def __init__(self):
"""
Load up the necessary sub-structures to be filled with
the code that follows
"""
self.Compressor = CompressorClass()
#Outdoor coil is a Condenser in cooling mode and evaporator in heating mode
self.Condenser = CondenserClass()
self.Condenser.Fins = FinInputs()
self.Evaporator = EvaporatorClass()
self.Evaporator.Fins = FinInputs()
self.CoolingCoil = CoolingCoilClass()
self.CoolingCoil.Fins = FinInputs()
self.Pump = PumpClass()
#Add both types of internal heat exchangers
self.CoaxialIHX = CoaxialHXClass()
self.PHEIHX = PHEHXClass()
self.LineSetSupply = LineSetClass()
self.LineSetReturn = LineSetClass()
#Make IHX an empty class for holding parameters common to PHE and Coaxial IHX
class struct:
pass
self.IHX = struct()
def __init__(self):
"""
Load up the necessary sub-structures to be filled with
the code that follows
"""
self.Compressor=CompressorClass()
self.Condenser=CondenserClass()
self.Condenser.Fins=FinInputs()
self.CoolingCoil=CoolingCoilClass()
self.CoolingCoil.Fins=FinInputs()
self.PHEHX=PHEHXClass()
self.Pump=PumpClass()
class SecondaryCycleClass():
def __init__(self):
"""
Load up the necessary sub-structures to be filled with
the code that follows
"""
self.Compressor=CompressorClass()
#Outdoor coil is a Condenser in cooling mode and evaporator in heating mode
self.Condenser=CondenserClass()
self.Condenser.Fins=FinInputs()
self.Evaporator=EvaporatorClass()
self.Evaporator.Fins=FinInputs()
self.CoolingCoil=CoolingCoilClass()
self.CoolingCoil.Fins=FinInputs()
self.Pump=PumpClass()
#Add both types of internal heat exchangers
self.CoaxialIHX=CoaxialHXClass()
self.PHEIHX=PHEHXClass()
self.LineSetSupply=LineSetClass()
self.LineSetReturn=LineSetClass()
#Make IHX an empty class for holding parameters common to PHE and Coaxial IHX
class struct: pass
self.IHX=struct()
def OutputList(self):
"""
Return a list of parameters for this component for further output
It is a list of tuples, and each tuple is formed of items:
[0] Description of value
[1] Units of value
[2] The value itself
"""
return [
('Charge','kg',self.Charge),
('Condenser Subcooling','K',self.DT_sc),
('Primary Ref.','-',self.Ref),
('Secondary Ref.','-',self.SecLoopFluid),
('Imposed Variable','-',self.ImposedVariable),
('IHX Type','-',self.IHXType),
('COP','-',self.COP),
('COSP','-',self.COSP),
('Net Capacity','W',self.CoolingCoil.Capacity),
('Net Power','W',self.Power),
('SHR','-',self.SHR),
('Condensation temp (dew)','K',self.Tdew_cond),
('Evaporation temp (dew)','K',self.Tdew_evap),
]
def Calculate(self,DT_evap,DT_cond,Tin_CC):
"""
Inputs are differences in temperature [K] between HX air inlet temperature
and the dew temperature for the heat exchanger.
