Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Low radius ratio fan for a gas turbine engine

Low radius ratio fan for a gas turbine engine

US Patent 9239062 · Granted Jan 19, 2016

Estimated economic value: $41,537,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Turbine engine with composite airfoils2025
Gas turbine engine2025
Rotor assembly for a gas turbine engine2025
Pitch change mechanism for a fan of a gas turbine engine2025
Turbine engine including a fan assembly having a damper2025
Turbine engine including a vane support and a vane2025
Variable pitch airfoil2025
Turbine engine having a variable pitch airfoil assembly2025
Turbine engine with composite airfoils2025
Outlet guide vane mount2025
Turbine engine with composite airfoils2025
Pitch-controlled blade retention collar2025