Gas turbine engine systems and methods involving enhanced fuel dispersion
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United States of America Patent
Stats
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Aug 25, 2015
Issued Date -
N/A
app pub date -
Sep 4, 2008
filing date -
Sep 4, 2008
priority date (Note) -
In Force
status (Latency Note)
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Abstract
Gas turbine engine systems and methods involving enhanced fuel dispersion are provided. In this regard, a representative method for operating a gas turbine engine includes: providing a gas path through the engine; introducing a spray of fuel along the gas path downstream of a turbine of the engine; and impinging the spray of fuel with a relatively higher velocity flow of air such that atomization of the fuel is increased.
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International Classification(s)
- 2008 Application Filing Year
- F02K Class
- 198 Applications Filed
- 143 Patents Issued To-Date
- 72.23 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 7 Citation Count
- F02K Class
- 10 % this patent is cited more than
- 10 Age
Maintenance Fees
| Fee | Large entity fee | small entity fee | micro entity fee | due date |
|---|---|---|---|---|
| 11.5 Year Payment | $7400.00 | $3700.00 | $1850.00 | Feb 25, 2027 |
