Method of unblocking an aircraft wheel brake

1. A method of unblocking an aircraft wheel brake performed by an operator on the ground, the brake having at least one electromechanical actuator ( 5 ) with at least one electric motor and a pusher ( 10 ) movable under drive from the motor facing friction elements ( 8 ) of the brake in order to apply a braking force selectively against the friction elements ( 8 ), the actuator ( 5 ) being provided with a blocking member ( 12 ) for blocking the pusher ( 10 ) in position, at least after the actuator has been operated to apply a parking brake force, the unblocking method being characterized in that it comprises the steps of:

the operator on the ground bringing an external control unit ( 25 ) to the proximity of the wheel in such a way that the operator on the ground can connect the external control unit ( 25 ) to the brake,

connecting the external control unit ( 25 ) to the brake, the external control unit being adapted to act at least on the blocking member ( 12 ) of the actuator; and

using the external control unit ( 25 ) to cause the blocking member ( 12 ) to unblock the pusher ( 10 ), the blocking member ( 12 ) having power supplied exclusively by the external control unit ( 25 ).

2. An unblocking method according to claim 1 , wherein the control unit ( 25 ) is also adapted to act on the motor of the actuator to move the pusher ( 10 ), the method including a step of using the external control unit ( 25 ) to cause the pusher ( 10 ) to reverse.

3. An unblocking method according to claim 1 , including, in addition to the above-mentioned steps:

an initial step consisting in disconnecting from the brake an electrical cable bundle ( 17 ) extending along the landing gear so as to enable the external control unit ( 25 ) to be connected to the brake instead of the electrical cable bundle ( 17 ); and

a final step consisting in disconnecting the external control unit ( 25 ) and in reconnecting the electrical cable bundle ( 17 ) to the brake.

4. An unblocking method according to claim 1 , wherein the external control unit ( 25 ) has a source of electrical energy ( 28 ) suitable for powering the brake while it is being controlled by the external control unit ( 25 ).

5. An unblocking method according to claim 1 , wherein the external control unit ( 25 ) is connected directly to the brake.

6. An external control unit ( 25 ) separate from an aircraft and configured for being brought into the proximity of an aircraft wheel by an operator on the ground in order to control a brake of the wheel, the brake including at least one electromechanical actuator ( 5 ) with at least one electric motor and a pusher ( 10 ) movable under drive from motor facing friction elements ( 8 ) of the brake in order to apply a braking force selectively against the friction elements ( 8 ), the actuator being provided with a blocking member ( 12 ) for blocking the pusher ( 10 ) in position, at least after the actuator has been operated to apply a parking brake force, the unit ( 25 ) comprising:

at least one electrical energy source ( 28 ),

brake connection means ( 26 , 27 ) for connection of the unit to the brake, and

control means ( 29 ) powered by the energy source ( 28 ) and adapted to act at least on the blocking member ( 12 ) of the brake via the brake connection means in order to unblock the pusher ( 10 ),

wherein the blocking member ( 12 ) has power supplied exclusively by the external control unit ( 25 ).