实现test_mql PNL0001管路动态

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huojiarong committed 2026-07-17 03:28:36 +00:00
1 parent 2d33a8f4bc
commit 1193b2dcee
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@@ -3859,6 +3859,7 @@ class TestMqlSystem:
def __init__(self, archive_path: Path | None = None) -> None:
self.archive_path = archive_path or Path(__file__).resolve().parents[2] / AMESIM_ARCHIVE_RELATIVE_PATH
self.network = SimulationNetwork(name=MODEL_NAME)
self.pnl0001_assembly = self._build_pnl0001_assembly()
self.pneumatic_assembly = self._build_pneumatic_assembly()
pneumatic_components = self._pneumatic_components_by_alias()
for spec in COMPONENT_SPECS:
@@ -3881,6 +3882,13 @@ class TestMqlSystem:
return build_test_mql_pneumatic_assembly()
def _build_pnl0001_assembly(self):
from PythonModels.systems.test_mql_pneumatic_lines import (
build_test_mql_pnl0001_assembly,
)
return build_test_mql_pnl0001_assembly(self.archive_path)
def _pneumatic_components_by_alias(self) -> dict[str, Component]:
return {
**self.pneumatic_assembly.fixed_chambers,
@@ -3893,6 +3901,10 @@ class TestMqlSystem:
def typed_pneumatic_component_count(self) -> int:
return len(self._pneumatic_components_by_alias())
@property
def typed_pnl0001_line_count(self) -> int:
return len(self.pnl0001_assembly.lines)
def pneumatic_state_vector(self) -> list[float]:
return self.network.initial_state_vector()
@@ -4071,6 +4083,84 @@ class TestMqlSystem:
t_eval=t_eval,
)
def pnl0001_chamber_segment_closure_from_spec(
self,
spec,
*,
inlet_node_pressure_pa: float,
outlet_pressure_pa: float,
inlet_node_temperature_k: float = 293.15,
outlet_temperature_k: float = 293.15,
):
"""Insert the topology-derived inlet PNL0001 into a chamber segment."""
from PythonModels.components.amesim_pneumatic import (
AmesimPneumaticOrifice,
AmesimPneumaticVolume,
)
from PythonModels.systems.test_mql_closure import (
TestMqlPneumaticBoundaryCondition,
TestMqlPnl0001ChamberSegmentClosure,
TestMqlPnl0001ChamberSegmentComponents,
)
inlet_line = self.pnl0001_assembly.lines[spec.inlet_line_alias]
volume = self.network.components[spec.volume_alias]
inlet_orifice = self.network.components[spec.inlet_orifice_alias]
outlet_orifice = self.network.components[spec.outlet_orifice_alias]
if not isinstance(volume, AmesimPneumaticVolume):
raise TypeError(f"{spec.volume_alias} is not an AMESim pneumatic volume")
if not isinstance(inlet_orifice, AmesimPneumaticOrifice):
raise TypeError(
f"{spec.inlet_orifice_alias} is not an AMESim pneumatic orifice"
)
if not isinstance(outlet_orifice, AmesimPneumaticOrifice):
raise TypeError(
f"{spec.outlet_orifice_alias} is not an AMESim pneumatic orifice"
)
return TestMqlPnl0001ChamberSegmentClosure(
components=TestMqlPnl0001ChamberSegmentComponents(
inlet_line=inlet_line,
volume=volume,
inlet_orifice=inlet_orifice,
outlet_orifice=outlet_orifice,
spec=spec,
),
inlet_node=TestMqlPneumaticBoundaryCondition(
pressure_pa=inlet_node_pressure_pa,
temperature_k=inlet_node_temperature_k,
),
outlet_boundary=TestMqlPneumaticBoundaryCondition(
pressure_pa=outlet_pressure_pa,
temperature_k=outlet_temperature_k,
),
)
def simulate_pnl0001_chamber_segment_from_spec(
self,
spec,
*,
inlet_node_pressure_pa: float,
outlet_pressure_pa: float,
inlet_node_temperature_k: float = 293.15,
outlet_temperature_k: float = 293.15,
config: SolveIVPConfig | None = None,
t_eval: list[float] | None = None,
):
closure = self.pnl0001_chamber_segment_closure_from_spec(
spec,
inlet_node_pressure_pa=inlet_node_pressure_pa,
outlet_pressure_pa=outlet_pressure_pa,
inlet_node_temperature_k=inlet_node_temperature_k,
outlet_temperature_k=outlet_temperature_k,
)
run_config = config or SolveIVPConfig(t_stop=1.0e-4, max_step=1.0e-5)
return integrate_ode(
rhs=lambda t, state: closure.rhs(state),
initial_state=closure.initial_state_vector(),
config=run_config,
t_eval=t_eval,
)
def pneumatic_branch_closure_from_spec(self, spec):
return self.pneumatic_branch_closure(
name=spec.name,