Inventor · disambiguated record
Becky E. Rose
Also filed as: ROSE BECKY · ROSE BECKY E
23 granted patents·5 pending applications·162 citations·filing 2006–2023
95Inventor score
Files withUNITED TECHNOLOGIES CORP15RAYTHEON TECH CORP7BRILLIANT LISA I2GALLAGHER EDWARD J2ROSE BECKY E1
Top patents by PatentIndex Score
28 records- 0197US10301971B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 28, 2019·13 cites·30 claims
- 0297US9932933B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2013·Granted Apr 3, 2018·33 cites·19 claims
- 0396US9920653B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2012·Granted Mar 20, 2018·17 cites·20 claims
- 0493US10526894B1Short inlet with low solidity fan exit guide vane arrangementsUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jan 7, 2020·8 cites·18 claims
- 0592US9121412B2Efficient, low pressure ratio propulsor for gas turbine enginesGALLAGHER EDWARD J·Filed 2011·Granted Sep 1, 2015·14 cites·11 claims
- 0691US9920708B2Nose cone assembly and method of circulating air in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 20, 2018·7 cites·19 claims
- 0790US9038366B2LPC flowpath shape with gas turbine engine shaft bearing configurationUNITED TECHNOLOGIES CORP·Filed 2013·Granted May 26, 2015·14 cites·22 claims
- 0888US10544802B2Compressor flowpathUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jan 28, 2020·3 cites·13 claims
- 0987US8452516B1Variable vane scheduling based on flight conditions for inclement weatherROSE BECKY E·Filed 2012·Granted May 28, 2013·17 cites·22 claims
- 1086US11286811B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 29, 2022·2 cites·26 claims
- 1186US8438832B1High turning fan exit statorBRILLIANT LISA I·Filed 2012·Granted May 14, 2013·14 cites·21 claims
- 1285US11680531B2Adaptive bleed schedule in a gas turbine engineRAYTHEON TECH CORP·Filed 2022·Granted Jun 20, 2023·1 cites·20 claims
- 1382US11125168B2Dirt mitigation in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 21, 2021·3 cites·20 claims
- 1481US11971051B2Compressor flowpathRTX CORP·Filed 2023·Granted Apr 30, 2024·0 cites·19 claims
- 1580US11015550B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 25, 2021·2 cites·18 claims
- 1677US11725670B2Compressor flowpathRAYTHEON TECH CORP·Filed 2022·Granted Aug 15, 2023·0 cites·30 claims
- 1772US11781447B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeRAYTHEON TECH CORP·Filed 2021·Granted Oct 10, 2023·0 cites·30 claims
- 1872US7963742B2Variable compressor stator vane having extended filletUNITED TECHNOLOGIES CORP·Filed 2006·Granted Jun 21, 2011·13 cites·19 claims
- 1970US11261800B2Adaptive bleed schedule in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Mar 1, 2022·1 cites·20 claims
- 2069US11781505B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeRAYTHEON TECH CORP·Filed 2021·Granted Oct 10, 2023·0 cites·30 claims
- 2168US11428242B2Compressor flowpathRAYTHEON TECH CORP·Filed 2019·Granted Aug 30, 2022·0 cites·20 claims
- 2266US2020063603A1Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2363US12509993B1Composite airfoil with integrated anti-icing for an aircraft propulsion systemRAYTHEON TECH CORP·Filed 2023·Granted Dec 30, 2025·0 cites·18 claims
- 2448US2023315938A1Systems and methods for aerodynamic analysis for inspected bladed rotorsRAYTHEON TECH CORP·Filed 2022·Application pending·0 cites
- 2544US9115649B2Fan stagger angle for dirt rejectionGALLAGHER EDWARD J·Filed 2011·Granted Aug 25, 2015·0 cites·23 claims
- 2644US2013192198A1Compressor flowpathBRILLIANT LISA I·Filed 2012·Application pending·0 cites
- 2741US2017314562A1Efficient low pressure ratio propulsor stage for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2016·Application pending·0 cites
- 2841US2016108854A1Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
Join the waitlist — get patent alerts
Get an alert when Becky E. Rose files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →