Inventor
FEULNER MATTHEW R
US28 patents
⚠️ This page may combine multiple inventors who share the name “FEULNER MATTHEW R”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
21 patentsUS6195982B1Mar 6, 2001
Apparatus and method of active flutter control
UNITED TECHNOLOGIES CORP78 citations95
US6059522AMay 9, 2000
Compressor stall diagnostics and avoidance
UNITED TECHNOLOGIES CORP62 citations93
US9540944B2Jan 10, 2017
Real time model based compressor control
UNITED TECHNOLOGIES CORP24 citations92
US6574965B1Jun 10, 2003
Rotor tip bleed in gas turbine engines
UNITED TECHNOLOGIES CORP50 citations92
US6010303AJan 4, 2000
Apparatus and method of predicting aerodynamic and aeromechanical instabilities in turbofan engines
UNITED TECHNOLOGIES CORP48 citations92
US10040577B2Aug 7, 2018
Modified start sequence of a gas turbine engine
UNITED TECHNOLOGIES CORP17 citations90
US10457401B2Oct 29, 2019
Dual-use air turbine system for a gas turbine engine
UNITED TECHNOLOGIES CORP14 citations85
US10774788B2Sep 15, 2020
Particle extraction system for a gas turbine engine
UNITED TECHNOLOGIES CORP8 citations84
US10125691B2Nov 13, 2018
Bowed rotor start using a variable position starter valve
UNITED TECHNOLOGIES CORP13 citations84
US9909497B2Mar 6, 2018
Combined stability and customer bleed with dirt, water and ice rejection
UNITED TECHNOLOGIES CORP6 citations73
US10293951B2May 21, 2019
Takeoff power management system and method for gas turbine engines
UNITED TECHNOLOGIES CORP4 citations71
US10625881B2Apr 21, 2020
Modified start sequence of a gas turbine engine
UNITED TECHNOLOGIES CORP3 citations69
US11339678B2May 24, 2022
Systems and methods for controlling blade tip clearances
UNITED TECHNOLOGIES CORP1 citations62
US11473510B2Oct 18, 2022
Active multi-effector control of high pressure turbine clearances
UNITED TECHNOLOGIES CORP1 citations58
US10495006B2Dec 3, 2019
Variable geometry gas turbine engine for use in inclement weather
UNITED TECHNOLOGIES CORP1 citations54
US10718272B2Jul 21, 2020
Variable-geometry boundary layer diverter
UNITED TECHNOLOGIES CORP0 citations52
US10330010B2Jun 25, 2019
Compressor core inner diameter cooling
UNITED TECHNOLOGIES CORP0 citations52
US9982689B2May 29, 2018
Apparatus and method for water and ice flow management in a gas turbine engine
UNITED TECHNOLOGIES CORP0 citations52
US11459946B2Oct 4, 2022
Gas turbine engine spool coupling
UNITED TECHNOLOGIES CORP0 citations51
US10060284B2Aug 28, 2018
Engine inlet total air temperature sensor
UNITED TECHNOLOGIES CORP1 citations51
US10787277B2Sep 29, 2020
Modified start sequence of a gas turbine engine
UNITED TECHNOLOGIES CORP0 citations48
RAYTHEON TECH CORP
4 patentsUS11674407B2Jun 13, 2023
Systems and methods for controlling blade tip clearances
RAYTHEON TECH CORP2 citations73
US11754000B2Sep 12, 2023
High and low spool configuration for a gas turbine engine
RAYTHEON TECH CORP0 citations61
US11391205B2Jul 19, 2022
Anti-icing core inlet stator assembly for a gas turbine engine
RAYTHEON TECH CORP0 citations57
US11719245B2Aug 8, 2023
Compressor arrangement for a gas turbine engine
RAYTHEON TECH CORP0 citations50