Patent · US Active

Rotor assembly for a rotorcraft

US9145205B2 · kind B2 · utility

1Cited by
30References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 6, 2010
Grant dateSep 29, 2015
Priority date
Expiry dateNov 9, 2032

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C27/59
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A rotor assembly (5) for a rotorcraft, such as a helicopter, includes rotors (7) rotatable about a hub (17). The assembly (5) is operable to vary the angular speed of the rotors (7) about the hub (17), relative to one another. The assembly (5) may include a drive operable to drive each of the rotors (7) at a different radial distance from the hub.

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