173623205-steam-turbine-ppt (1).pdf

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    STEAM TURBINE

    Dr. K.C. Yadav, Head,

    Training & Development

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    Learning Agenda Expansion of steam and work done

    Description of the nozzle angles (α), blade angles (β) andsurface roughness (µ) and their impact on turbine

    performance Velocity vector diagrams and estimation of turbine stage

    output and efficiency

    Purpose, principle, classification, construction andfunctioning of steam turbine

    Physical significance of turbo-supervisory parameters

    Performance of steam turbine

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    Purpose of Steam Turbine

    Steam turbine is prime-mover for electric power generation,

    which converts heat energy of steam to mechanical energy

    of Steam Turbine Rotor.

    This mechanical energy is utilized to spin rotor (magnet) of 

    the electricity generator to produce electric power.

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    Steam Expansion Steam expands, whenever it is subjected either to lower  

    pressure or to a higher temperature.

    It is considered to be free expansion when the expanding

    boundary is free from any resistance from the surrounding.Though the free expansion has no engineering application but

    it provides enough guidelines to the designers of steam

    turbines/engine to properly deal with steam operating

    parameter to avoid any possibility of free expansion.

    Expanding steam (thermodynamic System) does work onsurrounding irrespective of its being a solid, liquid or gas

    separated by well defined boundary.

    Expansion of steam in turbine is facilitated to do work on

    turbine blades mounted on the freely rotating shaft.

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    Principle of Steam TurbineWhen steam is allowed to expand through anozzle, then its heat is converted to kinetic energy

    of steam itself, which in turn converts into kineticenergy (mechanical energy) of Turbine Rotor  through the impact (impulse) or in an other way,when it expands through Turbine Rotor Blades

    without any change in its velocity then its heat isconverted directly in to kinetic energy (mechanicalenergy) of Turbine Rotor through reaction of  steam expansion against the blades.

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    Types of Steam Turbine Impulse Turbine (DR = 0)

    Reaction Turbine (DR = 1)

    Impulse - Reaction Turbine (DR > 0 &

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    Impulse Turbine Velocity compounded

    Pressure compounded

    Pressure - Velocity compounded

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    Reaction TurbineExpanding steam has to be accommodated in moving

    blades without any change in velocity by suitably

    increasing the space in the blade down stream, which isvery difficult and hence no steam turbine is constructed to

    be pure reaction turbine.

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    Impulse - Reaction TurbineExpanding steam does work on surrounding blade

    surface by virtue of its volume change and at the same

    time incremental velocity of steam stream also doessignificant work on moving blades by impaction.

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    Turbine Blade

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    Vector Diagram

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    Multistage Turbine Blade Arrangement

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    Multistage Turbine Blade Arrangement

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    3

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    Stationary Diaphragm

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    Components of Steam Turbine Foundation (TG & Pillar)

    Base plate / sole plate

    Bearing pedestal / pedestal plate

    CasingSingle / double (Inner or outer casing) / Triple casing

    Barrel type or axially spilt (bottom or top flange)

    Body liners and stationary diaphragm

    Rotor 

    Inbuilt (solid), key & shrunk fit and welded

    Moving diaphragm

    Studs and nuts

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    Components of Steam Turbine HP, IP & LP turbine.

    Bearings.

    Shaft sealing .

    Stop & control valves.

    Turbine control system.

    Turbine monitoring system.

    Turbine oil system.

    Turbine turning gear 

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    TG Foundation

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    *

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    IP Cylinder of a

    500 MW Unit

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    Barrel Type HP Turbine

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    Hydraulic Turning Gear The function of the hydraulic turning gear is

    to rotate the shaft system at sufficient speed

    before start-up and after shutdown in order to avoid irregular heating up or cooling down

    and also to avoid any distortion of the

    turbine rotors. The hydraulic turning gear is

    situated at the front end of the HP turbinefront bearing pedestal.

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    Hydraulic Turning Gear 

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    Mechanical Barring Gear The turbo- generator is equipped with a

    mechanical barring gear, which enables

    the combined shaft system to be

    rotated manually in the event of a

    failure of the normal hydraulic turning

    gear. It is located at IP-LP pedestal(Brg No-3).

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    Mechanical Barring Gear 

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    Low Pressure TurbineOuter casing ,upper half 

    Outer shel l , upper hal f Inner shel l , upper hal f  

    Inner shell, lower half Outer shell, lower half 

    Outer casing, lower half 

    STEAM FLOW

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    Fixed Points of a 250 MW Turbine

    Casing Expansion:

    HP Turbine outer Casing expands towards frontPedestal.

