mahmood19227
/
SimulationCore2


			
 SUBROUTINE DEALLOCATE_ARRAYS_CHOKE()
USE CHOKEVARIABLES
implicit none
write(*,*) 'deallocateeeeeeeeeeeee'
!===========================================================================
!                   	AIR PUMP LOSSES INPUT
!===========================================================================
!if(allocated(PIPINGS_AIRPUMP)) deallocate(PIPINGS_AIRPUMP)  

DEALLOCATE (PIPINGS_AIRPUMP,DIAM_AIR_INCH,  &
            Re_air,AREA_AIR,LENGT_AIR,ROUGHNESS_AIRPLINE,REL_ROUGHAIR,  &
           fric_air,fricloss_air)
   !================================================================ 
DEALLOCATE (MINORS_AIRPUMP,MINORDIAM_AIR_INCH,  &
            MINORAREA_AIR,LF_AIR,CV_AIR,NOTE_AIR &
            ,minlosspa_air,minloss_air)   

    END       
    
    
 SUBROUTINE LOSS_INPUTS_CHOKE()
USE CHOKEVARIABLES
implicit none
    Integer I


!===========================================================================
!                   	AIR PUMP LOSSES INPUT
!===========================================================================  
NO_PIPINGS_AIRPLINE=1

ALLOCATE (PIPINGS_AIRPUMP(NO_PIPINGS_AIRPLINE,3))
                !			ID(INCH)    L(MM)	  ROUGHNESS(MM)=e   DESCRIPTION	
PIPINGS_AIRPUMP(1,1:3)=		 (/0.5,      60960.,   0.03/)            !Avg.acc.distance
 
!60960= 200 ft

  
  ALLOCATE (DIAM_AIR_INCH(NO_PIPINGS_AIRPLINE),Re_air(NO_PIPINGS_AIRPLINE),AREA_AIR(NO_PIPINGS_AIRPLINE),  &
            LENGT_AIR(NO_PIPINGS_AIRPLINE),ROUGHNESS_AIRPLINE(NO_PIPINGS_AIRPLINE),REL_ROUGHAIR(NO_PIPINGS_AIRPLINE),  &
           fric_air(NO_PIPINGS_AIRPLINE),fricloss_air(NO_PIPINGS_AIRPLINE))


DO I=1,NO_PIPINGS_AIRPLINE
    DIAM_AIR_INCH(I)=PIPINGS_AIRPUMP(I,1)
    LENGT_AIR(I)=PIPINGS_AIRPUMP(I,2)
    ROUGHNESS_AIRPLINE(I)=PIPINGS_AIRPUMP(I,3)
    
    
    AREA_AIR(I)=PI*(DIAM_AIR_INCH(I)*0.0254)**2/4   !D(in), AREA(m)
    REL_ROUGHAIR(I)=ROUGHNESS_AIRPLINE(I)/(DIAM_AIR_INCH(I)*25.4)
    !DIAM_RAMLINE_MM(I)=DIAM_RAMLINE_MM(I)*.001  !  (m)
    LENGT_AIR(I)=LENGT_AIR(I)*.001      !  (m) 
    ENDDO

    
   !================================================================ 
NO_MINORS_AIRPLINE=6

ALLOCATE (MINORS_AIRPUMP(NO_MINORS_AIRPLINE,4))

                    !		ID(INCH)		LF	    CV	NOTE(BAR)      DESCRIPTION	
MINORS_AIRPUMP(1,1:4)=      (/2.,			10.,	0.,	    0./)       !Acc.tee	
MINORS_AIRPUMP(2,1:4)=      (/2.,			11.,	0.,	    0./)       !elbow	
MINORS_AIRPUMP(3,1:4)=      (/1.,			0.,	    0.,	    3.4/)      !filter
MINORS_AIRPUMP(4,1:4)=      (/2.,			0.,	    105.,	0./)       !valve	
MINORS_AIRPUMP(5,1:4)=      (/1.,			0.,	    9.2,	0./)       !valve	
MINORS_AIRPUMP(6,1:4)=      (/2.,			6.4,	0.,	    0./)       !unionA  
  

  ALLOCATE (MINORDIAM_AIR_INCH(NO_MINORS_AIRPLINE),MINORAREA_AIR(NO_MINORS_AIRPLINE),  &
            LF_AIR(NO_MINORS_AIRPLINE),CV_AIR(NO_MINORS_AIRPLINE),NOTE_AIR(NO_MINORS_AIRPLINE) &
            ,minlosspa_air(NO_MINORS_AIRPLINE),minloss_air(NO_MINORS_AIRPLINE))   
 

