Inventor
BALTAS CONSTANTINE
US15 patents
⚠️ This page may combine multiple inventors who share the name “BALTAS CONSTANTINE”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
BALTAS CONSTANTINE
7 patentsUS8418471B2Apr 16, 2013
Gas turbine engine having variable flow through a bifurcation having an intake with multiple louvers
BALTAS CONSTANTINE21 citations91
US9017037B2Apr 28, 2015
Rotor with flattened exit pressure profile
BALTAS CONSTANTINE12 citations83
US9885313B2Feb 6, 2018
Gas turbine engine bifurcation located fan variable area nozzle
BALTAS CONSTANTINE10 citations82
US9328695B2May 3, 2016
Variable fan nozzle using shape memory material
BALTAS CONSTANTINE4 citations71
US8291689B2Oct 23, 2012
Corrugated core cowl for a gas turbine engine
BALTAS CONSTANTINE4 citations61
US8256225B2Sep 4, 2012
Gas turbine engine with a variable exit area fan nozzle, nacelle assembly of such a engine, and corresponding operating method
BALTAS CONSTANTINE5 citations57
US8857151B2Oct 14, 2014
Corrugated core cowl for a gas turbine engine
BALTAS CONSTANTINE0 citations50
UNITED TECHNOLOGIES CORP
4 patentsUS10184340B2Jan 22, 2019
Geared turbofan engine having a reduced number of fan blades and improved acoustics
UNITED TECHNOLOGIES CORP29 citations93
US10066548B2Sep 4, 2018
Acoustic liner with varied properties
UNITED TECHNOLOGIES CORP34 citations93
US10371001B2Aug 6, 2019
Variable fan nozzle using shape memory material
UNITED TECHNOLOGIES CORP0 citations51
US10287987B2May 14, 2019
Noise reducing vane
UNITED TECHNOLOGIES CORP0 citations51
RAYTHEON TECH CORP
3 patentsUS10989143B2Apr 27, 2021
Gas turbine engine bifurcation located fan variable area nozzle
RAYTHEON TECH CORP1 citations72
USRE48980EMar 22, 2022
Acoustic liner with varied properties
RAYTHEON TECH CORP0 citations62
US11391240B2Jul 19, 2022
Gas turbine engine bifurcation located fan variable area nozzle
RAYTHEON TECH CORP0 citations61