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AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

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Page 1: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

AME 436

Energy and Propulsion

Lecture 6Unsteady-flow (reciprocating) engines 1:

Basic operating principles, design & performance parameters

Page 2: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

2AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Outline Classification of unsteady-flow engines Basic operating principles

Premixed-charge (gasoline) 4-stroke Premixed-charge (gasoline) 2-stroke Premixed-charge (gasoline) rotary or Wankel Nonpremixed-charge (Diesel) 4-stroke Nonpremixed-charge (Diesel) 2-stroke

Design and performance parameters Compression ratio, displacement, bore, stroke, etc. Power, torque, work, Mean Effective Pressure Thermal efficiency Volumetric efficiency Emissions

Page 3: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

3AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Classification of unsteady-flow engines

Most important distinction: premixed-charge vs. nonpremixed-charge

Premixed-charge: frequently called "Otto cycle," "gasoline" or "spark ignition" engine but most important distinction is that the fuel and air are mixed before or during the compression process and a premixed flame is ignited (usually by a spark, occasionally by a glow plug (e.g. model airplane engines), occasionally homogeneous ignition (Homogeneous Charge Compression Ignition (HCCI), under development)

Nonpremixed-charge: frequently called "Diesel" or "compression ignition" but key point is that only air is compressed (not fuel-air mixture) & fuel is injected into combustion chamber after air is compressed

Either premixed or nonpremixed-charge can be 2-stroke or 4-stroke, and can be piston/cylinder type or rotary (Wankel) type

Page 4: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

4AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Classification of unsteady-flow engines

Why is premixed-charge vs. nonpremixed-charge the most important distinction? Because it affects Choice of fuels and ignition system Choice of compression ratio (gasoline - lower, diesel - higher) Tradeoff between maximum power (gasoline) and efficiency (diesel) Relative amounts of pollutant formation (gasoline engines have

lower NOx & particulates; diesels have lower CO & UHC)

Page 5: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

5AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Classification of unsteady-flow engines

Page 6: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

6AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

4-stroke premixed-charge piston engine

Animation: http://auto.howstuffworks.com/engine3.htm

Note: ideally combustion occurs in zero time when piston is at the top of its travel between the compression and expansion strokes

Intake (piston moving down, intake valve open, exhaust valve closed)

Compression (piston moving up, both valves closed)

Expansion (piston moving down, both valves closed)

Exhaust (piston moving up, intake valve closed, exhaust valve open)

Page 7: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

7AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

2-stroke premixed-charge engine

Most designs have fuel-air mixture flowing first INTO CRANKCASE (?)

Fuel-air mixture must contain lubricating oil

On down-stroke of piston Exhaust ports are exposed & exhaust

gas flows out, crankcase is pressurized Reed valve prevents fuel-air mixture

from flowing back out intake manifold Intake ports are exposed, fresh fuel-air

mixture flows into intake portsOn up-stroke of piston

Intake & exhaust ports are covered Fuel-air mixture is compressed in

cylinder Spark & combustion occurs near top of

piston travel Work output occurs during 1st half of

down-stroke

Page 8: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

8AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

2-stroke premixed-charge engine

http://science.howstuffworks.com/two-stroke2.htm

Page 9: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

9AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

2-stroke premixed-charge engine

2-strokes gives ≈ 2x as much power since only 1 crankshaft revolution needed for 1 complete cycle (vs. 2 revolutions for 4-strokes)

Since intake & exhaust ports are open at same time, some fuel-air mixture flows directly out exhaust & some exhaust gas gets mixed with fresh gas

Since oil must be mixed with fuel, oil gets burned As a result of these factors, thermal efficiency is lower, emissions

are higher, and performance is near-optimal for a narrower range of engine speeds compared to 4-stroke engines

Page 10: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

10AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Rotary or Wankel engine Uses non-cylindrical combustion chamber Provides one complete cycle per engine revolution without "short circuit" flow of

2-strokes (but still need some oil injected at the rotor apexes) Simpler, fewer moving parts, higher RPM possible Very fuel-flexible - can incorporate catalyst in combustion chamber since fresh

gas is moved into chamber rather than being continually exposed to it (as in piston engine) – one engine could possibly use gasoline, Diesel, methanol, etc.

