WH

Wayne Charles Hasz

GE: 66 patents #125 of 36,430Top 1%
📍 Pownal, VT: #1 of 13 inventorsTop 8%
🗺 Vermont: #90 of 4,968 inventorsTop 2%
Overall (All Time): #32,902 of 4,157,543Top 1%
66
Patents All Time

Issued Patents All Time

Showing 26–50 of 66 patents

Patent #TitleCo-InventorsDate
6910620 Method for providing turbulation on the inner surface of holes in an article, and related articles Nesim Abuaf, Robert Alan Johnson, Ching-Pang Lee 2005-06-28
6846575 Article having turbulation and method of providing turbulation on an article Robert Alan Johnson, Ching-Pang Lee, Mark Gerard Rettig, Nesim Abuaf, John Howard Starkweather 2005-01-25
6827254 Turbine engine component having wear coating and method for coating a turbine engine component David Edwin Budinger 2004-12-07
6786982 Casting having an enhanced heat transfer, surface, and mold and pattern for forming same Ching-Pang Lee, Nesim Abuaf, Robert Alan Johnson 2004-09-07
6637643 Method of applying a bond coating and a thermal barrier coating on a metal substrate, and related articles Marcus P. Borom, Warren Arthur Nelson, James Viggiani, John Zanneti 2003-10-28
6610420 Thermal Barrier coating system of a turbine engine component Anthony Mark Thompson 2003-08-26
6598781 Article having turbulation and method of providing turbulation on an article Robert Alan Johnson, Ching-Pang Lee, Mark Gerard Rettig, Nesim Abuaf, John Howard Starkweather 2003-07-29
6589600 Turbine engine component having enhanced heat transfer characteristics and method for forming same Nesim Abuaf, Robert Alan Johnson, Ching-Pang Lee 2003-07-08
6546730 Method and apparatus for enhancing heat transfer in a combustor liner for a gas turbine Robert Alan Johnson, Anthony J. Loprinzo, Ching-Pang Lee, Nesim Abuaf, Harmon Lindsay Morton 2003-04-15
6541075 Method for forming a thermal barrier coating system Jeffrey A. Conner 2003-04-01
6526756 Method and apparatus for enhancing heat transfer in a combustor liner for a gas turbine Robert Alan Johnson, Anthony J. Loprinzo, Ching-Pang Lee, Nesim Abuaf, Harmon Lindsay Morton 2003-03-04
6505673 Method for forming a turbine engine component having enhanced heat transfer characteristics Nesim Abuaf, Ching-Pang Lee, Robert Alan Johnson, Frederick Alan Buck 2003-01-14
6502622 Casting having an enhanced heat transfer, surface, and mold and pattern for forming same Ching-Pang Lee, Nesim Abuaf, Robert Alan Johnson 2003-01-07
6497758 Method for applying a high-temperature bond coat on a metal substrate, and related compositions and articles D Sangeeta 2002-12-24
6468669 Article having turbulation and method of providing turbulation on an article Robert Alan Johnson, Ching-Pang Lee, Mark Gerard Rettig, Nesim Abuaf, John Howard Starkweather 2002-10-22
6451454 Turbine engine component having wear coating and method for coating a turbine engine component David Edwin Budinger 2002-09-17
6428904 X-ray target Mark Gilbert Benz, Charles Gitahi Mukira, Thomas Robert Raber, Gregory Alan Steinlage, Gregory Reznikov 2002-08-06
6426152 Salvaged castings and methods of salvaging castings with defective cast cooling bumps Robert Alan Johnson, Jon Conrad Schaeffer, Ching-Pang Lee, Nesim Abuaf 2002-07-30
6402464 Enhanced heat transfer surface for cast-in-bump-covered cooling surfaces and methods of enhancing heat transfer Rong-Shi Paul Chiu, Robert Alan Johnson, Ching-Pang Lee, Nesim Abuaf 2002-06-11
6399217 Article surface with metal wires and method for making Ching-Pang Lee, Nesim Abuaf, Robert Alan Johnson 2002-06-04
6398103 Method of providing wear-resistant coatings, and related articles Anthony Mark Thompson, Marcus P. Borom 2002-06-04
6390876 Composite X-ray target Mark Gilbert Benz, Charles Gitahi Mukira, Thomas Robert Raber, Constantinos Minas, Gregory Alan Steinlage +1 more 2002-05-21
6387527 Method of applying a bond coating and a thermal barrier coating on a metal substrate, and related articles Marcus P. Borom 2002-05-14
6382300 Casting having an enhanced heat transfer, surface, and mold and pattern for forming same Ching-Pang Lee, Nesim Abuaf, Robert Alan Johnson 2002-05-07
6368672 Method for forming a thermal barrier coating system of a turbine engine component Anthony Mark Thompson 2002-04-09