Patent · US Active

Aircraft brake system

US11548625B2 · kind B2 · utility

2Cited by
6References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 13, 2019
Grant dateJan 10, 2023
Priority date
Expiry dateApr 6, 2040

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB60T2270/88
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A braking system is disclosed. In various embodiments, the braking system includes a brake stack; an actuator configured to apply a compressive load to the brake stack; a servo valve coupled to a power source and to the actuator; and a brake control unit configured to operate the servo valve at a current ramp rate in response to a pedal deflection signal, wherein the current ramp rate is determined via a relationship between the current ramp rate and a brake pressure command signal.

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