Combustor having dilution cooled liner
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Aug 6, 2024
Grant Date -
Nov 30, 2023
app pub date -
Sep 16, 2022
filing date -
May 24, 2022
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A combustor for a gas turbine has a combustor liner including an upstream liner portion, and a downstream liner portion. The upstream liner portion includes an outer shell and a heat shield panel, with a baffle cavity therebetween. The outer shell includes an outer shell cooling opening for providing a flow of compressed air to the baffle cavity, and the heat shield panel includes a heat shield panel cooling opening at a downstream end of the heat shield panel. A fence is arranged at a downstream side of the heat shield panel cooling opening and extends beyond a hot side surface of the heat shield panel into a combustion chamber. The heat shield panel cooling opening provides a flow of the compressed air therethrough from the baffle cavity for cooling of the heat shield panel and for providing at least partial dilution of combustion gases within the combustion chamber.
First Claim
Other Claims data not available
Family
International Classification(s)
- 2022 Application Filing Year
- F23R Class
- 253 Applications Filed
- 151 Patents Issued To-Date
- 59.69 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 0 Citation Count
- F23R Class
- 0 % this patent is cited more than
- 1 Age
Maintenance Fees
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|---|---|---|---|---|
| 3.5 Year Payment | $1600.00 | $800.00 | $400.00 | Feb 6, 2028 |
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