libICEpost.src.engineModel.EngineGeometry.ConRod
@author: F. Ramognino <federico.ramognino@polimi.it> Last update: 12/06/2023
Attributes
Classes
Geometry for engine piston. |
Functions
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Returns the piston position at CA [m] (reference to TDC). |
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Returns the time (in CA) derivative of instantaneous piston position at CA [m/CA]. |
Module Contents
- libICEpost.src.engineModel.EngineGeometry.ConRod._pistonPos
- libICEpost.src.engineModel.EngineGeometry.ConRod.pistonPosition(CA: float | collections.abc.Iterable[float], *, S: float, lam: float, delta: float) float | collections.abc.Iterable[float][source]
Returns the piston position at CA [m] (reference to TDC).
- Parameters:
CA (float | Iterable[float]) – Time in CA
S (float) – Stroke [m]
lam (float) – conRodLen/crankRadius [-]
delta (float) – pinOffset/crankRadius [-]
- Returns:
Piston position [m]
- Return type:
float|Iterable[float]
- libICEpost.src.engineModel.EngineGeometry.ConRod._pistonPosDerivative
- libICEpost.src.engineModel.EngineGeometry.ConRod.pistonPosDerivative(CA: float | collections.abc.Iterable[float], *, S: float, lam: float, delta: float) float | collections.abc.Iterable[float][source]
Returns the time (in CA) derivative of instantaneous piston position at CA [m/CA].
- Parameters:
CA (float | Iterable[float]) – Time in CA
S (float) – Stroke [m]
lam (float) – conRodLen/crankRadius [-]
delta (float) – pinOffset/crankRadius [-]
- Returns:
ds/dCA [m/CA]
- Return type:
float|Iterable[float]
- class libICEpost.src.engineModel.EngineGeometry.ConRod.ConRodGeometry(*, bore: float, stroke: float, conRodLen: float, CR: float, pinOffset: float = 0.0, clearence: float = None, pistonCylAreaRatio: float = 1.0, headCylAreaRatio: float = 1.0)[source]
Bases:
libICEpost.src.engineModel.EngineGeometry.EngineGeometry.EngineGeometryGeometry for engine piston.
- Attibutes:
CR (float): Compression ratio [-]
lam (float): conRodLen/crankRadius [-]
delta (float): pinOffset/crankRadius [-]
D (float): Bore [m]
S (float): Stroke [m]
l (float): connecting-rod length [m]
pinOffset (float): Piston pin offset [m]
clearence (float): TDC clearence [m]
cylArea (float): cylinder cross section [m^2]
pistonArea (float): piston surface area [m^2]
headArea (float): cylinder head area [m^2]
Vs (float): Displacement volume [m^3]
Vmin (float): Mimimum volume [m^3]
Vmax (float): Maximum volume [m^3]
patches (list[str]): List of patches names
- _CR: float
The compression ratio
- _D: float
Bore [m]
- _S: float
Stroke [m]
- _l: float
connecting-rod length [m]
- _pinOffset: float = 0.0
Piston pin offset [m]
- _clearence: float = None
TDC clearence [m]
- _pistonCylAreaRatio: float = 1.0
piston surf. area / cyl. section
- _headCylAreaRatio: float = 1.0
head surf. area / cyl. section
- _patches: ClassVar[collections.abc.Iterable[str]] = ['liner', 'piston', 'head']
List of patches names
- property CR: float
Compression ratio [-]
- property D: float
Bore [m]
- property S: float
Stroke [m]
- property l: float
Connecting-rod length [m]
- property pinOffset: float
Piston pin offset [m]
- property clearence: float
TDC clearance [m]
- property pistonCylAreaRatio: float
Piston surface area / cylinder section
- property headCylAreaRatio: float
Head surface area / cylinder section
- property patches: collections.abc.Iterable[str]
Returns the list of patches names.
- Returns:
List of patches names
- Return type:
Iterable[str]
- property lam: float
lambda = R/L
- property delta: float
delta = PO/R
- property cylArea: float
Cylinder cross section area [m^2]
- property pistonArea: float
Piston surface area [m^2]
- property headArea: float
Cylinder head area [m^2]
- property Vs: float
Displacement volume [m^3]
- property Vmin: float
Minimum volume [m^3]
- property Vmax: float
Maximum volume [m^3]
- classmethod fromDictionary(inputDict: dict)[source]
Construct from dictionary containing the following parameters: - CR (float): Compression ratio [-] - bore (float): Bore [m] - stroke (float): Stroke [m] - conRodLen (float): connecting-rod length [m] - pinOffset (float): Piston pin offset [m] - clearence (float): TDC clearence [m] (optional) - pistonCylAreaRatio (float): piston surf. area / cyl. section (optional) - headCylAreaRatio (float): head surf. area / cyl. section (optional)
- Parameters:
inputDict (dict) – Dictionary containing the parameters
- s(CA: float | collections.abc.Iterable[float]) float | numpy.ndarray[source]
Returns the piston position at CA [m] (reference to TDC)
- Parameters:
CA (float | Iterable[float]) – Time in CA
- Returns:
Piston position [m]
- Return type:
float|np.ndarray
- V(CA: float | collections.abc.Iterable[float]) float | numpy.ndarray[source]
Returns the instantaneous in-cylinder volume at CA
- Parameters:
CA (float | Iterable[float]) – Time in CA
- Returns:
In-cylinder volume [m^3]
- Return type:
float|np.ndarray
- dsdCA(CA: float | collections.abc.Iterable[float]) float | numpy.ndarray[source]
Returns the time (in CA) derivative of instantaneous piston position at CA [m/CA]. :param CA: Time in CA :type CA: float | Iterable[float]
- Returns:
ds/dCA [m/CA]
- Return type:
float|np.ndarray
- dVdCA(CA: float | collections.abc.Iterable[float]) float | numpy.ndarray[source]
Returns the time (in CA) derivative of instantaneous in-cylinder volume at CA :param CA: Time in CA :type CA: float | Iterable[float]
- Returns:
dV/dCA [m^3/CA]
- Return type:
float|np.ndarray
- linerArea(CA: float | collections.abc.Iterable[float]) float | numpy.ndarray[source]
Returns the liner area at CA [m^2]. :param CA: Time in CA :type CA: float | Iterable
- Returns:
[m^2]
- Return type:
float|np.ndarray