Gas Turbine Baffle Datum Features for Precise Fabrication
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Solution Overview
Problem
Existing gas turbine engine baffles face dimensional and geometric variations during fabrication, leading to dimensional errors that can result in re-work or scrapping, due to the use of temporary reference points which introduce inaccuracies in forming operations.
Innovation Solution
Incorporating semi-spherical datum features on the baffle's aft wall, which serve as fixed reference points to establish a stable position during fabrication, allowing for accurate forming, drilling, and assembly of impingement orifices and other components, reducing the need for temporary reference points and minimizing errors.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Productivity
If temporary reference points are used during fabrication, then the fabrication process is simpler and faster, but dimensional errors increase leading to re-work or scrapping
Solution Approach 1:
The patent incorporates permanent datum features directly into the baffle component design during the manufacturing process. These datum features are formed as integral parts of the baffle (such as recesses, protrusions, or machined surfaces) that serve as reference points for subsequent fabrication operations. By establishing these reference features as part of the preliminary manufacturing steps rather than using temporary external fixtures, the process eliminates the need for separate temporary reference points while maintaining both productivity and dimensional accuracy.
2Manufacturing precision
If permanent datum features are incorporated into the baffle, then manufacturing precision improves, but device complexity increases
Solution Approach 1:
The patent applies datum features at specific localized positions on the baffle component where they are most effective for reference purposes. Rather than making the entire baffle complex, only specific regions (such as the forward wall, aft wall, or selected surfaces) incorporate these reference features. This localized approach minimizes the impact on overall device complexity while achieving the desired improvement in manufacturing precision for critical operations.
3Device complexity
If temporary reference points are used, then the fabrication process is less complex, but reliability of fabrication decreases due to dimensional errors
Solution Approach 1:
The patent enables the baffle component to serve its own reference function through self-contained datum features. These permanent features are integral to the baffle design and provide stable, repeatable reference points that eliminate the need for external temporary fixtures. The component essentially references itself during subsequent fabrication operations, improving reliability by eliminating the variability associated with temporary reference points while keeping the fabrication process relatively simple.
Data Source
AI summary
A gas turbine engine article includes a baffle that is configured to be mounted in a cavity of a gas turbine engine component. The baffle has a baffle wall that circumscribes an open interior region. The baffle wall includes a forward wall, side walls, and an aft wall. The side walls include impingement orifices, and the aft wall defines two datum features. At least one of the datum features is a dimple that is a portion of a sphere.


