Patent · US Active

High speed aerospace generator resilient mount, combined centering spring and squeeze film damper

US7648278B2 · kind B2 · utility

23Cited by
13References
13Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 5, 2007
Grant dateJan 19, 2010
Priority date
Expiry dateMay 11, 2028

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16C2380/26
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A rotor mount assembly for an electrical machine, such as a high speed aerospace generator, comprises a spring having a simple annular structure together with an oil squeeze film damper (SFD). The spring is engineered to move the rotor critical speeds outside of the extremes of the operating speed range and the SFD damps out the rotor responses as the speed passes through these points.

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