DO I=1,NO_MINORS_AIRPLINE
    MINORDIAM_AIR_INCH(I)=MINORS_AIRPUMP(I,1)
    LF_AIR(I)=MINORS_AIRPUMP(I,2)
    CV_AIR(I)=MINORS_AIRPUMP(I,3)
    NOTE_AIR(I)=MINORS_AIRPUMP(I,4)
    
    
    MINORAREA_AIR(I)=PI*(MINORDIAM_AIR_INCH(I)*0.0254)**2/4.   !D(in), AREA(m)
ENDDO    
    
 
    END   
    
    
SUBROUTINE PIPE_RAMS_CHOKE(CHNUMBER)
    USE CHOKEVARIABLES
    implicit none
    INTEGER CHNUMBER
    Integer I
    

    loop3: do while (ABS(ChokeControlLever)==1.0 .AND. ChokePanelRigAirSwitch == 1 .AND. CHOOKE(CHNUMBER)%FailMalf==0 .AND. ChokeAirFail==0)
           if (ChokeControlLever == 1.0) then
            CHOOKE(CHNUMBER)%ChokeIsClosing = .true.
            CHOOKE(CHNUMBER)%ChokeIsOpening = .false.
        endif
        
        if (ChokeControlLever == -1.0) then 
            CHOOKE(CHNUMBER)%ChokeIsOpening = .true.
            CHOOKE(CHNUMBER)%ChokeIsClosing = .false.
        endif

 
     time=time+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 CChokeManifoldVariables
use CSounds
USE CChokeProblemsVariables
implicit none
    Integer I

INTEGER CHNUMBER


QAIR_PUMP=Qiter+.1   !(gpm)  maximum flow for the start
diffp_air=-10
losses_air=10

!===================================================================
!                       AIR OPERATED PUMP
!                       MODEL 10-6000W030 RATIO 55:1   
!=================for air consumption at 100 psig=================== 
do while (diffp_air<0)
 QAIR_PUMP=QAIR_PUMP-.1
! Qup=QAIR_PUMP;
 !cc1 = 1354; cc2 = -2066; cc3 = -2109; cc4 = -513.6; cc5 = 5935     FOR OUTPUT IN GPM
 p_airp=cc1*(QAIR_PUMP**4) + cc2*(QAIR_PUMP**3) + cc3*(QAIR_PUMP**2) + cc4*QAIR_PUMP + cc5 !(psig)
! kinetic_air=sg*wdens*(QAIR_PUMP*6.30902e-5/((1/4.)*pi*(2*0.254e-1)**2))**2/(2*6895) !(psi)

 diffp_air= p_airp - Pdownstrem

end do    !returns Qup


 do while (abs((diffp_air-losses_air)/diffp_air)>tol_air) !finding correct QAIR_pump for 1 timecounter_ram

if (diffp_air-losses_air>0) then
    QAIR_PUMP=QAIR_PUMP+.005
else
    QAIR_PUMP=QAIR_PUMP-.005
endif

!===================================================================
!                       AIR OPERATED PUMP
!                       MODEL 10-6000W030 RATIO 55:1   
!=================for air consumption at 100 psig=================== 

 p_airp=cc1*(QAIR_PUMP**4) + cc2*(QAIR_PUMP**3) + cc3*(QAIR_PUMP**2) + cc4*QAIR_PUMP + cc5 !(psig)
 !kinetic_air=sg*wdens*(QAIR_PUMP*6.30902e-005/((1/4.)*pi*(2*0.254e-1)**2))**2/(2*6895) !(psi)

 diffp_air= p_airp - Pdownstrem


!===========================LOSSES====================================
 do i=1,NO_PIPINGS_AIRPLINE
Re_air(i)=QAIR_PUMP*6.30902e-005*DIAM_AIR_INCH(I)*0.0254/(area_air(i)*nu)
enddo


do i=1,NO_PIPINGS_AIRPLINE
     if (Re_air(i)<Re_cr) then
         fric_air(i)=64/Re_air(i)
     else
        fric_air(i)=1/(-1.8*log10((rel_roughair(i)/3.7)**1.11+6.9/Re_air(i)))**2
     endif
     
