02 Part6 Energy Balance

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    Energy Balances

    S.GunabalanAssociate ProfessorMechanical Engineering DepartmentBharathiyar College of Engineering & TechnologyKaraikal - 609 609.e-Mail : [email protected]

    Part - 2

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    Steady Flow Energy equation

    1 +1

    2

    + 1 +

    = 2 +

    2

    2

    + 2 +

    Energy Balances on Open Systems

    is Velocity

    111

    = 22

    2

    This is Equation of Continuity

    Velocity of flow

    Mass Balance

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    Study Flow process in NOZZLE

    Device which increases the velocity

    1 +1

    2 + 1 +

    = 2 +2

    2 + 2 +

    1 +1

    2 = 2 +

    2

    2

    No heat transfer & work transfer

    No potential energy change

    The inlet velocity of the nozzle is very small compared

    to the outlet velocity ie V2 >>>> V1

    So V1 is negligible and thus V1 = 0

    1 +1

    2 = 2 +

    22

    1 = 2 +2

    2

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    Study Flow process in Diffusor

    Device which increases the Pressure

    1 +1

    2 + 1 +

    = 2 +2

    2 + 2 +

    1 +1

    2 = 2 +

    2

    2

    No heat transfer & work transfer

    No potential energy change

    The inlet velocity of the diffuser is very high compared

    to the outlet velocity ie V1 >>>> V2

    So V2 is negligible and thus V2 = 0

    1 +1

    2 = 2 +

    22

    1 +1

    2 = 2

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    Study Flow process in Throttle valve

    Device which increases the Pressure

    1 +1

    2 + 1 +

    = 2 +2

    2 + 2 +

    1 +1

    2 = 2 +

    2

    2

    No heat transfer & work transfer

    No potential energy change

    The inlet velocity and outlet velocity are same

    V1 - V2 = 0 (or negligible)

    1 +1

    2 = 2 +

    22

    =

    Write down the steady flow

    Equation and reduce it for

    throttling process (4 marks)

    (Apr 2013)

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    Study Flow process in Turbine and

    CompressorDevice which increases the Pressure

    1 +1

    2 + 1 +

    = 2 +2

    2 + 2 +

    1 +1

    2 = 2 +

    2

    2 +

    No heat transfer & there is a Definite Work transfer

    No potential energy change

    If The inlet velocity and outlet velocity are negligible

    1

    + 1

    2 =

    2

    + 2

    2 +

    = +

    = +

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    Prob-1

    A steam power plant, steam flow steadily through a

    0.2m diameter pipeline from a boiler to a turbine.

    At the boiler end, the steam conditions are p =

    4MPa, T = 400C, h= 3213.6 KJ/kg, v = 0.073 m3/kgAt the turbine end, the steam conditions are p =

    3.5MPa, t = 392C, h= 3202.6 KJ/kg, v = 0.084 m3/kg

    There is a heat loss 8.5 KJ/kg from the pipeline.

    Calculate the steam flow rate(Apr 2013)

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    Prob-1

    A steam power plant,

    steam flow steadily through a 0.2m diameter pipeline

    boiler --->> turbine.

    At the boiler end

    p = 4MPa, T = 400C, h= 3213.6 KJ/kg, v = 0.073 m3/kgAt the turbine end

    p = 3.5MPa, t = 392C, h= 3202.6 KJ/kg, v = 0.084 m3/kg

    heat loss 8.5 KJ/kg (dQ/dm) so take as -ve.

    Calculate the steam flow rate (w kg/s)( Apr 2013)

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    Heat loss from the pipeSo

    = - 8.5 KJ/kg

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    =

    1 =

    2 ------ (1)

    1 + 1

    2 + 1 +

    = 2 + 2

    2 + 2 +

    ------ (2)

    (pipe Constant cross section)

    1 = 0.073 m3/kg2 = 0.084 m3/kg

    h1= 3213.6 KJ/kg

    h2= 3202.6 KJ/kg

    = - 8.5 KJ/kg

    Substitute eqn.(1) in (2)

    Get, v1 and even V2

    =

    1 = 0.073 m3

    /kgSubstitute in below equation

    get w

    Mass flow rate w =

    Pipe diameter = 0.2m

    In steady flow equation mass flow rate is constant

    Mass flow rate w =

    =

    This is Equation of Continuity

    Velocity of flow m/s2

    Specific Volume m3

    /kg

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    Prob-2

    Air at a temperature of 15 passes through aheat exchanger at a velocity of 30 m/s, where

    its temperature is raised to 800 .It is then

    enters a turbine with the same velocity of30m/s and expands until the temperature falls

    to 650 . On leaving the turbine, the air istaken at a velocity of 60m/s to a nozzle where

    it expands until the temperature has fallen to500 .If the air flow rate is 2 Kg/S

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    Prob-1

    Find

    a) The rate of heat transfer to the air at the

    heat exchanger

    b) The power output from the turbine

    assuming no heat loss

    c) The velocity at the exit of the nozzle,

    assume no heat lossTake the enthalpy of air as Cpt, Cp = 1.0005

    KJ/KgK (Nov-2010)

