class TestHeatPump: def setup(self): # %% network setup self.nw = Network(fluids=['water', 'NH3'], T_unit='C', p_unit='bar', h_unit='kJ / kg', m_unit='kg / s') # %% components # sources & sinks cc_coolant = CycleCloser('coolant cycle closer') cc_consumer = CycleCloser('consumer cycle closer') amb_in = Source('source ambient') amb_out = Sink('sink ambient') ic_in = Source('source intercool') ic_out = Sink('sink intercool') # consumer system cd = HeatExchanger('condenser') rp = Pump('recirculation pump') cons = HeatExchangerSimple('consumer') # evaporator system va = Valve('valve') dr = Drum('drum') ev = HeatExchanger('evaporator') su = HeatExchanger('superheater') pu = Pump('pump evaporator') # compressor-system cp1 = Compressor('compressor 1') cp2 = Compressor('compressor 2') he = HeatExchanger('intercooler') # busses self.power = Bus('total compressor power') self.power.add_comps({ 'comp': cp1, 'base': 'bus' }, { 'comp': cp2, 'base': 'bus' }) self.heat = Bus('total delivered heat') self.heat.add_comps({'comp': cd, 'char': -1}) self.nw.add_busses(self.power, self.heat) # %% connections # consumer system c_in_cd = Connection(cc_coolant, 'out1', cd, 'in1') cb_rp = Connection(cc_consumer, 'out1', rp, 'in1') rp_cd = Connection(rp, 'out1', cd, 'in2') self.cd_cons = Connection(cd, 'out2', cons, 'in1') cons_cf = Connection(cons, 'out1', cc_consumer, 'in1') self.nw.add_conns(c_in_cd, cb_rp, rp_cd, self.cd_cons, cons_cf) # connection condenser - evaporator system cd_va = Connection(cd, 'out1', va, 'in1') self.nw.add_conns(cd_va) # evaporator system va_dr = Connection(va, 'out1', dr, 'in1') dr_pu = Connection(dr, 'out1', pu, 'in1') pu_ev = Connection(pu, 'out1', ev, 'in2') ev_dr = Connection(ev, 'out2', dr, 'in2') dr_su = Connection(dr, 'out2', su, 'in2') self.nw.add_conns(va_dr, dr_pu, pu_ev, ev_dr, dr_su) self.amb_in_su = Connection(amb_in, 'out1', su, 'in1') su_ev = Connection(su, 'out1', ev, 'in1') ev_amb_out = Connection(ev, 'out1', amb_out, 'in1') self.nw.add_conns(self.amb_in_su, su_ev, ev_amb_out) # connection evaporator system - compressor system su_cp1 = Connection(su, 'out2', cp1, 'in1') self.nw.add_conns(su_cp1) # compressor-system cp1_he = Connection(cp1, 'out1', he, 'in1') he_cp2 = Connection(he, 'out1', cp2, 'in1') cp2_c_out = Connection(cp2, 'out1', cc_coolant, 'in1') ic_in_he = Connection(ic_in, 'out1', he, 'in2') he_ic_out = Connection(he, 'out2', ic_out, 'in1') self.nw.add_conns(cp1_he, he_cp2, ic_in_he, he_ic_out, cp2_c_out) # %% component parametrization # condenser system x = np.array([ 0, 0.0625, 0.125, 0.1875, 0.25, 0.3125, 0.375, 0.4375, 0.5, 0.5625, 0.6375, 0.7125, 0.7875, 0.9, 0.9875, 1, 1.0625, 1.125, 1.175, 1.2125, 1.2375, 1.25 ]) y = np.array([ 0.0076, 0.1390, 0.2731, 0.4003, 0.5185, 0.6263, 0.7224, 0.8056, 0.8754, 0.9312, 0.9729, 1.0006, 1.0203, 1.0158, 1.0051, 