Hyundai motor company (20240157808). Power Supply System of Aircraft and Control Method Thereof simplified abstract
Contents
- 1 Power Supply System of Aircraft and Control Method Thereof
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 Power Supply System of Aircraft and Control Method Thereof - A simplified explanation of the abstract
- 1.4 Simplified Explanation
- 1.5 Potential Applications
- 1.6 Problems Solved
- 1.7 Benefits
- 1.8 Potential Commercial Applications
- 1.9 Possible Prior Art
- 1.10 Original Abstract Submitted
Power Supply System of Aircraft and Control Method Thereof
Organization Name
Inventor(s)
Woo Young Lee of Yongin-Si (KR)
Jung Hyun Lee of Gunpo-Si (KR)
Sae Kwon Chang of Yongin-Si (KR)
Mi Jin Kim of Gwacheon-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 20240157808 titled 'Power Supply System of Aircraft and Control Method Thereof
Simplified Explanation
The power supply system for an aircraft described in the patent application includes a fuel cell, a converter device, a battery, and a processor. The system is designed to efficiently supply electrical energy to drive the aircraft using a combination of the fuel cell and battery depending on the driving mode.
- Fuel cell generates electrical energy
- Converter device supplies voltage to first motor device
- Battery supplies voltage to second motor device
- Processor controls connection between fuel cell and converter device
Potential Applications
The power supply system for aircraft can be used in various types of aircraft, including drones, electric airplanes, and other electrically powered aircraft.
Problems Solved
This technology solves the problem of efficiently managing power distribution in aircraft, ensuring optimal performance and reliability during flight.
Benefits
The benefits of this technology include increased energy efficiency, reduced emissions, and improved overall performance of the aircraft.
Potential Commercial Applications
This technology has potential commercial applications in the aerospace industry, specifically in the development of electric aircraft and drones for various purposes.
Possible Prior Art
One possible prior art for this technology could be existing power supply systems for electric vehicles, which also utilize a combination of fuel cells and batteries for energy storage and distribution.
Unanswered Questions
How does the system handle different driving modes in terms of power distribution?
The patent application mentions that the system can switch the connection with the fuel cell depending on a predetermined driving mode, but it does not provide specific details on how this process is carried out.
What are the specific voltage requirements for the first and second motor devices?
The abstract mentions that the converter device supplies voltage to the first motor device and the battery supplies voltage to the second motor device, but it does not specify the exact voltage levels needed for each device.
Original Abstract Submitted
a power supply system for an aircraft and a control method thereof are provided. the power supply system of the aircraft includes a fuel cell configured to generate electrical energy, a converter device configured to supply a voltage generated by the fuel cell to a first motor device for driving the aircraft through a first output terminal and switch a connection with the fuel cell depending on a predetermined driving mode, a battery configured to supply the voltage to a second motor device for driving the aircraft through a second output terminal, the second output terminal being connected with an output node of the fuel cell, and a processor configure to control a connection between the fuel cell and the converter device depending on the driving mode.
