Drying Technologies

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    Vacuum Drying of foods Methods of water removal

    to obtain final products of thehigh quality

    byreducing air pressure which results in drying at a

    lower temperature than is

    required at full pressure.

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    States of Water

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    Industry has grouped pressures

    below atmospheric level into

    Rough vacuum

    is used in about 90% of the chemical,petrochemical, and other processingindustries.

    vacuum distillation,

    filtration,

    crystallization,

    reaction,

    drying, others.

    Medium vacuum

    molten metals degassing, moleculesdistillation, freeze drying, and others.High and ultra-high vacuum thin films, research, and space

    simulation.(Power,2005)

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    Heat Transfer Mechanismsat Low Pressure

    fsh TThq

    xTkqC

    1/1/121

    44

    21

    ss

    C

    TTq

    Convection

    Conduction

    Radiation

    total pressure decreases, heat transfer coefficient (h) decreases

    h : negligible, under high vacuum,.

    k :lowest value at high vacuum

    total pressure decreases, thermal conductivity (k) decreases

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    Heat Transfer Mechanismsat Low Pressure

    Heat transfer ispoorly transferredunder vacuum.

    Heat is generallytransferred to the

    product byconduction andsometimes byradiation.

    Convection is raresince very few fluid

    molecules areavailable undervacuum.

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    Ejectors : Vacuum Pump

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    Problem of Vacuum Drying Main problem of drying processes under vacuum .

    The high operating and maintenance costs

    The long drying times under continuous vacuumincrease theirenergy consumption enormously and

    make the process considerably more expensive as

    compared to drying at atmospheric pressure.

    (Ratti, 2008)

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    Advantages of EjectorsMechanical Vacuum Pump Ejector

    energyconsumption very high lowmaintenance-cost very high Low(No moving part,

    Easy to operate)heat convection exhaust air affects its

    surrounding of theproduction machines

    no heat convection

    Space-requirement much more space LessEasy to Install

    oil-requirement oil-lubricated, oil separator oil-freeefficency expensive energy high efficency

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    Complete system of an ejector

    5

    6

    1

    4

    2

    3

    1 Compressed fluid

    2 Nozzle3 Suction pipe4 Vacuum connection5 Inlet filter6 Exhaust fluid

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    Diffuser and Nozzle (Subsonic Flow)A diffuser

    converts high speed, low pressure flowto low speed, high pressure flow

    A nozzleconverts high pressure, low speed flow

    to low pressure, high speed flow

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    Total energy of High-speed flow

    Common Assumptions No work or heat transfer

    Neglect changes in pe

    Energy Balance: Crossing out terms assumed 0

    2 2

    C CIN OUTIN OUT

    h h2

    h ke h kg 2g

    e

    v v

    INq

    0

    INw

    0

    h ke pe 0

    IN

    OUTq0

    OUTw0

    h ke pe 0OUT

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    Basic design of an ejector

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    Mathematical model The main steps used to establish mathematical

    modelsA. assumption proposalB. deriving the governing equations

    C. providing auxiliary relation to close the governingequations

    D. adopting proper mathematic approach to solve themodel

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    A: Assumption proposal1. The inner wall of the ejector is adiabatic.2. The flow inside the ejector is steady and isentropic.3. The primary fluid and secondary fluid are supplied to

    the ejector at zero velocity.4. The velocity at the ejectoroutlet is neglected.5. The two fluids begin to mix with a uniform pressure

    at the mixing section.

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    B: Governing equations

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    C: Auxiliary relation1. Boundary conditions:

    pressures at inlet and exit of the ejector.

    the mass flow rates or the velocities of the primary andsecondary fluids

    2. Initial conditions: expansion ratio entrainment ratio

    cross section area of the constant-area throat tube Auxiliary relations:

    Definition of Mach number

    Definition of sonic velocity

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    C: Auxiliary relation (Cont.)

    3. Auxiliary relations: Based on isentropic assumption, the following gas

    dynamic equations are frequently used in thethermodynamic models:

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    C: Auxiliary relation (Cont.)

    3. Auxiliary relations: (Cont.)

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    D: Mathematical Model

    Thermodynamicmodel

    Single-phase flow

    model

    Constant-pressure

    mixing model

    Keenan and Neumann (1942)

    Munday and Bagster (1977)

    Eames et al.(1995)

    Constant-area

    mixing model

    Keenan and Neumann (1942)

    Grazzini and Mariani (1998)

    Yapici and Ersoy (2005)

    Two-phaseflow model

    Sherif et al. (2000)Beithou and Aybar (2000)

    Empirical/semi-empirical

    model

    Huang et al. (1999)Cizungu et al. (2005)Balamurugan et al. (2007)Dessouky et al. (2002)

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    Thermodynamic model the model based on thermodynamic analysis is the simplest

    solve the equations in one dimension

    the isentropic relations and some gas dynamic equations are used to assist in the description of the relationship between

    the temperature pressure enthalpy Mach number velocity

    Single-phase flow assume that the inlet fluid is superheated and no phase change occurring in the ejector.

    Two-phase flow ejector works as a pump

    using high pressure liquid to entrain gas

    or higher pressure vapor to entrain liquid

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    Thermodynamic modelTwo-phase flow model

    Beithou and Aybar (2000) employed a one-dimensional control volume method to develop a local

    mathematical model

    performance prediction of the steam-driven jet pump.

    applied the conservation of mass and momentum equation as well as theentropy equation As the fluid is uncompressible,

    the Bernoulli equation can be used to calculate the entrained water velocity at thenozzle.

    at the mixing section, the steady-state energy equation was used to calculate thevelocity of the mixture with the assumption of

    adiabatic mixing process no potential energy change.

    Take the head loss into account, the Bernoulli equation was used in thediffuser to find out the pressure and velocity profiles along it.

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    Thermodynamic modelTwo-phase flow model

    section By usingBernoulli equation between the water tank and the exit of thewater nozzleContinuity equation

    WaternozzleMixing

    Diffuser

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    Effect of design and operatingparameter on suction pressure

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    Relationship betweenair (primary) mass flow rate and pressure drop

    (Balamurugan et al. 2006)

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    Relationship between

    water temperature and lowest suction pressure

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    Variation of the air entrainment rate

    with the pressure difference

    between the air entry and the throat exit:

    (Kandakureet al. 2005)

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    Schematic geometry of an ejector

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    Effect of projection ration (LTN/DT) on the rate of entrainment

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    Effect of area ratio ((DS2-DN

    2)/DN2) on the rate of

    entrainment for different values of projection ratios

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    Effect of angle on converging section ()on rate of entrainment

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    Conclusion Effect of design and operating parameter on suction pressure

    Parameter Value of parameter Suction pressureLTN/DT

    ((DS2-DN

    2)/DN2)

    mT

    Optimal valueOptimal valueOptimal value

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    ConclusionSteam ejector Water ejector

    Mostly use forVacuum ejector

    Expensive Cheap

    Design : GEOMETRY