Constantine Baltas has been granted 15 US patents while listed as an inventor at RTX (Raytheon) . The first was granted in 2012 and the most recent in July 2022. Constantine Baltas ranks #307,048 of 4,157,543 US inventors in our database (top 7.4%). Patent records list Constantine Baltas in Manchester, CT, US.
Patents per Year Patents granted per year, 2012 to 2022 Bar chart with a peak of 3 patents in 2019. peak 3 2012: 2 patents 2012 2013: 1 patents 2013 2014: 1 patents 2014 2015: 1 patents 2015 2016: 1 patents 2016 2018: 2 patents 2018 2019: 3 patents 2019 2020: 1 patents 2020 2021: 1 patents 2021 2022: 2 patents 2022
Issued Patents All Time
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Showing 1–15 of 15 patents
Patent # Title Co-Inventors Date Approx Value ⓘ
11391240 Gas turbine engine bifurcation located fan variable area nozzle — 2022-07-19
$33,487,000
RE48980 Acoustic liner with varied properties Jonathan Gilson 2022-03-22
10989143 Gas turbine engine bifurcation located fan variable area nozzle — 2021-04-27
$73,868,000
10808617 Split-zone flow metering T-tube Jorge I. Farah , Kalpendu J. Parekh 2020-10-20
$13,954,000
10371001 Variable fan nozzle using shape memory material Amr Ali 2019-08-06
$8,916,000
10287987 Noise reducing vane Oliver V. Atassi 2019-05-14
$12,268,000
10184340 Geared turbofan engine having a reduced number of fan blades and improved acoustics Jonathan Gilson 2019-01-22
$19,271,000
10066548 Acoustic liner with varied properties Jonathan Gilson 2018-09-04
$18,786,000
9885313 Gas turbine engine bifurcation located fan variable area nozzle — 2018-02-06
9328695 Variable fan nozzle using shape memory material Amr Ali 2016-05-03
$24,923,000
9017037 Rotor with flattened exit pressure profile Dilip Prasad , Edward J. Gallagher 2015-04-28
$31,064,000
8857151 Corrugated core cowl for a gas turbine engine — 2014-10-14
$15,224,000
8418471 Gas turbine engine having variable flow through a bifurcation having an intake with multiple louvers — 2013-04-16
$22,397,000
8291689 Corrugated core cowl for a gas turbine engine — 2012-10-23
$16,579,000
8256225 Gas turbine engine with a variable exit area fan nozzle, nacelle assembly of such a engine, and corresponding operating method Joseph R. Hauser 2012-09-04
$18,534,000
