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Python-DT_Slot_3/Turbinen/Turbinen_class_file.py

196 lines
9.4 KiB
Python

import numpy as np
#importing pressure conversion function
import sys
import os
from pyparsing import alphanums
current = os.path.dirname(os.path.realpath(__file__))
parent = os.path.dirname(current)
sys.path.append(parent)
from functions.pressure_conversion import pressure_conversion
class Francis_Turbine:
# units
# make sure that units and display units are the same
# units are used to label graphs and disp units are used to have a bearable format when using pythons print()
density_unit = r'$\mathrm{kg}/\mathrm{m}^3$'
flux_unit = r'$\mathrm{m}^3/\mathrm{s}$'
LA_unit = '%'
pressure_unit = 'Pa'
time_unit = 's'
velocity_unit = r'$\mathrm{m}/\mathrm{s}$'
volume_unit = r'$\mathrm{m}^3$'
density_unit_disp = 'kg/m³'
flux_unit_disp = 'm³/s'
LA_unit_disp = '%'
time_unit_disp = 's'
velocity_unit_disp = 'm/s'
volume_unit_disp = ''
g = 9.81 # m/s² gravitational acceleration
# init
def __init__(self,Q_nenn,p_nenn,t_closing,timestep,pressure_unit_disp):
"""
Creates a turbine with given attributes in this order: \n
Nominal flux [m³/s] \n
Nominal pressure [Pa] \n
Closing time [s] \n
Simulation timestep [s] \n
Pressure unit for displaying [string] \n
"""
self.Q_n = Q_nenn # nominal flux
self.p_n = p_nenn # nominal pressure
self.LA_n = 1. # 100% # nominal Leitapparatöffnung
self.dt = timestep # simulation timestep
self.t_c = t_closing # closing time
self.d_LA_max_dt = 1/t_closing # maximal change of LA per second
self.pressure_unit_disp = pressure_unit_disp
# initialize for get_info()
self.p = -np.inf
self.Q = -np.inf
self.LA = -np.inf
# setter - set attributes
def set_LA(self,LA,display_warning=True):
# warn user, that the .set_LA() method should not be used ot set LA manually
if display_warning == True:
print('You are setting the guide vane opening of the turbine manually. \n \
This is not an intended use of this method. \n \
Refer to the .update_LA() method instead.')
# set Leitapparatöffnung
self.LA = LA
def set_pressure(self,pressure):
# set pressure in front of the turbine
self.p = pressure
def set_steady_state(self,ss_flux,ss_pressure):
# calculate and set steady state LA, that allows the flow of ss_flux at ss_pressure through the
# turbine at the steady state LA
ss_LA = self.LA_n*ss_flux/self.Q_n*np.sqrt(self.p_n/ss_pressure)
if ss_LA < 0 or ss_LA > 1:
raise Exception('LA out of range [0;1]')
self.set_LA(ss_LA,display_warning=False)
self.set_pressure(ss_pressure)
self.get_current_Q()
#getter - get attributes
def get_current_Q(self):
# return the flux through the turbine, based on the current pressure in front
# of the turbine and the Leitapparatöffnung
if self.p < 0:
self.Q = 0
else:
self.Q = self.Q_n*(self.LA/self.LA_n)*np.sqrt(self.p/self.p_n)
return self.Q
def get_current_LA(self):
return self.LA
def get_current_pressure(self,disp_flag=True):
if disp_flag == True:
return pressure_conversion(self.p,self.pressure_unit,self.pressure_unit_disp)
else:
return self.p
def get_info(self, full = False):
new_line = '\n'
p = pressure_conversion(self.p,self.pressure_unit,self.pressure_unit_disp)
p_n = pressure_conversion(self.p_n,self.pressure_unit,self.pressure_unit_disp)
if full == True:
# :<10 pads the self.value to be 10 characters wide
print_str = (f"Turbine has the following attributes: {new_line}"
f"----------------------------- {new_line}"
f"Type = Francis {new_line}"
f"Nominal flux = {self.Q_n:<10} {self.flux_unit_disp} {new_line}"
