Patent · US Active

Aircraft brake control system

US12240593B2 · kind B2 · utility

0Cited by
1References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 15, 2023
Grant dateMar 4, 2025
Priority date
Expiry dateDec 15, 2043

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C25/42
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft brake control system for controlling antiskid braking of an aircraft wheel is disclosed including a control assembly having a mode controller which sets the mode of operation of an antiskid brake calculator, configured to set a first mode, when an input of the indication of a brake energy supply configuration indicates a first brake energy supply being used, in which the antiskid brake calculator applies a first restriction level on a rise rate of the antiskid brake command, and a second mode, when the input 305 indicates a second brake energy supply being used, in which the antiskid brake calculator applies a second, lower, restriction level on a rise rate of the antiskid brake command.

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