Inventor
HANRAHAN PAUL R
US75 patents
⚠️ This page may combine multiple inventors who share the name “HANRAHAN PAUL R”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
RAYTHEON TECH CORP
21 patentsUS11781506B2Oct 10, 2023
Splitter and guide vane arrangement for gas turbine engines
RAYTHEON TECH CORP9 citations86
US11639690B1May 2, 2023
Boost spool flow control and generator load matching via load compressor
RAYTHEON TECH CORP7 citations86
US11193425B2Dec 7, 2021
Gearbox for boost spool turbine engine
RAYTHEON TECH CORP11 citations84
US11891953B2Feb 6, 2024
Aircraft skin heat exchanger
RAYTHEON TECH CORP2 citations73
US11692491B1Jul 4, 2023
Transmission and method for control of boost spool
RAYTHEON TECH CORP3 citations73
US11674548B2Jun 13, 2023
Low profile rotating bearing centering spring
RAYTHEON TECH CORP2 citations73
US12253026B1Mar 18, 2025
Rear bearing air sourced and vented to nose cone
RAYTHEON TECH CORP1 citations64
US11506146B2Nov 22, 2022
Systems and methods for hybrid electric turbine engines
RAYTHEON TECH CORP1 citations63
US11408343B1Aug 9, 2022
Turboshaft engine with axial compressor
RAYTHEON TECH CORP1 citations63
US12163476B1Dec 10, 2024
Inter-rotating assembly power coupling system for turbine engine
RAYTHEON TECH CORP1 citations62
US12158112B1Dec 3, 2024
Selective power distribution for an aircraft propulsion system
RAYTHEON TECH CORP0 citations62
US12129802B2Oct 29, 2024
Selective power distribution for an aircraft propulsion system
RAYTHEON TECH CORP1 citations62
US12043405B2Jul 23, 2024
Selective power distribution for an aircraft propulsion system
RAYTHEON TECH CORP0 citations62
US11976598B2May 7, 2024
Transmission and method for control of boost spool
RAYTHEON TECH CORP1 citations62
US11958624B2Apr 16, 2024
Selective power distribution for an aircraft propulsion system
RAYTHEON TECH CORP0 citations62
US11898490B2Feb 13, 2024
Transmission and method for control of boost spool
RAYTHEON TECH CORP1 citations62
US11591911B2Feb 28, 2023
Pressure gain for cooling flow in aircraft engines
RAYTHEON TECH CORP0 citations62
US11268442B2Mar 8, 2022
Mid mount sleeve arrangement
RAYTHEON TECH CORP1 citations62
US11753990B2Sep 12, 2023
Augmented drive of compressors via differential and multistage turbine
RAYTHEON TECH CORP0 citations61
US11448125B2Sep 20, 2022
Multistage gas turbine engine with differential drive of compressor
RAYTHEON TECH CORP0 citations59
US12292005B2May 6, 2025
Aircraft propulsion system geartrain
RAYTHEON TECH CORP0 citations58
RTX CORP
14 patentsUS12071900B2Aug 27, 2024
Aircraft propulsion system geartrain
RTX CORP2 citations71
US12253021B2Mar 18, 2025
Transmission and method for control of boost spool
RTX CORP1 citations64
US12385449B2Aug 12, 2025
Splitter and guide vane arrangement for gas turbine engines
RTX CORP0 citations63
US12552545B1Feb 17, 2026
Drivetrain for aircraft powerplant with boosted turbine engine
RTX CORP0 citations62
US12497905B1Dec 16, 2025
Non-uniform and bi-tri stator spacing for swirl recovery vane (SRV) open rotor engines
RTX CORP0 citations62
US12492663B2Dec 9, 2025
Aircraft propulsion system geartrain
RTX CORP0 citations62
US12398679B2Aug 26, 2025
Transmission and method for control of boost spool
RTX CORP0 citations62
US12188551B1Jan 7, 2025
Reduced clearance interface between a fluid device and a rotating structure for a geartrain
RTX CORP0 citations62
US11840958B2Dec 12, 2023
Turbofan with offset gas generator and auxiliary power core
RTX CORP1 citations62
US12173644B2Dec 24, 2024
Augmented drive of compressors via differential and multistage turbine
RTX CORP0 citations61
US12540579B2Feb 3, 2026
Remote mounted accessory gearbox
RTX CORP0 citations60
US12466548B2Nov 11, 2025
Aircraft vertical stabilizer with air system
RTX CORP0 citations60
US12378000B2Aug 5, 2025
Aircraft propulsion system geartrain
RTX CORP0 citations58
US12292006B2May 6, 2025
Aircraft propulsion system with multi-direction bleed valve
RTX CORP0 citations58
UNITED TECHNOLOGIES CORP
12 patentsUS11143142B2Oct 12, 2021
Adaptive engine with boost spool
UNITED TECHNOLOGIES CORP17 citations86
US10100739B2Oct 16, 2018
Cooled cooling air system for a gas turbine engine
UNITED TECHNOLOGIES CORP10 citations84
US11073107B1Jul 27, 2021
Systems and methods for hybrid electric turbine engines
UNITED TECHNOLOGIES CORP4 citations73
US10731510B2Aug 4, 2020
Gas turbine engine with fluid damper
UNITED TECHNOLOGIES CORP5 citations73
US10094277B2Oct 9, 2018
Gas turbine engine configured for modular assembly/disassembly and method for same
UNITED TECHNOLOGIES CORP2 citations73
US9869250B2Jan 16, 2018
Particle tolerant turboshaft engine
UNITED TECHNOLOGIES CORP3 citations73
US10794193B2Oct 6, 2020
Air foil with galvanic protection
UNITED TECHNOLOGIES CORP4 citations72
US11421590B2Aug 23, 2022
Augmented drive of compressors via differential and multistage turbine
UNITED TECHNOLOGIES CORP2 citations71
US11578668B2Feb 14, 2023
Gas turbine engine control based on characteristic of cooled air
UNITED TECHNOLOGIES CORP3 citations70
US10914235B2Feb 9, 2021
Cooled cooling air system for a gas turbine engine
UNITED TECHNOLOGIES CORP0 citations63
US10364749B2Jul 30, 2019
Cooling air heat exchanger scoop
UNITED TECHNOLOGIES CORP1 citations63
US10844787B2Nov 24, 2020
Gas turbine engine configured for modular assembly/disassembly and method for same
UNITED TECHNOLOGIES CORP1 citations62
HANRAHAN PAUL R
1 patentISOM JOSHUA D
1 patentPRESTON JOHN L
1 patentShowing the top 50 of 75 patents by PatentIndex Score.