18345536. SYSTEMS AND METHODS FOR DEFORMATION CORRECTION OF A GAS TURBINE SHROUD simplified abstract (General Electric Company)
Contents
- 1 SYSTEMS AND METHODS FOR DEFORMATION CORRECTION OF A GAS TURBINE SHROUD
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 SYSTEMS AND METHODS FOR DEFORMATION CORRECTION OF A GAS TURBINE SHROUD - A simplified explanation of the abstract
- 1.4 Simplified Explanation
- 1.5 Potential Applications
- 1.6 Problems Solved
- 1.7 Benefits
- 1.8 Potential Commercial Applications
- 1.9 Possible Prior Art
- 1.10 Original Abstract Submitted
SYSTEMS AND METHODS FOR DEFORMATION CORRECTION OF A GAS TURBINE SHROUD
Organization Name
Inventor(s)
Joshua Depot of Greenville SC (US)
Jacob A. Salm of Greenville SC (US)
Jeremy E. Gard of Greenville SC (US)
Ellison Lenz of Greenville SC (US)
SYSTEMS AND METHODS FOR DEFORMATION CORRECTION OF A GAS TURBINE SHROUD - A simplified explanation of the abstract
This abstract first appeared for US patent application 18345536 titled 'SYSTEMS AND METHODS FOR DEFORMATION CORRECTION OF A GAS TURBINE SHROUD
Simplified Explanation
The present application provides a deformation correction system for a hot gas path surface of a turbine shroud. The deformation correction system may include a first die having a curved surface and a second die such that the hot gas path surface of the turbine shroud is positioned between the first die and the second die.
- Explanation of the patent/innovation:
- Deformation correction system for turbine shroud hot gas path surface - Includes first die with curved surface and second die - Hot gas path surface positioned between dies for correction
Potential Applications
The technology can be applied in: - Gas turbine manufacturing - Aerospace industry - Power generation sector
Problems Solved
- Correcting deformations in turbine shroud hot gas path surface - Ensuring optimal performance of gas turbines - Improving efficiency and reliability of turbine components
Benefits
- Enhanced performance of gas turbines - Increased efficiency in power generation - Extended lifespan of turbine components
Potential Commercial Applications
Title: Deformation Correction System for Turbine Shroud Hot Gas Path Surface in Industrial Applications - Gas turbine manufacturers - Aerospace companies - Power generation plants
Possible Prior Art
There may be prior art related to: - Deformation correction systems for turbine components - Hot gas path surface correction techniques in industrial machinery
Unanswered Questions
How does the deformation correction system impact the overall efficiency of the turbine?
The deformation correction system ensures that the hot gas path surface is properly aligned, leading to improved airflow and combustion efficiency within the turbine.
What materials are typically used in the construction of the first and second dies in such systems?
The first and second dies are often made of high-strength materials such as steel or ceramic to withstand the high temperatures and pressures involved in turbine operations.
Original Abstract Submitted
The present application provides a deformation correction system for a hot gas path surface of a turbine shroud. The deformation correction system may include a first die having a curved surface and a second die such that the hot gas path surface of the turbine shroud is positioned between the first die and the second die.
