SimulationCore2/Equipments/ChokeControl/ChokeControlMain.i90

# 1 "/home/admin/SimulationCore2/Equipments/ChokeControl/ChokeControlMain.f90"
module ChokeControlMain
    USE CHOKEVARIABLES
    use SimulationVariables !@
    implicit none
    public
    contains
    
! subroutine ChokeControl_Setup()
!     ! use CSimulationVariables
!     implicit none
!     call OnSimulationInitialization%Add(ChokeControl_Init)
!     call OnSimulationStop%Add(ChokeControl_Init)
! call OnChokeControlStep%Add(ChokeControl_Step)
!     call OnChokeControlOutput%Add(ChokeControl_Output)
!     call OnChokeControlMain%Add(ChokeControlMainBody)
! end subroutine
    
    subroutine ChokeControl_Init
        call Choke_StartUp()
    end subroutine ChokeControl_Init
    
    subroutine ChokeControl_Step
        use ChokeModule
        implicit none
        INTEGER CHNUMBER

        IF(data%Equipments%ChokeControlPanel%ChokeSelectorSwitch) THEN
            data%Equipments%ChokeControlPanel%Choke1LED=1
            data%Equipments%ChokeControlPanel%Choke2LED=0
            CHNUMBER=1
        ELSE
            data%Equipments%ChokeControlPanel%Choke2LED=1
            data%Equipments%ChokeControlPanel%Choke1LED=0
            CHNUMBER=2
        ENDIF
        if(ABS(data%Equipments%ChokeControlPanel%ChokeControlLever)==1.0 .AND. data%Equipments%ChokeControlPanel%ChokePanelRigAirSwitch .AND. data%State%CHOOKE(CHNUMBER)%FailMalf==0 .AND. data%State%AirDrivenPump%ChokeAirFail==0) then
            if (data%Equipments%ChokeControlPanel%ChokeControlLever == 1.0) then
                data%State%CHOOKE(CHNUMBER)%ChokeIsClosing = .true.
                data%State%CHOOKE(CHNUMBER)%ChokeIsOpening = .false.
            endif
            if (data%Equipments%ChokeControlPanel%ChokeControlLever == -1.0) then 
                data%State%CHOOKE(CHNUMBER)%ChokeIsOpening = .true.
                data%State%CHOOKE(CHNUMBER)%ChokeIsClosing = .false.
            endif
            data%State%AirPumpLine%TIME=data%State%AirPumpLine%TIME+data%State%AirPumpLine%DeltaT_Choke  !overal time (s)
            call airpump_code_CHOKE(CHNUMBER)
        else
            call CHOKE_MainBody2()
        endif
    end subroutine ChokeControl_Step
    
! subroutine ChokeControl_Output
!     implicit none
! end subroutine ChokeControl_Output
        
!     subroutine ChokeControlMainBody
!         use CRigSizeVariables
!         use CHOKE
!         implicit none

!          CALL Choke_StartUp()
!         loop1: DO
!             CALL CHOKE_MainBody
!             call sleepqq(100)
!             !IF (IsStopped==.true.) THEN
!             !    EXIT loop1
!             !ENDIF
!     !write(*,*) '1111111111111'
!       if(IsStopped) then
! !write(*,*) '22222222222222'
          
!           CALL DEALLOCATE_ARRAYS_CHOKE()
! !write(*,*) '333333333'
          
!           call Quit()
!       end if
            
            

!         ENDDO loop1
        
!         CLOSE(150)
        
!         !CALL DEALLOCATE_ARRAYS_CHOKE()
        
!     end subroutine ChokeControlMainBody
    
    SUBROUTINE Choke_StartUp()
    
        USE CHOKEVARIABLES
        use SimulationVariables
        USE CChokeProblemsVariables
        implicit none 
        
        CALL LOSS_INPUTS_CHOKE()
        
!OPEN(150,FILE='CHOKE_AIRPUMP_OUTPUTS.DAT')
        
        
!data%State%CHOOKE(1)%WashoutMalf=1
!data%State%CHOOKE(1)%PlugMalf=0
!data%State%CHOOKE(1)%FailMalf=0
!
!data%State%CHOOKE(2)%WashoutMalf=1
!data%State%CHOOKE(2)%PlugMalf=0
!data%State%CHOOKE(2)%FailMalf=0
!
!
!ChokeAirFail=0
!
!GaugeChokePositionMailf=0
    
        
        
        
        
        
        
        data%State%Choke%kRatio=1.4
        data%State%Choke%Cp=0.24
        data%State%Choke%CL=0.8
    
        data%State%Choke%x1=0.5  
        
        data%State%Choke%LiquidPPG=9.
        data%State%Choke%LiquidDensity=data%State%Choke%LiquidPPG*7.48 !lbm/ft**3
    
        data%State%Choke%VL=1.0/data%State%Choke%LiquidDensity   !SpecificVolume of Liquid
    
        data%State%Choke%Cv=data%State%Choke%Cp/data%State%Choke%kRatio
    
        data%State%Choke%nPolytripic=1+(data%State%Choke%x1*(data%State%Choke%Cp-data%State%Choke%Cv)/(data%State%Choke%x1*data%State%Choke%Cv+(1-data%State%Choke%x1)*data%State%Choke%CL))
            
        data%State%Choke%VG1=1./0.748    !lbm/ft**3 Specific Volume of Air, Upstream
    
        data%State%Choke%Cdrag=0.8
        data%State%Choke%Pwh=1400. !psi
    
    
        data%State%Choke%Patm=14.7
        data%State%Choke%MixDens2=data%State%Choke%x1*data%State%Choke%VG1 !lbm/ft**3
    
