Inventor
KUPRATIS DANIEL BERNARD
US135 patents
⚠️ This page may combine multiple inventors who share the name “KUPRATIS DANIEL BERNARD”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
32 patentsUS10794292B2Oct 6, 2020
Geared turbofan gas turbine engine architecture
UNITED TECHNOLOGIES CORP70 citations98
US9752511B2Sep 5, 2017
Geared architecture for high speed and small volume fan drive turbine
UNITED TECHNOLOGIES CORP39 citations98
US9631558B2Apr 25, 2017
Geared architecture for high speed and small volume fan drive turbine
UNITED TECHNOLOGIES CORP37 citations98
US8756908B2Jun 24, 2014
Fundamental gear system architecture
UNITED TECHNOLOGIES CORP78 citations98
US8747055B2Jun 10, 2014
Geared architecture for high speed and small volume fan drive turbine
UNITED TECHNOLOGIES CORP70 citations98
US10787996B2Sep 29, 2020
Gas turbine engine with stream diverter
UNITED TECHNOLOGIES CORP16 citations94
US10288010B2May 14, 2019
Geared turbofan gas turbine engine architecture
UNITED TECHNOLOGIES CORP18 citations94
US10240526B2Mar 26, 2019
Gas turbine engine with high speed low pressure turbine section
UNITED TECHNOLOGIES CORP26 citations94
US9695751B2Jul 4, 2017
Geared turbofan gas turbine engine architecture
UNITED TECHNOLOGIES CORP27 citations94
US8899915B2Dec 2, 2014
Geared architecture for high speed and small volume fan drive turbine
UNITED TECHNOLOGIES CORP24 citations93
US8887487B2Nov 18, 2014
Geared turbofan gas turbine engine architecture
UNITED TECHNOLOGIES CORP30 citations93
US11143142B2Oct 12, 2021
Adaptive engine with boost spool
UNITED TECHNOLOGIES CORP17 citations86
US10794216B2Oct 6, 2020
Fan drive gear system DC motor and generator
UNITED TECHNOLOGIES CORP11 citations86
US10072570B2Sep 11, 2018
Reverse flow gas turbine engine core
UNITED TECHNOLOGIES CORP17 citations86
US11015523B2May 25, 2021
Turbofan with bleed supercharged auxiliary engine
UNITED TECHNOLOGIES CORP9 citations85
US11168616B2Nov 9, 2021
Hybrid electric fan with improved low pressure compressor
UNITED TECHNOLOGIES CORP6 citations84
US10738694B1Aug 11, 2020
Turbofan with motorized rotating inlet guide vane
UNITED TECHNOLOGIES CORP9 citations84
US10502163B2Dec 10, 2019
Geared turbofan arrangement with core split power ratio
UNITED TECHNOLOGIES CORP8 citations84
US10287914B2May 14, 2019
Gas turbine engine with high speed low pressure turbine section and bearing support features
UNITED TECHNOLOGIES CORP6 citations84
US10288011B2May 14, 2019
Geared turbofan gas turbine engine architecture
UNITED TECHNOLOGIES CORP8 citations84
US10280757B2May 7, 2019
Gas turbine engine airfoil with auxiliary flow channel
UNITED TECHNOLOGIES CORP9 citations84
US10138809B2Nov 27, 2018
Geared turbofan engine with a high ratio of thrust to turbine volume
UNITED TECHNOLOGIES CORP4 citations84
US10125693B2Nov 13, 2018
Geared turbofan engine with power density range
UNITED TECHNOLOGIES CORP4 citations84
US10100739B2Oct 16, 2018
Cooled cooling air system for a gas turbine engine
UNITED TECHNOLOGIES CORP10 citations84
US9845726B2Dec 19, 2017
Gas turbine engine with high speed low pressure turbine section
UNITED TECHNOLOGIES CORP8 citations84
US9739206B2Aug 22, 2017
Geared turbofan gas turbine engine architecture
UNITED TECHNOLOGIES CORP7 citations84
US9523329B2Dec 20, 2016
Gas turbine engine with stream diverter
UNITED TECHNOLOGIES CORP7 citations84
US8935913B2Jan 20, 2015
Geared turbofan gas turbine engine architecture
UNITED TECHNOLOGIES CORP7 citations84
US10385774B2Aug 20, 2019
Split compressor turbine engine
UNITED TECHNOLOGIES CORP6 citations83
US10724395B2Jul 28, 2020
Turbofan with motorized rotating inlet guide vane
UNITED TECHNOLOGIES CORP8 citations79
US11566567B2Jan 31, 2023
Low pressure compressor control for a gas turbine engine
UNITED TECHNOLOGIES CORP5 citations75
US11415044B2Aug 16, 2022
Multi-engine architecture with linkages to multiple spools
UNITED TECHNOLOGIES CORP6 citations74
RAYTHEON TECH CORP
9 patentsUS11781506B2Oct 10, 2023
Splitter and guide vane arrangement for gas turbine engines
RAYTHEON TECH CORP9 citations86
US11608786B2Mar 21, 2023
Gas turbine engine with power density range
RAYTHEON TECH CORP5 citations86
US11597527B2Mar 7, 2023
Aircraft hybrid propulsion fan drive gear system DC motors and generators
RAYTHEON TECH CORP7 citations86
US11346286B2May 31, 2022
Geared turbofan engine with power density range
RAYTHEON TECH CORP4 citations84
US11193425B2Dec 7, 2021
Gearbox for boost spool turbine engine
RAYTHEON TECH CORP11 citations84
US11168617B2Nov 9, 2021
Electric enhanced transmission for multi-spool load-sharing turbofan engine
RAYTHEON TECH CORP7 citations84
US11091272B2Aug 17, 2021
Aircraft hybrid propulsion fan drive gear system DC motors and generators
RAYTHEON TECH CORP6 citations84
US10830153B2Nov 10, 2020
Geared turbofan engine with power density range
RAYTHEON TECH CORP7 citations84
US11319882B2May 3, 2022
Gear and electric amplification of generator motor compressor and turbine drives
RAYTHEON TECH CORP6 citations74
KUPRATIS DANIEL BERNARD
5 patentsUS9157366B2Oct 13, 2015
Adaptive fan with cold turbine
KUPRATIS DANIEL BERNARD35 citations94
US9239004B2Jan 19, 2016
Reverse core gear turbofan
KUPRATIS DANIEL BERNARD26 citations93
US9103227B2Aug 11, 2015
Gas turbine engine with fan-tied inducer section
KUPRATIS DANIEL BERNARD26 citations92
US8915700B2Dec 23, 2014
Gas turbine engine with fan-tied inducer section and multiple low pressure turbine sections
KUPRATIS DANIEL BERNARD28 citations92
US9222409B2Dec 29, 2015
Aerospace engine with augmenting turbojet
KUPRATIS DANIEL BERNARD7 citations84
SCHWARZ FREDERICK M
2 patentsMOON FRANCIS R
1 patentRTX CORP
1 patentShowing the top 50 of 135 patents by PatentIndex Score.