Source code for RCAIDE.Library.Components.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine
# RCAIDE/Library/Components/Propulsors/Constant_Speed_ICE_Propeller.py
#
#
# Created: Mar 2024, M. Clarke
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# IMPORT
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# RCAIDE imports
from . import Propulsor
from RCAIDE.Library.Methods.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine.append_constant_speed_internal_combustion_engine_conditions import append_constant_speed_internal_combustion_engine_conditions
from RCAIDE.Library.Methods.Powertrain.Propulsors.Constant_Speed_Internal_Combustion_Engine.compute_constant_speed_internal_combustion_engine_performance import compute_constant_speed_internal_combustion_engine_performance, reuse_stored_constant_speed_internal_combustion_engine_data
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# Constant_Speed_ICE_Propeller
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[docs]
class Constant_Speed_Internal_Combustion_Engine(Propulsor):
"""
A propulsion system class that combines an internal combustion engine with a constant-speed propeller.
Attributes
----------
tag : str
Identifier for the propulsion system, defaults to 'ice_constant_speed_propeller'
engine : None or Engine
The internal combustion engine component
propeller : None or Propeller
The constant-speed propeller component
Notes
-----
This class models a propulsion system that pairs an internal combustion engine with
a constant-speed propeller. The constant-speed propeller maintains a specified RPM
by adjusting blade pitch.
**Definitions**
'Constant-Speed Propeller'
A propeller that maintains a constant rotational speed by automatically
adjusting blade pitch to match power requirements
'Governor'
Mechanical or electronic device that controls propeller pitch to maintain
desired RPM
See Also
--------
RCAIDE.Library.Components.Powertrain.Propulsors.Propulsor
"""
def __defaults__(self):
# setting the default values
self.tag = 'ice_constant_speed_propeller'
self.engine = None
self.propeller = None
self.diameter = 0.4
self.length = 0.5
[docs]
def append_operating_conditions(self,segment,energy_conditions,noise_conditions=None):
append_constant_speed_internal_combustion_engine_conditions(self,segment,energy_conditions,noise_conditions)
return
[docs]
def unpack_propulsor_unknowns(self,segment):
return
[docs]
def pack_propulsor_residuals(self,segment):
return
[docs]
def append_propulsor_unknowns_and_residuals(self,segment):
return
[docs]
def reuse_stored_data(ICE_cs_prop, state,network,stored_propulsor_tag = None,center_of_gravity = [[0, 0, 0]]):
thrust,moment,power_mech,power_elec = reuse_stored_constant_speed_internal_combustion_engine_data(ICE_cs_prop,state,network,stored_propulsor_tag,center_of_gravity)
return thrust,moment,power_mech,power_elec