Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Gas turbine engine rotor disc with cooling fluid passage

Gas turbine engine rotor disc with cooling fluid passage

US Patent 5888049 · Granted Mar 30, 1999

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Keystoned blade track2022
Brazed blade track for a gas turbine engine2021
Impingement tubes for gas turbine engine assemblies with ceramic matrix composit2021
Segmented turbine shroud with sealing features2021
Keystoned blade track2020
Full hoop blade track with flanged segments2020
Brazed blade track for a gas turbine engine2019
Composite keystoned blade track2019
Impingement tubes for CMC seal segment cooling2018
Method of forming a rotating blade assembly2012
Cooling system for a gas turbine engine2009
Arrangement for internal passive turbine blade tip clearance control in a high p2009