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SystemSimulationApp/app/simulation/components/amesim/flow/orifices.py
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from __future__ import annotations
from functools import lru_cache
from collections.abc import Mapping
from math import isclose, log, sqrt, tanh
from app.simulation.components.amesim.gases import (
AMESIM_GAS_INDEX_PARAMETER,
normalize_amesim_gas_index,
)
from app.simulation.core.base import AlgebraicComponent
from app.simulation.core.catalog import (
ComponentDisplaySpec,
ParameterGroupDisplaySpec,
PortDisplaySpec,
)
from app.simulation.core.equations import EquationResidual
from app.simulation.core.metadata import (
ParameterCondition,
ParameterDefinition,
ParameterOption,
ResultVariableDefinition,
)
from app.simulation.core.medium import GasMedium
from app.simulation.core.ports import PortDefinition
_FLOW_COEFFICIENT_OPTIONS = (
ParameterOption(1.0, "Cq"),
ParameterOption(2.0, "Cv"),
ParameterOption(3.0, "Kv"),
)
_FLOWSET_USES_CQ = (ParameterCondition("flowset", (1.0,)),)
_FLOWSET_USES_CV = (ParameterCondition("flowset", (2.0,)),)
_FLOWSET_USES_KV = (ParameterCondition("flowset", (3.0,)),)
_PN_PRESSURE_RATIO_ACCURACY = 0.9999
_PN_LAMINAR_SMOOTHING_GAIN = 12.0
_PNOR001_FLOW_COEFFICIENT_GROUP = ParameterGroupDisplaySpec(
id="flow_coefficient",
label="流量系数",
parameters=("cq", "area", "Cv", "Kv"),
order=10,
)
_PNVO001_FLOW_COEFFICIENT_GROUP = ParameterGroupDisplaySpec(
id="flow_coefficient",
label="流量系数",
parameters=("cq", "area0", "Cv", "Kv"),
order=10,
)
class AmesimPnor001(AlgebraicComponent):
"""AMESim PNOR001 constant-flow-coefficient pneumatic orifice.
This public component preserves the PNOR001 catalog/XML contract and uses
real-gas pressure-ratio flow with AMESim-style near-equal-pressure smoothing.
"""
MODEL_TYPE = "amesim_pnor001"
MODEL_VERSION = "0.3.0"
PORTS = (
PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_2", nominal_role="bidirectional"),
)
PARAMETERS = (
AMESIM_GAS_INDEX_PARAMETER,
ParameterDefinition(
"cq",
0.72,
label="流量系数 Cq",
quantity="dimensionless",
unit="",
minimum=1.0e-10,
maximum=1.0,
description="孔口实际质量流量相对于理想可压缩流量的无量纲修正系数。",
visible_when=_FLOWSET_USES_CQ,
),
ParameterDefinition(
"area",
5.0e-6,
label="孔口面积",
quantity="area",
unit="m2",
minimum=0.0,
maximum=1.0,
description="选择 Cq/面积方式时用于流量计算的有效孔口面积。",
visible_when=_FLOWSET_USES_CQ,
),
ParameterDefinition(
"Cv",
0.5,
label="流量系数 Cv",
quantity="dimensionless",
unit="",
minimum=0.0,
description="选择 Cv 方式时使用的英制流量系数。",
visible_when=_FLOWSET_USES_CV,
),
ParameterDefinition(
"Kv",
0.4,
label="流量系数 Kv",
quantity="dimensionless",
unit="",
minimum=0.0,
description="选择 Kv 方式时使用的公制流量系数。",
visible_when=_FLOWSET_USES_KV,
),
ParameterDefinition(
"flowset",
1.0,
label="流量系数设置",
quantity="dimensionless",
unit="",
minimum=1.0,
maximum=3.0,
editor="choice",
options=_FLOW_COEFFICIENT_OPTIONS,
description="流量参数方式:1 使用 Cq 和面积,2 使用 Cv,3 使用 Kv。",
),
)
RESULT_VARIABLES = (
ResultVariableDefinition(
"cm",
label="质量流量参数",
quantity="dimensionless",
unit="",
category="derived",
order=10,
),
ResultVariableDefinition(
"gasvel",
label="缩流截面气体速度",
quantity="velocity",
unit="m/s",
category="derived",
order=20,
),
)
DISPLAY = ComponentDisplaySpec(
label="PNOR001 常系数气动孔口",
library_id="amesim",
category_id="flow",
symbol="amesim_pnor001",
ports=(
PortDisplaySpec("port_1", "left", order=10),
PortDisplaySpec("port_2", "right", order=20),
),
order=10,
parameter_groups=(_PNOR001_FLOW_COEFFICIENT_GROUP,),
)
def __init__(
self,
name: str,
medium: GasMedium,
*,
cq: float = 0.72,
area: float = 5.0e-6,
Cv: float = 0.5,
Kv: float = 0.4,
gi: float = 1.0,
flowset: float = 1.0,
) -> None:
super().__init__(name=name)
self.set_parameter_values(
{
"cq": cq,
"area": area,
"Cv": Cv,
"Kv": Kv,
"gi": gi,
"flowset": flowset,
}
)
self.medium = medium
self.cq = float(cq)
self.area = float(area)
self.Cv = float(Cv)
self.Kv = float(Kv)
self.gi = normalize_amesim_gas_index(gi)
self.flowset = self._integer_parameter("flowset", flowset)
if self.flowset not in {1, 2, 3}:
raise ValueError("PNOR001 flowset must be 1, 2, or 3.")
