Inventor · disambiguated record
Constantine Baltas
Also filed as: BALTAS CONSTANTINE
15 granted patents·2 pending applications·120 citations·filing 2006–2021
91Inventor score
Top patents by PatentIndex Score
17 records- 0197US10066548B2Acoustic liner with varied propertiesUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 4, 2018·34 cites·36 claims
- 0296US10184340B2Geared turbofan engine having a reduced number of fan blades and improved acousticsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jan 22, 2019·29 cites·13 claims
- 0389US9017037B2Rotor with flattened exit pressure profileBALTAS CONSTANTINE·Filed 2012·Granted Apr 28, 2015·12 cites·23 claims
- 0488US9885313B2Gas turbine engine bifurcation located fan variable area nozzleBALTAS CONSTANTINE·Filed 2012·Granted Feb 6, 2018·10 cites·31 claims
- 0581US8418471B2Gas turbine engine having variable flow through a bifurcation having an intake with multiple louversBALTAS CONSTANTINE·Filed 2006·Granted Apr 16, 2013·21 cites·22 claims
- 0674US10989143B2Gas turbine engine bifurcation located fan variable area nozzleRAYTHEON TECH CORP·Filed 2018·Granted Apr 27, 2021·1 cites·29 claims
- 0770US9328695B2Variable fan nozzle using shape memory materialBALTAS CONSTANTINE·Filed 2006·Granted May 3, 2016·4 cites·22 claims
- 0869US11391240B2Gas turbine engine bifurcation located fan variable area nozzleRAYTHEON TECH CORP·Filed 2021·Granted Jul 19, 2022·0 cites·30 claims
- 0959US8291689B2Corrugated core cowl for a gas turbine engineBALTAS CONSTANTINE·Filed 2006·Granted Oct 23, 2012·4 cites·24 claims
- 1056US8256225B2Gas turbine engine with a variable exit area fan nozzle, nacelle assembly of such a engine, and corresponding operating methodBALTAS CONSTANTINE·Filed 2006·Granted Sep 4, 2012·5 cites·15 claims
- 1154USRE48980EAcoustic liner with varied propertiesRAYTHEON TECH CORP·Filed 2014·Granted Mar 22, 2022·0 cites·64 claims
- 1249US10371001B2Variable fan nozzle using shape memory materialUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 6, 2019·0 cites·2 claims
- 1349US8857151B2Corrugated core cowl for a gas turbine engineBALTAS CONSTANTINE·Filed 2012·Granted Oct 14, 2014·0 cites·20 claims
- 1447US10808617B2Split-zone flow metering T-tubeOne Financial Plaza·Filed 2016·Granted Oct 20, 2020·0 cites·4 claims
- 1547US10287987B2Noise reducing vaneUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 14, 2019·0 cites·16 claims
- 1640US2015252751A1Geared gas turbine engine integrated with a variable area fan nozzle with reduced noiseUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
- 1739US2015233298A1Reduction in jet flap interaction noise with geared turbine engineUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
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