Gas turbine combustor with enhanced cooling features
Number of patents in Portfolio can not be more than 2000
United States of America
Stats
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Sep 10, 2024
Grant Date -
N/A
app pub date -
May 8, 2023
filing date -
May 8, 2023
priority date (Note) -
In Force
status (Latency Note)
Importance
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US Family Size
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Non-US Coverage
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Abstract
A combustor for a gas turbine engine includes a combustor liner with a wall defining a combustion chamber. The wall has an inner surface facing the combustion chamber and an outer surface across the wall from the inner surface. Fins are disposed on the outer surface. The wall defines air admission holes that extend through the wall from the outer surface to the inner surface. The wall also defines film cooling holes that extend through the wall from the outer surface to the inner surface. The fins are disposed in areas of the outer surface between the film cooling holes and the air admission holes to cool areas that would otherwise result in hot spots.
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International Classification(s)
- 2023 Application Filing Year
- F23R Class
- 254 Applications Filed
- 102 Patents Issued To-Date
- 40.16 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 0 Citation Count
- F23R Class
- 0 % this patent is cited more than
- 1 Age
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