Electronic control of blade pitch on a tiltrotor
US11952111B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Apr 29, 2020 |
| Grant date | Apr 9, 2024 |
| Priority date | — |
| Expiry date | Jan 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.