Patent · US Active

Rotor systems for rotorcraft

US10150567B2 · kind B2 · utility

3Cited by
10References
21Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 27, 2016
Grant dateDec 11, 2018
Priority date
Expiry dateJun 29, 2036

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A rotor system for a rotorcraft includes a first rotor assembly defining a rotation axis, a second rotor assembly offset from the first rotor assembly along the rotation axis, and a drive system connected to the first and second rotor assemblies. The drive system includes a first electric motor disposed along the rotation axis and operably connected to the first rotor assembly, and a second electric motor disposed along the rotation axis and operably connected to the second rotor assembly to rotate the second rotor assembly about the rotation axis independent of rotation of the first rotor assembly about the rotation axis.

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