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    THERMAL ENGINEERINGUNIT-1

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    FUELS

    Fuels can be in solid, liquid or gaseous

    state.

    Principle constituent of any fuel are

    carbon and hydrogen.

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    SOLID FUELS

    WOOD : It is natural available and used as

    commercial fuel in some industries.

    PEAT : It is a mixture of decayed vegetablematter with water. It is used in gas producer

    plant.

    COAL : It includes all solid fuels from lignite

    to anthracite . The quality of coal increases

    from lignite to anthracite

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    FORMATIONOF COAL

    PEAT

    LIGNITE

    BITUMINOUS COAL

    ANTHRACITE COAL

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    SOLID FUELS

    CHARCOAL : It is prepared by destructivedistillation of wood.

    COKE : It is a solid residue left after thedestructive distillation of certain soft coals. Itis mainly used in blast furnace.

    BRIQUETTED COAL : It is a block of

    compressed coal dust. PULVERIZED COAL : Reducing coal to powder

    or dust is pulverized coal.

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    LIQUID FUELS (Typical oil pool

    formation)

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    LIQUID FUELS (Typical oil pool refining)

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    PETROLEUM

    Petra = rock + oleum = oil

    It is a mixture of hydrocarbons like paraffins ,

    olefins, naphthenes and aromatics , with some

    sulphur and other impurities.Refining of petroleum is carried out through

    fractional distillation.

    Petroleum based liquid fuels are gasoline ,

    kerosene , diesel oil , fuel oils and lubricating oils.

    Non petroleum based liquid fuels are benzol,

    alcohol, acetone and di - ethyl ether.

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    GASEOUS FUELS

    Gaseous fuel present no difficulty regarding mixingwith air , however , it creates the problem of storageand handling large volumes especially in automobiles .Different gaseous fuels are :

    Natural gas : Its primary constituent is methane (85-99%) .Other constituents are hydrocarbons , inert gases, traces of hydrogen sulphide and water.

    Natural gas is an excellent fuel for SI engines. It need

    not be vaporized unlike liquid fuels , hence cold enginestarting is easier especially at low temperature andcold start enrichment , which is the major source of COemission , is prevented. It has high ignitiontemperature and excellent antiknock properties.

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    GASEOUS FUELS

    Liquified petroleum gas (LPG) : It is a product ofpetroleum gas , principally propane , propyleneand butane.

    This gas can be liquefied at normal temperaturesubjecting to a moderate pressure. It has higherheating value compared to gasoline.

    It is suitable for IC engines because of itsavailability and low carbon content.

    It has self-ignition temperature and a high octanenumber, which makes it suitable for SI engines.

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    GASEOUS FUELS

    Producer gas : It is produced by burning

    carbonaceous material with large deficiency of air

    and treating with steam. It has low heat value.

    Coal gas : Coal is heated to a temperature of1500C in the presence of very little air to

    decompose.

    Hydrogen : hydrogen, as an SI engine fuel

    acquires special significance in view of its

    unlimited supply potential and almost non-

    polluting characteristics. But it is a costly

    automotive fuel

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    INTERNAL COMBUSTION ENGINE

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    FLASH POINT

    The safety of a diesel oil is measured by its flashpoint and fire point.

    It is the lowest temperature at which a fuel willvaporize sufficiently to form a combustiblemixture of fuel vapour and air above the fuel.

    It can be determined by heating a quantity of fuelin a special container, while passing a flame overthe liquid to ignite vapours.

    A distinct flash of flame occurs when the flash

    point temperature has been reached.A minimum flash point of 65C is specified for

    safety.

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    FIRE POINT

    It is the temperature at which enough vapours

    will rise to produce a continuous flame above

    the liquid fuel.

    The flame must sustain at least for 5 sec.

    The fire hazard increases with increase in

    volatility.

    As the volatility of diesel oil is lesser than

    gasoline ,it is safer under most circumstances.

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    Heat of formation : The amount of heat

    evolved or absorbed in the formation of onemole of a substance from its component

    atoms is known as the heat of formation. It is

    the heat change when substance formed.

    Heat of combustion : The amount of heat

    produced when one mole of a substance is

    burned in oxygen. It is the heat produced by

    combustion.

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    NORMAL COMBUSTION

    The combustion in a gaseous fuel-air mixture ignited bya spark is characterized by a rapid development offlame that starts from the point of ignition and spread

    out in a continuous manner without any abrupt changein its speed and shape, is normal combustion.

