16998 Fuel Injection 2

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    Fuel Injection

    The purpose of carburetion and fuel-injection is the same viz,

    preparation of the combustible charge.

    But in the case of carburetion fuel is atomized by process relying on

    the air speed greater than fuel-injection.

    The fuel speed at the point of delivery is greater than the air speed

    to atomize the fuel.

    When the fuel is injected into the combustion chamber towards the

    end of compression stroke, it is atomised into very fine droplets.

    These droplets vaporise due to the heat transfer from the

    compressed air and form a fuel-air mixture.

    Due to continued heat transfer from hot air to the fuel, thetemperature reaches a value higher than its self-ignition temp.

    This causes the fuel-to ignite spontaneously.

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    Functional requirement of an injection

    system -For a proper running and good performance from the

    engine, the following requirements must be met by the injectionsystem

    Accurate metering

    Timing the injection

    Rate of injection Proper atomization

    Proper spray pattern

    Uniform distribution of fuel droplets

    Equal quantities of metered fuel to all cylinders for multicylinder engines.

    No lag thus eliminating dribbling.

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    Classification of injection systems -

    In a constant-pressure cycle or diesel engine, pure air is compressed in the

    cylinder and then fuel is injected into the cylinder by means of a fuel-

    injections system. For producing the required pressure for atomizing the

    fuel either air or a mechanical means is used. Accordingly the injection

    systems can be classified as

    1. Air injection system. In this system fuel is forced into the cylinder by

    means by compressed air. This system is little used now-a-days, because

    it requires a bulky multi-stage air compressor.

    2. Solid injection system (Misnomer). In this system the liquid fuel is

    injected directly into the combustion chamber without the aid of

    compressed air. Hence, it is also called airless mechanical injection or

    solid injection system

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    Solid injection systems can be classified into four types-

    (a) Individual pump and nozzle system

    (b) Unit injector system(c) Common rail system

    (d) Distributor system.

    All the above systems comprise mainly of the following components

    (i) Fuel tank

    (ii) Fuel feed pump

    (iii) Injection pump

    (iv) Governor

    (v) Injector

    (vi) Fuel fitters.

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    Solid Injection System used in CI Engine: A typical arrangement of

    various component of solid injection system used in CI Engine is

    shown below.

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    INJECTION PUMP

    The main objectives of fuel-injection pump is to deliver

    accurately metered quantity of fuel under high pressure (in the

    range of 120-200 bar) at the correct instant to the injector fitted

    on each cylinder.

    Injection pumps are generally of two types

    (I) Jerk type pumps

    (ii) Distributor type pumps

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    FUEL INJECTOR

    Quick and complete combustion is ensured by a well designed fuel injector. By

    atomizing the fuel into very fine droplets, it increases the surface area of the fuel

    droplets the surface area of the fuel droplets resulting in better mixing and

    subsequent combustion. Atomization is done by forcing the fuel through a smallorifice under high pressure.

    The injector assembly consists of

    (i) A nozzle value

    (ii) A compression spring

    (iii) A nozzle

    (iv) An injector body

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    FUEL INJECTOR (BOSCH)

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    NOZZLE

    Nozzle is that part of an injector through which the liquidfuel is sprayed into the combustion chamber. The nozzleshould fulfill the following functions

    (i) Atomization

    (ii) Distribution of fuel

    factors affecting this are-

    (a) Injection pressure

    (b) Density of air in the cylinder

    (c) Physical properties of fuel

    (iii) Prevention of impingement on walls

    (iv) Mixing

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    Various types of nozzles are used in C I engines.

    The most common types are

    (i) Pintle nozzle

    (ii) Single hole nozzle

    (iii) Multi-hole nozzle

    (iv) Pintaux nozzle.

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    (i) Pintle Nozzle -It provides a spray operating at low injection pressures of 8 -

    10 MPa. The spray cone angle is generally 60 0 . Advantage of this nozzle is

    that it avoids weak injection and dribbling. It prevents the carbon deposition

    on the nozzle hole.

    (ii) (ii) Single hole nozzle -The size of the hole is usually of the order of 0.2 mm.

    Injection pressure is of order of 8-10 MPa and spray cone angle is about 15 0

    . Ma-jor disadvantage with such nozzle is that they tend to brittle Besides,

    their spray angle is too narrow to facilitate good mixing unless highervelocities are used.

    (iii) Multi-hole nozzle -The number of holes varies from 4 to 18 and the size from

    35 to 200 um. The hole angle may be from 20 degree upwards. These nozzles

    operate at high injection pressures of the order of 18 MPa. Their advantage

    lies in the ability to distribute the fuel properly even with lower air motion

    available in open combustion chamber.

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    (iv) Pintaux nozzle -It is a type of pintle nozzle which has an auxiliary hole drilled

    in the nozzle body. This hole is used for pilot injection. The needle valve does not

    lift fully at low speeds and most of the fuel is injected through the auxiliary hole.

    Main advantage of this nozzle is better cold starting performance. A major

    drawback of this nozzle is that its injection, characteristics are poorer than the multi

    hole nozzle.

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    SPRAY FORMATION

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    At the start of the fuel-injection the pressure difference across the orifice is

    low. Therefore single droplets are formed as in the above fig(a). As the

    pressure difference increases the following process occur one after the

    other.

    (i) A stream of fuel emerges from the nozzle fig (b).

    (ii) The stream encounters aerodynamic resistance from the dense air present

    in the combustion chamber (12 to 14 times the ambient pressure) and

    breaks into a spray, say at a distance of l3, fig (c). The distance of this point

    where this event occurs from the orifice is called the break-up distance (l3)

    (iii) With further and further increase in the pressure difference the break-up

    distance decreases and the cone angle increases initial the apex of the cone

    practically coincides with the orifice, fig (d) , (e) , (f).

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    The droplets sizes depends on various factors which are listed

    below

    (i) Mean droplet size decreases with increase in injection

    pressure

    (ii) Mean droplet size decreases with increases in air density.

    (iii) Mean droplet size increases with increase in fuel viscosity.

    (iv) Size of droplets increases with increase in the size of the

    orifice.

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