18385549. Power Supply System of Aircraft and Control Method Thereof simplified abstract (Kia Corporation)
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 18385549 titled 'Power Supply System of Aircraft and Control Method Thereof
Simplified Explanation
The power supply system for an aircraft described in the abstract includes a fuel cell, a converter device, a battery, and a processor. The fuel cell generates electrical energy, which is then supplied to a first motor device through the converter device. The battery supplies voltage to a second motor device, and the processor controls the connection between the fuel cell and the converter device based on the driving mode of the aircraft.
- 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, helicopters, and small airplanes. It can also be applied in electric vehicles and other transportation systems that require efficient power management.
Problems Solved
This technology solves the problem of optimizing power distribution in aircraft, ensuring that the fuel cell and battery work together seamlessly to provide the necessary energy for propulsion. It also addresses the challenge of switching between different driving modes while maintaining a stable power supply.
Benefits
- Improved efficiency in power generation and distribution - Enhanced reliability and performance of the aircraft - Reduced environmental impact due to the use of fuel cells
Potential Commercial Applications
"Efficient Power Supply System for Aircraft: Commercial Applications"
The power supply system can be commercialized for use in commercial airlines, military aircraft, and unmanned aerial vehicles. It can also be integrated into electric propulsion systems for ships and other marine vessels.
Possible Prior Art
One possible prior art for this technology is the use of fuel cells in automotive applications, where they have been used to power electric vehicles. Another prior art could be the integration of batteries and converters in aircraft systems to optimize power distribution.
Unanswered Questions
How does the power supply system handle emergency situations in the aircraft?
The article does not provide information on how the power supply system responds to emergency situations such as power failures or malfunctions. This aspect is crucial for ensuring the safety and reliability of the aircraft.
What are the maintenance requirements for the power supply system?
The article does not mention the maintenance procedures or requirements for the power supply system. Understanding the maintenance needs of the system is essential for ensuring its long-term performance and durability.
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.
