18385549. Power Supply System of Aircraft and Control Method Thereof simplified abstract (Hyundai Motor Company)
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 How does the system handle transitions between different driving modes?
- 1.11 What are the specific voltage requirements for the first and second motor devices?
- 1.12 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 connection with the fuel cell can be switched depending on the driving mode. The battery supplies voltage to a second motor device, with its output terminal connected to an output node of the fuel cell. The processor controls the connection between the fuel cell and the converter device based 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
This technology could be applied in various aircraft systems, such as electric propulsion systems, to improve efficiency and reduce emissions.
Problems Solved
This technology solves the problem of efficiently managing power distribution in aircraft systems, ensuring optimal performance and reliability during different driving modes.
Benefits
The benefits of this technology include improved energy efficiency, reduced emissions, enhanced reliability, and optimized performance of aircraft systems.
Potential Commercial Applications
One potential commercial application of this technology could be in the aerospace industry for developing more sustainable and efficient aircraft propulsion systems.
Possible Prior Art
One possible prior art for this technology could be existing power supply systems for aircraft that may not have the same level of efficiency and control as the system described in the patent application.
Unanswered Questions
How does the system handle transitions between different driving modes?
The abstract mentions that the connection with the fuel cell can be switched depending on the driving mode, but it does not provide details on how this transition process is managed.
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 requirements 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.