fricloss_air(i)=((fric_air(i)*(wdens*sg*lengt_air(i)*(QAIR_PUMP*6.30902e-005/area_air(i))**2))/(2*DIAM_AIR_INCH(I)*0.0254))/6895

 enddo


pipe_loss1air=sum(fricloss_air)  !loss before regulator(psi)

do i=1,NO_MINORS_AIRPLINE
    if (LF_air(i)/=0) then
        minlosspa_air(i)=LF_air(i)*wdens*sg*(QAIR_PUMP*6.30902e-005/MINORAREA_AIR(i))**2/2  !(Pa)
        minloss_air(i)=minlosspa_air(i)/6895 !(psi)
    elseif (CV_air(i)/=0) then
        minlosspa_air(i)=1000*sg*((11.7*QAIR_PUMP*6.30902e-005*3600)/(CV_air(i)))**2 !(pa)
        minloss_air(i)=minlosspa_air(i)/6895 !(psi)
    else
        minlosspa_air(i)=NOTE_air(i)*1e5 !(pa)
        minloss_air(i)=minlosspa_air(i)/6895 !(psi)
    endif
enddo

        
minor_loss1air=sum(minloss_air)  !loss before regulator(psi)

static_loss1air=0

losses_air=pipe_loss1air+minor_loss1air+static_loss1air !(psi)
!=========================================================================


 end do  !returns correct QAIR_PUMP for 1 counter
 

   Qiter=QAIR_PUMP
   QAIR_PUMP=QAIR_PUMP*(ChokeRateControlKnob/10.)       ! final Q (gpm)
   
   Cumulative_AirVolume_Choke= Cumulative_AirVolume_Choke + ((QAIR_PUMP * DeltaT_Choke / 60.0 ) / (1.5*0.004329004) )        ! =strokes

   
   if ( Cumulative_AirVolume_Choke > 1.0 ) then
       SoundChokePump= 60
       Cumulative_AirVolume_Choke= Cumulative_AirVolume_Choke - 1.0
   else
       SoundChokePump= 0.0
   endif   
   
   !SoundChokePump= int (QAIR_PUMP/ (1.5*0.004329004)*DeltaT_Choke/60.0)   !  1.5: Volume per stroke (in^3)  , 0.004329004: in^3 to gal ,  60:seconds
   
   
deltav_air=QAIR_PUMP*DeltaT_Choke/60  !(galon) delta_t=1sec , Q(gpm)

if (CHOOKE(CHNUMBER)%ChokeIsClosing)  CHOOKE(CHNUMBER)%PassedCourse=CHOOKE(CHNUMBER)%PassedCourse + (deltav_air*3785.412/Acylinder)!*(ChokeRateControlKnob/10.)        ! 3785.412 : GALON TO CM^3
    
    
if (CHOOKE(CHNUMBER)%ChokeIsOpening)  CHOOKE(CHNUMBER)%PassedCourse=CHOOKE(CHNUMBER)%PassedCourse - (deltav_air*3785.412/Acylinder)!*(ChokeRateControlKnob/10.)

    
!DeltaT_Choke= 1sec or 2sec


!((((((((IN OUTER LOOP))))))

!===============AIR PUMP OUTPUTS=========================
alpha_timeair=time  ! overal time (s)
alpha_Pdownstrem=Pdownstrem
alpha_pairp=p_airp
alpha_Qair=QAIR_PUMP
!write(*,*) 'diffp_air=',diffp_air
!pause
alpha_diffpair=diffp_air

alpha_lossesair=losses_air
!========================================================
!OPEN(150,FILE='CHOKE_AIRPUMP_OUTPUTS.DAT')


       if (CHOOKE(CHNUMBER)%ChokeIsClosing .AND. CHOOKE(CHNUMBER)%PassedCourse>CourseBase) then
        CHOOKE(CHNUMBER)%PassedCourse=CourseBase
        SoundChokePump= 0.0
     endif
     
     if (CHOOKE(CHNUMBER)%ChokeIsOpening .AND. CHOOKE(CHNUMBER)%PassedCourse<0.) then
        CHOOKE(CHNUMBER)%PassedCourse=0.
        SoundChokePump= 0.0
     endif
     
     
     call SetSoundChokePump(SoundChokePump)

