Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Pitch control device for a ducted tail rotor of a rotorcraft

Pitch control device for a ducted tail rotor of a rotorcraft

US Patent 10654559 · Granted May 19, 2020

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Control system for controlling at least collective pitch of rotor blades of a mu2020
Multi-blade rotor for a rotary wing aircraft2019
Multi-blade rotor for a rotary wing aircraft2019
Blade attachment for a bearingless rotor of a helicopter2017
Connection joint for attaching an airfoil blade to a helicopter's bearingless ma2017
Partly cruciform flexbeam and method of manufacturing such a flexbeam2017
Separable blade attachment for a bearingless rotor of a helicopter2016
Aerodynamic blade attachment for a bearingless rotor of a helicopter2016
Rotor blade made of a fibre-reinforced composite material and production method 2015
Rotor blade in flat design2015
Rotor wing with integrated tension-torque-transmission element and method for it2014
Tension-torque-transmission element for a fenestron blade and method for produci2014