18532539. POWER SUPPLY SYSTEM OF AIRCRAFT AND CONTROL METHOD THEREOF simplified abstract (Kia Corporation)
Contents
POWER SUPPLY SYSTEM OF AIRCRAFT AND CONTROL METHOD THEREOF
Organization Name
Inventor(s)
Yoon Cheol Jeon of suwon-si (KR)
Ji Han Lee of Hwaseong-si (KR)
POWER SUPPLY SYSTEM OF AIRCRAFT AND CONTROL METHOD THEREOF - A simplified explanation of the abstract
This abstract first appeared for US patent application 18532539 titled 'POWER SUPPLY SYSTEM OF AIRCRAFT AND CONTROL METHOD THEREOF
Simplified Explanation: The patent application describes a power supply system for an aircraft that includes a fuel cell, a converter device with a mode switch, a battery device, and a processor to control the system.
- The system includes a fuel cell that generates electrical energy.
- A converter device with a mode switch supplies power to a motor device and switches connections between the fuel cell and the motor device.
- A battery device supplies voltage to another motor device and connects terminals under control of the mode switch.
- A processor controls the mode switch to enter an emergency mode in case of errors and connects the terminals of the battery devices.
Potential Applications: This technology can be used in various aircraft to provide a reliable power supply system that can switch to emergency mode when needed.
Problems Solved: The system addresses the need for a stable and efficient power supply in aircraft, as well as the ability to switch to emergency mode in case of errors.
Benefits: The system ensures a continuous power supply for critical systems in aircraft, enhancing safety and reliability during flights.
Commercial Applications: Title: Aircraft Power Supply System for Enhanced Safety and Reliability This technology can be commercially applied in the aviation industry to improve the power supply systems of aircraft, ensuring safety and reliability during flights.
Prior Art: Researchers can explore prior patents related to power supply systems in aircraft, fuel cell technology, and emergency mode switching in electrical systems.
Frequently Updated Research: Researchers can stay updated on advancements in fuel cell technology, battery systems, and aircraft power supply systems to enhance the efficiency and reliability of the technology.
Questions about Aircraft Power Supply System: 1. What are the key components of the power supply system described in the patent application?
- The key components include a fuel cell, a converter device with a mode switch, a battery device, and a processor.
2. How does the system switch to emergency mode in case of errors?
- The processor controls the mode switch to connect the terminals of the battery devices in emergency mode.
Original Abstract Submitted
A power supply system of an aircraft includes a fuel cell that generates electrical energy, a converter device including a mode switch device that supplies power to a first motor device through a first output terminal and switches a connection between an output node of the fuel cell and the first output terminal, a first battery device that supplies a voltage from a first battery to a second motor device through a second output terminal and connects the second output terminal with the first output terminal under control of the mode switch device, and a processor that controls the mode switch device to enter an emergency mode when detecting an error in the converter device or the first battery device and connects the first output terminal with the second output terminal.
