Geometrically Segmented Coating for Blade Outer Air Seal Spallation
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Solution Overview
Problem
Conventional blade outer air seals in gas turbine engines face issues with spallation, particularly at the leading end and circumferential side where the blade first encounters airflow, leading to reduced durability and potential exposure of the underlying alloy.
Innovation Solution
A geometrically segmented coating section with an array of cells, such as parallel elongated grooves, sloped grooves, or cylindrical cells, is applied on the leading end and circumferential side of the seal arc-segment to reduce internal stresses and enhance spallation durability, using a ceramic coating that fills the cells to create faults for stress relief.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If a conventional blade outer air seal is used, then the seal structure is simple, but spallation occurs at the leading end and circumferential side reducing durability
Solution Approach 1:
The coating is divided into multiple segments including a geometrically segmented coating section with an array of cells (such as elongated grooves, sloped grooves, or cylindrical cells) and a non-geometrically segmented coating section. This segmentation allows different regions of the coating to serve different functions: the geometrically segmented portion dissipates internal stresses through faults in the cells, while the non-geometrically segmented portion provides continuous protection. The segmentation resolves the contradiction by enabling stress management without requiring complete redesign of the entire coating structure.
Solution Approach 2:
The coating is designed with non-uniform properties: the geometrically segmented coating section is applied specifically to the leading end and circumferential side where spallation is most likely to occur, while the non-geometrically segmented coating section is applied to other areas. This local differentiation allows the coating to provide enhanced stress relief and spallation resistance exactly where needed, rather than uniformly across the entire seal surface, thus improving reliability without excessive complexity.
2Reliability
If a geometrically segmented coating with array of cells is applied, then internal stresses are dissipated and spallation durability is improved, but the manufacturing process becomes more complex
Solution Approach 1:
The coating structure is segmented into cells (elongated grooves, sloped grooves, or cylindrical cells) that are designed to fail in controlled ways. When internal stresses develop, faults form within these cells rather than causing delamination from the substrate. This segmentation transforms the manufacturing challenge into a manageable process where the coating is applied as a continuous layer over a pre-formed cellular structure, rather than requiring complex multi-step coating processes.
Solution Approach 2:
The geometrically segmented coating structure is designed beforehand to accommodate and dissipate internal stresses that will inevitably develop during operation. The array of cells creates a framework that can absorb stress through internal faulting before the stress can propagate to cause spallation. This beforehand cushioning approach allows the coating to be applied using standard techniques while the underlying cellular structure provides the stress management capability.
3Reliability
If the geometrically segmented coating is applied only to specific regions, then spallation resistance is enhanced at critical areas, but the coating application process requires precise positioning
Solution Approach 1:
The coating is applied with different geometric characteristics to different regions of the blade outer air seal. The geometrically segmented coating section is specifically applied to the leading end and circumferential side where spallation is most likely to occur due to blade encounter stresses. The non-geometrically segmented coating section is applied to other areas where continuous coverage is sufficient. This local quality approach targets protection precisely where needed while using simpler coating methods elsewhere, reducing the overall precision requirement compared to applying complex geometry everywhere.
Solution Approach 2:
The coating application is segmented into distinct zones: the geometrically segmented coating section covering the leading end and circumferential side, and the non-geometrically segmented coating section covering other areas. This segmentation allows each zone to be optimized independently for its specific functional requirements, with the geometrically segmented zone receiving enhanced protection and the other zones receiving standard protection, thereby managing manufacturing precision requirements effectively.
Data Source
Figure 1~2
Figure 3A~3C
Figure 4A~8B
AI summary
A blade outer air seal (60) for a gas turbine engine (20) includes a seal arc-segment (66;166;266;366;466;566) that defines a gaspath side (66a), a non-gaspath side (66b), leading and trailing ends (66c,66d), and first and second circumferential sides (66e,66f). A portion of the gaspath side (66a) has a geometrically segmented coating section (70). The geometrically segmented coating section (70) includes a wall (74) that has an array of cells (76;176;276;376;476;576;676;776), and a coating (78) disposed in the array of cells (76;176;276;376;476;576;676;776).