Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Aircraft turbomachine provided with an unducted propeller with blades having a composite-material insert bonded to their leading edges

Aircraft turbomachine provided with an unducted propeller with blades having a composite-material insert bonded to their leading edges

US Patent 11401823 · Granted Aug 2, 2022

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Aircraft turbine engine comprising variable-pitch propeller vanes2025
Assembly comprising a vane and a vane pitch setting system2025
Fastening assembly for a turbomachine blade2024
Blade comprising a composite material structure and associated manufacturing met2024
Unducted fan having variable pitch blades comprising reduced disturbance platfor2024
Vane comprising a structure made of composite material, and associated manufactu2024
Preform for a composite blade2024
Preform for a composite blade2024
Preform for a composite blade2024
System for controlling the pitch of a propeller vane for an aircraft turbine eng2024
Composite blade for a turbine engine rotor2024
Blade comprising a structure made of composite material and associated manufactu2024