initial_h = medium.specific_enthalpy(medium.T_ref)
self.port_1 = self.register_declared_port("port_1")
self.port_1.h_outflow = initial_h
self.port_2 = self.register_declared_port("port_2")
self.port_2.h_outflow = initial_h
self._connected_h: dict[str, float] = {}
@staticmethod
def _integer_parameter(name: str, value: float) -> int:
rounded = round(value)
if not isclose(value, rounded, rel_tol=0.0, abs_tol=1.0e-12):
raise ValueError(f"PNOR001 parameter {name} must be an integer value.")
return int(rounded)
@classmethod
def create(
cls,
*,
name: str,
medium: GasMedium,
parameters: Mapping[str, float],
) -> AmesimPnor001:
return cls(
name=name,
medium=medium,
cq=parameters["cq"],
area=parameters["area"],
Cv=parameters["Cv"],
Kv=parameters["Kv"],
gi=parameters["gi"],
flowset=parameters["flowset"],
)
@property
def effective_cq(self) -> float:
return self.cq if self.flowset == 1 else 0.72
@property
def effective_area(self) -> float:
if self.flowset == 1:
return self.area
if self.flowset == 2:
return self._area_from_cv(self.Cv, self.effective_cq)
return self._area_from_kv(self.Kv, self.effective_cq)
@staticmethod
def _area_from_cv(Cv: float, cq: float) -> float:
water_density = 999.0
reference_flow_m3_s = Cv * 6.30901964e-5
reference_dp_pa = 6894.75729
return reference_flow_m3_s / (cq * sqrt(2.0 * reference_dp_pa / water_density))
@staticmethod
def _area_from_kv(Kv: float, cq: float) -> float:
water_density = 999.0
reference_flow_m3_s = Kv / 3600.0
reference_dp_pa = 100000.0
return reference_flow_m3_s / (cq * sqrt(2.0 * reference_dp_pa / water_density))
def _upstream_temperature(self, port_name: str) -> float:
port = self.get_port(port_name)
inlet_h = self._connected_h.get(port_name, port.h_outflow)
return max(
self.medium.temperature_from_pressure_enthalpy(
max(port.p, 1.0),
inlet_h,
),
1.0,
)
@staticmethod
def _subsonic_mass_flow_parameter(
*,
pressure_ratio: float,
gamma_s: float,
density: float,
upstream_temperature: float,
upstream_pressure: float,
) -> float:
expansion = (
pressure_ratio ** (2.0 * gamma_s)
- pressure_ratio ** (1.0 + gamma_s)
)
return sqrt(
max(
2.0
/ (1.0 - gamma_s)
* density
* upstream_temperature
/ upstream_pressure
* expansion,
0.0,
)
)
@lru_cache(maxsize=32768)
def _one_way_flow_characteristics(
self,
*,
upstream_pressure: float,
downstream_pressure: float,
upstream_temperature: float,
) -> tuple[float, float]:
p_up = max(upstream_pressure, 1.0)
p_down = max(min(downstream_pressure, p_up), 0.0)
T_up = max(upstream_temperature, 1.0)
gamma_s = self.medium.isentropic_density_pressure_factor(
p_up,
T_up,
p_down,
)
gamma_s = min(max(gamma_s, 1.0e-9), 1.0 - 1.0e-9)
density = max(self.medium.density(p_up, T_up), 1.0e-12)
pressure_ratio = max(p_down / p_up, 0.0)
critical_ratio = (2.0 * gamma_s / (gamma_s + 1.0)) ** (
1.0 / (1.0 - gamma_s)
)
if pressure_ratio <= critical_ratio:
effective_pressure_ratio = critical_ratio
mass_flow_parameter = (
sqrt(2.0 / (1.0 + gamma_s) * density * T_up / p_up)
* (2.0 * gamma_s / (gamma_s + 1.0))
** (gamma_s / (1.0 - gamma_s))
)
gas_velocity = sqrt(2.0 / (1.0 + gamma_s) * p_up / density)
else:
effective_pressure_ratio = pressure_ratio
mass_flow_parameter = self._subsonic_mass_flow_parameter(
pressure_ratio=pressure_ratio,
