PDF 5.5 Energy Removal From the Core

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    1

    A Look at Nuclear Scienceand Technology

    Larry Foulke

    Module 5.5

    Energy removal from the core

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    Nuclear Engineering Program

    Constraints

    Least Favorable Local Temperatures &

    Coolant Flows Must Be Accommodated Cant Control to Average Parameters

    Must Assess Worst-Case Core Conditions

    Normal Operation Potential Energy Removal Degradation

    Transient & Accident Conditions

    Reactor Energy Removal

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    Nuclear Engineering Program

    Thermal-Hydraulic Analysis

    Consider Global Core Power Distributions

    Fuel and Clad and Coolant Temperatures

    Coolant & Moderator Feedbacks

    Local Element Power Density

    Fuel-Pin Temperature Distribution

    Coolant Flow Conditions

    Establish Operating Limits to Prevent Melting

    Reactor Energy Removal

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    Nuclear Engineering Program

    Power Density Peak-to-Average

    Power-Shaping (Peak-Reduction) Techniques Reflector

    Enrichment Zoning Example: Two Different (Higher/Lower)

    Homogeneous EnrichmentBatches

    Multiple-Batch Fuel Management

    Power Distribution

    Fmax(

    r

    )=

    Pmax(r)

    P(r)=max(r)

    (r)= unitless

    ,want

    itclose

    to

    1.0

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    Calvert Cliffs Assembly Inlet Temp: 560 K (~287 C)

    Pressure: 15 Mpa (~2235 psi)

    Flow Rate: 103.63 kg/s

    50 axial segments of 7 cm

    17,850 Thermal Regions

    Four control rod locations

    One instrument tube (center)

    Image Source: See Note 1

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    6

    Axial Location (cm)

    Temperature(

    K)

    Calvert Cliffs Assembly Axial Temperature Profile (Fuel & Coolant)

    Fuel Centerline Temperature

    Coolant Temperature

    Average Fuel Temperature

    Image Source: See Note 1

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    AxialPosition(cm)

    Tempera

    ture(

    K)

    Calvert Cliffs Assembly Axial Fuel & Coolant Temperature Distributions

    Image Source: See Note 1

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    AxialPosition(cm)

    Tempera

    ture(

    K)

    Calvert Cliffs Assembly Axial Coolant Temperature Distributions

    Image Source: See Note 1

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    Coolant Temperature Rise Factor

    Temperature Parameters

    Heat Flux From Surrounding Pins

    Coolant Heat Capacity Inlet Temperature

    Pressure

    FH

    (r) =temperature rise in channel at r

    temperature rise in core average channel

    Peaking Factors

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    Nuclear Engineering Program

    Reflector Peaking EffectPmaxPmax

    PavePave

    Image Source: See Note 2

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    Nuclear Engineering Program

    Enrichment Zoning Effect

    Same peak, but raised average

    Image Source: See Note 2

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    Nuclear Engineering Program

    Fuel Pin Heat Transport

    We have described the relative powerdistribution on a per fuel pin (or per channel)

    basis in the core; now lets consider localheating within a single fuel pin.

    Lets cover fuel pin heat transport in aqualitative way.

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    Nuclear Engineering Program

    Fuel Pin Temperatures depend upon:

    Fission Source Distribution

    Fuel Pin Heat Transport Properties

    Coolant Heat Sink

    Fuel Pin Geometry

    Fuel Pellet

    Gap

    Cladding Tube

    Coolant

    Fuel Pin Heat Transport

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    Nuclear Engineering Program

    rFOrFcl= 0

    rCI

    rCO

    Fuel Pin Radial Cross Section

    Image Source: See Note 2

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    Nuclear Engineering Program

    Fuel Pin Heat Transport

    Assume that fissions occur uniformly throughout thefuel region, therefore heat is produced uniformly in fuelregion.

    Heat generated in the fuel must pass through all of thefuel element layers before it is absorbed in the coolant.

    Fuel: Conduction (with uniform heat source)

    Gap: Convection

    Clad: Conduction

    Coolant: Convection

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    Nuclear Engineering Program

    200

    300

    400

    500

    600

    700

    800

    0.0 0.2 0.4 0.6 0.8

    Temperature

    ,C

    Fuel Pin Radial Distance, cm

    Fuel

    Gap

    CladCoolant

    PWR Fuel-Pin Temperature Profile

    Image Source: See Note 3

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    Nuclear Engineering Program

    Nuclear Limits

    We want to set operating limits so thatthe maximum centerline fuel temperature

    at the hottest axial position of the hottestfuel rod remains below the fuel meltingtemperature.

    17

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    Nuclear Engineering Program

    Departure from Nucleate Boiling (DNB)PWR BWR

    Image Source: See Note 2

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    Nuclear Engineering Program

    Reactor Control

    Maximum Hot-Spot

    Normal Operation Anticipated Transients

    Reactivity Control

    Control Rods

    Insertion Increases Peaking

    Radial

    Axial

    Feedbacks

    Design Considerations

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    Nuclear Engineering Program

    Axial

    Flux w/

    ControlRods

    Image Source: See Note 2

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    Nuclear Engineering Program

    Radial Flux w/ Control Rods

    Image Source: See Note 2

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    1. Reprinted with permission from David Griesheimer, DF Gill, J WLane, DL Aumiller, An Integrated Thermal Hydraulic FeedbackMethod for Monte Carlo Reactor Calculations, Presented at theInternational Conference on the Physics of Reactors (PHYSOR

    2010).2. Adapted and reprinted with permission from the American

    Nuclear Society. Nuclear Engineering Theory and Technologyof Commercial Nuclear Powerby Ronald Allen Knief, 2ndEdition. Copyright 2008 by the American Nuclear Society, La

    Grange Park, Illinois. Figure 7-1 (slide 10), 7-2 (slide 11), 7-3(slide 14), 7-7 (slide 18), 7-9 (slide 20), and 7-10 (slide 21).

    3. Reprinted with permission from Ron Knief.

    Image Source Notes