SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric Class Reference

Inheritance diagram for SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric:

Public Member Functions
def	__defaults__ (self)
def	energy_calc (self, conditions, numerics)

Public Attributes
	propellant
	oxidizer
	number_of_engines
	efficiency
	volume
	rated_power
	specific_power
	mass_density
	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 turboelectic component.

Assumptions:
None

Source:
None

Member Function Documentation

__defaults__()

def SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric.__defaults__

(

self

)

This sets the default values for the component to function.

Assumptions:
None

Source:
https://new.siemens.com/global/en/products/energy/power-generation/gas-turbines/sgt-a30-a35-rb.html

Inputs:
None

Outputs:
None

Properties Used:
None

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

energy_calc()

def SUAVE.Components.Energy.Converters.Turboelectric.Turboelectric.energy_calc	(		self,
			conditions,
			numerics
	)

This calls 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)

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

• /Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Energy/Converters/Turboelectric.py