Required Inputs:
DT_evap:
Difference in temperature [K] between cooling coil air inlet temperature and refrigerant dew temperature
DT_cond:
Difference in temperature [K] between condenser air inlet temperature and refrigerant dew temperature
Tin_CC:
Inlet "glycol" temperature to line set feeding cooling coil
"""
if self.Verbosity>1:
print 'Inputs: DTevap %7.4f DTcond %7.4f fT_IHX %7.4f'%(DT_evap,DT_cond,Tin_CC)
#Store the values to save on computation for later
self.DT_evap=DT_evap
self.DT_cond=DT_cond
self.Tin_CC=Tin_CC
#If the user doesn't include the Mode, set it to Air Conditioning
if not hasattr(self,'Mode'):
self.Mode='AC'
if self.Mode=='AC':
self.Tdew_cond=self.Condenser.Fins.Air.Tdb+DT_cond
self.Tdew_evap=self.CoolingCoil.Fins.Air.Tdb-DT_evap
elif self.Mode=='HP':
self.Tdew_cond=Tin_CC+DT_cond
self.Tdew_evap=self.Evaporator.Fins.Air.Tdb-DT_evap
else:
raise ValueError('Mode must be AC or HP')
psat_cond=Props('P','T',self.Tdew_cond,'Q',1,self.Ref)
psat_evap=Props('P','T',self.Tdew_evap,'Q',1,self.Ref)
self.Tbubble_evap=Props('T','P',psat_evap,'Q',0,self.Ref)
self.Tbubble_cond=Props('T','P',psat_cond,'Q',0,self.Ref)
if self.Mode=='AC':
params={ #dictionary -> key:value, e.g. 'key':2345,
'pin_r': psat_evap+self.DP_low,
'pout_r': psat_cond-self.DP_high,
'Tin_r': self.Tdew_evap+self.PHEIHX.DT_sh, # TrhoPhase_ph(self.Ref,psat_evap,self.LineSetReturn.hout,self.Tbubble_evap,self.Tdew_evap)[0],
'Ref': self.Ref
}
self.Compressor.Update(**params)
self.Compressor.Calculate()
params={
'mdot_r': self.Compressor.mdot_r,
'Tin_r': self.Compressor.Tout_r,
'psat_r': psat_cond,
'Ref': self.Ref
}
self.Condenser.Update(**params)
self.Condenser.Calculate()
params={
'mdot': self.Pump.mdot_g,
'hin': Props('H','T',Tin_CC,'P',self.Pump.pin_g,self.SecLoopFluid)*1000,
}
self.LineSetSupply.Update(**params)
self.LineSetSupply.Calculate()
#Now run CoolingCoil to predict inlet glycol temperature to IHX
params={
'mdot_g': self.Pump.mdot_g,
'Tin_g': self.LineSetSupply.Tout,
}
self.CoolingCoil.Update(**params)
self.CoolingCoil.Calculate()
params={
'mdot': self.Pump.mdot_g,
'hin': Props('H','T',self.CoolingCoil.Tout_g,'P',self.Pump.pin_g,self.SecLoopFluid)*1000,
}
self.LineSetReturn.Update(**params)
self.LineSetReturn.Calculate()
if self.IHXType=='Coaxial':
params={
'mdot_g': self.Pump.mdot_g,
'Tin_g': self.CoolingCoil.Tout_g,
'pin_r': psat_evap,
'hin_r': self.Condenser.hout_r,
'Ref_r': self.Ref,
'mdot_r': self.Compressor.mdot_r,
}
self.CoaxialIHX.Update(**params)
self.CoaxialIHX.Calculate()
self.IHX.Charge_r=self.CoaxialIHX.Charge_r
self.IHX.Q=self.CoaxialIHX.Q
self.IHX.Tout_g=self.CoaxialIHX.Tout_g
self.IHX.DP_g=self.CoaxialIHX.DP_g
self.IHX.hout_r=self.CoaxialIHX.hout_r
self.IHX.DP_r=self.CoaxialIHX.DP_r
if hasattr(self,'PHEIHX'):
del self.PHEIHX
elif self.IHXType=='PHE':
params={
'mdot_h': self.Pump.mdot_g,
'hin_h': Props('H','T',self.CoolingCoil.Tout_g,'P',self.PHEIHX.pin_h,self.SecLoopFluid)*1000,
'mdot_c': self.Compressor.mdot_r,
'pin_c': psat_evap,
'hin_c': self.Condenser.hout_r,
}
self.PHEIHX.Update(**params)
self.PHEIHX.Calculate()
self.IHX.Charge_r=self.PHEIHX.Charge_c
self.IHX.Q=self.PHEIHX.Q
self.IHX.Tout_g=self.PHEIHX.Tout_h
self.IHX.DP_g=self.PHEIHX.DP_h
self.IHX.DP_r=self.PHEIHX.DP_c
self.IHX.hout_r=self.PHEIHX.hout_c
if hasattr(self,'CoaxialIHX'):
del self.CoaxialIHX
params={
'DP_g': self.IHX.DP_g+self.CoolingCoil.DP_g+self.LineSetSupply.DP+self.LineSetReturn.DP,
'Tin_g': self.CoolingCoil.Tout_g
}
self.Pump.Update(**params)
self.Pump.Calculate()
self.Charge=self.Condenser.Charge+self.IHX.Charge_r
self.EnergyBalance=self.Compressor.CycleEnergyIn+self.Condenser.Q+self.IHX.Q
self.DT_sc=(Props('H','T',self.Tbubble_cond,'Q',0,self.Ref)*1000-self.Condenser.hout_r)/(Props('C','T',self.Tbubble_cond,'Q',0,self.Ref)*1000)
deltaH_sc=self.Compressor.mdot_r*(Props('H','T',self.Tbubble_cond,'Q',0,self.Ref)*1000-Props('H','T',self.Tbubble_cond-self.DT_sc_target,'P',psat_cond,self.Ref)*1000)
# ## Plot a p-h plot
# Ph(self.Ref,hbounds=(100,500))
# pylab.plot([self.Compressor.hin_r/1000,self.Compressor.hout_r/1000,self.Condenser.hout_r/1000,self.PHEIHX.hin_c/1000,self.Compressor.hin_r/1000],[psat_evap,psat_cond,psat_cond,psat_evap,psat_evap])
# pylab.show()
resid=np.zeros((3))
resid[0]=self.Compressor.mdot_r*(self.Compressor.hin_r-self.IHX.hout_r)
if self.ImposedVariable=='Subcooling':
resid[1]=self.Condenser.DT_sc-self.DT_sc_target
elif self.ImposedVariable=='Charge':
resid[1]=self.Charge-self.Charge_target
# resid[2]=self.IHX.Q-self.CoolingCoil.Q+self.Pump.W
self.residSL=self.IHX.Q-self.CoolingCoil.Q+self.Pump.W+self.LineSetSupply.Q+self.LineSetReturn.Q
resid[2]=self.residSL
if self.Verbosity>7:
print 'Wcomp % 12.6e Qcond: % 12.6e QPHE %10.4f ' %(self.Compressor.W,self.Condenser.Q,self.IHX.Q)
if self.Verbosity>1:
print 'Qres % 12.6e Resid2: % 12.6e ResSL %10.4f Charge %10.4f SC: %8.4f' %(resid[0],resid[1],self.residSL,self.Charge,self.Condenser.DT_sc)
self.Capacity=self.CoolingCoil.Capacity
self.COP=self.CoolingCoil.Q/self.Compressor.W
self.COSP=self.CoolingCoil.Capacity/(self.Compressor.W+self.Pump.W+self.CoolingCoil.Fins.Air.FanPower+self.Condenser.Fins.Air.FanPower)
self.SHR=self.CoolingCoil.SHR
self.Power=self.Compressor.W+self.Pump.W+self.CoolingCoil.Fins.Air.FanPower+self.Condenser.Fins.Air.FanPower
self.DP_high_Model=self.Condenser.DP_r #[Pa]
self.DP_low_Model=self.IHX.DP_r #[Pa]
elif self.Mode=='HP':
if psat_evap+self.DP_low<0:
raise ValueError('Compressor inlet pressure less than zero ['+str(psat_evap+self.DP_low)+' kPa] - is low side pressure drop too high?')
