Inventor
MAGGE SHANKAR S
US25 patents
⚠️ This page may combine multiple inventors who share the name “MAGGE SHANKAR S”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
9 patentsUS10060357B2Aug 28, 2018
Turbine section of high bypass turbofan
UNITED TECHNOLOGIES CORP23 citations94
US7094034B2Aug 22, 2006
Airfoil profile with optimized aerodynamic shape
UNITED TECHNOLOGIES CORP45 citations91
US8052388B2Nov 8, 2011
Gas turbine engine systems involving mechanically alterable vane throat areas
UNITED TECHNOLOGIES CORP20 citations90
US10371061B2Aug 6, 2019
Turbine section of high bypass turbofan
UNITED TECHNOLOGIES CORP11 citations84
US8850793B2Oct 7, 2014
Turbine section of high bypass turbofan
UNITED TECHNOLOGIES CORP11 citations84
US8915090B2Dec 23, 2014
Gas turbine engine mid turbine frame with flow turning features
UNITED TECHNOLOGIES CORP6 citations82
US8561414B1Oct 22, 2013
Gas turbine engine mid turbine frame with flow turning features
UNITED TECHNOLOGIES CORP12 citations82
US10794293B2Oct 6, 2020
Turbine section of high bypass turbofan
UNITED TECHNOLOGIES CORP0 citations52
US10662880B2May 26, 2020
Turbine section of high bypass turbofan
UNITED TECHNOLOGIES CORP0 citations52
RAYTHEON TECH CORP
7 patentsUS11149650B2Oct 19, 2021
Turbine section of high bypass turbofan
RAYTHEON TECH CORP7 citations84
US11480108B2Oct 25, 2022
Turbine section of high bypass turbofan
RAYTHEON TECH CORP2 citations73
US11346289B2May 31, 2022
Turbine section of high bypass turbofan
RAYTHEON TECH CORP2 citations73
US11242805B2Feb 8, 2022
Turbine section of high bypass turbofan
RAYTHEON TECH CORP5 citations73
US11614036B2Mar 28, 2023
Turbine section of gas turbine engine
RAYTHEON TECH CORP0 citations62
US11486311B2Nov 1, 2022
Turbine section of high bypass turbofan
RAYTHEON TECH CORP1 citations62
US11215123B2Jan 4, 2022
Turbine section of high bypass turbofan
RAYTHEON TECH CORP0 citations62