Very difficult to seal BOTH vertices and flat sides of rotor! Seal longevity a problem also Large surface area to volume ratio means more heat losses

http://static.howstuffworks.com/flash/rotary-engine-exploded.swf

Page 11: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

11AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Rotary or Wankel engine Source: http://auto.howstuffworks.com/rotary-engine4.htm

Page 12: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

12AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Rotary or Wankel engine

http://auto.howstuffworks.com/rotary-engine4.htm

Page 13: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

13AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

4-stroke Diesel engine Conceptually similar to 4-stroke gasoline, but only air is compressed

(not fuel-air mixture) and fuel is injected into combustion chamber after air is compressed

http://auto.howstuffworks.com/diesel2.htm

Page 14: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

14AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

2-stroke Diesel engine

Used in large engines, e.g. locomotives More differences between 2-stroke gasoline

vs. diesel engines than 4-stroke gasoline vs. diesel Air comes in directly through intake ports, not

via crankcase Must be turbocharged or supercharged to

provide pressure to force air into cylinder No oil mixed with air - crankcase has

lubrication like 4-stroke Exhaust valves rather than ports - not

necessary to have intake & exhaust paths open at same time

Because only air, not fuel/air mixture enters through intake ports, "short circuit" of intake gas out to exhaust not a problem

Because of the previous 3 points, 2-stroke diesels have far fewer environmental problems than 2-stroke gasoline engines

Page 15: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

15AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

2-stroke Diesel engine

Why can't gasoline engines use concept similar to 2-stroke Diesel? They can in principle but fuel must be injected & fuel+air fully mixed after the intake ports are covered but before spark is fired

Also, difficult to control ratio of fuel/air/exhaust residual precisely since relative amounts of exhaust & air leaving exhaust ports varies from cycle to cycle (due to turbulence) - ratio of fuel to (air + exhaust) critical to premixed-charge engine performance (combustion in non-premixed charge engines always occurs at stoichiometric surfaces in overall lean mixtures anyway, so not an issue for non-premixed charge engines)

Some companies have tried to make 2-stroke premixed-charge engines operating this way, e.g. http://www.orbeng.com.au/, but these engines have found only limited application

Page 16: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

16AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Engine design & performance parameters

See Heywood Chapter 2 for more details Compression ratio (rc)

Vd = displacement volume = volume of cylinder swept by piston (this is what auto manufacturers report, e.g. 5.7 liter engine means 5.7 liters is combined displacement volume of ALL cylinders

Vc = clearance volume = volume of cylinder NOT swept by piston

Bore (B) = cylinder diameter Stroke (L) = distance between maximum excursions of piston Displacment volume of 1 cylinder = πB2L/4; if B = L (typical), 5.7

liter, 8-cylinder engine, B = 9.7 cm Power = Angular speed (N) x Torque () = 2πN

Page 17: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

17AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Classification of unsteady-flow engines

Page 18: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

18AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Engine design & performance parameters

Engine performance is specified in both in terms of power and engine torque - which is more important? Wheel torque = engine torque x gear ratio tells you whether you can

climb the hill Gear ratio in transmission typically 3:1 or 4:1 in 1st gear, 1:1 in

highest gear; gear ratio in differential typically 3:1» Ratio of engine revolutions to wheel revolutions varies from 12:1 in

lowest gear to 3:1 in highest gear Power tells you how fast you can climb the hill Torque can be increased by transmission (e.g. 2:1 gear ratio ideally

multiplies torque by 2) Power can't be increased by transmission; in fact because of friction

and other losses, power will decrease in transmission Power really tells how fast you can accelerate or how fast you can

climb a hill, but power to torque ratio ~ N tells you what gear ratios you'll need to do the job

Page 19: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

19AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Engine design & performance parameters

Indicated work - work done for one cycle as determined by the cylinder P-V diagram = work acting on piston faceNote: it's called "indicated" power because historically (before oscilloscopes) the P and V were recorded by a pen moving in the x direction as V changed and moving in the y direction as P changed. The P-V plot was recorded on a card and the area inside the P-V was the "indicated" work (usually measured by cutting out the P-V and weighting that part of the card!)

