Title: Powertrain 101
1Powertrain 101
- John Bucknell
- DaimlerChrysler
- Powertrain Systems Engineering
- September 30, 2006
2Powertrain Topics
- Background
- Powertrain terms
- Thermodynamics
- Mechanical Design
- Combustion
- Architecture
- Cylinder Filling Emptying
- Momentum
- Pressure Wave
- Aerodynamics
- Flow Separation
- Wall Friction
- Junctions Bends
3What is a Powertrain?
- Engine that converts thermal energy to mechanical
work - Particularly, the architecture comprising all the
subsystems required to convert this energy to
work - Sometimes extends to drivetrain, which connects
powertrain to end-user of power
4Characteristics of Internal Combustion Heat
Engines
- High energy density of fuel leads to high power
to weight ratio, especially when combusting with
atmospheric oxygen - External combustion has losses due to multiple
inefficiencies, internal combustion has less
inefficiencies - Heat engines using working fluids which is the
simplest of all energy conversion methods
5Reciprocating Internal Combustion Heat Engines
- Characteristics
- Slider-crank mechanism has high mechanical
efficiency - Piston-cylinder mechanism has high single-stage
compression ratio capability leads to high
thermal efficiency capability - Fair to poor air pump, limiting power potential
without additional mechanisms
6- Reciprocating Engine Terms
- Vc Clearance Volume
- Vd Displacement or Swept Volume
- Vt Total Volume
- TC or TDC
- Top or Top Dead Center Position
- BC or BDC
- Bottom or Bottom Dead Center Position
- Compression Ratio (CR)
7Further explanation of aspects of Compression
Ratio
8- Reciprocating Engines
- Most layouts created during second World War as
aircraft manufacturers struggled to make the
least-compromised installation
9Thermodynamics
- Otto Cycle
- Diesel Cycle
- Throttled Cycle
- Supercharged Cycle
Source Internal Comb. Engine Fund.
10- Thermodynamic Terms
- MEP Mean Effective Pressure
- Average cylinder pressure over measuring period
- Torque Normalized to Engine Displacement (VD)
- BMEP Brake Mean Effective Pressure
-
- IMEP Indicated Mean Effective Pressure
- MEP of Compression and Expansion Strokes
- PMEP Pumping Mean Effective Pressure
- MEP of Exhaust and Intake Strokes
- FFMEP Firing Friction Mean Effective Pressure
-
- BMEP IMEP PMEP FFMEP
11- Thermodynamic Terms continued
- Work
- Power Work/Unit Time
- Specific Power Power per unit, typically
displacement or weight - Pressure/Volume Diagram Engineering tool to
graph cylinder pressure
12Indicated Work
TDC
BDC
Source Design and Sim of Four Strokes
13Pumping Work
TDC
BDC
Source Design and Sim of Four Strokes
14Spark Ignition
- 1878 Niklaus Otto built first successful four
stroke engine - 1885 Gottlieb Daimler built first high-speed four
stroke engine - 1878 saw Sir Dougald Clerk complete first
two-stroke engine (simplified by Joseph Day in
1891)
1891 Panhard-Levassor vehicle with front engine
built under Daimler license
15Energy Distribution in Passenger Car Engines
Source SAE 2000-01-2902 (Ricardo)
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17Using Exhaust Energy
- Highest expansion ratio recovers most thermal
energy - Turbines can recover heat energy left over from
gas exchange - Energy can be used to drive turbo-compressor or
fed back into crank train
Source Advanced Engine Technology
18Supercharging
- Increases specific output by increasing charge
density into reciprocator - Many methods of implementation, cost usually only
limiting factor
Source Internal Comb. Engine Fund.
