General electric company (20240280053). REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE simplified abstract
REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE
Organization Name
Inventor(s)
Arthur William Sibbach of Boxford MA (US)
Adam Tomasz Pazinski of Warsaw (PL)
REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE - A simplified explanation of the abstract
This abstract first appeared for US patent application 20240280053 titled 'REVERSE FLOW GAS TURBINE ENGINE HAVING ELECTRIC MACHINE
The abstract describes an aircraft engine assembly that includes a gas turbine engine with an intake channel designed to receive incoming air and create an intake flow of air. The intake channel redirects the incoming air from its original direction to align with the gas turbine engine's axial direction. Additionally, an electric machine is connected to the low-pressure shaft of the engine and positioned near the intake channel's aft end. The electric machine is in heat exchange communication with the intake flow of air, allowing it to transfer heat to the incoming air within the intake channel during operation.
- Gas turbine engine with intake channel for incoming air
- Electric machine connected to low-pressure shaft near intake channel
- Electric machine transfers heat to incoming air within intake channel
- Intake channel redirects incoming air to align with engine's axial direction
- Heat exchange communication between electric machine and intake flow of air
Potential Applications: - Aircraft engines - Power generation systems - Industrial machinery
Problems Solved: - Efficient heat transfer in aircraft engines - Improved performance and energy efficiency
Benefits: - Enhanced engine performance - Increased energy efficiency - Reduced fuel consumption
Commercial Applications: Title: Innovative Aircraft Engine Assembly for Enhanced Performance This technology can be utilized in the aerospace industry for aircraft engines, power generation systems, and various industrial applications. It offers improved efficiency, performance, and energy savings, making it a valuable asset for companies seeking advanced engine solutions.
Questions about the technology: 1. How does the electric machine enhance the performance of the gas turbine engine? The electric machine transfers heat to the incoming air within the intake channel, improving overall efficiency and performance. 2. What are the potential commercial applications of this innovative aircraft engine assembly? This technology can be applied in aircraft engines, power generation systems, and industrial machinery to enhance performance and energy efficiency.
Original Abstract Submitted
an aircraft engine assembly includes a gas turbine engine having an intake channel configured to receive an incoming flow of air and thereby form an intake flow of air, the intake channel configured to turn the received incoming flow of air from an incoming flow direction to a first axial direction of the gas turbine engine, the incoming flow direction reverse of the first axial direction, and an electric machine coupled with the low pressure shaft and located at the aft end of the gas turbine engine proximate the intake channel, the electric machine in heat exchange communication with the intake flow of air such that the electric machine transfers heat to the incoming flow of air within the intake channel when the electric machine is operated.