Inventor
ROSE BECKY E
US23 patents
⚠️ This page may combine multiple inventors who share the name “ROSE BECKY E”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
11 patentsUS9932933B2Apr 3, 2018
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
UNITED TECHNOLOGIES CORP33 citations93
US9920653B2Mar 20, 2018
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
UNITED TECHNOLOGIES CORP17 citations93
US10301971B2May 28, 2019
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
UNITED TECHNOLOGIES CORP13 citations92
US9920708B2Mar 20, 2018
Nose cone assembly and method of circulating air in a gas turbine engine
UNITED TECHNOLOGIES CORP7 citations84
US9038366B2May 26, 2015
LPC flowpath shape with gas turbine engine shaft bearing configuration
UNITED TECHNOLOGIES CORP14 citations84
US7963742B2Jun 21, 2011
Variable compressor stator vane having extended fillet
UNITED TECHNOLOGIES CORP13 citations81
US10544802B2Jan 28, 2020
Compressor flowpath
UNITED TECHNOLOGIES CORP3 citations73
US11286811B2Mar 29, 2022
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
UNITED TECHNOLOGIES CORP2 citations72
US11015550B2May 25, 2021
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
UNITED TECHNOLOGIES CORP2 citations72
US11125168B2Sep 21, 2021
Dirt mitigation in a gas turbine engine
UNITED TECHNOLOGIES CORP3 citations71
US11261800B2Mar 1, 2022
Adaptive bleed schedule in a gas turbine engine
UNITED TECHNOLOGIES CORP1 citations60
RAYTHEON TECH CORP
7 patentsUS12509993B1Dec 30, 2025
Composite airfoil with integrated anti-icing for an aircraft propulsion system
RAYTHEON TECH CORP0 citations62
US11781505B2Oct 10, 2023
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
RAYTHEON TECH CORP0 citations62
US11781447B2Oct 10, 2023
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
RAYTHEON TECH CORP0 citations62
US11725670B2Aug 15, 2023
Compressor flowpath
RAYTHEON TECH CORP0 citations62
US11428242B2Aug 30, 2022
Compressor flowpath
RAYTHEON TECH CORP0 citations62
US11680531B2Jun 20, 2023
Adaptive bleed schedule in a gas turbine engine
RAYTHEON TECH CORP1 citations60
US12523979B2Jan 13, 2026
Method of repairing a stack of integrally bladed rotors
RAYTHEON TECH CORP0 citations50