Hyundai motor company (20240336150). POWER SUPPLY SYSTEM OF AIRCRAFT AND CONTROL METHOD THEREOF simplified abstract
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 20240336150 titled 'POWER SUPPLY SYSTEM OF AIRCRAFT AND CONTROL METHOD THEREOF
Simplified Explanation:
The power supply system of an aircraft includes a fuel cell, a converter device with a mode switch, a first battery device, and a processor. The system can switch between power sources in case of an error.
- The system includes a fuel cell that generates electrical energy.
- A converter device with a mode switch supplies power to a first motor device and switches connections between the fuel cell and the motor.
- A first battery device supplies voltage to a second motor device and connects with the first motor device under control of the mode switch.
- A processor controls the mode switch to enter an emergency mode when errors are detected, connecting the first and second motor devices.
Potential Applications:
This technology can be used in various aircraft systems where a reliable power supply is crucial, such as in-flight entertainment systems, navigation equipment, and communication devices.
Problems Solved:
This system addresses the need for a reliable and efficient power supply in aircraft, especially in emergency situations where immediate power source switching is necessary.
Benefits:
The benefits of this technology include enhanced safety, improved power management, and increased reliability of the aircraft's electrical system.
Commercial Applications:
This technology could be commercially applied in the aviation industry for the development of more advanced and reliable aircraft power supply systems, potentially leading to safer and more efficient flights.
Questions about Aircraft Power Supply System: 1. How does the mode switch device in the power supply system work? 2. What are the potential implications of using a fuel cell in 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.