1.0000, 0.9746, 0.9289, 0.8832, 0.8376, 0.7843, 0.7614 ]) rp.set_attr(eta_s=0.8, design=['eta_s'], offdesign=['eta_s_char'], eta_s_char={ 'char_func': CharLine(x, y), 'param': 'm' }) cons.set_attr(pr=1, design=['pr'], offdesign=['zeta']) # evaporator system x = np.linspace(0, 2.5, 26) y = np.array([ 0.000, 0.164, 0.283, 0.389, 0.488, 0.581, 0.670, 0.756, 0.840, 0.921, 1.000, 1.078, 1.154, 1.228, 1.302, 1.374, 1.446, 1.516, 1.585, 1.654, 1.722, 1.789, 1.855, 1.921, 1.986, 2.051 ]) kA_char1 = {'char_func': CharLine(x, y), 'param': 'm'} x = np.array([ 0.0100, 0.0400, 0.0700, 0.1100, 0.1500, 0.2000, 0.2500, 0.3000, 0.3500, 0.4000, 0.4500, 0.5000, 0.5500, 0.6000, 0.6500, 0.7000, 0.7500, 0.8000, 0.8500, 0.9000, 0.9500, 1.0000, 1.5000, 2.0000 ]) y = np.array([ 0.0185, 0.0751, 0.1336, 0.2147, 0.2997, 0.4118, 0.5310, 0.6582, 0.7942, 0.9400, 0.9883, 0.9913, 0.9936, 0.9953, 0.9966, 0.9975, 0.9983, 0.9988, 0.9992, 0.9996, 0.9998, 1.0000, 1.0008, 1.0014 ]) kA_char2 = {'char_func': CharLine(x, y), 'param': 'm'} ev.set_attr(pr1=1, pr2=.999, ttd_l=5, design=['ttd_l'], offdesign=['kA_char'], kA_char1=kA_char1, kA_char2=kA_char2) # no kA modification for hot side! x = np.array([0, 1]) y = np.array([1, 1]) kA_char1 = {'char_func': CharLine(x, y), 'param': 'm'} # characteristic line for superheater kA x = np.array( [0, 0.045, 0.136, 0.244, 0.43, 0.6, 0.7, 0.8, 0.9, 1, 1.1, 1.2]) y = np.array( [0, 0.037, 0.112, 0.207, 0.5, 0.8, 0.85, 0.9, 0.95, 1, 1.04, 1.07]) kA_char2 = {'char_func': CharLine(x, y), 'param': 'm'} su.set_attr(kA_char1=kA_char1, kA_char2=kA_char2, offdesign=['zeta1', 'zeta2', 'kA_char']) x = np.array([ 0, 0.0625, 0.125, 0.1875, 0.25, 0.3125, 0.375, 0.4375, 0.5, 0.5625, 0.6375, 0.7125, 0.7875, 0.9, 0.9875, 1, 1.0625, 1.125, 1.175, 1.2125, 1.2375, 1.25 ]) y = np.array([ 0.0076, 0.1390, 0.2731, 0.4003, 0.5185, 0.6263, 0.7224, 0.8056, 0.8754, 0.9312, 0.9729, 1.0006, 1.0203, 1.0158, 1.0051, 1.0000, 0.9746, 0.9289, 0.8832, 0.8376, 0.7843, 0.7614 ]) pu.set_attr(eta_s=0.8, design=['eta_s'], offdesign=['eta_s_char'], eta_s_char={ 'char_func': CharLine(x, y), 'param': 'm' }) # compressor system x = np.array([0, 0.4, 1, 1.2]) y = np.array([0.5, 0.9, 1, 1.1]) cp1.set_attr(eta_s=0.8, design=['eta_s'], offdesign=['eta_s_char'], eta_s_char={ 'char_func': CharLine(x, y), 'param': 'm' }) cp2.set_attr(eta_s=0.8, design=['eta_s'], offdesign=['eta_s_char'], eta_s_char={ 'char_func': CharLine(x, y), 'param': 'm' }) # characteristic line for intercooler kA x = np.linspace(0, 2.5, 26) y = np.array([ 0.0000, 0.2455, 0.3747, 0.4798, 0.5718, 0.6552, 0.7323, 0.8045, 0.8727, 0.9378, 1.0000, 1.0599, 1.1176, 1.1736, 1.2278, 1.2806, 1.3320, 1.3822, 1.4313, 1.4792, 1.5263, 1.5724, 1.6176, 1.6621, 1.7058, 1.7488 ]) kA_char1 = {'char_func': CharLine(x, y), 'param': 'm'} x = np.linspace(0, 2.5, 26) y = np.array([ 