Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engine
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United States of America Patent
Stats
-
Aug 11, 2020
Grant Date -
Apr 5, 2018
app pub date -
Oct 3, 2016
filing date -
Oct 3, 2016
priority date (Note) -
In Force
status (Latency Note)
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Abstract
An injector of a radial fuel injection system for a combustor of a gas turbine engine includes a swirler; and a fuel nozzle located within the swirler, the fuel nozzle located within the swirler, the fuel nozzle operable to provide a biased radial fuel distribution within the swirler. A method of controlling a fuel flow to a combustor of a gas turbine engine includes selectively controlling a biased radial fuel distribution within a swirler of a radial fuel injection system.
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International Classification(s)
- 2016 Application Filing Year
- F23R Class
- 473 Applications Filed
- 309 Patents Issued To-Date
- 65.33 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 3 Citation Count
- F23R Class
- 38.74 % this patent is cited more than
- 5 Age
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|---|---|---|---|---|
| 7.5 Year Payment | $3600.00 | $1800.00 | $900.00 | Feb 11, 2028 |
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