SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell Class Reference
Inheritance diagram for SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell:
SUAVE.Components.Energy.Energy_Component.Energy_Component SUAVE.Components.Physical_Component.Physical_Component SUAVE.Components.Component.Component

Public Member Functions

def __defaults__ (self)
 
def energy_calc (self, conditions, numerics)
 

Public Attributes

 propellant
 
 oxidizer
 
 efficiency
 
 specific_power
 
 mass_density
 
 volume
 
 max_power
 
 discharge_model
 
- Public Attributes inherited from SUAVE.Components.Energy.Energy_Component.Energy_Component
 inputs
 
 outputs
 
- Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
 tag
 
 mass_properties
 
 origin
 
 symmetric
 
- Public Attributes inherited from SUAVE.Components.Component.Component
 tag
 
 origin
 
 generative_design_max_per_vehicle
 
 generative_design_characteristics
 
 generative_design_special_parent
 

Detailed Description

This is a fuel cell component.

Assumptions:
None

Source:
None

Member Function Documentation

◆ __defaults__()

def SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell.__defaults__ (   self)
This sets the default values for the component to function.

Assumptions:
None

Source:
Some default values come from a Nissan 2011 fuel cell

Inputs:
None

Outputs:
None

Properties Used:
None

Reimplemented from SUAVE.Components.Energy.Energy_Component.Energy_Component.

◆ energy_calc()

def SUAVE.Components.Energy.Converters.Fuel_Cell.Fuel_Cell.energy_calc (   self,
  conditions,
  numerics 
)
This call the assigned discharge method.

Assumptions:
None

Source:
N/A

Inputs:
see properties used

Outputs:
mdot     [kg/s] (units may change depending on selected model)

Properties Used:
self.discharge_model(self, conditions, numerics)

The documentation for this class was generated from the following file: