Inventor
GENERALE ADAM P
US21 patents
⚠️ This page may combine multiple inventors who share the name “GENERALE ADAM P”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
16 patentsUS11473444B2Oct 18, 2022
Ceramic airfoil with cooling air turn
UNITED TECHNOLOGIES CORP9 citations84
US11608749B2Mar 21, 2023
Airfoil having environmental barrier topcoats that vary in composition by location
UNITED TECHNOLOGIES CORP2 citations73
US10711624B2Jul 14, 2020
Airfoil with geometrically segmented coating section
UNITED TECHNOLOGIES CORP2 citations73
US11162368B2Nov 2, 2021
Airfoil assembly with ceramic airfoil pieces and seal
UNITED TECHNOLOGIES CORP3 citations72
US11131212B2Sep 28, 2021
Gas turbine engine cooling component
UNITED TECHNOLOGIES CORP2 citations72
US10934857B2Mar 2, 2021
Shell and spar airfoil
UNITED TECHNOLOGIES CORP5 citations72
US10822963B2Nov 3, 2020
Axial flow cooling scheme with castable structural rib for a gas turbine engine
UNITED TECHNOLOGIES CORP2 citations72
US11092015B2Aug 17, 2021
Airfoil with metallic shield
UNITED TECHNOLOGIES CORP0 citations62
US11078844B2Aug 3, 2021
Thermal gradient reducing device for gas turbine engine component
UNITED TECHNOLOGIES CORP1 citations62
US11280201B2Mar 22, 2022
Baffle with tail
UNITED TECHNOLOGIES CORP0 citations61
US11371360B2Jun 28, 2022
Components for gas turbine engines
UNITED TECHNOLOGIES CORP0 citations51
US10648351B2May 12, 2020
Gas turbine engine cooling component
UNITED TECHNOLOGIES CORP0 citations51
US11415002B2Aug 16, 2022
Baffle with impingement holes
UNITED TECHNOLOGIES CORP0 citations50
US10822962B2Nov 3, 2020
Vane platform leading edge recessed pocket with cover
UNITED TECHNOLOGIES CORP0 citations50
US10619492B2Apr 14, 2020
Vane air inlet with fillet
UNITED TECHNOLOGIES CORP0 citations44
US10655496B2May 19, 2020
Platform flow turning elements for gas turbine engine components
UNITED TECHNOLOGIES CORP0 citations41
RAYTHEON TECH CORP
5 patentsUS11492914B1Nov 8, 2022
Engine with cooling passage circuit for air prior to ceramic component
RAYTHEON TECH CORP2 citations71
US12044146B2Jul 23, 2024
Airfoil having environmental barrier topcoats that vary in composition by location
RAYTHEON TECH CORP0 citations62
US11261749B2Mar 1, 2022
Components for gas turbine engines
RAYTHEON TECH CORP0 citations62
US11242758B2Feb 8, 2022
Trailing edge insert for airfoil vane
RAYTHEON TECH CORP0 citations62
US11339667B2May 24, 2022
Cooling arrangement including overlapping diffusers
RAYTHEON TECH CORP0 citations51