Patent · US Active

Dual spring rate damper

US8857581B2 · kind B2 · utility

6Cited by
20References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 1, 2012
Grant dateOct 14, 2014
Priority date
Expiry dateMay 1, 2032

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16F2230/30
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A rotor hub and method to dampen a force exerted on a rotor hub by a rotor blade during flight. The rotor hub including a central member rotatably coupled to a rotor mast, a blade grip rigidly attached to a blade and movably coupled to the central member, and an adjustable damper operably associated with the blade grip. The method includes damping the force exerted on the rotor hub with the adjustable damper and selectively adjusting the adjustable damper between a first spring rate and a second spring rate.

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