params={ #dictionary -> key:value, e.g. 'key':2345,
'pin_r': psat_evap+self.DP_low,
'pout_r': psat_cond-self.DP_high,
'Tin_r': self.Tdew_evap+self.Evaporator.DT_sh, # TrhoPhase_ph(self.Ref,psat_evap,self.LineSetReturn.hout,self.Tbubble_evap,self.Tdew_evap)[0],
'Ref': self.Ref
}
self.Compressor.Update(**params)
self.Compressor.Calculate()
params={
'mdot': self.Pump.mdot_g,
'hin': Props('H','T',Tin_CC,'P',self.Pump.pin_g,self.SecLoopFluid)*1000,
}
self.LineSetSupply.Update(**params)
self.LineSetSupply.Calculate()
#Now run CoolingCoil to predict inlet glycol temperature to IHX
params={
'mdot_g': self.Pump.mdot_g,
'Tin_g': self.LineSetSupply.Tout,
}
self.CoolingCoil.Update(**params)
self.CoolingCoil.Calculate()
params={
'mdot': self.Pump.mdot_g,
'hin': Props('H','T',self.CoolingCoil.Tout_g,'P',self.Pump.pin_g,self.SecLoopFluid)*1000,
}
self.LineSetReturn.Update(**params)
self.LineSetReturn.Calculate()
params={
'mdot_h': self.Compressor.mdot_r,
'hin_h': self.Compressor.hout_r,
'pin_h': psat_cond,
'mdot_c': self.Pump.mdot_g,
'hin_c': Props('H','T',self.LineSetReturn.Tout,'P',self.PHEIHX.pin_c,self.SecLoopFluid)*1000,
}
self.PHEIHX.Update(**params)
self.PHEIHX.Calculate()
params={
'mdot_r': self.Compressor.mdot_r,
'psat_r': psat_evap,
'hin_r': self.PHEIHX.hout_h,
'Ref': self.Ref
}
self.Evaporator.Update(**params)
self.Evaporator.Calculate()
params={
'DP_g': self.PHEIHX.DP_c+self.CoolingCoil.DP_g,
'Tin_g': self.CoolingCoil.Tout_g
}
self.Pump.Update(**params)
self.Pump.Calculate()
self.Charge=self.Evaporator.Charge+self.PHEIHX.Charge_h
#Calculate an effective subcooling amount by deltah/cp_satL
#Can be positive or negative (negative is quality at outlet
self.DT_sc=self.PHEIHX.DT_sc_h#(Props('H','T',self.Tbubble_cond,'Q',0,self.Ref)*1000-self.PHEIHX.hout_h)/(Props('C','T',self.Tbubble_cond,'Q',0,self.Ref)*1000)
deltaH_sc=self.Compressor.mdot_r*(Props('H','T',self.Tbubble_cond,'Q',0,self.Ref)*1000-Props('H','T',self.Tbubble_cond-self.DT_sc_target,'P',psat_cond,self.Ref)*1000)
resid=np.zeros((3))
resid[0]=self.Compressor.mdot_r*(self.Compressor.hin_r-self.Evaporator.hout_r)
if self.ImposedVariable=='Subcooling':
resid[1]=self.DT_sc-self.DT_sc_target
elif self.ImposedVariable=='Charge':
resid[1]=self.Charge-self.Charge_target
self.residSL=self.PHEIHX.Q+self.CoolingCoil.Q+self.Pump.W+self.LineSetSupply.Q+self.LineSetReturn.Q
resid[2]=self.residSL
if self.Verbosity>1:
print 'Qres % 12.6e Resid2: % 12.6e ResSL %10.4f Charge %10.4f SC: %8.4f' %(resid[0],resid[1],self.residSL,self.Charge,self.DT_sc)
self.Capacity=-self.CoolingCoil.Q+self.CoolingCoil.Fins.Air.FanPower
self.COP=-self.CoolingCoil.Q/self.Compressor.W
self.COSP=self.Capacity/(self.Compressor.W+self.Pump.W+self.CoolingCoil.Fins.Air.FanPower+self.Evaporator.Fins.Air.FanPower)
self.Power=self.Compressor.W+self.Pump.W+self.CoolingCoil.Fins.Air.FanPower+self.Evaporator.Fins.Air.FanPower
self.SHR=-self.CoolingCoil.SHR
self.DP_high_Model=self.PHEIHX.DP_h #[Pa]
self.DP_low_Model=self.Evaporator.DP_r #[Pa]
self.DT_evap=DT_evap
self.DT_cond=DT_cond
return resid
def PreconditionedSolve(self,PrecondValues=None):
'''
PrecondValues = dictionary of values DT_evap, DT_cond and Tin_CC
'''
def OBJECTIVE(x):
"""
Takes the place of a lambda function since lambda functions do not bubble error properly
"""
return self.Calculate(x[0],x[1],x[2])
def OBJECTIVE2(x,Tin):
"""
Takes the place of a lambda function since lambda functions do not bubble error properly
"""
return self.Calculate(x[0],x[1],Tin)
def OBJECTIVE_SL(Tin_CC):
"""
Objective function for the inner loop of the vapor compression system
Using the MultiDimNewtRaph function will re-evaluate the Jacobian at
every step. Slower, but more robust since the solution surfaces aren't
smooth enough
Note: This function is not currently used!
