18150664. COMPLIANT FEEDTHROUGHS FOR GAS TURBINE ENGINES simplified abstract (GENERAL ELECTRIC COMPANY)
Contents
COMPLIANT FEEDTHROUGHS FOR GAS TURBINE ENGINES
Organization Name
Inventor(s)
Rodolfo Mena Dominguez of Querétaro (MX)
COMPLIANT FEEDTHROUGHS FOR GAS TURBINE ENGINES - A simplified explanation of the abstract
This abstract first appeared for US patent application 18150664 titled 'COMPLIANT FEEDTHROUGHS FOR GAS TURBINE ENGINES
The abstract describes separators for gas turbine engines, including a rod and joint within a scaling wall.
- The apparatus includes a rod and joint designed to be placed within a scaling wall.
- The joint consists of a bushing portion, with the rod extending through it, and a disk portion with a slot.
- The disk portion is concentric with the bushing portion.
Potential Applications: - Gas turbine engines - Aerospace industry - Power generation
Problems Solved: - Improved efficiency of gas turbine engines - Enhanced durability of separators - Precision in engine components
Benefits: - Increased performance of gas turbine engines - Extended lifespan of engine components - Reduced maintenance costs
Commercial Applications: - Manufacturers of gas turbine engines - Aerospace companies - Power generation companies
Questions about Gas Turbine Engine Separators: 1. How do these separators improve the efficiency of gas turbine engines? 2. What materials are typically used in manufacturing these separators?
Frequently Updated Research: - Ongoing studies on the impact of separators on gas turbine engine performance - Research on new materials for improved durability in separators.
Original Abstract Submitted
Separators for use with gas turbine engines are disclosed herein. An example apparatus disclosed herein includes a rod and a joint to be disposed within a scaling wall, the joint including a bushing portion, the rod extending through the bushing portion and a disk portion including a slot, the disk portion concentric with the bushing portion.