    Combustion spreads to the envelope of mixture at arate depending primarily on the temperature of flame

    front and secondarily on the temperature and densityof surrounding envelope.

    The amount of heat generated in the process ofcombustion out of mass fuel is known as calorific value.

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    THEORETICAL PRESSURE Vs CRANK

    ANGLE DIAGRAM

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    ABNORMAL COMBUSTION AUTOIGNITION

    ANDDETONATION

    If the temperature and pressure of the endgas (the gas ahead of the flame front) are highenough, it will ignite spontaneously before the

    flame front reaches it, then it is calledabnormal combustion.

    It varies from the process of normalcombustion only at the end of combustion.

    The sudden inflammation of remainingportion of the end-gas is called autoignition.

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    DELAY PERIOD

    In autoignition, the charge must remain above

    a critical temperature for a certain length of

    time known as the IGNITION DELAY OR DELAY

    PERIOD.

    During the delay period, certain chemical

    reaction takes place which prepare the change

    for autoignition.

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    COMBUSTIONWITH DETONATION

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    DETONATIONORKNOCKING

    Knocking or detonation is characterized by highpitched metallic ringing sound.

    In autoignition the burning is almost

    instantaneous which results in an extremely rapidrelease of energy causing pressure of end-gas toincrease almost 3 to 4 times.

    The excess pressure gives rise to severe pressure

    waves which strike the cylinder wall and set tovibrate, causing sound.

    The flame speed is of the order 300 to 1000 m/s.

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    DETRIMENTAL EFFECTSOF DETONATION

    Noise and vibration: The pitch of the sound depends upon thesize and shape of the combustion space and the velocity of wave at

    speed of sound in cylinder gases . It also causes vibration of various

    engine parts.

    Increase in heat transfer: The increase in the rate of heat transfer isbecause of higher temperature of gas in detonating engine due to rapid

    completion of combustion. The pressure waves scour away the protective

    layer of stagnant gas on cylinder.

    Pre ignition:-Ignition of the mixture by hot surface within the combustion space,before the normal spark ignition occurs is called pre ignition.

    -Over heating of the spark plug electrodes leads to pre ignition.

    -The burning time losses are generally increased and the power and efficiency are

    reduced.

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    Mechanical damage:

    Power and efficiency: Increase in heat loss of cylinder cause reduced

    power output and loss of thermal efficiency.

    Carbon in the exhaust: Over long period of running of engine, largeamount of carbon is deposited. As a result of detonation, deposited

    carbon is not only blown out as exhaust but also leaves the surface ofcombustion chamber and top of piston becomes rough and pitted.

    -The impact pressure causes the fracture of aluminium alloy

    piston

    -The increase in temperature causes overheating and burning of the

    gaskets between the cylinder and its head, electrodes and insulators

    of spark plug, piston crown and the head of valves.

    -In severe cases of detonation, increased cylinder and piston

    temperature causes collapsing of piston crown and sometimes the

    burning of cylinder head.

    -Under detonating condition, puffs of gray smoke occurs and during night, puffs

    are seen as light yellow flashes. Puffs of black exhaust smoke represents free

    carbon in exhaust gas.

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    OCTANE NUMBER The fuels octane number is the measure of a fuels resistance to knock in SI

    engines.

    The higher octane number (ON) indicates high resistance to knock and higher

    compression ratio maybe used without knocking.

    The octane number depends upon the engine design and the operating condition

    during test.

    The octane number scale is based on two hydrocarbons which define the ends ofthe scale.

    The scale has been set up in which isooctane (2-2-4-trimethyl pentane) being a

    very good anti-knock fuel is arbitrarily assigned a rating of 100 octane number.

    On the other hand, normal heptane has very poor anti-knock quality and it is

    given a rating of zero octane number. A gasoline is rated 90 octane number if its tendency to detonate in the test

    engine is the same as that of a mixture of 90% isooctane and 10% normal

    heptane by volume.

    Octane number is determined by either research method (TESTING CODE: ASTM

    D -2700) or motor method (TESTING CODE : ASTMD -2699)

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    SUPERCHARGING

    Supercharging is a method of increasing the power output of the engine without

    increasing its weight and size. This is made possible by increasing the density of thecharge, which ensures greater amount of charge aspirated into the same stroke

    volume.

    Supercharging can be defined as the admittance of more charge into the engine

    cylinder than what the engine can take during the normal suction stroke.

