P

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 patents
US6195982B1Mar 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 patents

FEULNER MATTHEW R

1 patent

RTX CORP

1 patent

COLLOPY GARY

1 patent