     CHOOKE(CHNUMBER)%PercentClose= CHOOKE(CHNUMBER)%PassedCourse/CourseBase
     
     
     IF (Choke1LED==1) THEN
         ChokePosition= (1 - GaugeChokePositionMailf) * CHOOKE(1)%PercentClose*10
     ELSE       ! Choke2LED==1
         ChokePosition= (1 - GaugeChokePositionMailf) * CHOOKE(2)%PercentClose*10
     ENDIF
     
    !CALL SetHydraulicChock1(nint(MIN(CHOOKE(1)%PercentClose / 0.91 , 1.0)*100))     
    ! CALL SetHydraulicChock2(nint(MIN(CHOOKE(2)%PercentClose / 0.91 , 1.0)*100)) 

     ! .91 >> 9 percent clearance
     
! =================== calculating Area     
     
      ! AreaChoke=0.5
     ! .91 >> 9 percent clearance

   CHOOKE(1)%AreaChoke=0.01334635-(0.01334635* MIN(CHOOKE(1)%PercentClose / 0.91 , 1.0)) !ft^2     0.01334635 is ChokeAreaFullyOpen (ft^2)
   CHOOKE(2)%AreaChoke=0.01334635-(0.01334635* MIN(CHOOKE(2)%PercentClose/ 0.91 , 1.0)) !ft^2
   
   !write(*,*) 'CHOOKE(1)%AreaChoke= ' , CHOOKE(1)%AreaChoke
   
   
    HydraulicChoke1WashoutCoef= HydraulicChoke1WashoutCoef * CHOOKE(1)%WashoutMalf    
    HydraulicChoke1WashoutCoef= MIN( 0.5 , HydraulicChoke1WashoutCoef+ CHOOKE(1)%WashoutMalf*(0.5/(60.0/DeltaT_Choke)) ) ! 0.5=maximum washout coef , 60.0 sec= 1min duration time
            
    HydraulicChoke2WashoutCoef= HydraulicChoke2WashoutCoef * CHOOKE(2)%WashoutMalf    
    HydraulicChoke2WashoutCoef= MIN( 0.5 , HydraulicChoke2WashoutCoef+ CHOOKE(2)%WashoutMalf*(0.5/(60.0/DeltaT_Choke)) ) ! 0.5=maximum washout coef , 60.0 sec= 1min duration time
    

    !write(*,*) 'HydraulicChoke1WashoutCoef=' , HydraulicChoke1WashoutCoef
    
    IF (CHOOKE(1)%PlugMalf == 1) THEN
        
            Present_HydraulicChoke1Plug= Present_HydraulicChoke1Plug * CHOOKE(1)%PlugMalf 
            ! integer: HydraulicChoke1PluggedPercent,HydraulicChoke1PluggedPercent_Old,PlugTimeCounter,ChokePlugTimeDelay
            ! real: Present_HydraulicChoke1Plug,DeltaPlug1Percent
    
            !write(*,*) 'HydraulicChoke1PluggedPercent=' , HydraulicChoke1PluggedPercent
    
            if ( (HydraulicChoke1PluggedPercent - HydraulicChoke1PluggedPercent_Old) /= 0) then
                DeltaPlug1Percent = (REAL(HydraulicChoke1PluggedPercent)/100.) - Present_HydraulicChoke1Plug
                Plug1TimeCounter = 0
                !write(*,*) 'DeltaPlug1Percent, Present_HydraulicChoke1Plug  =  ' ,DeltaPlug1Percent , Present_HydraulicChoke1Plug 
            endif
    
    
            Plug1TimeCounter= Plug1TimeCounter + 1

            HydraulicChoke1PluggedPercent_Old= HydraulicChoke1PluggedPercent
    
            if (Plug1TimeCounter <= ChokePlugTimeDelay) then    !ChokePlugTimeDelay=600
        
                Present_HydraulicChoke1Plug = Present_HydraulicChoke1Plug + CHOOKE(1)%PlugMalf* ((DeltaPlug1Percent / real(ChokePlugTimeDelay)))     ! real(ChokePlugTimeDelay)= 600.0
        
            endif
  
            !write(*,*) 'Present_HydraulicChoke1Plug=' , Present_HydraulicChoke1Plug
    
    ENDIF
    
    
    IF (CHOOKE(2)%PlugMalf == 1) THEN 

            Present_HydraulicChoke2Plug= Present_HydraulicChoke2Plug * CHOOKE(2)%PlugMalf 
            ! integer: HydraulicChoke2PluggedPercent,HydraulicChoke2PluggedPercent_Old,PlugTimeCounter,ChokePlugTimeDelay
            ! real: Present_HydraulicChoke2Plug,DeltaPlug2Percent
    
    
            if ( (HydraulicChoke2PluggedPercent - HydraulicChoke2PluggedPercent_Old) /= 0 ) then
                DeltaPlug2Percent = (REAL(HydraulicChoke2PluggedPercent)/100.) - Present_HydraulicChoke2Plug
                Plug2TimeCounter = 0
            endif
    
