Inventor
WAGNER JOEL H
US36 patents
⚠️ This page may combine multiple inventors who share the name “WAGNER JOEL H”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
27 patentsUS6547524B2Apr 15, 2003
Film cooled article with improved temperature tolerance
UNITED TECHNOLOGIES CORP63 citations96
US6669445B2Dec 30, 2003
Endwall shape for use in turbomachinery
UNITED TECHNOLOGIES CORP108 citations95
US10036258B2Jul 31, 2018
Gas turbine engine component having vascular engineered lattice structure
UNITED TECHNOLOGIES CORP30 citations94
US7195456B2Mar 27, 2007
Turbine engine guide vane and arrays thereof
UNITED TECHNOLOGIES CORP59 citations94
US10415419B2Sep 17, 2019
System for modulating turbine blade tip clearance
UNITED TECHNOLOGIES CORP22 citations93
US7887297B2Feb 15, 2011
Airfoil array with an endwall protrusion and components of the array
UNITED TECHNOLOGIES CORP46 citations93
US7534088B1May 19, 2009
Fluid injection system
UNITED TECHNOLOGIES CORP29 citations92
US8052388B2Nov 8, 2011
Gas turbine engine systems involving mechanically alterable vane throat areas
UNITED TECHNOLOGIES CORP20 citations90
US10662781B2May 26, 2020
Gas turbine engine component having vascular engineered lattice structure
UNITED TECHNOLOGIES CORP9 citations84
US9851105B2Dec 26, 2017
Self-cooled orifice structure
UNITED TECHNOLOGIES CORP7 citations84
US6932572B2Aug 23, 2005
Film cooled article with improved temperature tolerance
UNITED TECHNOLOGIES CORP11 citations74
US10669896B2Jun 2, 2020
Dirt separator for internally cooled components
UNITED TECHNOLOGIES CORP3 citations73
US10514171B2Dec 24, 2019
3D non-axisymmetric combustor liner
UNITED TECHNOLOGIES CORP3 citations73
US10156359B2Dec 18, 2018
Gas turbine engine component having vascular engineered lattice structure
UNITED TECHNOLOGIES CORP3 citations73
US10101029B2Oct 16, 2018
Combustor panels and configurations for a gas turbine engine
UNITED TECHNOLOGIES CORP4 citations73
US10040115B2Aug 7, 2018
Additively manufactured casting articles for manufacturing gas turbine engine parts
UNITED TECHNOLOGIES CORP5 citations73
US10913106B2Feb 9, 2021
Cast-in film cooling hole structures
UNITED TECHNOLOGIES CORP2 citations72
US10556269B1Feb 11, 2020
Apparatus for and method of making multi-walled passages in components
UNITED TECHNOLOGIES CORP2 citations70
US10450960B2Oct 22, 2019
Tangential on-board injectors for gas turbine engines
UNITED TECHNOLOGIES CORP1 citations61
US11334051B2May 17, 2022
Systems and methods for automated adaptive manufacturing of airfoil castings
UNITED TECHNOLOGIES CORP1 citations60
US11014151B2May 25, 2021
Method of making airfoils
UNITED TECHNOLOGIES CORP0 citations60
US10392968B2Aug 27, 2019
Turbine casing cooling structure
UNITED TECHNOLOGIES CORP0 citations52
US10307817B2Jun 4, 2019
Additively manufactured casting articles for manufacturing gas turbine engine parts
UNITED TECHNOLOGIES CORP0 citations52
US9649687B2May 16, 2017
Method including fiber reinforced casting article
UNITED TECHNOLOGIES CORP0 citations52
US9802288B2Oct 31, 2017
Machining system having a tool for finishing airfoils
UNITED TECHNOLOGIES CORP1 citations51
US10126175B2Nov 13, 2018
Long wave infrared sensing for turbomachine
UNITED TECHNOLOGIES CORP0 citations50
US11402304B2Aug 2, 2022
Environmental sampling system and method
UNITED TECHNOLOGIES CORP0 citations46
WAGNER JOEL H
3 patentsUS8707708B2Apr 29, 2014
3D non-axisymmetric combustor liner
WAGNER JOEL H6 citations83
US8197209B2Jun 12, 2012
Systems and methods involving variable throat area vanes
WAGNER JOEL H9 citations83
US8935926B2Jan 20, 2015
Centrifugal compressor with bleed flow splitter for a gas turbine engine
WAGNER JOEL H11 citations82