gamma_s=gamma_s,
density=density,
upstream_temperature=T_up,
upstream_pressure=p_up,
)
gas_velocity = sqrt(
max(
2.0
/ (1.0 - gamma_s)
* p_up
/ density
* (1.0 - pressure_ratio ** (1.0 - gamma_s)),
0.0,
)
)
reference = self._subsonic_mass_flow_parameter(
pressure_ratio=_PN_PRESSURE_RATIO_ACCURACY,
gamma_s=gamma_s,
density=density,
upstream_temperature=T_up,
upstream_pressure=p_up,
)
if mass_flow_parameter > 0.0 and reference > 0.0:
argument = (
_PN_LAMINAR_SMOOTHING_GAIN
* abs(mass_flow_parameter / reference)
* log(effective_pressure_ratio)
/ log(_PN_PRESSURE_RATIO_ACCURACY)
)
smoothing_factor = tanh(max(argument, 0.0))
mass_flow_parameter *= smoothing_factor
gas_velocity *= smoothing_factor
return mass_flow_parameter, gas_velocity
def mass_flow(self, p_1: float, p_2: float) -> float:
if (
isclose(p_1, p_2, rel_tol=0.0, abs_tol=1.0e-8)
or self.effective_area == 0.0
):
return 0.0
if p_1 > p_2:
return self._one_way_mass_flow(
upstream_pressure=p_1,
downstream_pressure=p_2,
upstream_temperature=self._upstream_temperature("port_1"),
)
return -self._one_way_mass_flow(
upstream_pressure=p_2,
downstream_pressure=p_1,
upstream_temperature=self._upstream_temperature("port_2"),
)
def _one_way_mass_flow(
self,
*,
upstream_pressure: float,
downstream_pressure: float,
upstream_temperature: float,
) -> float:
p_up = max(upstream_pressure, 1.0)
T_up = max(upstream_temperature, 1.0)
mass_flow_parameter, _ = self._one_way_flow_characteristics(
upstream_pressure=p_up,
downstream_pressure=downstream_pressure,
upstream_temperature=T_up,
)
return (
self.effective_cq
* self.effective_area
* p_up
* mass_flow_parameter
/ sqrt(T_up)
)
def component_result_values(self) -> Mapping[str, float]:
p_1 = max(self.port_1.p, 1.0)
p_2 = max(self.port_2.p, 1.0)
if p_1 >= p_2:
upstream_port_name = "port_1"
upstream_pressure = p_1
downstream_pressure = p_2
flow_direction = 1.0
else:
upstream_port_name = "port_2"
upstream_pressure = p_2
downstream_pressure = p_1
flow_direction = -1.0
mass_flow_parameter, gas_velocity = self._one_way_flow_characteristics(
upstream_pressure=upstream_pressure,
downstream_pressure=downstream_pressure,
upstream_temperature=self._upstream_temperature(upstream_port_name),
)
return {
"cm": mass_flow_parameter,
"gasvel": flow_direction * gas_velocity,
}
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
return (
EquationResidual(
id=f"{self.name}:mass_flow_balance",
owner="component",
owner_id=self.name,
relation="sumToZero",
variables=(
f"{self.name}.port_1.m_flow",
f"{self.name}.port_2.m_flow",
),
role="flow",
value=self.port_1.m_flow + self.port_2.m_flow,
),
EquationResidual(
id=f"{self.name}:pressure_flow_relation",
owner="component",
owner_id=self.name,
relation="constitutive",
variables=(
f"{self.name}.port_1.p",
f"{self.name}.port_2.p",
f"{self.name}.port_1.m_flow",
),
role="flow",
value=self.port_1.m_flow
- self.mass_flow(self.port_1.p, self.port_2.p),
),
)
def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
self._connected_h = dict(connected_h)
self.port_1.h_outflow = connected_h["port_2"]
self.port_2.h_outflow = connected_h["port_1"]
class AmesimPnvo001FixedOpening(AlgebraicComponent):
"""Fixed-opening public variant of AMESim PNVO001.