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    Ans: 1 +1

    2 + 1 +

    = 2 +

    2

    2 + 2 +

    w1 1 +

    + 1 + 12 = w2 2 +

    + 2 + 12

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    Ans: a)

    w1 1 +

    + 1 + 12 = w2 2 +

    + 2 + 12

    w1 1 + 12 = w2 2 air flow rate is w 1= w2 = 2 Kg/SSpecific enthalpy

    = 2 1 = 2 1 Find

    12 = w2 2 w1 1 W2 = w112 = w(h2h1) = w 2 1

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    Ans:b) The power output (W) from the

    turbine assuming no heat loss (Q =0)w2 2 +

    + 2 + 23 = w3 3 +

    + 3 + 23

    w2 2 +

    = w3 3 +

    + 23

    w 2 3 + w = 23wcp 2 3 + w

    = 23

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    Ans:c) The velocity at the exit of the

    nozzle, assume no heat loss (Q =0)w2 2 +

    + 2 + 23 = w3 3 +

    + 3 + 23

    w2 3 +

    = w3 4 +

    (3 4) +3

    2 = 4

    2

    (3 4) +3

    2 =

    2

    = ?

    Specific enthalpy

    = 2 1 = 2 1

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    Prob-3

    A blower handles 1 kg/s of air at 20oC and

    consumes 15KW power. The inlet and outlet

    velocities of air are 100m/s and 150 m/s. find

    exit air temperature, assuming adiabaticcondition. Take Cp of air 1.005 Kj/Kgk.

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    Blower

    Mass flow rate w = 1 kg/s

    T1 = 20oC

    Power or work done = 15KW

    The inlet velocities V1 = 100m/s

    and outlet velocities V2 = 150 m/s.

    find exit air temperature

    assuming adiabatic condition.

    Take Cp of air 1.005 Kj/Kgk.

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    Blower

    General Steady Flow Energy equation for Blower

    w1 1 +

    + 1 + 12 = w2 2 +

    + 2 + 12

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    Steady Flow Energy equation for

    Blower

    No potential energy term involved in the process

    w1 1 +

    + 1 + 12 = w2 2 +

    + 2 + 12

    assuming adiabatic condition.

    w1 1 +

    + 1 + 12 = w2 2 +

    + 2 + 12

    w1 1 +

    + 12 = w2 2 +

    For steady flow , w1 = w2 = ww 1 +

    + 12 = w 2 +

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    Blower

    For steady flow , w1 = w2 = w = 1 kg/s (given)

    w 1 +

    + 12 = w 2 +

    w 1

    2

    + 12

    = w

    w (1 2) + 12 = w

    1/ 1.0051000/(20 2) + 151000 = 1 kg/s

    T2 = ----- oC

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    Prob-4A turbine operates under steady flow conditions, receives steam at the

    following state

    Pressure = 1.2 Mpa

    Temperature = 188oC

    Enthalpy = 2785 KJ/kg

    Velocity = 33.3 m/s

    Elevation = 3 mSteam leaves the turbine in the following state

    Pressure = 20 Mpa

    Enthalpy = 2512 KJ/kg

    Velocity = 100 m/s

    Elevation = 0 m

    Heat is lost to the surrounding at the rate of 0.29 KJ/s

    Rate of steam flow through the turbine is 0.42 kg/s

    What is the power output of the turbine in Kw

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    w1 1 +

    + 1 12 = w2 2 +

    + 2 + 12

    Heat is lost to the surrounding at the rate of 0.29 KJ/s (Q)

    Rate of steam flow through the turbine is 0.42 kg/s (w1= w2)

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    w1 1 +

    + 1 12 = w2 2 +

    + 2 + 12

    Heat is lost to the surrounding at the rate of 0.29 KJ/s (Q)

    Rate of steam flow through the turbine is 0.42 kg/s (w1= w2)

    0.42kg/s 2785

    + .

    + 9.81

    3 0.29/

    = 0.42kg/s 2512

    + 100

    2 + 0

    + 12

    W = ----- KW

    W = 112.6264729 KW

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    Prob-5- Exercise

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    a) Find the velocity at the exit of the nozzle

    w1 1 +

    = w2 2 +

    (1 2) + 1

    2 = 2

    2

    = ?

    w1 = 2 (steady flow)

    b) If the inlet area is A1 = 0.1 m2,and specific volume at inlet is = 0.187 m3/kgFind the mass flow rate

    W =

    c) Find the specific volume at the exit is of the nozzle is 0.498 m3/kg,Find the Exit area of the nozzle (A2)

    W =

    W =

    =

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    Reference

    Rajput, R. K. 2010. Engineering thermodynamics. Jones and Bartlett

    Publishers, Sudbury, Mass.

    Nag, P. K. 2002. Basic and applied thermodynamics. Tata McGraw-Hill, New

    Delhi.