GEARED TURBINE ENGINE WITH A D-DUCT AND A THRUST REVERSER
Number of patents in Portfolio can not be more than 2000
United States of America Patent
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N/A
Issued Date -
Oct 1, 2015
app pub date -
Oct 10, 2013
filing date -
Oct 10, 2012
priority date (Note) -
Published
status (Latency Note)
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Abstract
A geared turbine engine includes a first rotor, a second rotor, a gear train and an engine casing. The rotors and the gear train are arranged along an axial centerline. The gear train connects the first rotor to the second rotor. The casing extends circumferentially around the centerline and houses the first rotor, the second rotor and/or the gear train. The casing includes a casing door. The casing door includes a duct and a thrust reverser. The duct extends axially along and at least partially around the centerline.
First Claim
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| Country | kind | publication No. | Filing Date |
|---|---|---|---|
| WO | A2 | WO2014116308 | Oct 10, 2013 |
| EP | A2 | EP2906808 | Oct 10, 2013 |
International Classification(s)
- 2013 Application Filing Year
- F02K Class
- 252 Applications Filed
- 226 Patents Issued To-Date
- 89.69 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 8 Citation Count
- F02K Class
- 10 % this patent is cited more than
- 10 Age