f"Nominal pressure = {round(p_n,3):<10} {self.pressure_unit_disp}{new_line}"
f"Nominal LA = {self.LA_n*100:<10} {self.LA_unit_disp} {new_line}"
f"Closing time = {self.t_c:<10} {self.time_unit_disp} {new_line}"
f"Current flux = {round(self.Q,3):<10} {self.flux_unit_disp} {new_line}"
f"Current pipe pressure = {round(p,3):<10} {self.pressure_unit_disp} {new_line}"
f"Current LA = {round(self.LA,4)*100:<10} {self.LA_unit_disp} {new_line}"
f"Simulation timestep = {self.dt:<10} {self.time_unit_disp} {new_line}"
f"----------------------------- {new_line}")
else:
# :<10 pads the self.value to be 10 characters wide
print_str = (f"The current attributes are: {new_line}"
f"----------------------------- {new_line}"
f"Current flux = {round(self.Q,3):<10} {self.flux_unit_disp} {new_line}"
f"Current pipe pressure = {round(p,3):<10} {self.pressure_unit_disp} {new_line}"
f"Current LA = {round(self.LA,4)*100:<10} {self.LA_unit_disp} {new_line}"
f"----------------------------- {new_line}")
print(print_str)
def get_Q_n(self):
# needed for Kraftwerk_class
return self.Q_n
# update methods
def update_LA(self,LA_soll):
# update the Leitappartöffnung and consider the restrictions of the closing time of the turbine
LA_diff = self.LA-LA_soll # calculate the difference to the target LA
LA_diff_max = self.d_LA_max_dt*self.dt # calculate the maximum possible change in LA based on the given timestep
LA_diff = np.sign(LA_diff)*np.min(np.abs([LA_diff,LA_diff_max])) # calulate the correct change in LA
# make sure that the LA is not out of the range [0;1]
LA_new = self.LA-LA_diff
if LA_new < 0.:
LA_new = 0.
elif LA_new > 1.:
LA_new = 1.
self.set_LA(LA_new,display_warning=False)
# methods
def converge(self,convergence_parameters):
# small numerical disturbances (~1e-12 m/s) in the velocity can get amplified at the turbine node, because the new velocity of the turbine and the
# new pressure from the forward characteristic are not perfectly compatible.
# Therefore, iterate the flux and the pressure so long, until they converge
eps = 1e-12 # convergence criterion: iteration change < eps
iteration_change = 1. # change in Q from one iteration to the next
i = 0 # safety variable. break loop if it exceeds 1e6 iterations
g = self.g # gravitational acceleration
p = convergence_parameters[0] # pressure at second to last node (see method of characterisctics - boundary condidtions)
v = convergence_parameters[1] # velocity at second to last node (see method of characterisctics - boundary condidtions)
D = convergence_parameters[2] # diameter of the pipeline
area_pipe = convergence_parameters[3] # area of the pipeline
alpha = convergence_parameters[4] # elevation angle of the pipeline
f_D = convergence_parameters[5] # Darcy friction coefficient
c = convergence_parameters[6] # pressure wave propagtation velocity
rho = convergence_parameters[7] # density of the liquid
dt = convergence_parameters[8] # timestep of the characteristic method
p_old = convergence_parameters[9] # pressure of previous timestep
Q_old = self.get_current_Q()
v_old = Q_old/area_pipe
while iteration_change > eps:
p_new = p-rho*c*(v_old-v)+rho*c*dt*g*np.sin(alpha)-f_D*rho*c*dt/(2*D)*abs(v)*v
# print(p_new)
p_new = p_old+(p_new-p_old)/3
# print(p_new)
self.set_pressure(p_new)
Q_new = self.get_current_Q()
v_new = Q_new/area_pipe
# print(Q_old,Q_new)
iteration_change = abs(Q_old-Q_new)
Q_old = Q_new.copy()
v_old = v_new.copy()
p_old = p_new.copy()
i = i+1
if i == 1e6:
print('did not converge')
break
# print(i)