ic engines - abstracted

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    IC ENGINES

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    1. Basics

    2. Classification

    3. Terminology

    4. Components

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    Basics Combustion Engines Chemical energy in fuel converted to thermal energy by

    combustion or o idation !eat engine converts chemical energy into mechanical energy Thermal energy raises temperature and pressure of gases "ithin

    engine# and gas e pands against mechanical mechanisms ofengine

    Combustion $nternal% fuel is burned "ithin the engine properly &including e.g.

    roc'et engines# (et engines) E ternal% combustion is e ternal to the engine &e.g. steam# *tirling

    engine)

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    Jetengine

    Stirlingengine

    Steamengine

    Gas

    Turbine

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    1. Basics

    2. Classification

    3. Terminology

    4. Components

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    Classification of $C engines $gnition +umber of stro'es ,alve location

    -esign osition and number of cylinders /ir inta'e 0uel input method 0uel used Cooling /pplication

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    $gnition Spark ignition &*$)% high voltage electrical discharge bet"een t"o

    electrodes ignites air fuel mi ture in combustion chambersurrounding spar' plug# etrol Engine Compression ignition &C$)% air fuel mi ture self ignites due to high

    temperature in combustion chamber caused by high compression#-iesel engine

    +o. of stro'es

    0our stro'e % four piston movements over t"oengine revolutions for each engine cycle T"o stro'e % t"o piston movements over one

    revolution for each engine cycle

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    ,alve location ,alves in head ,alves in bloc' ne valve in head and one in bloc' &less common)-esign

    eciprocatingo Engine has one or more cylinders in "hich pistonsreciprocate bac' forth

    o Combustion chamber in closed end of the cylindero o"er delivered to rotating output cran'shaft by mechanical

    lin'age "ith pistons otary

    o Engine made of bloc' built around large nonconcentric rotor cran'shaft

    o

    Combustion chambers are built into the non rotatingbloc'

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    Reciprocating engine

    Rotaryengine

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    osition +o. of Cylinders *ingle cylinder &e.g. la"nmo"ers) $n line or straight% cylinders in straight line# one behind the other

    in length of cran'shaft ,% t"o ban's of cylinders at an angle "ith each other along a

    single cran'shaft# angle typically 56 768 0lat or opposed cylinder &, "ith 1968)% t"o ban's of cylinders

    opposite each other on a single cran'shaft &small aircrafts) :% three ban's of cylinders on same cran'shaft &not common) pposed piston engine% t"o pistons in each cylinder# combustion

    chamber bet"een pistons adial engine% cylinders positioned radially around cran'shaft

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    Inline engineV engine

    Flat/opposed cylinderengine

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    W engine

    pposed piston engine Radial engine

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    Superc!arged

    Turboc!arged

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    0uel input method Carburated % air fuel mi ed at throat Fuel injection

    ;ultipoint ort 0uel $n(ection % one or more in(ectors ateach cylinder inta'e

    Throttle Body 0uel $n(ection % in(ectors upstream ofinta'e manifold

    Cooling /ir cooled

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    0uel used >asoline -iesel or fuel oil >as &natural gas or methane) )% mainly propane#

    propylene# butane and butylene /lcohol &ethyl# methyl) -ual fuel &e.g. methane?diesel) >asohol &e.g. 76@ gasoline# 16@ alcohol) Biodiesel % cleaner burning diesel fuel made from

    natural# rene"able sources such as vegetableoils

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    1. Basics

    2. Classification

    3. Terminology

    4. Components

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    Terminology TDC % top dead center# piston position farthest from

    cran'shaft BDC % bottom dead center# piston position nearest to

    cran'shaft Direct fuel injection % into main combustion chamber

    Indirect fuel injection % into a secondary chamber Bore % diameter of cylinder or piston face Stroke % distance that piston moves Clearance volume % volume in combustion chamber at T-C Displacement volume % volume displaced by piston Ignition delay % Time bet"een start of ignition and start of

    combustion

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    Terminology &Contd.) Air-fuel ratio % atio of mass flo" rate of air to

    that of fuel Specific fuel consumption % fuel used per unit

    po"er

    missions % + # C # !C# solids

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    1. Basics

    2. Classification

    3. Terminology

    4. Components

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    Components of an engine

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    Components Block % body of engine containing cylinders Bearing % main bearing for cran'shaft Cams!aft % rotating shaft used to push open valves at the

    proper time in engine cycle Carburetor % ,enturi flo" device to dra" fuel and mi "ith

    air Catalytic converter % reduces emissions by chemical

    reaction Combustion c!amber % volume bet"een cylinder head

    and piston face Connecting rod % connects piston "ith cran'shaft Crankcase % part of engine bloc' surrounding cran'shaft Cranks!aft % rotating shaft through "hich engine "or'

    output is supplied to e ternal systems# rotated byreciprocating pistons through connecting rods

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    Components &Contd.) "!aust manifold % piping "hich carries e haust gases

    a"ay from engine cylinders Fan % to increase air flo" through radiator Fly#!eel % to smoothen engine rotation Fuel injector % pressuriAed noAAle to in(ect fuel into air or

    cylinder Fuel pump % to move fuel from tan' to engine $lo# plug % electrical resistance inside combustion

    chamber to help cold start %ead % piece "hich closes end of cylinders %ead gasket % sealant bet"een engine bloc' and head Intake manifold % piping "hich delivers incoming air to

    cylinders &il pan % oil reservoir on bottom of engine bloc'# part of

    the cran'case

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    Components &Contd.) il pump % to distribute oil from sump il sump % reservoir for the oil system of the engine iston rings % metal rings around piston to seal gap

    bet"een piston and cylinder ush rods % lin'age bet"een camshaft and valves on

    !, engines adiator % li=uid to air heat e changer to cool engine od bearing % rod connecting the piston "ith the rotating

    cran'shaft *par' plug % creates high voltage discharge across an

    electrode gap *peed control cruise control % control system *tarter % hand starter# electric motor# or small $C engines

    for large $C engines

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    Components &Contd.) Superc!arger % compressor po"ered from cran'shaft to

    compress incoming air T!rottle % butterfly valve at upstream end of inta'e

    manifold to control air flo" rate into *$ engine Turboc!arger % turbine compressor po"ered by e haust

    flo" to compress incoming air 'alves % controls flo" of air in and out of the cylinders (ater jacket % li=uid flo" passages around cylinder for

    cooling (ater pump % to circulate coolant