Coanda device for a round exhaust nozzle
Number of patents in Portfolio can not be more than 2000
United States of America
Stats
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Feb 18, 2020
Grant Date -
May 25, 2017
app pub date -
Jul 26, 2016
filing date -
Jul 26, 2016
priority date (Note) -
In Force
status (Latency Note)
Importance
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Abstract
A gas turbine engine system is disclosed herein. The gas turbine engine system includes an engine core configured to discharge air through an exhaust nozzle along a central axis and a thrust director arranged near the exhaust nozzle and configured to redirect the discharge air by applying flow to the discharge air near the exhaust nozzle.
First Claim
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International Classification(s)
- 2016 Application Filing Year
- F02K Class
- 527 Applications Filed
- 379 Patents Issued To-Date
- 71.92 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 0 Citation Count
- F02K Class
- 0 % this patent is cited more than
- 5 Age
Maintenance Fees
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| 7.5 Year Payment | $3600.00 | $1800.00 | $900.00 | Aug 18, 2027 |
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