General electric company (20240247614). TURBINE ENGINE WITH SHOCKWAVE ATTENUATION simplified abstract
TURBINE ENGINE WITH SHOCKWAVE ATTENUATION
Organization Name
Inventor(s)
Christopher Ryan Johnson of Fairfield OH (US)
Paul Hadley Vitt of Liberty Twp OH (US)
Eric Joseph Schroeder of Loveland OH (US)
Carlos Gilberto Fernandez-soto of Fairfield Twp OH (US)
TURBINE ENGINE WITH SHOCKWAVE ATTENUATION - A simplified explanation of the abstract
This abstract first appeared for US patent application 20240247614 titled 'TURBINE ENGINE WITH SHOCKWAVE ATTENUATION
Simplified Explanation:
This patent application describes a turbine engine with a compressor, combustor, and turbine arranged in axial flow. The engine core has a flow path for working airflow from the compressor to the turbine.
- The patent describes a turbine engine with components arranged in axial flow.
- The engine core includes a compressor, combustor, and turbine.
- A flow path guides working airflow from the compressor to the turbine.
- The design optimizes the flow direction for efficient operation.
- The innovation aims to enhance the performance of turbine engines.
Potential Applications:
The technology could be applied in aircraft engines, power generation systems, and industrial machinery where efficient airflow is crucial.
Problems Solved:
This technology addresses the need for improved airflow efficiency in turbine engines, leading to enhanced performance and fuel efficiency.
Benefits:
The benefits of this technology include increased engine efficiency, reduced fuel consumption, and improved overall performance in various applications.
Commercial Applications:
Title: Enhanced Efficiency Turbine Engine Technology for Aerospace and Industrial Applications
This technology could be utilized in commercial aircraft engines, power plants, and industrial machinery to improve operational efficiency and reduce fuel costs.
Prior Art:
Readers interested in prior art related to this technology could explore patents and research papers on turbine engine design, axial flow arrangements, and airflow optimization in engine cores.
Frequently Updated Research:
Researchers are continually exploring ways to enhance turbine engine efficiency through improved airflow management and component design. Stay updated on the latest advancements in turbine engine technology for potential future applications.
Questions about Turbine Engine Technology: 1. What are the key components of a turbine engine and how do they work together? 2. How does airflow optimization impact the performance of turbine engines?
Original Abstract Submitted
a turbine engine and method of operating includes an engine core with a compressor, a combustor, and a turbine in axial flow arrangement. a flow path extends through the engine core from the compressor to the turbine to define a flow direction for a working airflow through the engine core.