    
    
        data%State%Choke%epsilon_abs= 1e-5
        data%State%Choke%epsilon_step= 1e-5
    
    
!ChokeDiameter= 32/64.  !in
    
        data%State%CHOOKE%PercentClose= 0.0
!AreaChoke=0.01334635
    
! data%State%CHOOKE(1)%AreaChoke=0.01334635
!ChokeAreaFullyOpen = 123.d0 / 64.d0     ! fully open area is 123/64 in^2 = 0.01334635 ft^2
    
        data%State%AirPumpLine%DeltaT_Choke=0.1
!TotalStrokes1=0.
!TotalStrokes2=0.
    
        data%State%Choke%HydraulicChoke1WashoutCoef= 0.0
        data%State%Choke%HydraulicChoke2WashoutCoef= 0.0
    
    
    
        data%State%Choke%ChokePlugTimeDelay = int(180./data%State%AirPumpLine%DeltaT_Choke)       ! =1800 = 180/0.1 : for 3 min delay
    
        data%State%Choke%Present_HydraulicChoke1Plug = REAL(data%problems%ChokeProblems%HydraulicChoke1PluggedPercent)/100.
        data%State%Choke%HydraulicChoke1PluggedPercent_Old= data%problems%ChokeProblems%HydraulicChoke1PluggedPercent
        data%State%Choke%Plug1TimeCounter= 0
        data%State%Choke%DeltaPlug1Percent = 0.0
    
        data%State%Choke%Present_HydraulicChoke2Plug = REAL(data%problems%ChokeProblems%HydraulicChoke2PluggedPercent)/100.
        data%State%Choke%HydraulicChoke2PluggedPercent_Old= data%problems%ChokeProblems%HydraulicChoke2PluggedPercent
        data%State%Choke%Plug2TimeCounter= 0
        data%State%Choke%DeltaPlug2Percent = 0.0
    
!======================AIRPUMP INPUTS(CONSTANTS)===========================
        data%State%AirPumpLine%CourseBase= 24. !cm
        data%State%CHOOKE%PassedCourse= 0.
        data%Equipments%ChokeControlPanel%ChokePosition=0.
    
        data%State%AirPumpLine%Acylinder= PI*(8.**2)/4.        !  (CM^2),  8=DIAMETER,   24=course ,  3785.412: cm^3 to galon
    
    
        data%State%CHOOKE%ChokeIsOpening = .false.
        data%State%CHOOKE%ChokeIsClosing = .false. 
             
             
        data%State%AirPumpLine%P_AIRP=0
    
        data%State%AirDrivenPump%cc1 =  0.1354; data%State%AirDrivenPump%cc2 = -2.066; data%State%AirDrivenPump%cc3 = -21.09; data%State%AirDrivenPump%cc4 = -51.36; data%State%AirDrivenPump%cc5 = 5935           ! FOR OUTPUT IN GPM
! cc1 = 4.754e-07; cc2 = -0.0001676; cc3 = -0.03953; cc4 = -2.223; cc5 = 5935         FOR OUTPUT IN IN^3/MIN
    
    
        data%State%AirPumpLine%Pdownstrem= 4950 !+0.01*Pchoke   (psi)       <<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<
        data%State%AirPumpLine%QITER=5.  !(gpm)
    
! Q=0.0003585; true
        data%State%AirPumpLine%TIME=0
        data%State%AirPumpLine%TOL_AIR=0.05
    
        data%State%AirPumpLine%alpha_Qair=0
        data%State%AirPumpLine%alpha_timeair=0
        data%State%AirPumpLine%alpha_Pdownstrem=data%State%AirPumpLine%Pdownstrem
        data%State%AirPumpLine%alpha_diffpair=0
        data%State%AirPumpLine%alpha_lossesair=0
    
    end

    SUBROUTINE DEALLOCATE_ARRAYS_CHOKE()    
        USE CHOKEVARIABLES
        use SimulationVariables !@
    
        implicit none
        write(*,*) 'deallocateeeeeeeeeeeee'
!===========================================================================
!                   	AIR PUMP LOSSES INPUT
!===========================================================================
!if(allocated(PIPINGS_AIRPUMP)) deallocate(PIPINGS_AIRPUMP)
    
