Patent · US Active

Rotor assembly with static mast and pivoting rotor hub

US11691723B2 · kind B2 · utility

0Cited by
2References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 4, 2021
Grant dateJul 4, 2023
Priority date
Expiry dateMay 4, 2041

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C27/605
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A gimbaled rotor assembly for an aircraft. The gimbaled rotor assembly including a static mast; a spherical bearing comprising an inner component and an outer component pivotable relative to each other about a bearing focus, the inner component fixedly coupled to the static mast; a rotor hub rotatably coupled to the outer component, allowing for relative rotation of the rotor hub about a rotor axis and for pivoting together with the outer component about the bearing focus; and a primary hub spring coupling the outer component to the static mast and configured for opposing pivoting of the rotor hub about the bearing focus from a neutral position.

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