IP Library Granted Patent US 8,602,505
Granted Patent B2
US 8,602,505 · App. 12/914,492 · Granted Dec 10, 2013

Architecture for an electromechanical braking system

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Quick Facts
Patent No.
US 8,602,505
App. No.
12/914,492
Granted
Dec 10, 2013
Kind
B2
Abstract

The invention relates to an architecture for powering aircraft brakes for an aircraft having at least two undercarriages, each having a certain number of wheels, each of the wheels being fitted with brakes, each having a certain number of electromechanical braking actuators, the architecture including controllers for delivering power signals to the actuators in response to a braking order, the wheels on each of the undercarriages being grouped together in first and second complementary groups such that for each group of wheels, a first group of actuators is controlled by one controller that controls those actuators only, and a complementary second group of actuators is controlled by another controller that controls only those actuators.

Claims (12)

1. An architecture for powering aircraft brakes for an aircraft having at least two undercarriages, each undercarriage having a plurality of wheels, the architecture comprising:

a brake fitted to each of said wheels, each brake having a plurality of electromechanical braking actuators;

a plurality of controllers, each controller being configured for delivering power signals to a respective one or more of the actuators in response to a braking order,

wherein, the plurality of wheels on each of the at least two undercarriages being grouped together in first and second complementary groups, and

wherein, for each wheel in said first and second complementary groups of wheels, a first group of actuators is controlled by one controller that controls those actuators only, and a complementary second group of actuators is controlled by another controller that controls only those actuators.

2. An architecture according to claim 1 , wherein the two controllers controlling the actuators of a given group of wheels are powered by distinct power supplies.

3. An architecture according to claim 2 , having power supply units for powering the controllers from power supplies of the aircraft, each of the power supply units powering two controllers.

4. An architecture according to claim 3 , wherein the power supply units include first, second, third and fourth power supply units that power the controllers as follows:

the first power supply unit powers the controller that controls one group of actuators of the first group of wheels of the first undercarriage, and the controller that controls one group of actuators of the first group of wheels of the second undercarriage;

the second power supply unit powers the controller that controls a complementary group of actuators of the first group of wheels of the first undercarriage, and the controller that controls a group of actuators of the second group of wheels of the second undercarriage;

the third power supply unit powers the controller that controls a group of actuators of the second group of wheels of the first undercarriage, and the controller that controls a complementary group of actuators of the first group of wheels of the second undercarriage; and

the fourth power supply unit powers the controller that controls a complementary group of actuators of the second group of wheels of the first undercarriage, and the controller that controls a complementary group of actuators of the first group of wheels of the second undercarriage.

Assignments (3)
CHANGE OF NAME Recorded Dec 8, 2016
From: MESSIER-BUGATTI-DOWTY
To: SAFRAN LANDING SYSTEMS
Reel/Frame 040851/0908 →
CHANGE OF NAME Recorded Oct 4, 2011
From: MESSIER-BUGATTI
To: MESSIER-BUGATTI-DOWTY
Reel/Frame 027015/0397 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 29, 2010
From: FRANK, DAVID
To: MESSIER-BUGATTI
Reel/Frame 025218/0236 →