        DEALLOCATE (data%State%AirPumpLine%PIPINGS_AIRPUMP,data%State%AirPumpLine%DIAM_AIR_INCH,  &
            data%State%AirPumpLine%Re_air,data%State%AirPumpLine%AREA_AIR,data%State%AirPumpLine%LENGT_AIR,data%State%AirPumpLine%ROUGHNESS_AIRPLINE,data%State%AirPumpLine%REL_ROUGHAIR,  &
            data%State%AirPumpLine%fric_air,data%State%AirPumpLine%fricloss_air)
!================================================================
        DEALLOCATE (data%State%AirPumpLine%MINORS_AIRPUMP,data%State%AirPumpLine%MINORDIAM_AIR_INCH,  &
            data%State%AirPumpLine%MINORAREA_AIR,data%State%AirPumpLine%LF_AIR,data%State%AirPumpLine%CV_AIR,data%State%AirPumpLine%NOTE_AIR &
            ,data%State%AirPumpLine%minlosspa_air,data%State%AirPumpLine%minloss_air)   
    END
        
        
        
        
        
    SUBROUTINE LOSS_INPUTS_CHOKE()
        USE CHOKEVARIABLES
        use SimulationVariables
        implicit none
        Integer I
    
!===========================================================================
!                   	AIR PUMP LOSSES INPUT
!===========================================================================
        data%State%AirPumpLine%NO_PIPINGS_AIRPLINE=1
    
        ALLOCATE (data%State%AirPumpLine%PIPINGS_AIRPUMP(data%State%AirPumpLine%NO_PIPINGS_AIRPLINE,3))
!			ID(INCH)    L(MM)	  ROUGHNESS(MM)=e   DESCRIPTION
        data%State%AirPumpLine%PIPINGS_AIRPUMP(1,1:3)=		 (/0.5,      60960.,   0.03/)            !Avg.acc.distance
        
!60960= 200 ft
        ALLOCATE(data%State%AirPumpLine%DIAM_AIR_INCH(data%State%AirPumpLine%NO_PIPINGS_AIRPLINE))
        ALLOCATE(data%State%AirPumpLine%Re_air(data%State%AirPumpLine%NO_PIPINGS_AIRPLINE))
    
        ALLOCATE(data%State%AirPumpLine%AREA_AIR(data%State%AirPumpLine%NO_PIPINGS_AIRPLINE))
        ALLOCATE(data%State%AirPumpLine%LENGT_AIR(data%State%AirPumpLine%NO_PIPINGS_AIRPLINE))
        ALLOCATE(data%State%AirPumpLine%ROUGHNESS_AIRPLINE(data%State%AirPumpLine%NO_PIPINGS_AIRPLINE))
        ALLOCATE(data%State%AirPumpLine%REL_ROUGHAIR(data%State%AirPumpLine%NO_PIPINGS_AIRPLINE))
        ALLOCATE(data%State%AirPumpLine%fric_air(data%State%AirPumpLine%NO_PIPINGS_AIRPLINE))
        ALLOCATE(data%State%AirPumpLine%fricloss_air(data%State%AirPumpLine%NO_PIPINGS_AIRPLINE))
    
        DO I=1,data%State%AirPumpLine%NO_PIPINGS_AIRPLINE
            data%State%AirPumpLine%DIAM_AIR_INCH(I)=data%State%AirPumpLine%PIPINGS_AIRPUMP(I,1)
            data%State%AirPumpLine%LENGT_AIR(I)=data%State%AirPumpLine%PIPINGS_AIRPUMP(I,2)
            data%State%AirPumpLine%ROUGHNESS_AIRPLINE(I)=data%State%AirPumpLine%PIPINGS_AIRPUMP(I,3)    
            data%State%AirPumpLine%AREA_AIR(I)=PI*(data%State%AirPumpLine%DIAM_AIR_INCH(I)*0.0254)**2/4   !D(in), AREA(m)
            data%State%AirPumpLine%REL_ROUGHAIR(I)=data%State%AirPumpLine%ROUGHNESS_AIRPLINE(I)/(data%State%AirPumpLine%DIAM_AIR_INCH(I)*25.4)
!DIAM_RAMLINE_MM(I)=DIAM_RAMLINE_MM(I)*.001  !  (m)
            data%State%AirPumpLine%LENGT_AIR(I)=data%State%AirPumpLine%LENGT_AIR(I)*.001      !  (m)
        ENDDO
    
            
!================================================================
        data%State%AirPumpLine%NO_MINORS_AIRPLINE=6
    
        ALLOCATE (data%State%AirPumpLine%MINORS_AIRPUMP(data%State%AirPumpLine%NO_MINORS_AIRPLINE,4))
    
!		ID(INCH)		LF	    CV	NOTE(BAR)      DESCRIPTION
        data%State%AirPumpLine%MINORS_AIRPUMP(1,1:4)=      (/2.,			10.,	0.,	    0./)       !Acc.tee
        data%State%AirPumpLine%MINORS_AIRPUMP(2,1:4)=      (/2.,			11.,	0.,	    0./)       !elbow
        data%State%AirPumpLine%MINORS_AIRPUMP(3,1:4)=      (/1.,			0.,	    0.,	    3.4/)      !filter
        data%State%AirPumpLine%MINORS_AIRPUMP(4,1:4)=      (/2.,			0.,	    105.,	0./)       !valve
        data%State%AirPumpLine%MINORS_AIRPUMP(5,1:4)=      (/1.,			0.,	    9.2,	0./)       !valve
        data%State%AirPumpLine%MINORS_AIRPUMP(6,1:4)=      (/2.,			6.4,	0.,	    0./)       !unionA
    
