Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Device for de-icing a leading edge of a turbine engine by slanting notches

Device for de-icing a leading edge of a turbine engine by slanting notches

US Patent 10107138 · Granted Oct 23, 2018

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Inlet cone for an aircraft turbomachine2024
Inlet cone for an aircraft turbomachine2024
Aircraft propulsion unit and process for reducing a ventilation air flow in the 2023
Anti-icing system for a turbine engine vane2020
Anti-icing system for a turbine engine vane2020
System for detecting the first signs of a malfunction of an aircraft engine valv2014
System for deicing an aircraft turbine engine inlet cone2010
System for deicing the nose cone of an aircraft turbojet with oil2010
Blade for a turbine comprising a cooling air deflector2006