0.000, 0.164, 0.283, 0.389, 0.488, 0.581, 0.670, 0.756, 0.840, 0.921, 1.000, 1.078, 1.154, 1.228, 1.302, 1.374, 1.446, 1.516, 1.585, 1.654, 1.722, 1.789, 1.855, 1.921, 1.986, 2.051 ]) kA_char2 = {'char_func': CharLine(x, y), 'param': 'm'} he.set_attr(kA_char1=kA_char1, kA_char2=kA_char2, offdesign=['zeta1', 'zeta2', 'kA_char']) # characteristic line for condenser kA x = np.linspace(0, 2.5, 26) y = np.array([ 0.0000, 0.2455, 0.3747, 0.4798, 0.5718, 0.6552, 0.7323, 0.8045, 0.8727, 0.9378, 1.0000, 1.0599, 1.1176, 1.1736, 1.2278, 1.2806, 1.3320, 1.3822, 1.4313, 1.4792, 1.5263, 1.5724, 1.6176, 1.6621, 1.7058, 1.7488 ]) kA_char1 = {'char_func': CharLine(x, y), 'param': 'm'} x = np.linspace(0, 2.5, 26) y = np.array([ 0.000, 0.164, 0.283, 0.389, 0.488, 0.581, 0.670, 0.756, 0.840, 0.921, 1.000, 1.078, 1.154, 1.228, 1.302, 1.374, 1.446, 1.516, 1.585, 1.654, 1.722, 1.789, 1.855, 1.921, 1.986, 2.051 ]) kA_char2 = {'char_func': CharLine(x, y), 'param': 'm'} cd.set_attr(kA_char1=kA_char1, kA_char2=kA_char2, pr2=0.9998, design=['pr2'], offdesign=['zeta2', 'kA_char']) # %% connection parametrization # condenser system c_in_cd.set_attr(fluid={'water': 0, 'NH3': 1}, p=60) rp_cd.set_attr(T=60, fluid={'water': 1, 'NH3': 0}, p=10) self.cd_cons.set_attr(T=105) cd_va.set_attr(p=Ref(c_in_cd, 1, -0.01), Td_bp=-5, design=['Td_bp']) # evaporator system cold side pu_ev.set_attr(m=Ref(va_dr, 10, 0), p0=5) dr_su.set_attr(p0=5, T=5) su_cp1.set_attr(p=Ref(dr_su, 1, -0.05), Td_bp=5, design=['Td_bp', 'p']) # evaporator system hot side self.amb_in_su.set_attr(m=20, T=12, p=1, fluid={'water': 1, 'NH3': 0}) su_ev.set_attr(p=Ref(self.amb_in_su, 1, -0.001), design=['p']) ev_amb_out.set_attr() # compressor-system cp1_he.set_attr(p=15) he_cp2.set_attr(T=40, p=Ref(cp1_he, 1, -0.01), design=['T', 'p']) ic_in_he.set_attr(p=1, T=20, m=5, fluid={'water': 1, 'NH3': 0}) he_ic_out.set_attr(p=Ref(ic_in_he, 1, -0.002), design=['p']) def test_model(self): """ Test the operating points of the heat pump against a different model. By now, not all characteristic functions of the original model are available in detail, thus perfect matching is not possible! """ self.nw.solve('design') self.nw.save('tmp') self.nw.print_results() # input values from ebsilon T = [105, 100, 90, 80] m_source = np.array([[23, 22, 20, 18, 16], [27, 24, 20, 16, 12], [31, 25, 20, 15, 10], [33, 26, 20, 15, 10]]) COP = np.array([[2.436, 2.414, 2.368, 2.338, 2.287], [2.591, 2.523, 2.448, 2.355, 2.216], [2.777, 2.635, 2.557, 2.442, 2.243], [2.866, 2.711, 2.629, 2.528, 2.351]]) i = 0 for T in T: j = 0 self.cd_cons.set_attr(T=T) for m in m_source[i]: self.amb_in_su.set_attr(m=m) if j == 0: self.nw.solve('offdesign', design_path='tmp', init_path='tmp') else: self.nw.solve('offdesign', design_path='tmp') # relative deviation should not exceed 6.5 % # this should be much