            
        ALLOCATE (data%State%AirPumpLine%MINORDIAM_AIR_INCH(data%State%AirPumpLine%NO_MINORS_AIRPLINE),data%State%AirPumpLine%MINORAREA_AIR(data%State%AirPumpLine%NO_MINORS_AIRPLINE),  &
                data%State%AirPumpLine%LF_AIR(data%State%AirPumpLine%NO_MINORS_AIRPLINE),data%State%AirPumpLine%CV_AIR(data%State%AirPumpLine%NO_MINORS_AIRPLINE),data%State%AirPumpLine%NOTE_AIR(data%State%AirPumpLine%NO_MINORS_AIRPLINE) &
                ,data%State%AirPumpLine%minlosspa_air(data%State%AirPumpLine%NO_MINORS_AIRPLINE),data%State%AirPumpLine%minloss_air(data%State%AirPumpLine%NO_MINORS_AIRPLINE))
    
        
        DO I=1,data%State%AirPumpLine%NO_MINORS_AIRPLINE
            data%State%AirPumpLine%MINORDIAM_AIR_INCH(I)=data%State%AirPumpLine%MINORS_AIRPUMP(I,1)
            data%State%AirPumpLine%LF_AIR(I)=data%State%AirPumpLine%MINORS_AIRPUMP(I,2)
            data%State%AirPumpLine%CV_AIR(I)=data%State%AirPumpLine%MINORS_AIRPUMP(I,3)
            data%State%AirPumpLine%NOTE_AIR(I)=data%State%AirPumpLine%MINORS_AIRPUMP(I,4)        
            data%State%AirPumpLine%MINORAREA_AIR(I)=PI*(data%State%AirPumpLine%MINORDIAM_AIR_INCH(I)*0.0254)**2/4.   !D(in), AREA(m)
        ENDDO    
         
    END   
        
        
        
    
    
! SUBROUTINE PIPE_RAMS_CHOKE(CHNUMBER)
!     USE CHOKEVARIABLES
! use ConfigurationVariables !@
!     Use CSimulationVariables
!     implicit none
!     INTEGER CHNUMBER
!     Integer I
        
!     loop3: do while (ABS(data%Equipments%ChokeControlPanel%ChokeControlLever)==1.0 .AND. data%Equipments%ChokeControlPanel%ChokePanelRigAirSwitch == 1 .AND. data%State%CHOOKE(CHNUMBER)%FailMalf==0 .AND. data%State%AirDrivenPump%ChokeAirFail==0)
!         if (data%Equipments%ChokeControlPanel%ChokeControlLever == 1.0) then
!             data%State%CHOOKE(CHNUMBER)%ChokeIsClosing = .true.
!             data%State%CHOOKE(CHNUMBER)%ChokeIsOpening = .false.
!         endif
!         if (data%Equipments%ChokeControlPanel%ChokeControlLever == -1.0) then
!             data%State%CHOOKE(CHNUMBER)%ChokeIsOpening = .true.
!             data%State%CHOOKE(CHNUMBER)%ChokeIsClosing = .false.
!         endif
!         data%State%AirPumpLine%TIME=data%State%AirPumpLine%TIME+data%State%AirPumpLine%DeltaT_Choke  !overal time (s)
!         call airpump_code_CHOKE(CHNUMBER)
!         call sleepqq(100)
!         if (IsStopped == .true.) return
!     end do  loop3   !while finished_Choke==0
!     end
        
     
        
        
        
        
    SUBROUTINE airpump_code_CHOKE(CHNUMBER)    
        USE CHOKEVARIABLES
        use SimulationVariables !@
        use CChokeManifold
        use SimulationVariables
        use CSounds
        USE CChokeProblemsVariables
        implicit none
        Integer I

        INTEGER CHNUMBER
    
        data%State%AirDrivenPump%QAIR_PUMP=data%State%AirPumpLine%QITER+.1   !(gpm)  maximum flow for the start
        data%State%AirPumpLine%diffp_air=-10
        data%State%AirPumpLine%losses_air=10
    
!===================================================================
!                       AIR OPERATED PUMP
!                       MODEL 10-6000W030 RATIO 55:1
!=================for air consumption at 100 psig===================
        do while (data%State%AirPumpLine%diffp_air<0)
            data%State%AirDrivenPump%QAIR_PUMP=data%State%AirDrivenPump%QAIR_PUMP-.1
! Qup=data%State%AirDrivenPump%QAIR_PUMP;
!cc1 = 1354; cc2 = -2066; cc3 = -2109; cc4 = -513.6; cc5 = 5935     FOR OUTPUT IN GPM
            data%State%AirPumpLine%P_AIRP=data%State%AirDrivenPump%cc1*(data%State%AirDrivenPump%QAIR_PUMP**4) + data%State%AirDrivenPump%cc2*(data%State%AirDrivenPump%QAIR_PUMP**3) + data%State%AirDrivenPump%cc3*(data%State%AirDrivenPump%QAIR_PUMP**2) + data%State%AirDrivenPump%cc4*data%State%AirDrivenPump%QAIR_PUMP + data%State%AirDrivenPump%cc5 !(psig)
! kinetic_air=sg*wdens*(QAIR_PUMP*6.30902e-5/((1/4.)*pi*(2*0.254e-1)**2))**2/(2*6895) !(psi)
            data%State%AirPumpLine%diffp_air= data%State%AirPumpLine%P_AIRP - data%State%AirPumpLine%Pdownstrem
        end do    !returns Qup
    