Net indicated work = Wi,net = ∫ PdV over whole cycle = net area inside P-V diagram

Indicated work consists of 2 parts Gross indicated work Wi,gross - work done during power cycle Pumping work Wi,p - work done during intake/exhaust pumping cycle

Wi.net = Wi,gross - Wi,pump

Indicated power = Wi,xN/n, where x could be net, gross, pumping and n = 2 for 4-stroke engine, n = 1 for 2 stroke engine (since 4-stroke needs 2 complete revolutions of engine for one complete thermodynamic cycle as seen on P-V diagram whereas 2-stroke needs only 1 revolution)

Page 20: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

20AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Engine design & performance parameters

Animation: gross & net indicated work, pumping work

Gross indicated workPumping work

Net indicated work(+)

(-)

Page 21: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

21AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Real engine P-V diagram

0 5 10 15 20 25 30 35 40 450

20

40

60

80

100

120

140

160

180

Volume (in3)

Pre

ssu

re (

psi

)Displacement volume

Clearance volume

Expansion stroke

Compression stroke

Intake stroke

Exhaust strokeExhaust pressure

≈ 1 atm

Intake pressure ≈ 0.3 atm

Page 22: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

22AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Engine design & performance parameters

Brake work (Wb) or brake power (Pb) = work or power that appears at the shaft coming out of the engine

Historically called "brake" because a mechanical brake [like that on your car wheels] was used in laboratory to simulate the "road load" that would be placed on an engine in a vehicle)

What's the difference between brake and indicated work or power? FRICTION Gross Indicated work = brake work + friction work (Wf)

Wi,g = Wb + Wf

Note that this definition of friction work includes not only the "rubbing friction" but also the pumping work; I prefer

Wi,g = Wb + Wf + Wp

which separates rubbing friction (which cannot be seen on a P-V diagram) from pumping friction (which IS seen on the P-V)

The latter definition makes friction the difference between your actual (brake) work/power output and the work seen on the P-V

Note the friction work also includes work/power needed to drive the cooling fan, water pump, oil pump, generator, air conditioner, …

Moral - know which definition you're using

Page 23: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

23AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Indicated vs. brake work or power

Indicated Measure cylinder P vs. time Measure crank angle vs. time Translate crank angle to volume (V)

with engine geometry (piston / crankshaft / connecting rod)

Plot P vs. V ∫PdV = indicated work (Wind) Power = WindN/n

Brake Connect engine to dynamometer

(typically electrical generator) to simulate load that vehicle places on engine

Measure torque required to spin generator at a particular speed (N)

Horsepower = Torque x N / 5252

0 5 10 15 20 25 30 35 40 450

20

40

60

80

100

120

140

160

180

Volume (in^3)

Pre

ssu

re (

psi)

Page 24: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

24AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Engine design & performance parameters

Mechanical efficiency = (brake power) / (indicated power) - measure of importance of friction loss

Thermal efficiency (th) = (what you get / what you pay for) = (power ouput) / (fuel heating value input)

Specific fuel consumption (sfc) = (mdotfuel)/(Power)

units usually pounds of fuel per horsepower-hour (yuk!) Note also

Page 25: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

25AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Engine design & performance parameters

Volumetric efficiency (v) = (mass of air actually drawn into cylinder) / (mass of air that ideally could be drawn into cylinder)

where air is at ambient conditions = Pambient/RTambient

Volumetric efficiency indicates how well the engine "breathes" - what lowers v below 100%? Pressure drops in intake system (e.g. throttling to reduce power) & intake

valves Temperature rise due to heating of air as it flows through intake system Volume occupied by fuel Non-ideal valve timing "Choking" (air flow reaching speed of sound) in part of intake system having

smallest area (passing intake valves) Will be > 100% with turbocharging or supercharging See figure on p. 217 of Heywood for good summary of all these effects

Page 26: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

26AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Engine design & performance parameters

Mean effective pressure (MEP)

Power could be brake, indicated, friction or pumping power, leading to BMEP, IMEP, FMEP, PMEP

Note Power = Torque x 2πN, thus

MEP can be interpreted as the first moment of pressure with respect to cylinder volume, or average pressure, with volume as the weighting function for the averaging process

Page 27: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

27AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Engine design & performance parameters

MEP is useful for 2 reasons Since it's proportional to power or work, we can add and subtract

pressures just like we would power or work (More important) it normalizes out the effects of engine size (Vd),

speed (N) and 2-stroke vs. 4-stroke (n), so it provides a way of comparing different engines and operating conditions

