Inventor
DUBE BRYAN P
US72 patents
⚠️ This page may combine multiple inventors who share the name “DUBE BRYAN P”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
32 patentsUS6929054B2Aug 16, 2005
Investment casting cores
UNITED TECHNOLOGIES CORP145 citations98
US6607355B2Aug 19, 2003
Turbine airfoil with enhanced heat transfer
UNITED TECHNOLOGIES CORP143 citations98
US7396205B2Jul 8, 2008
Rotor blade for a rotary machine
UNITED TECHNOLOGIES CORP70 citations97
US7270170B2Sep 18, 2007
Investment casting core methods
UNITED TECHNOLOGIES CORP66 citations97
US10072516B2Sep 11, 2018
Clamped vane arc segment having load-transmitting features
UNITED TECHNOLOGIES CORP29 citations93
US9816387B2Nov 14, 2017
Attachment faces for clamped turbine stator of a gas turbine engine
UNITED TECHNOLOGIES CORP30 citations93
US7273353B2Sep 25, 2007
Shroud honeycomb cutter
UNITED TECHNOLOGIES CORP15 citations92
US6997675B2Feb 14, 2006
Turbulated hole configurations for turbine blades
UNITED TECHNOLOGIES CORP24 citations92
US6007628ADec 28, 1999
Clamping fixture for a rotor blade shroud
UNITED TECHNOLOGIES CORP23 citations92
US7549846B2Jun 23, 2009
Turbine blades
UNITED TECHNOLOGIES CORP24 citations90
US10975706B2Apr 13, 2021
Frustic load transmission feature for composite structures
UNITED TECHNOLOGIES CORP10 citations85
US11125093B2Sep 21, 2021
Vane with L-shaped seal
UNITED TECHNOLOGIES CORP7 citations84
US7094023B2Aug 22, 2006
Shroud honeycomb cutter
UNITED TECHNOLOGIES CORP13 citations84
US9845694B2Dec 19, 2017
Flow directing cover for engine component
UNITED TECHNOLOGIES CORP5 citations83
US7134838B2Nov 14, 2006
Rotor blade for a rotary machine
UNITED TECHNOLOGIES CORP18 citations83
US7114916B2Oct 3, 2006
Tailored turbulation for turbine blades
UNITED TECHNOLOGIES CORP15 citations83
US7066713B2Jun 27, 2006
Rotor blade for a rotary machine
UNITED TECHNOLOGIES CORP20 citations83
US9038700B2May 26, 2015
Process and refractory metal core for creating varying thickness microcircuits for turbine engine components
UNITED TECHNOLOGIES CORP7 citations82
US8347947B2Jan 8, 2013
Process and refractory metal core for creating varying thickness microcircuits for turbine engine components
UNITED TECHNOLOGIES CORP11 citations82
US6034344AMar 7, 2000
Method for applying material to a face of a flow directing assembly for a gas turbine engine
UNITED TECHNOLOGIES CORP19 citations81
US11092022B2Aug 17, 2021
Vane with chevron face
UNITED TECHNOLOGIES CORP6 citations73
US10041357B2Aug 7, 2018
Cored airfoil platform with outlet slots
UNITED TECHNOLOGIES CORP2 citations73
US11280214B2Mar 22, 2022
Gas turbine engine component
UNITED TECHNOLOGIES CORP2 citations72
US11268393B2Mar 8, 2022
Vane retention feature
UNITED TECHNOLOGIES CORP3 citations72
US11041392B2Jun 22, 2021
Attachment faces for clamped turbine stator of a gas turbine engine
UNITED TECHNOLOGIES CORP2 citations72
US10465540B2Nov 5, 2019
Airfoil assembly with spacer and tie-spar
UNITED TECHNOLOGIES CORP3 citations72
US10392951B2Aug 27, 2019
Vane assembly with trapped segmented vane structures
UNITED TECHNOLOGIES CORP4 citations72
US10107117B2Oct 23, 2018
Airfoil assembly with spacer and tie-spar
UNITED TECHNOLOGIES CORP4 citations72
US10526905B2Jan 7, 2020
Asymmetric vane assembly
UNITED TECHNOLOGIES CORP4 citations71
US11242762B2Feb 8, 2022
Vane with collar
UNITED TECHNOLOGIES CORP2 citations68
US11697994B2Jul 11, 2023
CMC component with cooling protection
UNITED TECHNOLOGIES CORP0 citations63
US11624287B2Apr 11, 2023
Ceramic matrix composite component having low density core and method of making
UNITED TECHNOLOGIES CORP0 citations63
RAYTHEON TECH CORP
11 patentsUS11346228B1May 31, 2022
Airfoil with flange formed of wishbone-shaped fiber layer structure
RAYTHEON TECH CORP22 citations93
US11530614B2Dec 20, 2022
Vane arc segment formed of fiber-reinforced composite
RAYTHEON TECH CORP7 citations84
US11454129B1Sep 27, 2022
CMC component flow discourager flanges
RAYTHEON TECH CORP7 citations83
US11536147B2Dec 27, 2022
Vane arc segment with flange and gusset
RAYTHEON TECH CORP4 citations73
US11299995B1Apr 12, 2022
Vane arc segment having spar with pin fairing
RAYTHEON TECH CORP3 citations72
US11215059B1Jan 4, 2022
Gas turbine engine airfoil with variable pitch cooling holes
RAYTHEON TECH CORP4 citations72
US12006837B2Jun 11, 2024
Ceramic matrix composite article and method of making the same
RAYTHEON TECH CORP0 citations63
US12352172B2Jul 8, 2025
Seal slot with coating
RAYTHEON TECH CORP0 citations62
US12071864B2Aug 27, 2024
Turbine section with ceramic support rings and ceramic vane arc segments
RAYTHEON TECH CORP0 citations62
US11719130B2Aug 8, 2023
Vane system with continuous support ring
RAYTHEON TECH CORP0 citations62
US11549385B2Jan 10, 2023
Airfoil assembly with seal plate and seal
RAYTHEON TECH CORP0 citations62
RTX CORP
5 patentsUS12173621B2Dec 24, 2024
Hybrid platform manufacturing
RTX CORP2 citations71
US11976568B2May 7, 2024
Ceramic matrix composite component having low density core and method of making
RTX CORP0 citations63
US12258881B2Mar 25, 2025
Turbine section with ceramic support rings and ceramic vane arc segments
RTX CORP0 citations62
US12025020B2Jul 2, 2024
Vane system with continuous support ring
RTX CORP0 citations62
US12006845B2Jun 11, 2024
Vane arc segment with flange and gusset
RTX CORP0 citations62
TRINDADE RICARDO
1 patentPINERO SANDRA S
1 patentShowing the top 50 of 72 patents by PatentIndex Score.