        do while (abs((data%State%AirPumpLine%diffp_air-data%State%AirPumpLine%losses_air)/data%State%AirPumpLine%diffp_air)>data%State%AirPumpLine%TOL_AIR) !finding correct QAIR_pump for 1 timecounter_ram
            if (data%State%AirPumpLine%diffp_air-data%State%AirPumpLine%losses_air>0) then
                data%State%AirDrivenPump%QAIR_PUMP=data%State%AirDrivenPump%QAIR_PUMP+.005
            else
                data%State%AirDrivenPump%QAIR_PUMP=data%State%AirDrivenPump%QAIR_PUMP-.005
            endif
!===================================================================
!                       AIR OPERATED PUMP
!                       MODEL 10-6000W030 RATIO 55:1
!=================for air consumption at 100 psig===================
            data%State%AirPumpLine%P_AIRP=data%State%AirDrivenPump%cc1*(data%State%AirDrivenPump%QAIR_PUMP**4) + data%State%AirDrivenPump%cc2*(data%State%AirDrivenPump%QAIR_PUMP**3) + data%State%AirDrivenPump%cc3*(data%State%AirDrivenPump%QAIR_PUMP**2) + data%State%AirDrivenPump%cc4*data%State%AirDrivenPump%QAIR_PUMP + data%State%AirDrivenPump%cc5 !(psig)
!kinetic_air=sg*wdens*(QAIR_PUMP*6.30902e-005/((1/4.)*pi*(2*0.254e-1)**2))**2/(2*6895) !(psi)
            data%State%AirPumpLine%diffp_air= data%State%AirPumpLine%P_AIRP - data%State%AirPumpLine%Pdownstrem
!===========================LOSSES====================================
            do i=1,data%State%AirPumpLine%NO_PIPINGS_AIRPLINE
                data%State%AirPumpLine%Re_air(i)=data%State%AirDrivenPump%QAIR_PUMP*6.30902e-005*data%State%AirPumpLine%DIAM_AIR_INCH(I)*0.0254/(data%State%AirPumpLine%AREA_AIR(i)*nu)
            enddo
            do i=1,data%State%AirPumpLine%NO_PIPINGS_AIRPLINE
                if (data%State%AirPumpLine%Re_air(i)<Re_cr) then
                    data%State%AirPumpLine%fric_air(i)=64/data%State%AirPumpLine%Re_air(i)
                else
                    data%State%AirPumpLine%fric_air(i)=1/(-1.8*log10((data%State%AirPumpLine%REL_ROUGHAIR(i)/3.7)**1.11+6.9/data%State%AirPumpLine%Re_air(i)))**2
                endif
                data%State%AirPumpLine%fricloss_air(i)=((data%State%AirPumpLine%fric_air(i)*(wdens*sg*data%State%AirPumpLine%LENGT_AIR(i)*(data%State%AirDrivenPump%QAIR_PUMP*6.30902e-005/data%State%AirPumpLine%AREA_AIR(i))**2))/(2*data%State%AirPumpLine%DIAM_AIR_INCH(I)*0.0254))/6895
            enddo
    
            data%State%AirPumpLine%pipe_loss1air=sum(data%State%AirPumpLine%fricloss_air)  !loss before regulator(psi)
    
            do i=1,data%State%AirPumpLine%NO_MINORS_AIRPLINE
                if (data%State%AirPumpLine%LF_AIR(i)/=0) then
                    data%State%AirPumpLine%minlosspa_air(i)=data%State%AirPumpLine%LF_AIR(i)*wdens*sg*(data%State%AirDrivenPump%QAIR_PUMP*6.30902e-005/data%State%AirPumpLine%MINORAREA_AIR(i))**2/2  !(Pa)
                    data%State%AirPumpLine%minloss_air(i)=data%State%AirPumpLine%minlosspa_air(i)/6895 !(psi)
                elseif (data%State%AirPumpLine%CV_AIR(i)/=0) then
                    data%State%AirPumpLine%minlosspa_air(i)=1000*sg*((11.7*data%State%AirDrivenPump%QAIR_PUMP*6.30902e-005*3600)/(data%State%AirPumpLine%CV_AIR(i)))**2 !(pa)
                    data%State%AirPumpLine%minloss_air(i)=data%State%AirPumpLine%minlosspa_air(i)/6895 !(psi)
                else
                    data%State%AirPumpLine%minlosspa_air(i)=data%State%AirPumpLine%NOTE_AIR(i)*1e5 !(pa)
                    data%State%AirPumpLine%minloss_air(i)=data%State%AirPumpLine%minlosspa_air(i)/6895 !(psi)
                endif
            enddo
    