Full PNVO001 has a signal input port. The current public component library
does not support signal simulation, so this model exposes the pneumatic
ports and replaces the signal with a normalized `opening` parameter.
"""
MODEL_TYPE = "amesim_pnvo001_fixed"
MODEL_VERSION = "0.2.0"
PORTS = (
PortDefinition.pneumatic("port_2", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_3", nominal_role="bidirectional"),
)
PARAMETERS = (
AMESIM_GAS_INDEX_PARAMETER,
ParameterDefinition(
"cq",
0.72,
label="流量系数 Cq",
quantity="dimensionless",
unit="",
minimum=1.0e-10,
maximum=1.0,
description="孔口实际质量流量相对于理想可压缩流量的无量纲修正系数。",
visible_when=_FLOWSET_USES_CQ,
),
ParameterDefinition(
"area0",
5.0e-6,
label="最大孔口面积",
quantity="area",
unit="m2",
minimum=0.0,
maximum=1.0,
description="阀门完全开启时的最大有效孔口面积。",
visible_when=_FLOWSET_USES_CQ,
),
ParameterDefinition(
"Cv",
0.5,
label="最大流量系数 Cv",
quantity="dimensionless",
unit="",
minimum=0.0,
description="选择 Cv 方式时使用的最大英制流量系数。",
visible_when=_FLOWSET_USES_CV,
),
ParameterDefinition(
"Kv",
0.4,
label="最大流量系数 Kv",
quantity="dimensionless",
unit="",
minimum=0.0,
description="选择 Kv 方式时使用的最大公制流量系数。",
visible_when=_FLOWSET_USES_KV,
),
ParameterDefinition(
"flowset",
1.0,
label="流量系数设置",
quantity="dimensionless",
unit="",
minimum=1.0,
maximum=3.0,
editor="choice",
options=_FLOW_COEFFICIENT_OPTIONS,
description="流量参数方式:1 使用 Cq 和面积,2 使用 Cv,3 使用 Kv。",
),
ParameterDefinition(
"opening",
1.0,
label="固定开度",
quantity="dimensionless",
unit="",
minimum=0.0,
maximum=1.0,
description="固定的归一化阀门开度;0 表示关闭,1 表示完全开启。",
),
)
RESULT_VARIABLES = (
ResultVariableDefinition(
"xv",
label="有效开度",
quantity="dimensionless",
unit="",
category="derived",
order=10,
),
ResultVariableDefinition(
"cm",
label="质量流量参数",
quantity="dimensionless",
unit="",
category="derived",
order=20,
),
ResultVariableDefinition(
"gasvel",
label="缩流截面气体速度",
quantity="velocity",
unit="m/s",
category="derived",
order=30,
),
)
DISPLAY = ComponentDisplaySpec(
label="PNVO001 固定开度气动孔口",
library_id="amesim",
category_id="flow",
symbol="amesim_pnvo001_fixed",
ports=(
PortDisplaySpec("port_2", "left", order=10),
PortDisplaySpec("port_3", "right", order=20),
),
order=30,
parameter_groups=(_PNVO001_FLOW_COEFFICIENT_GROUP,),
)
def __init__(
self,
name: str,
medium: GasMedium,
*,
cq: float = 0.72,
area0: float = 5.0e-6,
Cv: float = 0.5,
Kv: float = 0.4,
gi: float = 1.0,
flowset: float = 1.0,
opening: float = 1.0,
) -> None:
super().__init__(name=name)
self.set_parameter_values(
{
"cq": cq,
"area0": area0,
"Cv": Cv,
"Kv": Kv,
"gi": gi,
"flowset": flowset,
"opening": opening,
}
)
self.medium = medium
self.cq = float(cq)
self.area0 = float(area0)
self.Cv = float(Cv)
self.Kv = float(Kv)
self.gi = normalize_amesim_gas_index(gi)
self.flowset = self._integer_parameter("flowset", flowset)
if self.flowset not in {1, 2, 3}:
raise ValueError("PNVO001 fixed-opening flowset must be 1, 2, or 3.")