19Mechanical Design
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21Two Valve Valvetrain
22Four Valve Valvetrain
23Valvetrain
- Specific Power f(Air Flow, Thermal
Efficiency) - Air flow is an easier variable to change than
thermal efficiency - 90 of restriction of induction system occurs in
cylinder head - Cylinder head layouts that allow the greatest
airflow will have highest specific power
potential - Peak flow from poppet valve engines primarily a
function of total valve area - More/larger valves equals greater valve area
24Combustion Terms
- Brake Power Power measured by the absorber
(brake) at the crankshaft - BSFC - Brake Specific Fuel Consumption Fuel
Mass Flow Rate / Brake Power grams/kW-h or
lbs/hp-h - LBT Fuelling - Lean Best Torque
Leanest Fuel/Air to Achieve
Best Torque LBT 0.0780-0.0800 FA or 0.85-0.9
Lambda - Thermal Enrichment Fuel added for cooling due
to component temperature limit - Injector Pulse Width - Time Injector is Open
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26Combustion Terms continued
- Spark Advance Timing in crank degrees prior to
TDC for start of combustion event (ignition)
- MBT Spark Maximum Brake Torque Spark
Minimum Spark Advance to
Achieve Best Torque - Burn Rate Speed of Combustion Expressed as
a fraction of total heat released versus crank
degrees - MAP - Manifold Absolute Pressure Absolute
not Gauge (does not reference barometer)
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28Burn Rate
- Burn Rate f(Spark, Dilution Rate/FA Ratio,
Chamber Volume Distribution, Engine Speed/Mixture
Motion/Turbulent Intensity) - Spark
- Closer to MBT the faster the burn with trace
knock the fastest - Dilution Rate/FA Ratio
- Least dilution (exhaust residual or anything
unburnable) fastest - FA Ratio best rate around LBT
- Chamber Volume Distribution
- Smallest chamber with shortest flame path best
(multiple ignition sources shorten flame path) - Engine Speed/Mixture Motion/Turbulent Intensity
- Crank angle time for complete burn nearly
constant with increasing engine speed indicating
other factors speeding burn rate - Mixture motion-contributed angular momentum
conserved as cylinder volume decreases during
compression stroke, eventually breaking down into
vortices around TDC increasing kinetic energy in
charge - Turbulent Intensity a measure of total kinetic
energy available to move flame front faster than
laminar flame speed. More Turbulent Intensity
equals faster burn.
29Combustion Terms continued
- Knock Autoignition of end-gasses in combustion
chamber, causing extreme rates of pressure rise. - Knock Limit Spark - Maximum Spark Allowed due to
Knock can be higher or lower than MBT - Pre-Ignition Autoignition of mixture prior to
spark timing, typically due to high temperatures
of components - Combustion Stability Cycle to cycle variation
in burn rate, trapped mass, location of peak
pressure, etc. The lower the variation the
better the stability.
30Combustion Summary
- Peak Thermal Efficiency at desired load
- Highest compression ratio will have best
combustion, usually with highest expansion ratio
for best use of thermal energy - MBT spark with fastest burn rate
- 10 lean of stoichiometry will provide best
compromise between heat losses and pumping work,
but not used because of catalyst performance
impacts - Peak Specific Power
- LBT fuelling for best compromise between
available oxygen and charge density - MBT spark if possible, fast burn rate assumed at
peak load - Highest engine speed to allow highest compression
ratio - Highest octane
31Engine Architecture Influence on Performance
- Intake Exhaust Manifold Tuning
- Cylinder Filling Emptying
- Momentum
- Pressure Wave
- Aerodynamics
- Flow Separation
- Wall Friction
- Junctions Bends
- Induction Restriction
- Exhaust Restriction (Backpressure)
- Compression Ratio
- Valve Events
32Intake Tuning for WOT Performance
- Intake manifolds have ducts (runners) that tune
at frequencies corresponding to engine speed,
like an organ pipe - Longer runners tune at lower frequencies
- Shorter runners tune at higher frequencies
- Tuning increases local pressure at intake valve
thereby increasing flow rate - Duct diameter is a trade-off between velocity and
wall friction of passing charge
33Exhaust Tuning for WOT Performance
- Exhaust manifolds tune just as intake manifolds
do, but since no fresh charge is being introduced
as a result not as much impact on volumetric
efficiency (8 maximum for headers) - Catalyst performance usually limits production
exhaust systems that flow acceptably with little
to no tuning
34Tuned Headers
Tuned Headers generally do not appear on
production engines due to the impairment to
catalyst light-off performance (usually a minimum
of 150 additional distance for cold-start
exhaust heat to be lost). Performance can be
enhanced by 3-8 across 60 of the operating
range.
35Momentum Effects
- Pressure loss influences dictate that duct
diameter be as large as possible for minimum
friction - Increasing charge momentum enhances cylinder
filling by extending induction process past
unsteady direct energy transfer of induction
stroke - Decreasing duct diameter increases available
kinetic energy for a given mass flux - Therefore duct diameter is a trade-off between
velocity and wall friction of passing charge
36Pressure Wave Effects
- Induction process and exhaust blowdown both cause
pressure pulsations - Abrupt changes of increased cross-section in the
path of a pressure wave will reflect a wave of
opposite magnitude back down the path of the wave - Closed-ended ducts reflect pressure waves
directly, therefore a wave will echo with same
amplitude
37Pressure Wave Effects cont
- Friction decreases energy of pressure waves,
therefore the 1st order reflection is the
strongest but up to 5th order have been
utilized to good effect in high speed engines
(thus active runners in F1) - Plenums also resonate and through superposition
increase the amplitude of pressure waves in
runners small impact relative to runner
geometry
38Effects of Intake Runner Geometry
39Tuning in Production I4 Engine
40Aerodynamics
- Losses due to poor aerodynamics can be equal in
magnitude to the gains from pressure wave tuning - Often the dominant factory in poorly performing
OE components - If properly designed, flow of a single-entry
intake manifold can approach 98 of an ideal
entrance on a cylinder head (steady state on a
flow bench).
