Inventor
HARRIS MEGGAN
US17 patents
⚠️ This page may combine multiple inventors who share the name “HARRIS MEGGAN”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
15 patentsUS7032835B2Apr 25, 2006
Convergent/divergent nozzle with modulated cooling
UNITED TECHNOLOGIES CORP53 citations91
US9371738B2Jun 21, 2016
Variable outer air seal support
UNITED TECHNOLOGIES CORP9 citations83
US7377099B2May 27, 2008
System and method for cooling lateral edge regions of a divergent seal of an axisymmetric nozzle
UNITED TECHNOLOGIES CORP15 citations82
US10598381B2Mar 24, 2020
Swirler mount interface for gas turbine engine combustor
UNITED TECHNOLOGIES CORP3 citations72
US10337339B2Jul 2, 2019
Structural honeycomb panel
UNITED TECHNOLOGIES CORP4 citations72
US10088166B2Oct 2, 2018
Swirler mount interface for gas turbine engine combustor
UNITED TECHNOLOGIES CORP3 citations72
US10662792B2May 26, 2020
Gas turbine engine cooling fluid composite tube
UNITED TECHNOLOGIES CORP4 citations69
US11092025B2Aug 17, 2021
Gas turbine engine with dove-tailed TOBI vane
UNITED TECHNOLOGIES CORP1 citations62
US11002390B2May 11, 2021
Fuel fitting
UNITED TECHNOLOGIES CORP1 citations62
US10494938B2Dec 3, 2019
Gas turbine engine with dove-tailed TOBI vane
UNITED TECHNOLOGIES CORP1 citations62
US9255524B2Feb 9, 2016
Variable outer air seal fluid control
UNITED TECHNOLOGIES CORP0 citations51
US7856827B2Dec 28, 2010
Structural track support of spraybars/tubing
UNITED TECHNOLOGIES CORP0 citations51
US9945236B2Apr 17, 2018
Gas turbine hub
UNITED TECHNOLOGIES CORP0 citations50
US7578133B2Aug 25, 2009
Reduced radar cross section exhaust nozzle assembly
UNITED TECHNOLOGIES CORP0 citations42
US10519897B2Dec 31, 2019
Divergent flap
UNITED TECHNOLOGIES CORP0 citations41