Patent · US Active

Electromechanical aircraft brake with tiltable actuators

US8844682B2 · kind B2 · utility

1Cited by
10References
6Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 8, 2006
Grant dateSep 30, 2014
Priority date
Expiry dateNov 4, 2028

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16D2121/24
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

The invention relates to an electromechanical brake, in particular for aircraft, the brake comprising a support carrying at least one electromechanical actuator comprising a pusher that is axially displaceable towards friction elements in order to apply a braking force to the friction elements, selectively, wherein the actuator is mounted on the support via a connection member allowing at least a portion of the actuator carrying the pusher to tilt angularly.

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