Patent · US Active

Fan blade with internal magnetorheological fluid damping

US11560801B1 · kind B1 · utility

0Cited by
38References
19Claims
0Family size

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Key dates

Filing dateDec 23, 2021
Grant dateJan 24, 2023
Priority date
Expiry dateDec 23, 2041

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

An airfoil for use in a gas turbine engine is formed to define a cavity formed in the airfoil. The airfoil further includes at least one obstructing member arranged within the cavity and a magnetorheological fluid disposed in the cavity. A viscosity of the magnetorheological fluid increases in response to a magnetic field being generated proximate to the fluid in response to the airfoil experiencing an aeromechanic response or vibrations. As such, the obstruction of the movement of the thicker fluid by the obstructing member dampens the vibrations of the airfoil and reduces negative effects of a dynamic response of the airfoil.

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