Patent · US Active

Aircraft load and vibration attenuation

US10647418B2 · kind B2 · utility

3Cited by
7References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 27, 2017
Grant dateMay 12, 2020
Priority date
Expiry dateApr 16, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16F2224/0275
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

In one embodiment, an apparatus comprises a particle damper for damping a component when the particle damper is attached to the component. The particle damper comprises a plurality of pockets configured to hold a plurality of particles, and the particle damper also comprises an attachment fitting for coupling the particle damper to the component.

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