self.opening = min(1.0, max(0.0, float(opening)))
initial_h = medium.specific_enthalpy(medium.T_ref)
self.port_2 = self.register_declared_port("port_2")
self.port_2.h_outflow = initial_h
self.port_3 = self.register_declared_port("port_3")
self.port_3.h_outflow = initial_h
self._connected_h: dict[str, float] = {}
@staticmethod
def _integer_parameter(name: str, value: float) -> int:
rounded = round(value)
if not isclose(value, rounded, rel_tol=0.0, abs_tol=1.0e-12):
raise ValueError(f"PNVO001 fixed-opening parameter {name} must be an integer value.")
return int(rounded)
@classmethod
def create(
cls,
*,
name: str,
medium: GasMedium,
parameters: Mapping[str, float],
) -> AmesimPnvo001FixedOpening:
return cls(
name=name,
medium=medium,
cq=parameters["cq"],
area0=parameters["area0"],
Cv=parameters["Cv"],
Kv=parameters["Kv"],
gi=parameters["gi"],
flowset=parameters["flowset"],
opening=parameters["opening"],
)
@property
def effective_cq(self) -> float:
return self.cq if self.flowset == 1 else 0.72
@property
def maximum_area(self) -> float:
if self.flowset == 1:
return self.area0
if self.flowset == 2:
return AmesimPnor001._area_from_cv(self.Cv, self.effective_cq)
return AmesimPnor001._area_from_kv(self.Kv, self.effective_cq)
@property
def effective_area(self) -> float:
return self.opening * self.maximum_area
def _upstream_temperature(self, port_name: str) -> float:
port = self.get_port(port_name)
# A component port's h_outflow describes fluid leaving the valve; the
# upstream state comes from the connection on that same physical side.
inlet_h = self._connected_h.get(port_name, port.h_outflow)
return max(
self.medium.temperature_from_pressure_enthalpy(
max(port.p, 1.0),
inlet_h,
),
1.0,
)
@staticmethod
def _subsonic_mass_flow_parameter(
*,
pressure_ratio: float,
gamma_s: float,
density: float,
upstream_temperature: float,
upstream_pressure: float,
) -> float:
expansion = (
pressure_ratio ** (2.0 * gamma_s)
- pressure_ratio ** (1.0 + gamma_s)
)
return sqrt(
max(
2.0
/ (1.0 - gamma_s)
* density
* upstream_temperature
/ upstream_pressure
* expansion,
0.0,
)
)
def mass_flow(self, p_2: float, p_3: float) -> float:
if (
isclose(p_2, p_3, rel_tol=1.0e-7, abs_tol=1.0e-9)
or self.effective_area == 0.0
):
return 0.0
if p_2 > p_3:
return self._one_way_mass_flow(
upstream_pressure=p_2,
downstream_pressure=p_3,
upstream_temperature=self._upstream_temperature("port_2"),
)
return -self._one_way_mass_flow(
upstream_pressure=p_3,
downstream_pressure=p_2,
upstream_temperature=self._upstream_temperature("port_3"),
)
def _one_way_flow_characteristics(
self,
*,
upstream_pressure: float,
downstream_pressure: float,
upstream_temperature: float,
) -> tuple[float, float]:
p_up = max(upstream_pressure, 1.0)
p_down = max(min(downstream_pressure, p_up), 0.0)
T_up = max(upstream_temperature, 1.0)
gamma_s = self.medium.isentropic_density_pressure_factor(
p_up,
T_up,
p_down,
)
gamma_s = min(max(gamma_s, 1.0e-9), 1.0 - 1.0e-9)
density = max(self.medium.density(p_up, T_up), 1.0e-12)
pressure_ratio = max(p_down / p_up, 0.0)
critical_ratio = (2.0 * gamma_s / (gamma_s + 1.0)) ** (
1.0 / (1.0 - gamma_s)
)
if pressure_ratio <= critical_ratio:
effective_pressure_ratio = critical_ratio
mass_flow_parameter = (
sqrt(2.0 / (1.0 + gamma_s) * density * T_up / p_up)
* (2.0 * gamma_s / (gamma_s + 1.0))
** (gamma_s / (1.0 - gamma_s))
)
gas_velocity = sqrt(
2.0 / (1.0 + gamma_s) * p_up / density
)
else:
effective_pressure_ratio = pressure_ratio
mass_flow_parameter = self._subsonic_mass_flow_parameter(
pressure_ratio=pressure_ratio,
gamma_s=gamma_s,
density=density,
upstream_temperature=T_up,
upstream_pressure=p_up,
)
gas_velocity = sqrt(
max(
2.0
/ (1.0 - gamma_s)
* p_up
/ density
* (1.0 - pressure_ratio ** (1.0 - gamma_s)),
0.0,
)
)