            Plug2TimeCounter= Plug2TimeCounter + 1

            HydraulicChoke2PluggedPercent_Old= HydraulicChoke2PluggedPercent
    
            if (Plug2TimeCounter <= ChokePlugTimeDelay) then    !ChokePlugTimeDelay=600
        
                Present_HydraulicChoke2Plug = Present_HydraulicChoke2Plug + CHOOKE(2)%PlugMalf *((DeltaPlug2Percent / real(ChokePlugTimeDelay)))     ! real(ChokePlugTimeDelay)= 600.0
        
            endif 
    
    ENDIF
    

   ! fully open area is 123/64 in^2 = 0.01334635 ft^2
   CHOOKE(1)%AreaChoke=CHOOKE(1)%AreaChoke+(CHOOKE(1)%WashoutMalf*HydraulicChoke1WashoutCoef*ChokeAreaFullyOpen/144.0)      ! Initialised in Choke Startup
   
   !write(*,*) 'CHOOKE(1)%WashoutMalf , CHOOKE(1)%AreaChoke='  ,CHOOKE(1)%WashoutMalf , CHOOKE(1)%AreaChoke
   
   CHOOKE(1)%AreaChoke=CHOOKE(1)%AreaChoke-(CHOOKE(1)%PlugMalf* Present_HydraulicChoke1Plug *CHOOKE(1)%AreaChoke)         ! Initialised in Choke Startup
   
   CHOOKE(2)%AreaChoke=CHOOKE(2)%AreaChoke+(CHOOKE(2)%WashoutMalf*HydraulicChoke2WashoutCoef*ChokeAreaFullyOpen/144.0)      ! Initialised in Choke Startup
   CHOOKE(2)%AreaChoke=CHOOKE(2)%AreaChoke-(CHOOKE(2)%PlugMalf* Present_HydraulicChoke2Plug *CHOOKE(2)%AreaChoke)         ! Initialised in Choke Startup
   !write(*,*) 'CHOOKE(2)%WashoutMalf , CHOOKE(2)%AreaChoke='  ,CHOOKE(2)%WashoutMalf , CHOOKE(2)%AreaChoke
   
   
   CHOOKE(1)%AreaChokeFinal= CHOOKE(1)%AreaChoke
   CHOOKE(2)%AreaChokeFinal= CHOOKE(2)%AreaChoke 
   
   !    144: ft^2 to in^2
    CALL SetHydraulicChock1(100 - nint((CHOOKE(1)%AreaChokeFinal/(ChokeAreaFullyOpen/144.))*100))     ! for manifold valve    
    CALL SetHydraulicChock2(100 - nint((CHOOKE(2)%AreaChokeFinal/(ChokeAreaFullyOpen/144.))*100))     ! for manifold valve     
   
   
    !write(*,*) 'CHOOKE(1)%PercentClose=' , CHOOKE(1)%PercentClose     ! close percent 0 to 100
    !write(*,*) 'ChokePosition=' , ChokePosition     ! close position 0 to 10 for display
    !write(*,*) 'CHOOKE(1)%AreaChokeFinal=' , CHOOKE(1)%AreaChokeFinal       ! Open Area (in^2) with clearance
    !write(*,*) '(ChokeAreaFullyOpen/144.)=' , (ChokeAreaFullyOpen/144.)
    !write(*,*) 'valve value=' , 100 - nint((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(*,*) 'CHOOKE(1)%AreaChoke= ' , CHOOKE(1)%AreaChoke
   
   
!         WRITE(150,50) alpha_timeair,alpha_Qair,alpha_pairp, &
!             alpha_Pdownstrem,alpha_diffpair,alpha_lossesair,CHOOKE(CHNUMBER)%PassedCourse
!50           FORMAT(7(f15.5))

  
!========================================================================================            
!========================================================================================           
    
           !  write(*,*) PassedCourse
             
     
    end