    USES:

    The three basic methods used for supercharging are MECHANICAL

    SUPERCHARGING, TURBOCHARGING and PRESSURE WAVE SUPER CHARGING.

    -It is used in high altitudes where the suction pressure of charge in cylinder

    reduces, which in turn reduces the power output.

    -In case of motor vehicle climbing hill, the power output reduces. Therefore,

    with increase in height the degree of supercharge is increased.

    -It is necessary in case of racing-car engines and aircraft engines where specificoutput is of prime importance.

    -It is used where a limited space is only available for the engine.

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    TURBOCHARGING In turbocharging, a turbocharger (a compressor and a turbine mounted on a

    single shaft) is used to increase the inlet air density. The exhaust gases from the engine having sufficient energy to drive the

    turbine which in turn drives the compressor mounted on the same shaft,

    which increases the inlet air density before the air enters the cylinder.

    The combination of an engine driven compressor and a turbocharger is

    used in large marine engines.

    The combination of 2 stage turbocharging provides very high boost pressure

    to obtain higher power output.

    In the arrangement of turbocompounding, the second turbine is directly

    geared to the engine drive shaft, thus increasing engine power andefficiency.

    The arrangement of charge cooling with a heat exchanger after

    compression and prior to entry to the cylinder, cooling of the charge further

    increases density.

    The above combination are shown the figure below :

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    TURBOCHARGING

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    COMBUSTION CHAMBER TYPES

    The combustion chamber is important as it

    affects the engine performance, its knocking

    tendencies and exhaust pollutants.

    Brief description of a few important types ofcombustion chambers, with location of valves

    and spark plug, showing their developments

    are given below :

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    T-HEAD TYPE COMBUSTION CHAMBER

    This was the earlier type used by Ford Motor Corporation duringearly stages of engine development in 1908.

    The T-head suffers following disadvantages :

    There was a violent knocking even at compression ratio 4:1, this wasalso because of low octane number of the petrol available at that

    time, which varied from 45 to 50.

    -The distance across the combustion chamber is very long. The spark plug is

    located near the exhaust valve, so the flame travel distance from the spark plug tothe end-gas (near the inlet valve) increases. Therefore, knocking tendency is

    increased.

    -The configuration provides two valves on either side of combustion chamber,

    requiring two camshafts.

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    T-HEAD TYPE COMBUSTION CHAMBER

    Combustion Chamber

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    L-head or side valve combustion

    chamber

    The combustion chamber is in the form of more or less flat slab, extending over thepiston.

    The disadvantage of T-head combustion chamber forced the development ofL-

    head, in which two valves are placed on the same side of the combustion chamber,

    thus reducing the flame distance, and the valve are operated by a single camshaft.

    During 1910-1930 this type of combustion chamber were commonly used in SI

    engines, in which, the valves are placed side by side in a detachable block.

    Manufacturing and maintenance of this type of combustion chamber are both easy.

    The detachable head can easily be removed for decarbonising without disturbing

    either the valve gear or the main pipe work.

    In its original form, this type of engine gave poor performance because of the

    following limitation : lack of turbulence, extremely prone to knock, extremely

    sensitive to ignition timing.

    The side valve engines are not preferred for higher compression ratio on account of

    inadequate volumetric efficiency, no compactness and additional requirement of

    cooling.

    This engine do not compare well with overhead valve engines

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    L-head or side valve combustion

    chamber

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    RICHARDO TURBULENT HEADSIDE VALVE

    COMBUSTION CHAMBER

    The main objective of this design was to increase turbulence in order to obtain a

    higher flame speed and to reduce the knocking tendency.

    During compression stroke the gases were forced back to the main body through

    restricted passage-way that creates additional turbulence

    By varying the throat area of the restricted passage it was possible to achieve any

    desired degree of turbulence. The rate of combustion during the second stage ofcombustion was improved and this resulted in improved performance.

    In order to reduce knocking tendency to minimum, the distance of effective flame

    travel was shortened by forming a very thin layer of entrapped gas between the

    piston crown and portion of chamber at end gas region, where the piston was at

    TDC. The flame distance is further reduced by placing the spark plug in the center of

    effective combustion space with a slight shift towards exhaust valve.

    With the relatively high octane petrol available today, the compression ratio has

    been increased resulting in lack of space to accommodate the engine. Hence this

    engine can no longer compete with the overhead design.

