Inventor
MUNSELL PETER M
US29 patents
⚠️ This page may combine multiple inventors who share the name “MUNSELL PETER M”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
15 patentsUS9416677B2Aug 16, 2016
Gas turbine engine forward bearing compartment architecture
UNITED TECHNOLOGIES CORP22 citations92
US6663346B2Dec 16, 2003
Compressor stator inner diameter platform bleed system
UNITED TECHNOLOGIES CORP51 citations92
US10487734B2Nov 26, 2019
Gas turbine engine buffer system
UNITED TECHNOLOGIES CORP8 citations84
US10465549B2Nov 5, 2019
Gas turbine engine forward bearing compartment architecture
UNITED TECHNOLOGIES CORP3 citations84
US9885249B2Feb 6, 2018
Gas turbine engine forward bearing compartment architecture
UNITED TECHNOLOGIES CORP5 citations84
US7797941B2Sep 21, 2010
Gas turbine engine systems involving hydrostatic face seals
UNITED TECHNOLOGIES CORP17 citations84
US10087782B2Oct 2, 2018
Engine mid-turbine frame transfer tube for low pressure turbine case cooling
UNITED TECHNOLOGIES CORP7 citations82
US11098644B2Aug 24, 2021
Gas turbine engine buffer system
UNITED TECHNOLOGIES CORP2 citations73
US10920603B2Feb 16, 2021
Gas turbine engine forward bearing compartment architecture
UNITED TECHNOLOGIES CORP2 citations73
US10731563B2Aug 4, 2020
Compressed air bleed supply for buffer system
UNITED TECHNOLOGIES CORP2 citations73
US9410483B2Aug 9, 2016
Gas turbine engine forward bearing compartment architecture
UNITED TECHNOLOGIES CORP3 citations73
US11286852B2Mar 29, 2022
Gas turbine engine buffer system
UNITED TECHNOLOGIES CORP0 citations62
US10550714B2Feb 4, 2020
Gas turbine engine forward bearing compartment architecture
UNITED TECHNOLOGIES CORP0 citations52
US10550713B2Feb 4, 2020
Gas turbine engine forward bearing compartment architecture
UNITED TECHNOLOGIES CORP0 citations52
US9879602B2Jan 30, 2018
Compressed air bleed supply for buffer system
UNITED TECHNOLOGIES CORP1 citations52
GLAHN JORN A
6 patentsUS8167545B2May 1, 2012
Self-balancing face seals and gas turbine engine systems involving such seals
GLAHN JORN A24 citations92
US8109717B2Feb 7, 2012
Gas turbine engine systems involving hydrostatic face seals with integrated back-up seals
GLAHN JORN A22 citations92
US8109716B2Feb 7, 2012
Gas turbine engine systems involving hydrostatic face seals with anti-fouling provisioning
GLAHN JORN A23 citations92
US8459040B2Jun 11, 2013
Rear hub cooling for high pressure compressor
GLAHN JORN A15 citations84
US8256229B2Sep 4, 2012
Rear hub cooling for high pressure compressor
GLAHN JORN A8 citations84
US8105021B2Jan 31, 2012
Gas turbine engine systems involving hydrostatic face seals with integrated back-up seals
GLAHN JORN A16 citations84
RAYTHEON TECH CORP
4 patentsUS11560839B2Jan 24, 2023
Gas turbine engine buffer system
RAYTHEON TECH CORP0 citations62
US11549387B2Jan 10, 2023
Gas turbine engine forward bearing compartment architecture
RAYTHEON TECH CORP0 citations62
US11499476B2Nov 15, 2022
Gas turbine engine buffer system
RAYTHEON TECH CORP1 citations62
US11293299B2Apr 5, 2022
Gas turbine engine forward bearing compartment architecture
RAYTHEON TECH CORP0 citations62