18537983. METHOD AND SYSTEM FOR INSPECTING COOLING HOLES OF A TURBINE ENGINE COMPONENT simplified abstract (General Electric Company)
Contents
- 1 METHOD AND SYSTEM FOR INSPECTING COOLING HOLES OF A TURBINE ENGINE COMPONENT
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 METHOD AND SYSTEM FOR INSPECTING COOLING HOLES OF A TURBINE ENGINE COMPONENT - 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 Unanswered Questions
- 1.11 Original Abstract Submitted
METHOD AND SYSTEM FOR INSPECTING COOLING HOLES OF A TURBINE ENGINE COMPONENT
Organization Name
Inventor(s)
Guanghua Wang of Clifton Park NY (US)
Bryon Edward Knight of Ballston Lake NY (US)
Andrew Lee Trimmer of Niskayuna NY (US)
Jason Edward Dees of Liberty Township OH (US)
Bernard Patrick Bewlay of Niskayuna NY (US)
Sean Robert Farrell of Brookline MA (US)
METHOD AND SYSTEM FOR INSPECTING COOLING HOLES OF A TURBINE ENGINE COMPONENT - A simplified explanation of the abstract
This abstract first appeared for US patent application 18537983 titled 'METHOD AND SYSTEM FOR INSPECTING COOLING HOLES OF A TURBINE ENGINE COMPONENT
Simplified Explanation
The patent application describes a method of imaging a turbine engine test component with film holes for airflow. Thermographic data is obtained to calculate a performance score.
- Turbine engine test component has a first surface and a second surface with film holes.
- Airflow is flowed through the film holes of the component.
- Thermographic data is obtained to analyze the performance of the component.
- A test dataset is determined based on the thermographic data.
- A performance score is calculated to evaluate the efficiency of the component.
Potential Applications
The technology can be applied in the aerospace industry for testing and optimizing turbine engine components.
Problems Solved
This technology helps in evaluating the performance and efficiency of turbine engine components, ensuring optimal functionality.
Benefits
The method provides a non-intrusive way to assess the performance of turbine engine components, leading to improved efficiency and reliability.
Potential Commercial Applications
"Improving Turbine Engine Component Performance with Thermographic Data Analysis"
Possible Prior Art
There may be prior art related to thermographic analysis of turbine engine components for performance evaluation.
Unanswered Questions
How does the method compare to traditional testing techniques for turbine engine components?
The article does not provide a comparison between this method and traditional testing techniques for turbine engine components.
Are there any limitations to using thermographic data for performance evaluation of turbine engine components?
The article does not discuss any limitations or challenges associated with using thermographic data for performance evaluation.
Original Abstract Submitted
A method of imaging a turbine engine test component with a first surface and a second surface that is spaced from the first surface. The turbine engine test component includes a plurality of film holes with inlets formed in the second surface or interior that are fluidly coupled to outlets formed in the first surface or exterior. The method includes flowing airflow through the plurality of film holes of the turbine engine test component, obtaining thermographic data, determining a test dataset, and calculating a performance score.