    IP Turbine Casing expands towards Generator side. LP Turbine outer casing expands towards both ends

    from center.

    Rotor Expansion:

    HP Rotor towards front Bearing.

    IP Rotor towards Generator side.

    LPT Rotor towards Generator.

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    Casing ExpansionThe bearing pedestals are anchored to the foundation bymeans of anchor bolts and are fixed in position. The HP

    and IP turbines rest with their lateral support horns on the

    bearing pedestals at the turbine centerline level. The HPand IP casings are connected with the bearing pedestals

    by casing guides which establish the centerline alignment

    of the turbine casings.   The axial position of HP and IP

    casings is fixed at the HP-IP pedestal. Hence, when there

    is a temperature rise, the outer casings of the HP turbineexpand from their fixed points towards Front pedestal.

    Casing of IP Turbine expand from its fixed point towards

    the generator.

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    Casing ExpansionThe LP Turbine outer casing is held in placeaxially, at centre area of longitudinal girder by

    means of fitted keys. Free lateral expansion isallowed. Centering of LP outer casing is providedby guides which run in recesses in the foundationcross beam. Axial movement of the casings isunrestrained. LP Casing expands from its fixed

    point at front end, towards the generator at centrearea of longitudinal girder by means of fittedkeys. Free lateral expansion is allowed.

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    Rotor ExpansionThe thrust bearing is housed in the rear bearing pedestal

    of the HP turbine. The HP turbine rotor expands from the

    thrust bearing towards the front bearing pedestal of theHP turbine and the IP turbine rotor from the thrust bearing

    towards the generator. The LP turbine rotor is displaced

    towards the generator by the expansion of the shaft

    assembly, originating from the thrust bearing.

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    Turbo Supervisory Parameters

    Over all expansion

     Axial shift

    Differential expansion

    Eccentricity

    Vibration

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    Performance of Steam Turbine THR = [(Qms*Hms – Qfw*hfw) + Qrh*(Hhrh – Hcrh)]/P

    P = PGen.Ter. – (Pexc + Pmin)

    ηta = 3600/THR = ηt*ηg*ηc

    ηt = Wt/Hise

    ηg = MW/Wt

    ηc = Hise /[(Qms*Hms – Qfw*hfw) + Qrh*(Hhrh – Hcrh)] or 

    ηc = [Qms*(Hms –Hcrh)+Qrh*(Hhrh – Hexh)–Sum(qb*Hb)] /[(Qms*Hms –Qfw*hfw)+Qrh*(Hhrh –Hcrh)]

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    Enthalpy Drop Across the TurbineHPT

    Qms*(Hms-H7) + (Qms-q7)*(H7-Hcrh)

    IPT

    + Qrh*(Hhrh-H5) + (Qrh-q5-qd)*(H5-H4)+ (Qrh-q4-q5-qd)*(H4-H3)

    + (Qrh-q3-q4-q5-qd)*(H3-H2)

    LPT

    + (Qrh-q2-q3-q4-q5-qd)*(H2-H1)+ (Qrh-q1-q2-q3-q4-q5-qd)*(H1-Hexh)

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    Velocity Vector Diagram forPure Impulse Turbine

    β1α1 β2α2

    β1α1

    β2

    α2

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    Blade Performance of Pure Impulse Turbine

    Wo = C2 Cos α2 (clockwise tangential component)

    Wi = C1 Cos α1 (anticlockwise tangential component)

    R2 < R1 & R2 = µ*R1

    For smooth surface µ = 1 & R2 = R1

    P = [Wi - (-Wo)]*u = [C2 Cos α2 + C1 Cos α1]*u

    C2 Cos α2 = R2 Cos β2 –u = R1 Cos β1 –u

    or C2 Cos α2 = C1 Cos α1 - u – u = C1 Cos α1 – 2u

    P = [C1 Cos α1 + C1 Cos α1 – 2u]*u = 2*u*[C1 Cos α1 – u]

    ηb = 2*P/C1**2 = 4*[(u/C1)*Cos α1 – (u/C1)**2]

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    Velocity VectorDiagram for Impulse-

    Reaction Turbine

    β1α1   β2α2

    β1 α1

    β2α2

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    Work Done in Imp-Reaction Steam Turbine

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    Deduction of C2 & R1 in terms of R2 & C1

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    Stage Efficiency

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    Internal Losses

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    Thank you