18085728. ELECTRIC MACHINE ASSEMBLY simplified abstract (GENERAL ELECTRIC COMPANY)
Contents
ELECTRIC MACHINE ASSEMBLY
Organization Name
Inventor(s)
Ethan Patrick O'connor of Hamilton OH (US)
Gert Johannes Van Der Merwe of Lebanon OH (US)
Alexander Thomas Hills of Cincinnati OH (US)
ELECTRIC MACHINE ASSEMBLY - A simplified explanation of the abstract
This abstract first appeared for US patent application 18085728 titled 'ELECTRIC MACHINE ASSEMBLY
Simplified Explanation: The patent application describes a hybrid electric gas turbine engine that combines a turbomachine with an electric machine assembly to improve efficiency.
Key Features and Innovation:
- Turbomachine with compressor and turbine sections
- Electric machine assembly connected to the turbine section
- Core air flowpath defined by the compressor and turbine sections
- Electric machine located aft of the core air flowpath exhaust
Potential Applications: This technology could be used in aircraft engines, power generation systems, and marine propulsion systems.
Problems Solved: The hybrid electric gas turbine engine addresses the need for increased efficiency and reduced emissions in traditional gas turbine engines.
Benefits:
- Improved fuel efficiency
- Lower emissions
- Enhanced overall performance
Commercial Applications: Potential commercial applications include aircraft propulsion systems, power plants, and marine vessels.
Prior Art: Readers can start searching for prior art related to hybrid electric gas turbine engines in academic journals, patent databases, and industry publications.
Frequently Updated Research: Stay updated on the latest advancements in hybrid electric gas turbine engine technology by following research publications and industry conferences.
Questions about Hybrid Electric Gas Turbine Engines: 1. What are the main advantages of using a hybrid electric gas turbine engine? 2. How does the electric machine assembly improve the performance of the turbomachine?
Original Abstract Submitted
A hybrid electric gas turbine engine is provided. The hybrid electric gas turbine engine includes: a turbomachine having a compressor section and a turbine section arranged in serial flow order, the compressor section and turbine section together defining a core air flowpath, the turbomachine defining a core air flowpath exhaust; and an electric machine assembly having an electric machine disposed aft of the core air flowpath exhaust and mechanically connected to the turbine section.
