18088957. COMPOSITE AIRFOIL ASSEMBLY HAVING A DOVETAIL PORTION simplified abstract (GENERAL ELECTRIC COMPANY)
Contents
COMPOSITE AIRFOIL ASSEMBLY HAVING A DOVETAIL PORTION
Organization Name
Inventor(s)
Nicholas Joseph Kray of Mason OH (US)
Elzbieta Kryj-kos of Evendale OH (US)
Tod Winton Davis of Liberty Township OH (US)
Gary Willard Bryant, Jr. of Loveland OH (US)
COMPOSITE AIRFOIL ASSEMBLY HAVING A DOVETAIL PORTION - A simplified explanation of the abstract
This abstract first appeared for US patent application 18088957 titled 'COMPOSITE AIRFOIL ASSEMBLY HAVING A DOVETAIL PORTION
The abstract describes a composite blade assembly for a turbine engine, consisting of a core, a first skin, and a second skin, all made of composite materials with different radii.
- The composite blade assembly includes a core with a composite structure.
- The first skin and second skin are made of composite plies.
- The first skin has a first radius, while the second skin has a second radius.
Potential Applications: - Aerospace industry for turbine engines - Wind turbine blades - Marine propulsion systems
Problems Solved: - Increased strength and durability - Reduced weight for improved efficiency - Enhanced performance in harsh environments
Benefits: - Improved fuel efficiency - Longer lifespan - Reduced maintenance costs
Commercial Applications: Title: Advanced Composite Blade Assembly for Turbine Engines This technology can be used in the aerospace industry for turbine engines, wind turbine blades, and marine propulsion systems. The innovation offers increased strength, durability, and efficiency, making it a valuable solution for various commercial applications.
Questions about Composite Blade Assembly for a Turbine Engine: 1. How does the composite structure of the core enhance the performance of the blade assembly? The composite structure of the core provides increased strength and durability, improving the overall performance of the blade assembly.
2. What are the advantages of using composite plies in the first and second skins of the blade assembly? Using composite plies in the skins enhances the lightweight properties of the assembly while maintaining structural integrity and durability.
Original Abstract Submitted
A composite blade assembly for a turbine engine. The composite blade assembly having a core, a first skin and a second skin. The core having a composite structure. The first skin having at least one composite ply. The second skin having at least one composite ply. The first skin having a first radius. The second skin having a second radius.