"""
x=MultiDimNewtRaph(OBJECTIVE2,[self.DT_evap,self.DT_cond],args=(Tin_CC,))
# Update the guess values for Delta Ts starting
# at the third step (after at least one update away
# from the boundaries)
if self.OBJ_SL_counter>=0:
self.DT_evap=x[0]
self.DT_cond=x[1]
pass
self.OBJ_SL_counter+=1
return self.residSL
def PrintDPs():
print 'DP_LP :: Input:',self.DP_low,'kPa / Model calc:',self.DP_low_Model/1000,'kPa'
print 'DP_HP :: Input:',self.DP_high,'kPa / Model calc:',self.DP_high_Model/1000,'kPa'
#Some variables need to be initialized
self.DP_low=0 #The actual low-side pressure drop to be used in kPa
self.DP_high=0 #The actual low-side pressure drop to be used in kPa
self.OBJ_SL_counter=0
#Run the preconditioner to get guess values for the temperatures
if PrecondValues is None:
self.DT_evap,self.DT_cond,Tin_CC=SecondaryLoopPreconditioner(self)
else:
self.DT_evap=PrecondValues['DT_evap']
self.DT_cond=PrecondValues['DT_cond']
Tin_CC=PrecondValues['Tin_CC']
#Remove the other, non-used IHX class if found
if self.IHXType=='PHE':
if hasattr(self,'CoaxialIHX'):
del self.CoaxialIHX
else:
if hasattr(self,'PHEIHX'):
del self.PHEIHX
#Remove the condenser if in heating mode and condenser found
if self.Mode=='HP':
if hasattr(self,'Condenser'):
del self.Condenser
iter=1
max_error_DP=999
#Outer loop with a more relaxed convergence criterion
while max_error_DP>0.5:
iter_inner=1
#Inner loop to determine pressure drop for high and low sides
while max_error_DP>0.05 and iter_inner<10:
#Run to calculate the pressure drop as starting point
OBJECTIVE([self.DT_evap,self.DT_cond,Tin_CC])
#Calculate the max error
max_error_DP=max([abs(self.DP_low_Model/1000-self.DP_low),abs(self.DP_high_Model/1000-self.DP_high)])
if self.Verbosity>0:
PrintDPs()
print 'Max pressure drop error [inner loop] is',max_error_DP,'kPa'
#Update the pressure drop terms
self.DP_low=self.DP_low_Model/1000
self.DP_high=self.DP_high_Model/1000
iter_inner+=1
if self.Verbosity > 0:
print "Done with the inner loop on pressure drop"
# Use Newton-Raphson solver
(self.DT_evap,self.DT_cond,Tin_CC)=MultiDimNewtRaph(OBJECTIVE,[self.DT_evap,self.DT_cond,Tin_CC],dx=0.1)
#Calculate the error
max_error_DP=max([abs(self.DP_low_Model/1000-self.DP_low),abs(self.DP_high_Model/1000-self.DP_high)])
if self.Verbosity>0:
PrintDPs()
print 'Max pressure drop error [outer loop] is',max_error_DP,'kPa'
if self.Verbosity>1:
print 'Capacity: ', self.Capacity
print 'COP: ',self.COP
print 'COP (w/ both fans): ',self.COSP
