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    2011 General AssemblyMumbai, India

    Implementation of FF in KGD6

    Harvindar Gambhir/MadhuriAllika

    Vice President/Manager

    Reliance

    Place Company

    Logo Here

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation2

    KGD6-General informationOnshore Gas Plant and Offshore Platform.

    Distance between them is 25KM.Master Control system used for Well Controls.

    FF technology for Control.

    IS design

    Total no of DCS/ECS controllers: 68, distributed

    over 12 buildings

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation3

    Integrated Control system block Diagram

    SUBSEA CONTROL CENTRE HOOFFSHORE PLATFORM

    Data Transfer to HO(via Fibre)

    CENTRAL CONTROL ROOM (CCR)Distributed Control System (DCS)

    Emergency Shutdown System (ESD)

    Sub-sea Control System(SCS)

    Fire & Gas Detection (F&G)CCTV System

    M05M0

    9

    M07

    M06

    M04

    M03

    Safety Guarding System(ESD, F&G CCTV)

    BACKUP CONTROL ROOM

    BACK-UPCOMMUNICATION

    (MICROWAVE )

    FIBRE OPTIC LINK

    SCADA for pipeline

    Emergency Shutdown System (ESD)Fire & Gas Detection (F&G), CCTVSystem

    F I B R E

    OP T I C L I N K

    R E D

    U N D A N T

    ON SHORE TERMINAL

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation4

    IO CountSystem Conventional

    (including HART)FF Serial

    DCS 7500 1300 135000

    ESD 3600

    FGS 1200

    220 FF Segments

    250 Cabinets (including System, Marshalling,

    Server, Network and PDB cabinets)

    Few critical control loops taken on HART

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation6

    FF General ChallengesDURING DESIGN PHASE

    Grouping of devices --Quantity of Devices,Location of devices, loop criticalityCritical Valves

    H-1 RedundancyMacro cycle Execution TimePower ConsumptionSegment Length

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    1994 2011 Fieldbus Foundation8

    SolutionUpfront collaboration of design with Consultantand System vendor to avoid design problems.

    DCS supports EDDL (Electronic Device

    Description language) & FDT (Field device

    Tool). So field devices --vendor independent.

    Used High Power Trunk concept.

    4 H1 segments per interface Card, so reduced

    cabinet foot print.

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation9

    SolutionUsed DCS Vendor interoperability test lab in US

    and Mumbai for upfront device type testing and

    creation of templates.

    Training for all Project, O&M personnel.

    Used Advance Diagnostic module

    One Team of RIL(Project, Constr, Maintenance)

    & DCS vendor during implementation.

    Audits

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation10

    Design Pre-requisitesP&IDs

    Plot Plan, 3D model

    Area Classification

    Foundation Field bus Specification (ProjectSpecific)

    List of Critical Control LoopsControl Narratives (process control strategy)

    I/O Lists

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation11

    Segment DesignSegment length (Total of the trunk and all the spurs)

    Device Assignments to Segments

    Critical Loops : Use of redundant H1 interface cards &

    power supplies.

    Primary and Backup LAS

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation12

    When a control loop has multiple inputs, all the input

    devices shall be on the same segment.This shall also apply to Cascade loops where the

    master/slave shall reside on the same segment.Transmitters on duty/standby pumps, assigned to two

    different segments.

    Segment Design

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation13

    The voltage at each device should not be less than

    13 VDC. The minimum for any device to operate is 9

    VDC. The additional 4 vdc provides for segment

    growth.

    Make sure the total current draw for all devices on

    the segment is well within the capacity of the

    segment power supply about 350 mA.

    Segment Design

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation15

    KGD6 Design Features

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    1994 2011 Fieldbus Foundation16

    KGD6 Design Features

    Maximum of 12 devices per segment.

    Maximum 3 Control Valves per segment.

