# US 10,246,182 B2 · Differential emergency/park electric brake system

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- Number: US 10,246,182 B2
- Document ID: US10246182B2
- Status: Granted
- Kind: B2
- Application number: 15/427,262
- Filed: 2017-02-08
- Published: 2017-05-25
- Granted: 2019-04-02
- Earliest claimed: 2009-04-30
- Assignees: Goodrich Corporation
- Applicants: Goodrich Corproation
- Inventors: Eric D Cahill
- Web page: https://patentgrep.com/patent/US10246182B2

## CPC

- B64C 25/48: differentially operated for steering purposes
- B60T 7/085: {by electrical means, e.g. travel, force sensors}
- B60T 7/105: {the lock being released by means of a push button}
- B60T 8/1703: {for aircrafts}
- B60T 8/885: {using electrical circuitry}
- B60T 2270/402: Back-up
- B64C: AEROPLANES; HELICOPTERS
- B60T: VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL (electrodynamic brake systems for vehicle, in general B60L; brakes per se, i.e. devices where braking effect occurs, including ultimate brake actuators, F16D); ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES

## Abstract

A system, apparatus and method provide emergency differential braking for effecting braked steering of an aircraft. A brake input device is provided that not only allows for emergency and parking brake functions, but also enables differential braking. The brake input device (e.g., a parking and/or emergency brake lever, pedal, handle, etc.) can be used in a brake system including a brake system control unit (BSCU), one or more electro-mechanical actuator controllers (EMACs) and a brake assembly including one or more electrical actuators. Each EMAC is electrically coupled to one or more of the actuators so as to provide electrical power for driving the actuators. Each EMAC is also communicatively coupled to the BSCU so as to receive braking data therefrom. In an emergency, the input device sends braking signals directly to the brake actuators.

## Claims

### Claim 1

An emergency brake input device for providing emergency braking signals to at least two brake assemblies, the device comprising:
an input member movable in a first direction corresponding to a braking magnitude and movable in a second direction corresponding to a relative distribution of the braking magnitude between first and second brake signals for the control of the at least two brake assemblies;
a first cog belt and a second cog belt, the first cog belt passing around a first angular displacement sensor and the second cog belt passing around a second angular displacement sensor,
wherein the first and second brake signals are configured to be modulated during emergency braking so as to apply differential braking to separate wheels of an aircraft; and
wherein the member is a handle, the handle that is movable linearly with respect to a guide in a direction 90 degrees relative to a pivot axis of the handle to indicate braking magnitude and rotatable about the pivot axis to indicate relative distribution of the braking magnitude,
wherein the handle is coupled to both the first cog belt and the second cog belt.

### Claim 2 (depends on 1)

The emergency brake input device as set forth in claim 1, wherein the first brake signal and the second brake signal are electric.

### Claim 3 (depends on 1)

The emergency brake input device as set forth in claim 1, wherein the handle is coupled to both the first cog belt and the second cog belt via a plurality of idler wheels.

### Claim 4 (depends on 3)

The emergency brake input device as set forth in claim 3, further comprising a carriage, the carriage supporting the plurality of idler wheels and the handle.

### Claim 5 (depends on 4)

The emergency brake input device as set forth in claim 4, further comprising a first idler pulley and a second idler pulley, wherein the first cog belt passes through the first idler pulley and wherein the second cog belt passes through the second idler pulley.