Inventor
HOUSTON DAVID P
US22 patents
⚠️ This page may combine multiple inventors who share the name “HOUSTON DAVID P”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
17 patentsUS10288010B2May 14, 2019
Geared turbofan gas turbine engine architecture
UNITED TECHNOLOGIES CORP18 citations94
US5924699AJul 20, 1999
Turbine blade platform seal
UNITED TECHNOLOGIES CORP103 citations94
US5785499AJul 28, 1998
Turbine blade damper and seal
UNITED TECHNOLOGIES CORP76 citations92
US5284421AFeb 8, 1994
Rotor blade with platform support and damper positioning means
UNITED TECHNOLOGIES CORP28 citations92
US5827047AOct 27, 1998
Turbine blade damper and seal
UNITED TECHNOLOGIES CORP91 citations91
US9394793B1Jul 19, 2016
Turbomachine blade
UNITED TECHNOLOGIES CORP38 citations90
US5313786AMay 24, 1994
Gas turbine blade damper
UNITED TECHNOLOGIES CORP40 citations88
US10288011B2May 14, 2019
Geared turbofan gas turbine engine architecture
UNITED TECHNOLOGIES CORP8 citations84
US9739206B2Aug 22, 2017
Geared turbofan gas turbine engine architecture
UNITED TECHNOLOGIES CORP7 citations84
US10151204B2Dec 11, 2018
Airfoil including loose damper
UNITED TECHNOLOGIES CORP8 citations83
US9885242B2Feb 6, 2018
Turbomachine blade
UNITED TECHNOLOGIES CORP8 citations80
US10570755B2Feb 25, 2020
Fan blade root
UNITED TECHNOLOGIES CORP2 citations71
US10982551B1Apr 20, 2021
Turbomachine blade
UNITED TECHNOLOGIES CORP2 citations69
US10234359B2Mar 19, 2019
Gas turbine engine with lifing calculations based upon actual usage
UNITED TECHNOLOGIES CORP2 citations67
US9828944B2Nov 28, 2017
Geared turbofan gas turbine engine architecture
UNITED TECHNOLOGIES CORP1 citations63
US10072507B2Sep 11, 2018
Redundant airfoil attachment
UNITED TECHNOLOGIES CORP0 citations52
US10704989B2Jul 7, 2020
Gas turbine engine with lifing calculations based upon actual usage
UNITED TECHNOLOGIES CORP0 citations47