P

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 patents
US6929054B2Aug 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 patents

RTX CORP

5 patents

TRINDADE RICARDO

1 patent

PINERO SANDRA S

1 patent

Showing the top 50 of 72 patents by PatentIndex Score.