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

Public Member Functions

def __defaults__ (self)
 
def power (self, current, ambient_temp)
 

Public Attributes

 temperature
 
 skin_temp
 
 current
 
 resistance
 
 length
 
 diameter
 
 surface_area
 
 R_value
 
 number_of_engines
 
- 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 represents just the rotor of a HTS motor, i.e. the superconducting components.
This is used to estimate the power and cooling required for the HTS components.
The power used here could be considered the same as that used by the motor as inefficiency, however many publications consider the overall motor efficiency, i.e. including cryocooler and/or motor drive electronics.

Assumptions:
No ACLoss in the HTS,
HTS is operated within the Ic and Tc limits.
i.e the power used by the coil is only due to solder resistances only, and is not affected by the motor output power or speed.

Source:
None

Member Function Documentation

◆ __defaults__()

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

Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
None

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

◆ power()

def SUAVE.Components.Energy.Converters.Motor_HTS_Rotor.Motor_HTS_Rotor.power (   self,
  current,
  ambient_temp 
)
Calculates the electrical power draw from the HTS coils, and the total heating load on the HTS rotor cryostat.

Assumptions:
No ACLoss in the HTS,
HTS is operated within the Ic and Tc limits.
i.e the power used by the coil is only due to solder resistances only.

Source:
N/A

Inputs:
current             [A]
ambient_temp        [K]

Outputs:
input_power         [W]
cryogenic_load      [W]

Properties Used:
self.
    temperature     [K]
    resistance      [ohm]
    surface_area    [m2]
    R_value         [K.m2/W]

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