print 'SHR: ',self.SHR
return
FinsTubes.Fins.Pd = 0.001
FinsTubes.Fins.xf = 0.001
FinsTubes.Fins.t = 0.00011
FinsTubes.Fins.k_fin = 237
FinsTubes.Air.Vdot_ha = 0.5663
FinsTubes.Air.Tmean = 299.8
FinsTubes.Air.Tdb = 299.8
FinsTubes.Air.p = 101325 #Air pressure in Pa
FinsTubes.Air.RH = 0.51
FinsTubes.Air.RHmean = 0.51
FinsTubes.Air.FanPower = 438 #fan power in Watts
# Here are two equivalent methods for setting parameters
# 1. Create an empty instance of the class, then set parameters CC=CoolingCoilClass()
CC = CoolingCoilClass()
CC.Fins = FinsTubes
CC.FinsType = 'WavyLouveredFins' #Choose fin Type: 'WavyLouveredFins' or 'HerringboneFins'or 'PlainFins'
CC.Ref_g = 'Water'
CC.mdot_g = 0.15
CC.Tin_g = 278
CC.pin_g = 300000 #Refrigerant vapor pressure in Pa
CC.Verbosity = 3
CC.Calculate()
print "Method 1:"
print "Cooling Coil Q: " + str(CC.Q) + " W"
print "Cooling Coil SHR: " + str(CC.SHR) + " "
# 2. Build a dictionary of values, then use that to initialize the class
kwds = {
FinsTubes.Fins.Pd=0.001
FinsTubes.Fins.xf=0.001
FinsTubes.Fins.t=0.00011
FinsTubes.Fins.k_fin=237
FinsTubes.Air.Vdot_ha=0.5663
FinsTubes.Air.Tmean=299.8
FinsTubes.Air.Tdb= 299.8
FinsTubes.Air.p=101325 #Air pressure in Pa
FinsTubes.Air.RH=0.51
FinsTubes.Air.RHmean=0.51
FinsTubes.Air.FanPower=438 #fan power in Watts
# Here are two equivalent methods for setting parameters
# 1. Create an empty instance of the class, then set parameters CC=CoolingCoilClass()
CC=CoolingCoilClass()
CC.Fins = FinsTubes
CC.FinsType = 'WavyLouveredFins' #Choose fin Type: 'WavyLouveredFins' or 'HerringboneFins'or 'PlainFins'
CC.Ref_g = 'Water'
CC.mdot_g = 0.15
CC.Tin_g = 278
CC.pin_g = 300000 #Refrigerant vapor pressure in Pa
CC.Verbosity = 3
CC.Calculate()
print "Method 1:"
print "Cooling Coil Q: " + str(CC.Q) + " W"
print "Cooling Coil SHR: " + str(CC.SHR) + " "
# 2. Build a dictionary of values, then use that to initialize the class
kwds={'Fins':FinsTubes,
class SecondaryCycleClass():
def __init__(self):
"""
Load up the necessary sub-structures to be filled with
the code that follows
"""
self.Compressor=CompressorClass()
self.Condenser=CondenserClass()
self.Condenser.Fins=FinInputs()
self.CoolingCoil=CoolingCoilClass()
self.CoolingCoil.Fins=FinInputs()
self.PHEHX=PHEHXClass()
self.Pump=PumpClass()
def Calculate(self,DT_evap,DT_cond,Tin_IHX):
"""
Inputs are differences in temperature [K] between HX air inlet temperature
and the dew temperature for the heat exchanger.