Typical 4-stroke engine, IMEP ≈ 120 lb/in2 ≈ 9 atm - how to get more? Turbocharge - increase Pintake above 1 atm, more fuel & air stuffed into cylinder, more heat release, more power

Page 28: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

28AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Engine design & performance parameters

Pumping power = (pumping work)(N)/n = (P)(V)(N)/n= (Pexhaust - Pintake)VdN/n

but PMEP = (pumping power)n/(VdN), thus PMEP = (Pexhaust - Pintake)

(wasn't that easy?) (this assumes "pumping loop" is a rectangle) Estimate of IMEP

Typical engine at wide-open throttle (Pintake = Pambient):

th,i,g ≈ 35%, v ≈ 90%, f ≈ 0.064 (at stoichiometric),

QR = 4.3 x 107 J/kg, R = 287 J/kgK, Tintake = 300K

IMEPg / Pintake ≈ 10.1

Page 29: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

29AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Engine design & performance parameters

Emissions performance usually reported in grams of pollutant emitted per brake horsepower-hour (yuk!) or grams per kilowatt hour (slightly less yuk), e.g.

One can also think of this as (mass/time) / (energy/time) = mass / energy = grams of pollutant per Joule of work done

…but Environmental Protection Agency standards (for passenger vehicles) are in terms of grams per mile, not brake power hour, thus smaller cars can have larger BSNOx (or BSCO, BSHC, etc.) because (presumably) less horsepower (thus less fuel) is needed to move the car a certain number of miles in a certain time, and still fit into a particular emissions "bin" (see lecture 5)

Larger vehicles (> 8500 lb) and stationary engines (e.g. for power generation) are regulated based on brake specific emissions directly

Page 30: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

30AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Example #1

How much power does a 5.7 liter (= 0.0057 m3) Hemi 4-stroke (n = 2) engine at 6000 RPM with thermal efficiency th = 30% = 0.30 and volumetric efficiency v = 90% = 0.90 generate using a stoichiometric gasoline-air mixture (fstoich = 0.0641, QR = 4.3 x 107 J/kg)?

Page 31: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

31AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Example #2

In a laboratory test of a 4-stroke engine with Vd = 3.05 liters at N = 3000 RPM the following performance data are measured: net IMEP 107.9 lbf/in2, 70.32 brake horsepower, fuel flow rate 16.66 kg/hr, air flow rate 269.6 kg/hr. The fuel is C8H18 (QR = 4.3 x 107 J/kg.) The ambient air temperature is 295K. The intake pressure gauge is broken, so the intake pressure is not known. Determine:

a) BMEP

b) Friction MEPFMEP = IMEP – BMEPIMEP = (107.9 lb/in2)(4.448N/lb)(in/0.0254m)2 = 7.44 x 105 N/m2

FMEP = 7.44 x 105 N/m2 – 6.88 x 105 N/m2 = 5.6 x 104 N/m2 = 0.55 atm

c) Equivalence ratioC8H18 + 12.5(O2 + 3.77N2) 8 CO2 + 9 H2O + 12.5(3.77) N2

Stoichiometric fuel/air: (8(12)+18(1))/[12.5((32)+3.77(28))] = 0.0663Actual fuel/air: (16.66 kg/hr)/(269.6 kg/hr) = 0.06179Equivalence ratio = 0.06179/0.0663 = 0.932

Page 32: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

32AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Example #2 (continued)

d) Brake thermal efficiency

e) Indicated torque

f) Is this engine throttled, turbocharged or neither? Explain. (Hint: compute the volumetric efficiency.)

Page 33: AME 436 Energy and Propulsion Lecture 6 Unsteady-flow (reciprocating) engines 1: Basic operating principles, design & performance parameters

33AME 436 - Spring 2015 - Lecture 6 - Unsteady flow engines I: principles

Summary - engine design & performance parameters

Many mechanical implementations of unsteady-flow engines exist, but all are based on a thermodynamic cycle consisting of compression, combustion, expansion

The factor that affects engine design and performance more than any other is whether the engine is premixed-charge or nonpremixed-charge

Many measures of engine performance are employed - be careful! Work and power - indicated vs. brake Efficiencies - thermal vs. volumetric Mean Effective Pressure - brake, indicated, pumping, friction