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    RICHARDO TURBULENT HEADSIDE VALVE

    COMBUSTION CHAMBER

    COMBUSTION CHAMBER

    EX

    INLET VALVE

    EXHAUST

    VALVE

    EXHAUST

    VALVE

    PISTON

    CYLINDER

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    OVERHEADVALVE ORI-HEAD TYPE

    COMBUSTION CHAMBER

    The two important arrangements of this type of chamber are :bath-tub typeand wedge type combustion chamber.

    ADVANTAGES : The volumetric efficiency is higher because of better breathing of engine from

    larger valves and the pumping losses are less because of more direct passageways

    with less pressure drop through valves. The average flame travel distance is reduced and the engine is less prone to knock,

    resulting in less octane requirement.

    The surface to volume ratio is decreased which results in an increase in thermalefficiency of the engine. Its also provides more complete combustion of fuel, thusproducing more power and reducing air pollution.

    Hot exhaust valve is placed over the head instead of in the cylinder block, thusconfirming thermal failures only to cylinder head which can be easily removed andreplaced.

    The possibility of leakage of compression gases and jacket water is reduced as inthis type the cylinder head bolts are subjected to less force.

    The casting process is easier, thus leading to reduction in costs.

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    BATH-TUB TYPE OF COMBUSTION CHAMBER

    It is the most simple and convenient form of overhead valvecombustion chamber with an oval-shaped combustion chamber

    bolted over the main cylinder in such a way that some part of oval

    portion overhangs the cylinder. This part maybe used for squish

    (squish is the rapid injection of gas trapped between the piston and

    some flat or corresponding surface in the cylinder head).

    Both the valves are mounted vertically overhead, with spark plug at

    side.

    The main disadvantage is that the valves are placed in a single row

    along the cylinder block, resulting in less space to locate valves forlarge diameter. It reduces volumetric efficiency.

    More space for valves within the bore diameter can be made

    available if the stroke/bore ratio is kept unity or less.

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    BATH-TUB TYPE OF COMBUSTION CHAMBER

    PISTON

    CYLINDER

    COMBUSTION

    CXHAMBER

    EXHAUST VALVE

    SPARK

    PLUG

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    WEDGE-SHAPED COMBUSTION CHAMBER

    The combustion chamber is wedge-shaped with slightly inclined

    valves .

    This type has also given satisfactory performance.

    The wedge-shaped combustion chamber is shown below :

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    WEDGE-SHAPED COMBUSTION CHAMBER

    PISTON

    CYLINDER

    SPARK

    PLUG

    EXHAUST

    VALVE

    EXHAUST

    MANIFOLD

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    F-HEAD TYPE COMBUSTION CHAMBER

    The type of combustion chamber in which one valve is located in the

    head and the other in the block is known as F-head combustionchamber.

    It has a well shaped piston crown with a correspondingly matched

    sloping cylinder head.

    The inlet and exhaust valve are inclined. The inlet valve is located inthe head and the exhaust valve in the block.

    The plug is in an excellent position in the flat roof of the chamber.

    The flat roof allows the larger use of a larger size of the inlet valve

    than the exhaust valve. The cooling of spark plug and exhaust valve is efficient.

    The flame travel distance is short and the end-gas is reduced to a thin

    layer, so the knocking tendency is reduced.

    The operation of the valves involves a complex mechanism.

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    Hemispherical combustion chamber

    A hemispherical chamber with inclined valves is the best design to

    use where maximum specific output is required, involving pistonspeeds exceeding 15m/s.

    Nearly all racing cars have used the hemispherical cylinder head with

    domed piston.

    ADVANTAGES :-The combustion chamber is very compact.

    -The surface-to-volume ratio is small which reduces the heat loss of

    the cylinder wall, thus providing a higher thermal efficiency.

    -the larger diameter valves employed increases the volumetricefficiency.

    However, the operation of the valves and placing of the spark plugs in

    a multi-cylinder engine present difficulties unless a twin overhead

    camshaft mechanism is used.

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    PISTON CAVITY COMBUSTION CHAMBER

    The combustion chamber comprises a bowl in the piston crown in

    conjunction with a flat cylinder head.

    It resembles the combustion chamber of the normal direct-injection

    compression ignition engine.

    Here an almost ideal chamber shape is provided with all surface

    machined to give an accurately defined volume.

    Such a design was not possible in past when long strokes and low

    compression ratios were used, but now with the use of high

    compression ratios and stroke/bore ratios near one less, this

    configuration has become practical and likely to appear more infuture.

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    END