Patent · US Active

Aircraft brake actuator assemblies

US9605723B2 · kind B2 · utility

3Cited by
2References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 21, 2015
Grant dateMar 28, 2017
Priority date
Expiry dateAug 13, 2035

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16H2025/2087
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

The present disclosure provides an actuator assembly comprising a ballnut having a helical track, an actuator drive unit (“ADU”) housing having an ADU track, and a ballscrew. In various embodiments, the ballscrew comprises a first translation bearing track, wherein the helical track and the first translation bearing track form a first translation bearing raceway in which a plurality of first translation bearing balls having a first diameter are disposed, and a second translation bearing track, wherein the helical track and the second translation bearing track form a second translation bearing raceway in which a plurality of second translation bearing balls having a second diameter are disposed, wherein the first diameter and the second diameter are not equal.

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