            data%State%AirPumpLine%minor_loss1air=sum(data%State%AirPumpLine%minloss_air)  !loss before regulator(psi)
            data%State%AirPumpLine%static_loss1air=0
            data%State%AirPumpLine%losses_air=data%State%AirPumpLine%pipe_loss1air+data%State%AirPumpLine%minor_loss1air+data%State%AirPumpLine%static_loss1air !(psi)
!=========================================================================
        end do  !returns correct QAIR_PUMP for 1 counter
    
        data%State%AirPumpLine%QITER=data%State%AirDrivenPump%QAIR_PUMP
        data%State%AirDrivenPump%QAIR_PUMP=data%State%AirDrivenPump%QAIR_PUMP*(data%Equipments%ChokeControlPanel%ChokeRateControlKnob/10.)       ! final Q (gpm)
        data%State%Choke%Cumulative_AirVolume_Choke= data%State%Choke%Cumulative_AirVolume_Choke + ((data%State%AirDrivenPump%QAIR_PUMP * data%State%AirPumpLine%DeltaT_Choke / 60.0 ) / (1.5*0.004329004) )        ! =strokes
        
        if ( data%State%Choke%Cumulative_AirVolume_Choke > 1.0 ) then
            data%State%Choke%SoundChokePump= 60
            data%State%Choke%Cumulative_AirVolume_Choke= data%State%Choke%Cumulative_AirVolume_Choke - 1.0
        else
            data%State%Choke%SoundChokePump= 0.0
        endif   
        data%State%AirPumpLine%DELTAV_AIR=data%State%AirDrivenPump%QAIR_PUMP*data%State%AirPumpLine%DeltaT_Choke/60  !(galon) delta_t=1sec , Q(gpm)
        if (data%State%CHOOKE(CHNUMBER)%ChokeIsClosing)  data%State%CHOOKE(CHNUMBER)%PassedCourse=data%State%CHOOKE(CHNUMBER)%PassedCourse + (data%State%AirPumpLine%DELTAV_AIR*3785.412/data%State%AirPumpLine%Acylinder)!*(ChokeRateControlKnob/10.)        ! 3785.412 : GALON TO CM^3
        if (data%State%CHOOKE(CHNUMBER)%ChokeIsOpening)  data%State%CHOOKE(CHNUMBER)%PassedCourse=data%State%CHOOKE(CHNUMBER)%PassedCourse - (data%State%AirPumpLine%DELTAV_AIR*3785.412/data%State%AirPumpLine%Acylinder)!*(ChokeRateControlKnob/10.)
!DeltaT_Choke= 1sec or 2sec
!((((((((IN OUTER LOOP))))))
!===============AIR PUMP OUTPUTS=========================
        data%State%AirPumpLine%alpha_timeair=data%State%AirPumpLine%TIME  ! overal time (s)
        data%State%AirPumpLine%alpha_Pdownstrem=data%State%AirPumpLine%Pdownstrem
        data%State%AirPumpLine%alpha_pairp=data%State%AirPumpLine%P_AIRP
        data%State%AirPumpLine%alpha_Qair=data%State%AirDrivenPump%QAIR_PUMP
!write(*,*) 'diffp_air=',diffp_air
!pause
        data%State%AirPumpLine%alpha_diffpair=data%State%AirPumpLine%diffp_air
        data%State%AirPumpLine%alpha_lossesair=data%State%AirPumpLine%losses_air
!========================================================
!OPEN(150,FILE='CHOKE_AIRPUMP_OUTPUTS.DAT')
    
        if (data%State%CHOOKE(CHNUMBER)%ChokeIsClosing .AND. data%State%CHOOKE(CHNUMBER)%PassedCourse>data%State%AirPumpLine%CourseBase) then
            data%State%CHOOKE(CHNUMBER)%PassedCourse=data%State%AirPumpLine%CourseBase
            data%State%Choke%SoundChokePump= 0.0
        endif
        if (data%State%CHOOKE(CHNUMBER)%ChokeIsOpening .AND. data%State%CHOOKE(CHNUMBER)%PassedCourse<0.) then
            data%State%CHOOKE(CHNUMBER)%PassedCourse=0.
            data%State%Choke%SoundChokePump= 0.0
        endif
        
        call SetSoundChokePump(data%State%Choke%SoundChokePump)
        data%State%CHOOKE(CHNUMBER)%PercentClose= data%State%CHOOKE(CHNUMBER)%PassedCourse/data%State%AirPumpLine%CourseBase
        IF (data%Equipments%ChokeControlPanel%Choke1LED==1) THEN
            data%Equipments%ChokeControlPanel%ChokePosition= (1 - data%State%Choke%GaugeChokePositionMailf) * data%State%CHOOKE(1)%PercentClose*10
        ELSE       ! Choke2LED==1
            data%Equipments%ChokeControlPanel%ChokePosition= (1 - data%State%Choke%GaugeChokePositionMailf) * data%State%CHOOKE(2)%PercentClose*10
        ENDIF
!CALL SetHydraulicChock1(nint(MIN(data%State%CHOOKE(1)%PercentClose / 0.91 , 1.0)*100))
! CALL SetHydraulicChock2(nint(MIN(data%State%CHOOKE(2)%PercentClose / 0.91 , 1.0)*100))
! .91 >> 9 percent clearance
    
