Inventor
MERRY BRIAN
US65 patents
⚠️ This page may combine multiple inventors who share the name “MERRY BRIAN”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
37 patentsUS6254333B1Jul 3, 2001
Method for forming a cooling passage and for cooling a turbine section of a rotary machine
UNITED TECHNOLOGIES CORP159 citations99
US7500365B2Mar 10, 2009
Accessory gearbox
UNITED TECHNOLOGIES CORP136 citations97
US6241467B1Jun 5, 2001
Stator vane for a rotary machine
UNITED TECHNOLOGIES CORP101 citations96
US8033094B2Oct 11, 2011
Cantilevered tip turbine engine
UNITED TECHNOLOGIES CORP49 citations94
US7959532B2Jun 14, 2011
Hydraulic seal for a gearbox of a tip turbine engine
UNITED TECHNOLOGIES CORP52 citations94
US7976273B2Jul 12, 2011
Tip turbine engine support structure
UNITED TECHNOLOGIES CORP36 citations93
US7883315B2Feb 8, 2011
Seal assembly for a fan rotor of a tip turbine engine
UNITED TECHNOLOGIES CORP20 citations93
US7631485B2Dec 15, 2009
Tip turbine engine with a heat exchanger
UNITED TECHNOLOGIES CORP20 citations93
US7937927B2May 10, 2011
Counter-rotating gearbox for tip turbine engine
UNITED TECHNOLOGIES CORP23 citations92
US7882694B2Feb 8, 2011
Variable fan inlet guide vane assembly for gas turbine engine
UNITED TECHNOLOGIES CORP28 citations92
US7249929B2Jul 31, 2007
Bleed housing
UNITED TECHNOLOGIES CORP41 citations89
US10995673B2May 4, 2021
Gas turbine engine with intercooled cooling air and dual towershaft accessory gearbox
UNITED TECHNOLOGIES CORP9 citations86
US10422243B2Sep 24, 2019
Gas turbine engine dual towershaft accessory gearbox and starter generator assembly
UNITED TECHNOLOGIES CORP11 citations84
US8033092B2Oct 11, 2011
Tip turbine engine integral fan, combustor, and turbine case
UNITED TECHNOLOGIES CORP14 citations84
US7976272B2Jul 12, 2011
Inflatable bleed valve for a turbine engine
UNITED TECHNOLOGIES CORP7 citations84
US7959406B2Jun 14, 2011
Close coupled gearbox assembly for a tip turbine engine
UNITED TECHNOLOGIES CORP8 citations84
US7927075B2Apr 19, 2011
Fan-turbine rotor assembly for a tip turbine engine
UNITED TECHNOLOGIES CORP8 citations84
US7921635B2Apr 12, 2011
Peripheral combustor for tip turbine engine
UNITED TECHNOLOGIES CORP9 citations84
US7845157B2Dec 7, 2010
Axial compressor for tip turbine engine
UNITED TECHNOLOGIES CORP11 citations84
US7631480B2Dec 15, 2009
Modular tip turbine engine
UNITED TECHNOLOGIES CORP10 citations84
US10385774B2Aug 20, 2019
Split compressor turbine engine
UNITED TECHNOLOGIES CORP6 citations83
US11156161B2Oct 26, 2021
Aircraft thermal management system
UNITED TECHNOLOGIES CORP2 citations73
US11130580B2Sep 28, 2021
Electro-pneumatic environmental control system air circuit
UNITED TECHNOLOGIES CORP2 citations73
US10794214B2Oct 6, 2020
Tip clearance control for gas turbine engine
UNITED TECHNOLOGIES CORP3 citations73
US10619483B2Apr 14, 2020
Partially shrouded gas turbine engine fan
UNITED TECHNOLOGIES CORP5 citations73
US10590852B2Mar 17, 2020
Gas turbine engine dual towershaft accessory gearbox assembly with a transmission
UNITED TECHNOLOGIES CORP2 citations73
US10526976B2Jan 7, 2020
Tangential drive for gas turbine engine accessories
UNITED TECHNOLOGIES CORP3 citations73
US10502142B2Dec 10, 2019
Turbine engine gearbox assembly with sets of inline gears
UNITED TECHNOLOGIES CORP2 citations73
US9988935B2Jun 5, 2018
Gas turbine engine with axial compressor with internal cooling pathways
UNITED TECHNOLOGIES CORP2 citations73
US9897098B2Feb 20, 2018
Gas turbine engine axial drum-style compressor rotor assembly
UNITED TECHNOLOGIES CORP3 citations73
US7128535B2Oct 31, 2006
Turbine drum rotor for a turbine engine
UNITED TECHNOLOGIES CORP7 citations66
US11118481B2Sep 14, 2021
Ceramic matrix composite turbine exhaust assembly for a gas turbine engine
UNITED TECHNOLOGIES CORP1 citations63
US10815814B2Oct 27, 2020
Re-use and modulated cooling from tip clearance control system for gas turbine engine
UNITED TECHNOLOGIES CORP1 citations63
US10731560B2Aug 4, 2020
Intercooled cooling air
UNITED TECHNOLOGIES CORP1 citations63
US7934902B2May 3, 2011
Compressor variable stage remote actuation for turbine engine
UNITED TECHNOLOGIES CORP4 citations63
US7921636B2Apr 12, 2011
Tip turbine engine and corresponding operating method
UNITED TECHNOLOGIES CORP4 citations63
US7887296B2Feb 15, 2011
Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
UNITED TECHNOLOGIES CORP5 citations63
SUCIU GABRIEL L
7 patentsUS8087885B2Jan 3, 2012
Stacked annular components for turbine engines
SUCIU GABRIEL L65 citations98
US8276362B2Oct 2, 2012
Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
SUCIU GABRIEL L22 citations92
US9003768B2Apr 14, 2015
Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
SUCIU GABRIEL L11 citations84
US8152469B2Apr 10, 2012
Annular turbine ring rotor
SUCIU GABRIEL L9 citations84
US8757959B2Jun 24, 2014
Tip turbine engine comprising a nonrotable compartment
SUCIU GABRIEL L10 citations79
US9845727B2Dec 19, 2017
Tip turbine engine composite tailcone
SUCIU GABRIEL L2 citations73
US8672630B2Mar 18, 2014
Annular turbine ring rotor
SUCIU GABRIEL L2 citations63
RAYTHEON TECH CORP
3 patentsSUCIU GABRIEL
2 patentsMERRY BRIAN
1 patentShowing the top 50 of 65 patents by PatentIndex Score.