SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply Class Reference
Inheritance diagram for SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply:
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, power_out)
 

Public Attributes

 efficiency
 
 rated_current
 
 rated_power
 
- 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
 

Member Function Documentation

◆ __defaults__()

def SUAVE.Components.Energy.Distributors.HTS_DC_Supply.HTS_DC_Supply.__defaults__ (   self)
This sets the default values.
    
    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.Distributors.HTS_DC_Supply.HTS_DC_Supply.power (   self,
  current,
  power_out 
)
The power that must be supplied to the DC supply to power the HTS coils.

    Assumptions:
    Supply cable is solid copper, i.e. not a rotating joint.
    Power supply has static efficiency across current output range.
    Power supply performance is not affected by altitude or other environmental factors. This is not generally true (Ametek SGe datasheet should be derated by 10% per 1000 feet) for current supplies designed for ground use however a supply specifically designed for airborne use can be expected to have a more appropriate cooling design that would allow high altitude use.

    Source:
    N/A

    Inputs:
    current             [A]
    power_out           [W]
    self.efficiency

    Outputs:
    power_in            [W]

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