! =================== calculating Area
! AreaChoke=0.5
! .91 >> 9 percent clearance
    
        data%State%CHOOKE(1)%AreaChoke=0.01334635-(0.01334635* MIN(data%State%CHOOKE(1)%PercentClose / 0.91 , 1.0)) !ft^2     0.01334635 is ChokeAreaFullyOpen (ft^2)
        data%State%CHOOKE(2)%AreaChoke=0.01334635-(0.01334635* MIN(data%State%CHOOKE(2)%PercentClose/ 0.91 , 1.0)) !ft^2
        data%State%Choke%HydraulicChoke1WashoutCoef= data%State%Choke%HydraulicChoke1WashoutCoef * data%State%CHOOKE(1)%WashoutMalf    
        data%State%Choke%HydraulicChoke1WashoutCoef= MIN( 0.5 , data%State%Choke%HydraulicChoke1WashoutCoef+ data%State%CHOOKE(1)%WashoutMalf*(0.5/(60.0/data%State%AirPumpLine%DeltaT_Choke)) ) ! 0.5=maximum washout coef , 60.0 sec= 1min duration time
        data%State%Choke%HydraulicChoke2WashoutCoef= data%State%Choke%HydraulicChoke2WashoutCoef * data%State%CHOOKE(2)%WashoutMalf    
        data%State%Choke%HydraulicChoke2WashoutCoef= MIN( 0.5 , data%State%Choke%HydraulicChoke2WashoutCoef+ data%State%CHOOKE(2)%WashoutMalf*(0.5/(60.0/data%State%AirPumpLine%DeltaT_Choke)) ) ! 0.5=maximum washout coef , 60.0 sec= 1min duration time
!write(*,*) 'HydraulicChoke1WashoutCoef=' , HydraulicChoke1WashoutCoef
        
        IF (data%State%CHOOKE(1)%PlugMalf == 1) THEN
            data%State%Choke%Present_HydraulicChoke1Plug= data%State%Choke%Present_HydraulicChoke1Plug * data%State%CHOOKE(1)%PlugMalf 
! integer: HydraulicChoke1PluggedPercent,HydraulicChoke1PluggedPercent_Old,PlugTimeCounter,ChokePlugTimeDelay
! real: Present_HydraulicChoke1Plug,DeltaPlug1Percent
!write(*,*) 'HydraulicChoke1PluggedPercent=' , HydraulicChoke1PluggedPercent
    
            if ( (data%problems%ChokeProblems%HydraulicChoke1PluggedPercent - data%State%Choke%HydraulicChoke1PluggedPercent_Old) /= 0) then
                data%State%Choke%DeltaPlug1Percent = (REAL(data%problems%ChokeProblems%HydraulicChoke1PluggedPercent)/100.) - data%State%Choke%Present_HydraulicChoke1Plug
                data%State%Choke%Plug1TimeCounter = 0
!write(*,*) 'DeltaPlug1Percent, Present_HydraulicChoke1Plug  =  ' ,DeltaPlug1Percent , Present_HydraulicChoke1Plug
            endif
            data%State%Choke%Plug1TimeCounter= data%State%Choke%Plug1TimeCounter + 1
            data%State%Choke%HydraulicChoke1PluggedPercent_Old= data%problems%ChokeProblems%HydraulicChoke1PluggedPercent
    
            if (data%State%Choke%Plug1TimeCounter <= data%State%Choke%ChokePlugTimeDelay) then    !ChokePlugTimeDelay=600
                data%State%Choke%Present_HydraulicChoke1Plug = data%State%Choke%Present_HydraulicChoke1Plug + data%State%CHOOKE(1)%PlugMalf* ((data%State%Choke%DeltaPlug1Percent / real(data%State%Choke%ChokePlugTimeDelay)))     ! real(ChokePlugTimeDelay)= 600.0
            endif
!write(*,*) 'Present_HydraulicChoke1Plug=' , Present_HydraulicChoke1Plug
        ENDIF
    
        IF (data%State%CHOOKE(2)%PlugMalf == 1) THEN 
            data%State%Choke%Present_HydraulicChoke2Plug= data%State%Choke%Present_HydraulicChoke2Plug * data%State%CHOOKE(2)%PlugMalf 
! integer: HydraulicChoke2PluggedPercent,HydraulicChoke2PluggedPercent_Old,PlugTimeCounter,ChokePlugTimeDelay
! real: Present_HydraulicChoke2Plug,DeltaPlug2Percent
            if ( (data%problems%ChokeProblems%HydraulicChoke2PluggedPercent - data%State%Choke%HydraulicChoke2PluggedPercent_Old) /= 0 ) then
                data%State%Choke%DeltaPlug2Percent = (REAL(data%problems%ChokeProblems%HydraulicChoke2PluggedPercent)/100.) - data%State%Choke%Present_HydraulicChoke2Plug
                data%State%Choke%Plug2TimeCounter = 0
            endif
            data%State%Choke%Plug2TimeCounter= data%State%Choke%Plug2TimeCounter + 1
            data%State%Choke%HydraulicChoke2PluggedPercent_Old= data%problems%ChokeProblems%HydraulicChoke2PluggedPercent
            if (data%State%Choke%Plug2TimeCounter <= data%State%Choke%ChokePlugTimeDelay) then    !ChokePlugTimeDelay=600
                data%State%Choke%Present_HydraulicChoke2Plug = data%State%Choke%Present_HydraulicChoke2Plug + data%State%CHOOKE(2)%PlugMalf *((data%State%Choke%DeltaPlug2Percent / real(data%State%Choke%ChokePlugTimeDelay)))     ! real(ChokePlugTimeDelay)= 600.0
            endif
        ENDIF
! fully open area is 123/64 in^2 = 0.01334635 ft^2
        data%State%CHOOKE(1)%AreaChoke=data%State%CHOOKE(1)%AreaChoke+(data%State%CHOOKE(1)%WashoutMalf*data%State%Choke%HydraulicChoke1WashoutCoef*data%State%Choke%ChokeAreaFullyOpen/144.0)      ! Initialised in Choke Startup
        
!write(*,*) 'data%State%CHOOKE(1)%WashoutMalf , data%State%CHOOKE(1)%AreaChoke='  ,data%State%CHOOKE(1)%WashoutMalf , data%State%CHOOKE(1)%AreaChoke
        
        data%State%CHOOKE(1)%AreaChoke=data%State%CHOOKE(1)%AreaChoke-(data%State%CHOOKE(1)%PlugMalf* data%State%Choke%Present_HydraulicChoke1Plug *data%State%CHOOKE(1)%AreaChoke)         ! Initialised in Choke Startup
        
        data%State%CHOOKE(2)%AreaChoke=data%State%CHOOKE(2)%AreaChoke+(data%State%CHOOKE(2)%WashoutMalf*data%State%Choke%HydraulicChoke2WashoutCoef*data%State%Choke%ChokeAreaFullyOpen/144.0)      ! Initialised in Choke Startup
        data%State%CHOOKE(2)%AreaChoke=data%State%CHOOKE(2)%AreaChoke-(data%State%CHOOKE(2)%PlugMalf* data%State%Choke%Present_HydraulicChoke2Plug *data%State%CHOOKE(2)%AreaChoke)         ! Initialised in Choke Startup
!write(*,*) 'data%State%CHOOKE(2)%WashoutMalf , data%State%CHOOKE(2)%AreaChoke='  ,data%State%CHOOKE(2)%WashoutMalf , data%State%CHOOKE(2)%AreaChoke
        
        
        data%State%CHOOKE(1)%AreaChokeFinal= data%State%CHOOKE(1)%AreaChoke
        data%State%CHOOKE(2)%AreaChokeFinal= data%State%CHOOKE(2)%AreaChoke
        
!    144: ft^2 to in^2
        CALL SetHydraulicChock1(100 - nint((data%State%CHOOKE(1)%AreaChokeFinal/(data%State%Choke%ChokeAreaFullyOpen/144.))*100))     ! for manifold valve
        CALL SetHydraulicChock2(100 - nint((data%State%CHOOKE(2)%AreaChokeFinal/(data%State%Choke%ChokeAreaFullyOpen/144.))*100))     ! for manifold valve
    
    
!write(*,*) 'data%State%CHOOKE(1)%PercentClose=' , data%State%CHOOKE(1)%PercentClose     ! close percent 0 to 100
!write(*,*) 'ChokePosition=' , ChokePosition     ! close position 0 to 10 for display
!write(*,*) 'data%State%CHOOKE(1)%AreaChokeFinal=' , data%State%CHOOKE(1)%AreaChokeFinal       ! Open Area (in^2) with clearance
!write(*,*) '(ChokeAreaFullyOpen/144.)=' , (ChokeAreaFullyOpen/144.)
!write(*,*) 'valve value=' , 100 - nint((data%State%CHOOKE(1)%AreaChokeFinal/(ChokeAreaFullyOpen/144.))*100)        ! percent close 0 to 100 with clearance
!write(*,*) 'Valve(33)%Status=' , Valve(33)%Status       ! T : open , F: close
! =================== calculating Area
!write(*,*) 'data%State%CHOOKE(1)%AreaChoke= ' , data%State%CHOOKE(1)%AreaChoke
!WRITE(150,50) alpha_timeair,alpha_Qair,alpha_pairp, &
!alpha_Pdownstrem,alpha_diffpair,alpha_lossesair,data%State%CHOOKE(CHNUMBER)%PassedCourse
!50           FORMAT(7(f15.5))
!========================================================================================
!========================================================================================
!  write(*,*) PassedCourse
    end    

end module ChokeControlMain