18532539. POWER SUPPLY SYSTEM OF AIRCRAFT AND CONTROL METHOD THEREOF simplified abstract (Hyundai Motor Company)
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 first battery device, and a processor. The system can enter an emergency mode when errors are detected and connect the output terminals of the fuel cell and battery device.
Key Features and Innovation:
- Power supply system for aircraft
- Includes fuel cell, converter device, battery device, and processor
- Emergency mode activation when errors are detected
- Connection between fuel cell and battery device output terminals
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: This technology addresses the need for a robust power supply system in aircraft that can quickly switch to emergency mode in case of errors.
Benefits:
- Enhanced safety in aircraft power supply systems
- Reliable performance during emergencies
- Efficient power distribution
Commercial Applications: Potential commercial applications include aviation industry suppliers, aircraft manufacturers, and companies involved in aircraft maintenance and repair services.
Prior Art: Readers can start searching for prior art related to this technology by looking into patents related to aircraft power supply systems, fuel cell technology, and emergency power systems in aviation.
Frequently Updated Research: Stay updated on the latest advancements in fuel cell technology, aircraft power supply systems, and emergency power systems in aviation to enhance the efficiency and reliability of this technology.
Questions about Aircraft Power Supply Systems: 1. What are the key components of an aircraft power supply system? 2. How does emergency mode activation improve the safety of aircraft power systems?
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.
