Inventor
PIXTON STEPHEN G
US15 patents
⚠️ This page may combine multiple inventors who share the name “PIXTON STEPHEN G”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
RAYTHEON TECH CORP
7 patentsUS11454129B1Sep 27, 2022
CMC component flow discourager flanges
RAYTHEON TECH CORP7 citations83
US11814968B2Nov 14, 2023
Gas turbine engine with idle thrust ratio
RAYTHEON TECH CORP2 citations69
US11754000B2Sep 12, 2023
High and low spool configuration for a gas turbine engine
RAYTHEON TECH CORP0 citations61
US11808154B2Nov 7, 2023
CMC component flow discourager flanges
RAYTHEON TECH CORP1 citations60
US12392280B2Aug 19, 2025
Gas turbine engine with high low spool power extraction ratio
RAYTHEON TECH CORP0 citations51
US12123356B2Oct 22, 2024
Gas turbine engine with higher low spool torque-to-thrust ratio
RAYTHEON TECH CORP0 citations51
US11719245B2Aug 8, 2023
Compressor arrangement for a gas turbine engine
RAYTHEON TECH CORP0 citations50
RTX CORP
4 patentsUS12203385B1Jan 21, 2025
Telescoping guide vane for aircraft propulsion system
RTX CORP2 citations73
US12352287B1Jul 8, 2025
Variable guide vane for aircraft propulsion system
RTX CORP0 citations61
US12098681B2Sep 24, 2024
High and low spool configuration for a gas turbine engine
RTX CORP0 citations61
US12123310B2Oct 22, 2024
Gas turbine engine with idle thrust ratio
RTX CORP0 citations59
UNITED TECHNOLOGIES CORP
3 patentsUS9771863B2Sep 26, 2017
Gas turbine engine with embedded distributed fans
UNITED TECHNOLOGIES CORP1 citations52
US9897001B2Feb 20, 2018
Compressor areas for high overall pressure ratio gas turbine engine
UNITED TECHNOLOGIES CORP1 citations51
US10472071B2Nov 12, 2019
Hybrid compressor bleed air for aircraft use
UNITED TECHNOLOGIES CORP0 citations41