# AMESim's gas_cm_prc_ applies this factor continuously over the
# complete pressure-ratio range. It is effectively one outside the
# near-equal-pressure region and makes Cm (and vena-contracta
# velocity) approach zero quadratically as the pressure ratio tends
# to one. The reference Cm intentionally reuses the current gamma_s.
reference_mass_flow_parameter = self._subsonic_mass_flow_parameter(
pressure_ratio=_PN_PRESSURE_RATIO_ACCURACY,
gamma_s=gamma_s,
density=density,
upstream_temperature=T_up,
upstream_pressure=p_up,
)
if mass_flow_parameter > 0.0 and reference_mass_flow_parameter > 0.0:
smoothing_argument = (
_PN_LAMINAR_SMOOTHING_GAIN
* abs(mass_flow_parameter / reference_mass_flow_parameter)
* log(effective_pressure_ratio)
/ log(_PN_PRESSURE_RATIO_ACCURACY)
)
smoothing_factor = tanh(max(smoothing_argument, 0.0))
mass_flow_parameter *= smoothing_factor
gas_velocity *= smoothing_factor
return mass_flow_parameter, gas_velocity
def _one_way_mass_flow(
self,
*,
upstream_pressure: float,
downstream_pressure: float,
upstream_temperature: float,
) -> float:
p_up = max(upstream_pressure, 1.0)
T_up = max(upstream_temperature, 1.0)
mass_flow_parameter, _gas_velocity = self._one_way_flow_characteristics(
upstream_pressure=p_up,
downstream_pressure=downstream_pressure,
upstream_temperature=T_up,
)
return (
self.effective_cq
* self.effective_area
* p_up
* mass_flow_parameter
/ sqrt(T_up)
)
def component_result_values(self) -> Mapping[str, float]:
p_2 = max(self.port_2.p, 1.0)
p_3 = max(self.port_3.p, 1.0)
if p_2 >= p_3:
upstream_port_name = "port_2"
upstream_pressure = p_2
downstream_pressure = p_3
flow_direction = 1.0
else:
upstream_port_name = "port_3"
upstream_pressure = p_3
downstream_pressure = p_2
flow_direction = -1.0
upstream_temperature = self._upstream_temperature(
upstream_port_name
)
mass_flow_parameter, gas_velocity = self._one_way_flow_characteristics(
upstream_pressure=upstream_pressure,
downstream_pressure=downstream_pressure,
upstream_temperature=upstream_temperature,
)
return {
"xv": self.opening,
"cm": mass_flow_parameter,
"gasvel": flow_direction * gas_velocity,
}
def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
return (
EquationResidual(
id=f"{self.name}:mass_flow_balance",
owner="component",
owner_id=self.name,
relation="sumToZero",
variables=(
f"{self.name}.port_2.m_flow",
f"{self.name}.port_3.m_flow",
),
role="flow",
value=self.port_2.m_flow + self.port_3.m_flow,
),
EquationResidual(
id=f"{self.name}:pressure_flow_relation",
owner="component",
owner_id=self.name,
relation="constitutive",
variables=(
f"{self.name}.port_2.p",
f"{self.name}.port_3.p",
f"{self.name}.port_2.m_flow",
),
role="flow",
value=self.port_2.m_flow
- self.mass_flow(self.port_2.p, self.port_3.p),
),
)
def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
self._connected_h = dict(connected_h)
self.port_2.h_outflow = connected_h["port_3"]
self.port_3.h_outflow = connected_h["port_2"]
class AmesimPnvo001SignalOpening(AmesimPnvo001FixedOpening):
"""AMESim PNVO001 signal-controlled pneumatic orifice."""