    However installed 2 control valves in mostof the segments

    Macro cycle for all the segments is

    maintained at less than 1200 msec

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation17

    KGD6 Design FeaturesOnly 1 Fieldbus device per spur

    Max segment(trunk + all spurs) length - 1600 m

    Spur length - 90 m

    All FF devices are Entity compliant

    No Repeators

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    1994 2011 Fieldbus Foundation18

    The method of protection is a high power trunk Hybridconcept. This method uses Increased Safety (Ex e)

    protection for the Field bus Trunk.

    IS spurs by using field mounted 4 channel Field Barriers.

    This implementation allows full access to the field devices

    when they are energized inside the hazardous area.

    The spurs are galvanically isolated from the trunk and from

    each other, have spur surge protection.

    KGD6 - Design Features

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation19

    KGD6 - Design FeaturesDCS system in KGD6 is I/A system.

    Segment Allocation carried out by Engineering

    Consultant and approved by RIL

    Segment macro-cycle validation carried out by DCS

    vendor and approved by RIL

    Control functionality in DCS, not in field.

    Primary FBM 228 module is acting as a link activescheduler; secondary FBM 228 module as back up LAS

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    1994 2011 Fieldbus Foundation20

    MacroCycle Calculation Tool

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    1994 2011 Fieldbus Foundation22

    FF JB

    It may be installed in a Zone 1 T4 IIC hazardous area.

    12 intrinsically safe spurs. EEx ia IIC spur connections. Bus powered

    Fieldbus barrier modules replaceable under power in Zone1 hazardous area

    EEx e trunk wiring connection

    Integrated fixed fieldbus terminator

    Compatible with Entity and FISCO field devices

    Spur surge protection provided for extra safety

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    1994 2011 Fieldbus Foundation23

    Spur

    Trunk

    FCP270

    FBM228

    FF Segment Interconnection

    ADM

    23

    I-JB

    FP32 SurgeProtectors

    FCS-835112-way JB

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    1994 2011 Fieldbus Foundation25

    ADM (Advanced Diagnostic Module)

    809FMTL --for physical layer diagnostics

    Installed on the base plate and providesdiagnostics of 8 segment.

    Diagnostic information of FF devices is also

    available in Asset Management System

    through Block error parameter

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    1994 2011 Fieldbus Foundation26

    5-pair or 10-pair overall and individually shielded

    Trunk cables from system cabinets to intermediate junction boxes located within the various plant areas

    Single pair cable run between the Intermediate FFJ-Box and the FF Spur J-Box and to the devices

    Cables and Grounding

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    1994 2011 Fieldbus Foundation27

    Earthing Arrangement

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    Shield are cut and taped to avoid any possibility of inadvertentgrounding at the device end

    Safety (case) ground of FF devices, Intermediate FF Junction

    Boxes and FF Spur Junction Boxes are made at each

    component.

    Cables and Grounding

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    2011 General AssemblyMumbai, India

    1994 2011 Fieldbus Foundation29

    Interoperability-Field DevicesDevices shall have a Check mark logo which signifies

    that the device is approved by Foundation Field bus

    Device shall be certified as passing the ITK 4.61 or

    later

    Latest version of DD (Device Description), CFF

    (Common File format) files shall be provided by the

    Seller.

    Hand Held Communicator shall be upgraded at

    regular intervals

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    1994 2011 Fieldbus Foundation30

    Interoperability-DCSEnsure DCS supplier with the FF solution have

    been tested extensively

    The Field bus Foundation does not give a tick

    marking(Logo) for host systems.

    Host Interoperability Support Test in accordance

    with FF-569.

    DCS FAT included verification of interoperability of

    the HOST system with each type of FF Device

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    1994 2011 Fieldbus Foundation31

