiles, have sensitive areas of dimensional tolerance
at the point where the flank joins the ramp, and the contour over the nose.
Even at the point of original manufacture from the high precision master cam, small but acceptable
contour discrepancies occur.
However, any attempt to further copy the camshaft will degrade the profile contour, just as
videotape degrades with copying.
In order to avoid the problems that this causes in the valve train dynamics, together with the
subsequent reductions in performance and reliability, you should confirm that your camshaft
supplier is the original designer and production originator, rather than a machine shop specialising
in producing copies of other manufacturers' original designs.
Reputable camshaft manufacturers and suppliers will themselves take several other precautions by:
1. Supplying cam profile designs that are not overloaded or highly stressed.
2. Provide cams with the correct machined finish.
3. Phosphate or otherwise treat cams to assist oil retention.
4. Supply or recommend special oil for assembly.
The mechanic handling the installation bears the greatest responsibility for break-in of the
camshaft.
The following outlined steps will help ensure long and trouble-free life from the camshaft and
associated components :
1. Coat the cam lobes and cam face of the tappet with lubricant.
If a proprietary cam lube containing Zinc-Dio-Thio-Phosphate (ZDTP), like Piper Cam Lube, is
not available, then an E.P. 140 or 90 Hypoid rear axle oil is the next best alternative.
2. Check entire valve train for interference before attempting to start engine, and particularly
check that the cam eccentricity or wipe path across the follower, does not run off the edges.
High velocity cams will wipe across a much wider face path than standard cams.
3.Set pushrod engine valve clearances 0.003in to 0.005in smaller than specified for initial start-
up.
4.Before starting any engines, prime the oil by turning oil pump manually. Fill carburettor with
petrol, fill radiator and ensure correct ignition timing. Engine must start right away and not be
subjected to a long grind on the starter.
5.Do not idle engine during the first twenty minutes of operation.
Rpm should be kept at 2500 or above.
In pushrod engines oil throw-off from the crank may not be sufficient to lubricate the cam
followers. Also contact stresses at the nose of the cam are very high at low speed. Engines
may be run in the shop or on the road or strip. If adjustments need to be made during the
twenty minutes break- in period, shut the engine down. DO NOT LET IT IDLE!
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If the engine is dismantled for repair, maintenance or inspection, after any running at all, it is
important that the tappets be kept in order.
Each tappet will have mated to a cam lobe and swapping tappets may cause failure.
CAMSHAFT - SELECTING, CHECKING AND SETTING TIMING