Inventor
BOULDIN LEE E
US8 patents
Patents
8 patentsUS10684017B2Jun 16, 2020
Passage geometry for gas turbine engine combustor
UNITED TECHNOLOGIES CORP19 citations84
US10731858B2Aug 4, 2020
Controlled variation of pressure drop through effusion cooling in a double walled combustor of a gas turbine engine
UNITED TECHNOLOGIES CORP10 citations82
US10648666B2May 12, 2020
Angled combustor liner cooling holes through transverse structure within a gas turbine engine combustor
UNITED TECHNOLOGIES CORP10 citations82
US10690348B2Jun 23, 2020
Turbine engine combustor heat shield with one or more cooling elements
UNITED TECHNOLOGIES CORP2 citations71
US10215410B2Feb 26, 2019
Turbine engine combustor heat shield with multi-angled cooling apertures
UNITED TECHNOLOGIES CORP2 citations71
US11287132B2Mar 29, 2022
Quench aperture body for a turbine engine combustor
UNITED TECHNOLOGIES CORP0 citations61
US10571125B2Feb 25, 2020
Quench aperture body for a turbine engine combustor
UNITED TECHNOLOGIES CORP1 citations61
US10655856B2May 19, 2020
Dilution passage arrangement for gas turbine engine combustor
UNITED TECHNOLOGIES CORP0 citations51