Patent · US Active

Architecture of an aircraft braking system

US9950785B2 · kind B2 · utility

4Cited by
0References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 30, 2016
Grant dateApr 24, 2018
Priority date
Expiry dateNov 30, 2036

Classification

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

Abstract

Architecture of an aircraft braking system having a brake (20) comprising a plurality of electromechanical actuators (25), with each electromechanical actuator (25) comprising a power module and a digital communication module (26). The brake digital communication modules are interconnected to form a digital network (30). The system also has two control units (22a, 22b) adapted for generating digital signals for controlling electric motors and one network interconnection member (23) connected to two control units and incorporated in the digital network for distributing the digital control signals to the digital communication modules via the digital network.

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