IP Library › Granted Patent US 10,899,325
Granted Patent B2
US 10,899,325 · App. 16/378,227 · Granted Jan 26, 2021

Brake load balance and runway centering techniques

Inventors: Marc Georgin (Dayton, OH); Efrem E. Ayichew (Troy, OH)
Assignee: Goodrich Corporation
B60T8/1703B60T8/17613B60W10/188B64C25/426B64C25/48B60T8/1701B60T8/1761B60T8/24B60T2201/03B60T2230/02B60T2250/03B60W10/184G05D1/0816
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Quick Facts
Patent No.
US 10,899,325
App. No.
16/378,227
Granted
Jan 26, 2021
Kind
B2
Abstract

A method for controlling brakes includes receiving, by a controller, a first wheel speed from a first wheel speed sensor of a first wheel arrangement, receiving, by the controller, a second wheel speed from a second wheel speed sensor of a second wheel arrangement, calculating, by the controller, a pressure correction, and adjusting, by the controller, a pressure command for at least one of the first wheel arrangement and the second wheel arrangement.

Claims (43)

1. A method for controlling brakes of an aircraft, comprising:

receiving, by a controller, a first wheel speed from a first wheel speed sensor of a first wheel arrangement, wherein the first wheel arrangement comprises a first brake of the aircraft, the first brake comprises a first brake stack;

receiving, by the controller, a second wheel speed from a second wheel speed sensor of a second wheel arrangement, wherein the second wheel arrangement comprises a second brake of the aircraft, the second brake comprises a second brake stack;

calculating, by the controller, a brake pressure correction based upon the first wheel speed and the second wheel speed; and

adjusting, by the controller, a brake pressure command for at least one of the first brake and the second brake;

wherein the brake pressure command is adjusted based upon the brake pressure correction;

the brake pressure correction is calculated for balancing a first tire drag force of the first wheel arrangement and a second tire drag force of the second wheel arrangement; and

the brake pressure correction is calculated using equation

Δ

⁢

⁢

P_j

=

±

I

wh

_x

⁡

(

ω

.

xr

-

ω

.

xj

)

A

·

k

·

n

·

R

b

·

μ

cc

,

wherein ΔP_j denotes the brake pressure correction, I wh _x denotes a rotational moment of inertia of at least one of the first wheel arrangement and the second wheel arrangement, {dot over (ω)} xr denotes a wheel deceleration of at least one of the first wheel arrangement and the second wheel arrangement, {dot over (ω)} xj denotes a wheel deceleration of the other of the first wheel arrangement and the second wheel arrangement, A denotes a piston area, k denotes a number of carbon friction surfaces, n denotes a number of brake stacks, R b denotes a brake force torque arm, and μ cc denotes a coefficient of friction.

2. The method of claim 1 , further comprising sending, by the controller, the adjusted brake pressure command to a brake control device of the second wheel arrangement.

3. The method of claim 2 , wherein the adjusted brake pressure command comprises the brake pressure command adjusted by the brake pressure correction.

4. The method of claim 1 , wherein the brake pressure command is adjusted by a value of the brake pressure correction.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 8, 2019
From: GEORGIN, MARC; AYICHEW, EFREM E.
To: GOODRICH CORPORATION
Reel/Frame 048826/0504 →
Continuity (2)
Division 15595573 · May 15, 2017
Related Publication 20190232932A1 · Aug 1, 2019
Cited By (1)
US 12,576,823