Inventor
CHEUNG ALBERT K
US27 patents
⚠️ This page may combine multiple inventors who share the name “CHEUNG ALBERT K”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
17 patentsUS7093441B2Aug 22, 2006
Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume
UNITED TECHNOLOGIES CORP79 citations95
US7464554B2Dec 16, 2008
Gas turbine combustor heat shield panel or exhaust panel including a cooling device
UNITED TECHNOLOGIES CORP63 citations94
US7954325B2Jun 7, 2011
Gas turbine combustor
UNITED TECHNOLOGIES CORP43 citations92
US7631502B2Dec 15, 2009
Local cooling hole pattern
UNITED TECHNOLOGIES CORP30 citations92
US7614235B2Nov 10, 2009
Combustor cooling hole pattern
UNITED TECHNOLOGIES CORP30 citations92
US9797601B2Oct 24, 2017
Bluff body fuel mixer
UNITED TECHNOLOGIES CORP6 citations83
US11143407B2Oct 12, 2021
Combustor with axial staging for a gas turbine engine
UNITED TECHNOLOGIES CORP3 citations72
US8028528B2Oct 4, 2011
Annular gas turbine combustor
UNITED TECHNOLOGIES CORP6 citations68
US11391461B2Jul 19, 2022
Combustor bulkhead with circular impingement hole pattern
UNITED TECHNOLOGIES CORP1 citations62
US10677161B2Jun 9, 2020
Gas turbine engine diffuser cooling and mixing arrangement
UNITED TECHNOLOGIES CORP1 citations62
US10551065B2Feb 4, 2020
Heat shield for a combustor
UNITED TECHNOLOGIES CORP0 citations52
US10533502B2Jan 14, 2020
Combustor fuel manifold
UNITED TECHNOLOGIES CORP0 citations52
US9562690B2Feb 7, 2017
Swirler, fuel and air assembly and combustor
UNITED TECHNOLOGIES CORP0 citations52
US9068749B2Jun 30, 2015
Swirler for gas turbine engine fuel injector
UNITED TECHNOLOGIES CORP1 citations52
US10816209B2Oct 27, 2020
Bluff body fuel mixer
UNITED TECHNOLOGIES CORP0 citations51
US10024538B2Jul 17, 2018
Apparatus and method for air extraction at a gas turbine engine combustor
UNITED TECHNOLOGIES CORP0 citations47
US10670267B2Jun 2, 2020
Combustor hole arrangement for gas turbine engine
UNITED TECHNOLOGIES CORP0 citations45