SYSTEM AND METHOD FOR MAXIMUM BRAKING

摘要

Systems and methods for reducing the speed of an aircraft are disclosed herein. An electronic brake control system may include a first braked wheel of a landing gear system, a brake pedal electronically coupled to the first braked wheel, and a first actuator. The first actuator may be configured to deliver a scalable clamping force on the first braked wheel via a brake stack. The first actuator may be configured to deliver an emergency maximum clamping force on the first braked wheel in response to the electronic brake control unit being in an emergency condition braking mode and a signal being received proportional to the brake pedal displacement. The emergency maximum clamping force results in the first actuator being driven in an overdriven state.

主权项

1. An electronic brake control system comprising:
a first braked wheel of a landing gear system; a brake pedal electronically coupled to a brake control unit; and a first actuator, wherein the first actuator is configured to deliver a scalable clamping force on the first braked wheel via a brake stack, wherein the first actuator is configured to deliver a clamping force on the first braked wheel in accordance with a first force level designated by a first lookup table; wherein the first actuator is configured to deliver an emergency maximum clamping force on the first braked wheel, in accordance with a second force level designated by a second lookup table, in response to the electronic brake control system being in an emergency braking mode and at least one of: a signal being received at the brake control unit, proportional to a brake pedal displacement, and an automatic emergency command,wherein an emergency maximum clamping force results in the first actuator being driven in an overdriven state.