Required Inputs:
DT_evap:
Difference in temperature [K] between cooling coil air inlet temperature and refrigerant dew temperature
DT_cond:
Difference in temperature [K] between condenser air inlet temperature and refrigeant dew temperature
Tin_IHX:
Inlet "glycol" temperature to IHX
"""
if self.Verbosity>1:
print 'Inputs: DTevap %7.4f DTcond %7.4f fT_IHX %7.4f'%(DT_evap,DT_cond,Tin_IHX)
#AbstractState
if hasattr(self,'Backend'): #check if backend is given
AS = CP.AbstractState(self.Backend, self.Ref)
if hasattr(self,'MassFrac'):
AS.set_mass_fractions([self.MassFrac])
else: #otherwise, use the defualt backend
AS = CP.AbstractState('HEOS', self.Ref)
self.Backend = 'HEOS'
self.AS = AS
#AbstractState for SecLoopFluid
if hasattr(self,'Backend_SLF'): #check if backend_SLF is given
AS_SLF = CP.AbstractState(self.Backend_SLF, self.SecLoopFluid)
if hasattr(self,'MassFrac_SLF'):
AS_SLF.set_mass_fractions([self.MassFrac_SLF])
else: #otherwise, use the defualt backend
AS_SLF = CP.AbstractState('HEOS', self.SecLoopFluid)
self.Backend_SLF = 'HEOS'
self.AS_SLF = AS_SLF
"""
The coldest the glycol entering the cooling coil could be would be the
"""
self.Tdew_cond=self.Condenser.Fins.Air.Tdb+DT_cond
self.Tdew_evap=self.CoolingCoil.Fins.Air.Tdb-DT_evap
AS.update(CP.QT_INPUTS,1.0,self.Tdew_cond)
psat_cond=AS.p() #[Pa]
AS.update(CP.QT_INPUTS,1.0,self.Tdew_evap)
psat_evap=AS.p() #[Pa]
AS.update(CP.PQ_INPUTS,psat_evap,0.0)
self.Tbubble_evap=AS.T() #[K]
params={ #dictionary -> key:value, e.g. 'key':2345,
'pin_r': psat_evap,
'pout_r': psat_cond,
'Tin_r': self.Tdew_evap+self.Compressor.DT_sh,
'Ref': self.Ref,
'Backend': self.Backend
}
self.Compressor.Update(**params)
self.Compressor.Calculate()
params={
'mdot_r': self.Compressor.mdot_r,
'Tin_r': self.Compressor.Tout_r,
'psat_r': psat_cond,
'Ref': self.Ref,
'Backend': self.Backend
}
self.Condenser.Update(**params)
self.Condenser.Calculate()
AS.update(CP.QT_INPUTS,0.0,self.Tbubble_evap)
hL=AS.hmass() #[J/kg]
AS.update(CP.QT_INPUTS,1.0,self.Tdew_evap)
hV=AS.hmass() #[J/kg]
xin_r=(self.Condenser.hout_r-hL)/(hV-hL)
AS_SLF.update(CP.PT_INPUTS,300000,Tin_IHX)
h_in = AS_SLF.hmass() #[J/kg]
params={
'mdot_h': self.Pump.mdot_g,
'hin_h': h_in,
'hin_c': self.Condenser.hout_r,
'mdot_c': self.Compressor.mdot_r,
'pin_c': psat_evap,
'xin_c': xin_r
}
self.PHEHX.Update(**params)
self.PHEHX.Calculate()
#Now run CoolingCoil to predict inlet glycol temperature to IHX
params={
'mdot_g': self.Pump.mdot_g,
'Tin_g': self.PHEHX.Tout_h,
}
self.CoolingCoil.Update(**params)
self.CoolingCoil.Calculate()
params={
'DP_g': self.PHEHX.DP_h+self.CoolingCoil.DP_g,
'Tin_g': self.CoolingCoil.Tout_g
}
self.Pump.Update(**params)
self.Pump.Calculate()
self.Charge=self.Condenser.Charge+self.PHEHX.Charge_c
self.EnergyBalance=self.Compressor.CycleEnergyIn+self.Condenser.Q+self.PHEHX.Q
resid=np.zeros((3))
resid[0]=self.EnergyBalance
if self.ImposedVariable=='Subcooling':
resid[1]=self.Condenser.DT_sc-self.DT_sc_target
elif self.ImposedVariable=='Charge':
resid[1]=self.Charge-self.Charge_target
resid[2]=self.PHEHX.Q-self.CoolingCoil.Q
if self.Verbosity>1:
print 'Qres % 12.6e Resid2: % 12.6e ResSL %10.4f Charge %10.4f SC: %8.4f' %(resid[0],resid[1],resid[2],self.Charge,self.Condenser.DT_sc)
self.Capacity=self.CoolingCoil.Capacity
self.COP=self.CoolingCoil.Q/self.Compressor.W
self.COSP=self.CoolingCoil.Capacity/(self.Compressor.W+self.Pump.W+self.CoolingCoil.Fins.Air.FanPower+self.Condenser.Fins.Air.FanPower)
self.SHR=self.CoolingCoil.SHR
return resid
def PreconditionedSolve(self):
# Takes the place of a lambda function since lambda functions do not
# bubble the error up properly
def OBJECTIVE(x):
return self.Calculate(x[0],x[1],x[2])
# Increase DT_evap in increments of 0.5 K until the system solves, and
# two steps cause a sign change in cycle energy balance
# Should give a starting point quite close to the "right" soluton
oldDT_evap=None
oldQresid=None
Tin_IHX=None
for DT_evap in np.linspace(12,25,21):
try:
#Run the cooler to get a good starting inlet temperature for IHX
self.CoolingCoil.mdot_g=self.Pump.mdot_g
self.CoolingCoil.Tin_g=self.CoolingCoil.Fins.Air.Tdb-DT_evap
self.CoolingCoil.Calculate()
Tin_IHX=self.CoolingCoil.Tout_g
resid=self.Calculate(DT_evap,8,Tin_IHX)
except Exception,e:
if self.Verbosity>1:
print 'Failed: ',e.__str__()
raise
pass
else:
#Not set yet, first one that works
if oldQresid==None:
oldQresid=resid[0]
oldDT_evap=DT_evap
#Has been set, and sign changes, use average of old and new DT
elif oldQresid*resid[0]<0:
DT_evap=(DT_evap+oldDT_evap)/2
break
#Run the Newton-Raphson solver to solve the system
x=fsolve(OBJECTIVE,[DT_evap,20,Tin_IHX])
if self.Verbosity>1:
print 'Capacity: ', self.Capacity
print 'COP: ',self.COP
print 'COP (w/ both fans): ',self.COSP
print 'SHR: ',self.SHR
FinsTubes.Fins.Pd=0.001
FinsTubes.Fins.xf=0.001
FinsTubes.Fins.t=0.00011
FinsTubes.Fins.k_fin=237
FinsTubes.Air.Vdot_ha=0.5663
FinsTubes.Air.Tmean=299.8
FinsTubes.Air.Tdb=299.8
FinsTubes.Air.p=101.325
FinsTubes.Air.RH=0.51
FinsTubes.Air.RHmean=0.51
FinsTubes.Air.FanPower=438
# Here are two equivalent methods for setting parameters
# 1. Create an empty instance of the class, then set parameters
CC=CoolingCoilClass()
CC.Fins = FinsTubes
CC.Ref_g = 'Water'
CC.mdot_g = 0.15
CC.Tin_g = 278
CC.pin_g = 300
CC.Verbosity = 3
CC.Calculate()
print "Method 1:"
print "Cooling Coil Q: " + str(CC.Q) + " W"
print "Cooling Coil SHR: " + str(CC.SHR) + " "
# 2. Build a dictionary of values, then use that to initialize the class
kwds={'Fins':FinsTubes,
'Ref_g': 'Water',
FinsTubes.Fins.Pd = 0.001 FinsTubes.Fins.xf = 0.001 FinsTubes.Fins.t = 0.00011 FinsTubes.Fins.k_fin = 237 FinsTubes.Air.Vdot_ha = 0.5663 FinsTubes.Air.Tmean = 299.8 FinsTubes.Air.Tdb = 299.8 FinsTubes.Air.p = 101325 #Air pressure in Pa FinsTubes.Air.RH = 0.51 FinsTubes.Air.RHmean = 0.51 FinsTubes.Air.FanPower = 438 #fan power in Watts # Here are two equivalent methods for setting parameters # 1. Create an empty instance of the class, then set parameters CC=CoolingCoilClass() CC = CoolingCoilClass() CC.Fins = FinsTubes CC.FinsType = 'WavyLouveredFins' #Choose fin Type: 'WavyLouveredFins' or 'HerringboneFins'or 'PlainFins' CC.Ref_g = 'Water' CC.Backend_g = 'HEOS' #choose between: 'HEOS','TTSE&HEOS','BICUBIC&HEOS','REFPROP','SRK','PR' CC.mdot_g = 0.15 CC.Tin_g = 278 CC.pin_g = 300000 #Refrigerant vapor pressure in Pa CC.Verbosity = 3 CC.Calculate() print "Method 1 (HEOS):" print "Cooling Coil Q: " + str(CC.Q) + " W" print "Cooling Coil SHR: " + str(CC.SHR) + " " # 2. Build a dictionary of values, then use that to initialize the class