41Aerodynamics cont
- Flow Separation
- Literally same phenomenon as stall in wing
elements pressure in free stream insufficient
to push flow along wall of short side radius - Recirculation pushes flow away from wall, thereby
reducing effective cross-section so-called
vena contracta - Simple guidelines can prevent flow separation in
ducts studies performed by NACA in the 1930s
empirically established the best duct
configurations
42Aerodynamics cont
- Wall Friction
- Surface finish of ducts need to be as smooth as
possible to prevent tripping of flow on a macro
level - Junctions Bends
- Everything from your fluid dynamics textbook
applies - Radiused inlets and free-standing pipe outlets
are best - Minimize number of bends
- Avoid S bends if at all possible
43Induction Restriction
- Air cleaner and intake manifolds provide some
resistance to incoming charge - Power loss related to restriction almost directly
a function of ratio between manifold pressure
(plenum pressure upstream of runners) and
atmospheric
44Exhaust Restriction
45Compression Ratio
- The highest possible compression ratio is always
the design point, as higher will always be more
thermally efficient with better idle quality - Knock limits compression ratio because of
combustion stability issues at low engine speed - Most engines are designed with higher compression
than is best for combustion stability because of
the associated part-load BSFC benefits
46Valve Events
- Valve events define how an engine breathes all
the time, and so are an important aspect of low
load as well as high load performance - Valve events also effectively define compression
expansion ratio, as compression will not
begin until the piston-cylinder mechanism is
sealed same with expansion
47Valve Event Timing Diagram
- Spider Plot - Describes timing points for valve
events with respect to Crank Position - Cam Centerline - Peak Valve Lift with respect to
TDC in Crank Degrees
48Valve Events for Power
- Maximize Trapping Efficiency
- Intake closing that is best compromise between
compression stroke back flow and induction
momentum (retard with increasing engine speed) - Early intake closing usefulness limited at low
engine speed due to knock limit - Early intake opening will impart some exhaust
blowdown or pressure wave tuning momentum to
intake charge - Maximize Thermal Efficiency
- Earliest intake closing to maximize compression
ratio for best burn rate (optimum is
instantaneous after TDC) - Latest exhaust opening to maximize expansion
ratio for best use of heat energy and lowest EGT
(least thermal protection enrichment beyond LBT)
49Valve Events for Power
- Minimize Flow Loss
- Achieve maximum valve lift (max flow usually at
L/D gt 0.25-0.3) as long as possible (square lift
curves are optimum for poppet valves) - Minimize Exhaust Pumping Work
- Earliest exhaust opening that blows down cylinder
pressure to backpressure levels before exhaust
stroke (advance with increasing engine speed) - Earliest exhaust closing that avoids
recompression spike (retard with increasing
engine speed)
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51Engine Power and BSFC vs Engine Speed
52Summary
- Components Relative Impact on Performance
- Cylinder Head Ports Valve Area
- Valve Events
- Intake Manifold Runner Geometry
- Compression Ratio
- Exhaust Header Geometry
- Exhaust Restriction
- Air Cleaner Restriction
53References
- Internal Combustion Engine Fundamentals, John B
Heywood, 1988 McGraw-Hill - The Design and Tuning of Competition Engines
Sixth Edition, Philip H Smith, 1977 Robert
Bentley - The Development of Piston Aero Engines, Bill
Gunston, 1993 Haynes Publishing - Design and Simulation of Four-Stroke Engines,
Gordon P. Blair, 1999 SAE - Advanced Engine Technology, Heinz Heisler, 1995
SAE - Vehicle and Engine Technology, Heinz Heisler,
1999 SAE
54Closing Remarks
- Powertrain is compromise
- Four-stroke engines are volumetric flow rate
devices the only route to more power is
increased engine speed, more valve area or
increased charge density - More speed, charge density or valve area are
expensive or difficult to develop therefore
minimizing losses is the most efficient path with
existing engine architectures
55Q A