Inventor
ARISI ALLAN N
US23 patents
⚠️ This page may combine multiple inventors who share the name “ARISI ALLAN N”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
18 patentsUS11041390B1Jun 22, 2021
Turbine airfoil having film cooling hole arrangement
UNITED TECHNOLOGIES CORP6 citations82
US11512597B2Nov 29, 2022
Airfoil with cavity lobe adjacent cooling passage network
UNITED TECHNOLOGIES CORP2 citations73
US11377964B2Jul 5, 2022
Airfoil with cooling passage network having arced leading edge
UNITED TECHNOLOGIES CORP2 citations73
US11339718B2May 24, 2022
Minicore cooling passage network having trip strips
UNITED TECHNOLOGIES CORP4 citations73
US11028702B2Jun 8, 2021
Airfoil with cooling passage network having flow guides
UNITED TECHNOLOGIES CORP3 citations73
US11092017B2Aug 17, 2021
Mini core passage with protrusion
UNITED TECHNOLOGIES CORP1 citations62
US11028700B2Jun 8, 2021
Airfoil with cooling passage circuit through platforms and airfoil section
UNITED TECHNOLOGIES CORP1 citations62
US10844729B2Nov 24, 2020
Turbine vane for gas turbine engine
UNITED TECHNOLOGIES CORP1 citations62
US10584596B2Mar 10, 2020
Gas turbine engine components having internal cooling features
UNITED TECHNOLOGIES CORP1 citations62
US11939883B2Mar 26, 2024
Airfoil with arced pedestal row
UNITED TECHNOLOGIES CORP0 citations52
US11753944B2Sep 12, 2023
Airfoil with wall that tapers in thickness
UNITED TECHNOLOGIES CORP0 citations52
US11333023B2May 17, 2022
Article having cooling passage network with inter-row sub-passages
UNITED TECHNOLOGIES CORP0 citations52
US11293347B2Apr 5, 2022
Airfoil with baffle showerhead and cooling passage network having aft inlet
UNITED TECHNOLOGIES CORP0 citations52
US11248470B2Feb 15, 2022
Airfoil with core cavity that extends into platform shelf
UNITED TECHNOLOGIES CORP0 citations52
US11180998B2Nov 23, 2021
Airfoil with skincore passage resupply
UNITED TECHNOLOGIES CORP0 citations52
US11149556B2Oct 19, 2021
Minicore cooling passage network having sloped impingement surface
UNITED TECHNOLOGIES CORP0 citations51
US10975710B2Apr 13, 2021
Cooling circuit for gas turbine engine component
UNITED TECHNOLOGIES CORP0 citations51
US10677071B2Jun 9, 2020
Turbine vane for gas turbine engine
UNITED TECHNOLOGIES CORP0 citations51
RAYTHEON TECH CORP
5 patentsUS11203981B1Dec 21, 2021
Baffle systems for airfoils
RAYTHEON TECH CORP11 citations85
US11959397B2Apr 16, 2024
Airfoil with cooling passage network having arced leading edge
RAYTHEON TECH CORP0 citations62
US11486257B2Nov 1, 2022
Cooling passage configuration
RAYTHEON TECH CORP0 citations62
US10968752B2Apr 6, 2021
Turbine airfoil with minicore passage having sloped diffuser orifice
RAYTHEON TECH CORP1 citations62
US11339667B2May 24, 2022
Cooling arrangement including overlapping diffusers
RAYTHEON TECH CORP0 citations51