18147138. COOLING HOLE POSITIONING SYSTEMS AND METHODS simplified abstract (General Electric Company)
Contents
- 1 COOLING HOLE POSITIONING SYSTEMS AND METHODS
- 1.1 Organization Name
- 1.2 Inventor(s)
- 1.3 COOLING HOLE POSITIONING SYSTEMS AND METHODS - A simplified explanation of the abstract
- 1.4 Simplified Explanation
- 1.5 Potential Applications
- 1.6 Problems Solved
- 1.7 Benefits
- 1.8 Commercial Applications
- 1.9 Prior Art
- 1.10 Frequently Updated Research
- 1.11 Questions about Turbine Engine Component Inspection and Manufacturing
- 1.12 Original Abstract Submitted
COOLING HOLE POSITIONING SYSTEMS AND METHODS
Organization Name
Inventor(s)
Yusuf Eren Ozturk of Istanbul (TR)
Ertugrul Dursun of Kadikoy (TR)
COOLING HOLE POSITIONING SYSTEMS AND METHODS - A simplified explanation of the abstract
This abstract first appeared for US patent application 18147138 titled 'COOLING HOLE POSITIONING SYSTEMS AND METHODS
Simplified Explanation
The patent application describes systems and methods to locate cooling holes on a turbine engine component's outer surface using three-dimensional and two-dimensional measurements. By analyzing geometric features, a scan area is determined, and the cooling hole's position is located. The surface profile and orientation of the cooling hole are extracted to calculate its three-dimensional coordinates.
- Three-dimensional and two-dimensional measurements used to locate cooling holes on a turbine engine component's outer surface.
- Analysis of geometric features to determine a scan area for locating the cooling hole.
- Extraction of surface profile and orientation to calculate three-dimensional coordinates of the cooling hole.
Potential Applications
This technology can be applied in the aerospace industry for efficiently locating and analyzing cooling holes on turbine engine components. It can also be used in manufacturing processes to ensure precise placement of cooling holes for optimal engine performance.
Problems Solved
This technology addresses the challenge of accurately locating cooling holes on complex turbine engine components. It streamlines the measurement process and enhances the overall efficiency of maintenance and manufacturing operations.
Benefits
- Improved accuracy in locating cooling holes on turbine engine components - Enhanced efficiency in maintenance and manufacturing processes - Optimal performance of turbine engines due to precise placement of cooling holes
Commercial Applications
Title: Advanced Turbine Engine Component Inspection and Manufacturing This technology can be commercially utilized by aerospace companies, turbine engine manufacturers, and maintenance facilities. It offers a competitive advantage by ensuring precise cooling hole placement, leading to enhanced engine performance and reliability.
Prior Art
Further research can be conducted in the field of turbine engine component inspection and measurement techniques to explore existing technologies related to locating cooling holes on outer surfaces.
Frequently Updated Research
Researchers are continuously developing new methods and technologies for improving the inspection and maintenance of turbine engine components. Stay updated on the latest advancements in this field to leverage cutting-edge solutions for cooling hole detection.
Questions about Turbine Engine Component Inspection and Manufacturing
How does this technology benefit the aerospace industry?
This technology benefits the aerospace industry by enabling precise location and analysis of cooling holes on turbine engine components, leading to improved engine performance and reliability.
What are the potential applications of this technology beyond the aerospace industry?
This technology can also be applied in manufacturing processes to ensure accurate placement of cooling holes in various components for optimal performance.
Original Abstract Submitted
Systems and methods to locate the position of cooling holes on an outer surface of a turbine engine component, based on a three-dimensional measurement along an X-axis, a Y-axis, and a Z-axis, and an extracted two-dimensional measurement along the X-axis and the Y-axis. The two-dimensional data is analyzed to find a common geometric feature of the component and determine a scan area based on the common geometric feature. The component is measured within the scan area to locate a cooling hole located on the outer surface of the component. A surface profile of the cooling hole is extracted along the X-axis and the Y-axis, and an orientation of the cooling hole is extracted along the Z-axis. A three-dimensional coordinate set of the cooling hole is calculated based on the surface profile and the orientation.