MODEL_TYPE = "amesim_pnvo001"
MODEL_VERSION = "0.2.0"
PORTS = (
PortDefinition.signal("res", nominal_role="input"),
PortDefinition.pneumatic("port_2", nominal_role="bidirectional"),
PortDefinition.pneumatic("port_3", nominal_role="bidirectional"),
)
PARAMETERS = (
AMESIM_GAS_INDEX_PARAMETER,
ParameterDefinition(
"cq",
0.72,
label="流量系数 Cq",
quantity="dimensionless",
unit="",
minimum=1.0e-10,
maximum=1.0,
description="孔口实际质量流量相对于理想可压缩流量的无量纲修正系数。",
visible_when=_FLOWSET_USES_CQ,
),
ParameterDefinition(
"area0",
5.0e-6,
label="最大孔口面积",
quantity="area",
unit="m2",
minimum=0.0,
maximum=1.0,
description="阀门完全开启时的最大有效孔口面积。",
visible_when=_FLOWSET_USES_CQ,
),
ParameterDefinition(
"Cv",
0.5,
label="最大流量系数 Cv",
quantity="dimensionless",
unit="",
minimum=0.0,
description="选择 Cv 方式时使用的最大英制流量系数。",
visible_when=_FLOWSET_USES_CV,
),
ParameterDefinition(
"Kv",
0.4,
label="最大流量系数 Kv",
quantity="dimensionless",
unit="",
minimum=0.0,
description="选择 Kv 方式时使用的最大公制流量系数。",
visible_when=_FLOWSET_USES_KV,
),
ParameterDefinition(
"flowset",
1.0,
label="流量系数设置",
quantity="dimensionless",
unit="",
minimum=1.0,
maximum=3.0,
editor="choice",
options=_FLOW_COEFFICIENT_OPTIONS,
description="流量参数方式:1 使用 Cq 和面积,2 使用 Cv,3 使用 Kv。",
),
ParameterDefinition(
"opening0",
1.0,
label="初始开度",
quantity="dimensionless",
unit="",
minimum=0.0,
maximum=1.0,
description="信号尚未传播时使用的归一化初始开度;0 表示关闭,1 表示完全开启。",
),
)
RESULT_VARIABLES = AmesimPnvo001FixedOpening.RESULT_VARIABLES
DISPLAY = ComponentDisplaySpec(
label="PNVO001 信号开度气动孔口",
library_id="amesim",
category_id="flow",
symbol="amesim_pnvo001",
ports=(
PortDisplaySpec("res", "left", order=5),
PortDisplaySpec("port_2", "left", order=10),
PortDisplaySpec("port_3", "right", order=20),
),
order=35,
parameter_groups=(_PNVO001_FLOW_COEFFICIENT_GROUP,),
)
def __init__(
self,
name: str,
medium: GasMedium,
*,
cq: float = 0.72,
area0: float = 5.0e-6,
Cv: float = 0.5,
Kv: float = 0.4,
gi: float = 1.0,
flowset: float = 1.0,
opening0: float = 1.0,
) -> None:
AlgebraicComponent.__init__(self, name=name)
self.set_parameter_values(
{
"cq": cq,
"area0": area0,
"Cv": Cv,
"Kv": Kv,
"gi": gi,
"flowset": flowset,
"opening0": opening0,
}
)
self.medium = medium
self.cq = float(cq)
self.area0 = float(area0)
self.Cv = float(Cv)
self.Kv = float(Kv)
self.gi = normalize_amesim_gas_index(gi)
self.flowset = self._integer_parameter("flowset", flowset)
if self.flowset not in {1, 2, 3}:
raise ValueError("PNVO001 signal-opening flowset must be 1, 2, or 3.")
self.opening0 = min(1.0, max(0.0, float(opening0)))
self.res = self.register_declared_port("res")
self.res.signal = self.opening0
initial_h = medium.specific_enthalpy(medium.T_ref)
self.port_2 = self.register_declared_port("port_2")
self.port_2.h_outflow = initial_h
self.port_3 = self.register_declared_port("port_3")
self.port_3.h_outflow = initial_h
self._connected_h: dict[str, float] = {}
@classmethod
def create(
cls,
*,
name: str,
medium: GasMedium,
parameters: Mapping[str, float],
) -> "AmesimPnvo001SignalOpening":
return cls(name=name, medium=medium, **dict(parameters))
@property
def opening(self) -> float:
return min(1.0, max(0.0, self.res.signal))