Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Gas turbine engine component with upstream-directed cooling film holes

Gas turbine engine component with upstream-directed cooling film holes

US Patent 9958160 · Granted May 1, 2018

Estimated economic value: $8,732,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Combustor panel with increased durability2021
Ceramic attachment configuration and method for manufacturing same2019
Gas turbine engine component paired film cooling holes2018
Structures with adaptive cooling2017
Insert adjacent to a heat shield element for a gas turbine engine combustor2017
Segmented thermally insulating coating2015
Strain tolerant combustor panel for gas turbine engine2015
Floatwell panel assemblies and related systems2014
Ceramic combustor liner panel for a gas turbine engine2013
Combustor liner segment seal member2013
Combustor liner segment seal member2013
Mechanical attachment of ceramic or metallic foam materials2012