AIRCRAFT DC POWER BUS REGULATION AND WING DE-ICER
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United States of America
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Issued Date -
Nov 14, 2024
app pub date -
May 8, 2023
filing date -
May 8, 2023
priority date (Note) -
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Abstract
A power distribution system for an aircraft includes a wing, a power supply circuit, and a controller. The supply circuit includes a DC power bus having a voltage, a resistive heating element electrically connected with the DC power bus and coupled with the wing, and a voltage manipulation element configured to selectively adjust an amount of voltage that is directed to the heating element. The controller is connected to the manipulation element and is configured to regulate the voltage of the DC power bus. The controller is programmed to control the manipulation element when the voltage of the DC power bus is greater than a threshold voltage to vary an amount of voltage that is directed to the heating element to cause the heating element to convert the amount of the voltage into heat and thereby regulate overvoltage of the voltage of the DC power bus.
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