Patent · US Active

Electronic control of blade pitch on a tiltrotor

US11952111B2 · kind B2 · utility

0Cited by
0References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 29, 2020
Grant dateApr 9, 2024
Priority date
Expiry dateJan 29, 2042

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C27/68
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A system is provided for controlling the pitch of blades of a rotor, the system comprising an actuator for each blade, each actuator being configured for selective control of the pitch of an associated blade about a pitch axis. Sensors are configured for determining aerodynamic forces acting on the rotor, and a flight control system is configured to receive signals from the sensors and for operating the actuators in response to the signals to achieve a desired pitch-flap coupling value.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.