Source code for RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Electric.Common.compute_wiring_weight

# RCAIDE/Library/Methods/Weights/Buildups/Common/compute_boom_weight.py
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# Created:  Sep 2024, M. Clarke

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#  IMPORT
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# package imports 
import numpy as np

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# Compute wiring weight
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[docs] def compute_wiring_weight(wing, config, cablePower): """ Calculates mass of wiring required for a wing, including DC power cables and communication cables, assuming power cables run an average of half the fuselage length and height in addition to reaching the motor location on the wingspan, and that communication and sesor wires run an additional length based on the fuselage and wing dimensions. Sources: Project Vahana Conceptual Trade Study Inputs: config RCAIDE Config Data Structure max_power_draw Maximum DC Power Draw [W] Outputs: weight: Wiring Mass [kg] """ weight = 0.0 cableLength = 0.0 for network in config.networks: for propulsor in network.propulsors: motor = propulsor.motor if propulsor.wing_mounted == True: MSL = np.array(motor.origin) #- np.array(bus.origin) WHAT DO WE DO HERE SINCE WE DONT HAVE A BUS DEFINED YET AT THIS STAGE cableLength += np.sum(abs(MSL)) cableDensity = 5.7e-6 massCables = cableDensity * cablePower * cableLength # Determine mass of sensor/communication wires fLength = 0 for fus in config.fuselages: fLength += fus.lengths.total wiresPerBundle = 6 wireDensity = 460e-5 wireLength = cableLength + (10 * fLength) + 4*wing.spans.projected massWires = wireDensity * wiresPerBundle * wireLength # Sum Total weight += massCables + massWires return weight