less, unfortunately not all ebsilon # characteristics are available, thus it is # difficult/impossible to match the models perfectly! d_rel_COP = abs(self.heat.P.val / self.power.P.val - COP[i, j]) / COP[i, j] msg = ('The deviation in COP should be less than 0.065, is ' + str(d_rel_COP) + ' at mass flow ' + str(m) + ' and temperature ' + str(T) + '.') assert d_rel_COP < 0.065, msg j += 1 i += 1 shutil.rmtree('./tmp', ignore_errors=True)
dh_c.set_attr(T=60, p=5, fluid={ 'CO2': 0, 'Ar': 0, 'N2': 0, 'O2': 0, 'H2O': 1, 'CH4': 0 }) dh_w.set_attr(T=90) # %% nw.solve(mode='design') nw.print_results() nw.save('design_point') document_model(nw, filename='report_design.tex') power.set_attr(P=-100e6) nw.solve(mode='offdesign', init_path='design_point', design_path='design_point') nw.print_results() document_model(nw, filename='report_offdesign.tex') power.set_attr(P=1 / 0.9 * 0.8 * power.P.val) nw.solve(mode='offdesign', design_path='design_point') nw.print_results()
class TestPiping: def setup_piping_network(self, instance): self.nw = Network(['CH4'], T_unit='C', p_unit='bar') self.source = Source('source') self.sink = Sink('sink') self.c1 = Connection(self.source, 'out1', instance, 'in1') self.c2 = Connection(instance, 'out1', self.sink, 'in1') self.nw.add_conns(self.c1, self.c2) def test_Valve(self): """Test component properties of valves.""" instance = Valve('valve') self.setup_piping_network(instance) # parameter specification self.c1.set_attr(fluid={'CH4': 1}, m=10, p=10, T=120) self.c2.set_attr(p=1) # test variable pressure ration instance.set_attr(pr='var') self.nw.solve('design') convergence_check(self.nw.lin_dep) pr = round(self.c2.p.val_SI / self.c1.p.val_SI, 2) msg = ('Value of pressure ratio must be ' + str(pr) + ', is ' + str(round(instance.pr.val, 2)) + '.') assert pr == round(instance.pr.val, 2), msg # test variable zeta value zeta = round(instance.zeta.val, 0) instance.set_attr(zeta='var', pr=None) self.nw.solve('design') convergence_check(self.nw.lin_dep) msg = ('Value of dimension independent zeta value must be ' + str(zeta) + ', is ' + str(round(instance.zeta.val, 0)) + '.') assert zeta == round(instance.zeta.val, 0), msg # dp char x = np.array([8, 9, 10, 11, 12]) y = np.array([5, 8, 9, 9.5, 9.6]) * 1e5 dp_char = CharLine(x, y) instance.set_attr(zeta=None, dp_char={ 'char_func': dp_char, 'is_set': True }) m = 11 self.c1.set_attr(m=m) self.c2.set_attr(p=np.nan) self.nw.solve('design') convergence_check(self.nw.lin_dep) self.nw.print_results() dp = round(-dp_char.evaluate(m), 0) dp_act = round(self.c2.p.val_SI - self.c1.p.val_SI) msg = ('The pressure drop at the valve should be ' + str(dp) + ' but ' 'is ' + str(dp_act) + '.') assert dp == dp_act, msg def test_Pipe(self): """Test component properties of pipe.""" instance = Pipe('pipe') self.setup_piping_network(instance)