    Devices tested in FAT for InteroperabilitySr. No. Supplier Description Model

    1 Emerson Radar Level Transmitter 5402AF

    2 Emerson Radar Level Transmitter 5301FA

    3 Emerson Radar Level Transmitter 5402AH

    4 Emerson Radar Level Transmitter 5301HA

    5 Emerson Pressure & DP Transmitter 3051S

    6 Emerson Pressure & DP Transmitter 3051CD

    7 Emerson Temperature Transmitter 644HF

    8 Emerson Temperature Transmitter 3144PD

    9 Emerson Coriolis Mass Flow meter 2700R

    10 Emerson Vortex Flow meter 8800DF

    11 Emerson pH Transmitter XMT-P-FF-10-73

    12 Emerson FF Valve Positioner DVC 6000f13 K- Patents MEG Analyzers IT-RM-GP

    14 Chemtrols O2 Analyzers 3020T-H

    15 GE Sensing Ultrasonic Flowmeters GF868

    16 GE Sensing Ultrasonic Flowmeters XMT868

    17 Dresser Valves Displacer type Level Transmitter 12322-058

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    1994 2011 Fieldbus Foundation32

    Device Installation and CommissioningWhat we used to test, calibrate and configure?

    HART 375- Used for Addressing, tagging &

    Configuration of FF devices

    MTL Relcom FBT 6- Used for segment parameters

    and diagnostics

    Beamex MC5: For Calibration, tagging , Addressing

    and configuration

    32

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    Installation Practices

    Some contents and photographs in

    this section are from variousaudits conducted at KGD6 site.

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    Installation Practices

    Bring the inner jacket through the cable gland into the JB. This is to make sure

    the overall shield and any individual pair shield do not accidentally make contact

    with the gland and the JB ground

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    1994 2011 Fieldbus Foundation35

    Cable Termination in FF cabinet

    Inside jacket removed close to the

    termination points such that the min. am t. of

    individual pair shield is exposed.

    At the point where the jacket is

    Removed, place a 2 heat shrinksection over the area to maintain integrity

    and label the cable.

    4 of the 5 Pair terminate at the FP32 Surge protectors. The extra Pair terminates to the

    standalone Grounded terminations below the FP32s. Overall shield terminates to the

    standalone Grounded terminations

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    Mumbai, India

    1994 2011 Fieldbus Foundation36

    Cable Termination in FF cabinetEnsure that the shields

    of individual pairs are

    maintained.

    Place sleeve over eachindividual pair shield drain wire

    and the overall drain wire

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    1994 2011 Fieldbus Foundation38

    Installation Practices

    The shield drain wire must be cut back to

    the shield foil and isolated under heat

    shrink so it does not touch the instrument

    case.

    Cut the signal lines as short as possible to

    make the instrument connection. Spare

    wire has the possibility of getting caught in

    the threads and cutting the insulation thus

    shorting out the signal to the case.

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    1994 2011 Fieldbus Foundation39

    Lessons Learnt

    Take care of grounding

    Avoid sharp bends as same can distort the

    shield and also may cause shorts.

    Do not untwist the Twisted pair cable

    Do not loop the FF wiring in the tray and in

    cabinets

    Turn off the barrier Terminators

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    Mumbai, India

    1994 2011 Fieldbus Foundation40

    Lessons LearntEnsure that device addresses are unique and

    between 18 and 247

    To reduce Commissioning time each FF device

    shall be pre-configured by the Device seller with

    Device tag and Channel address setting.

    While removing a live FF device formaintenance, take the device in OOS mode (Out

    of Service mode) and then remove the device

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    Mumbai, India

    1994 2011 Fieldbus Foundation41

    Dedicated specifications for FF implementation &FF cables

    Ensure all field devices procured are type tested

    Ensure all devices with FF check markTraining on installation and maintenance by experts

    Ensure proper cable laying and terminations

    Criticality study/Control risk assessment

    Audit by FF expert, by experts within the company and by

    DCS vendor experts. Implementation of audit points

    Macro cycle verification

    Snap shots of all segments for record ADM report

    Summary -Implementation steps KGD6

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    Consider using control in the field for non-critical loops.

    As long as the segment retains power (and one device

    has backup LAS), automatic control can be maintained

    in the field devices.

    Non-Redundant FF H1 cards can be used on all non-

    critical segments; however a spare slot shall be left

    adjacent to each H1 card to allow for redundant card inthe future if required.

    Future suggestions

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    Thank You

    This presentation is dedicated tothe team comprising of :

    RIL, Vendors, Consultants &Contractors

    who made it happen