18513916. Propulsion System for an Aircraft simplified abstract (GENERAL ELECTRIC COMPANY)
Contents
- 1 Propulsion System for an Aircraft
Propulsion System for an Aircraft
Organization Name
Inventor(s)
Randy M. Vondrell of Cincinnati OH (US)
Anthony Austin Bouvette of Hamilton OH (US)
Glenn David Crabtree of Oregonia OH (US)
Propulsion System for an Aircraft - A simplified explanation of the abstract
This abstract first appeared for US patent application 18513916 titled 'Propulsion System for an Aircraft
Simplified Explanation
The propulsion system for an aircraft described in the abstract includes an electric power source, an electric propulsion assembly with an electric motor and a propulsor, an electric power bus connecting the power source to the propulsion assembly, and an inverter converter controller along the power bus.
- The electric power source provides electrical power to the electric power bus.
- The electric motor powers the propulsor for aircraft propulsion.
- The inverter converter controller is positioned along the power bus to manage power flow.
Potential Applications
This technology could be applied in electric aircraft, drones, and other electrically powered aerial vehicles.
Problems Solved
This innovation helps reduce reliance on traditional fuel sources, decreases emissions, and provides a more sustainable propulsion solution for aircraft.
Benefits
The benefits of this technology include lower environmental impact, reduced operating costs, and improved efficiency in aircraft propulsion systems.
Potential Commercial Applications
The potential commercial applications of this technology could include electric aircraft manufacturing, drone development, and aerospace engineering companies.
Possible Prior Art
One possible prior art could be electric propulsion systems used in electric vehicles, as the technology has similarities in terms of electric motor power and energy management.
Unanswered Questions
How does this technology impact aircraft performance compared to traditional propulsion systems?
This article does not delve into specific performance metrics or comparisons between electric propulsion systems and traditional systems. It would be interesting to explore factors such as speed, range, and efficiency in future research.
What are the safety considerations associated with implementing this technology in aircraft?
The safety aspects of integrating electric propulsion systems into aircraft are crucial but not discussed in detail in this article. Understanding potential risks, mitigation strategies, and regulatory requirements would be essential for the successful adoption of this technology in the aviation industry.
Original Abstract Submitted
A propulsion system for an aircraft can include an electric power source and an electric propulsion assembly having an electric motor and a propulsor. The propulsor can be powered by the electric motor. An electric power bus can electrically connect the electric power source to the electric propulsion assembly. The electric power source can be configured to provide electrical power to the electric power bus. An inverter converter controller can be positioned along the electric power bus and can be electrically connected to the electric power source at a location downstream of the electric power source and upstream of the electric propulsion assembly.
