Brake for an aircraft wheel
A brake for an aircraft wheel comprising an actuator-carrier 14 that carries at least one electromechanical actuator 15 having a pusher 19 that is movable along a direction parallel to an axis of rotation X of the wheel 2 and facing friction elements 7, 10 in order to apply a braking force selectively against the friction elements 7, 10 . The actuator-carrier 14 and the actuator 15 include guide means 25, 32 for guiding the actuator 15 while being installed on the actuator-carrier 14 in a radial direction Y until it reaches a service position. The guide means forms a bearing surface for transmitting braking forces from the actuator to the actuator-carrier. Position-holder means 37 holds the position of the actuator in its service position and comprises a strap 37 fastened to the actuator-carrier 14 to prevent the actuator 15 from moving on the actuator-carrier 14 in the service position.
1. A brake for an aircraft wheel, the brake comprising:
an actuator-carrier ( 14 );
at least one electromechanical actuator ( 15 ) carried by the actuator-carrier and having a pusher ( 19 ) that is movable along a direction parallel to an axis of rotation (X) of the wheel ( 2 ) and facing friction elements ( 7 , 10 ) in order to apply a braking force selectively against the friction elements ( 7 , 10 ),
the actuator-carrier ( 14 ) and the actuator ( 15 ) including guide means ( 25 , 32 ) for guiding the actuator ( 15 ) while it is being installed on the actuator-carrier ( 14 ) in a radial direction (Y) until it reaches a service position, said guide means forming a bearing surface suitable for transmitting braking forces from the actuator to the actuator-carrier, and
position-holder means ( 37 ) for holding the position of the actuator in its service position,
wherein the position-holder means ( 37 ) comprises a strap ( 37 ) fastened to the actuator-carrier ( 14 ) in order to prevent the actuator ( 15 ) from moving on the actuator-carrier ( 14 ) in the service position, and
wherein the guide means includes a groove located on the actuator and the strap is at least partially seated within the groove.
2. A brake according to claim 1 , wherein the strap ( 37 ) is removable radially and is fastened to the actuator-carrier ( 14 ) by fastener means ( 39 ) including at least one screw ( 39 ) that extends radially.
3. A brake according to claim 2 , wherein the strap ( 37 ) comes to bear against a bearing face of the actuator-carrier ( 38 ) that is perpendicular to the radial direction (Y) for installing the actuator ( 15 ).
4. A brake according to claim 1 , wherein the guide means ( 25 , 32 ) form the groove ( 25 ) in the actuator ( 15 ) and form a projection ( 32 , 42 ) on the actuator carrier suitable for penetrating in the groove ( 25 ) in order to provide radial guidance for the actuator ( 15 ) in the actuator-carrier ( 14 ).
5. A brake according to claim 4 , wherein the groove ( 25 ) is defined on the actuator between a face of a ring ( 27 ) surrounding a body ( 16 , 18 ) of the actuator ( 15 ) and a facing face of a base ( 24 ) projecting from the body ( 16 , 18 ) of the actuator ( 15 ).
6. A brake according to claim 4 , wherein the groove is defined on the actuator ( 15 ) by a ring ( 44 ) surrounding a body ( 16 , 18 ) of the actuator ( 15 ).
7. A brake according to claim 1 , wherein the guide means ( 25 , 32 ) are shaped to provide positive guidance preventing any axial movement of the actuator ( 15 ) while it is being installed.
8. A brake according to claim 1 , wherein the strap is a structure separate from the actuator ( 15 ) and is operative to secure the actuator to the actuator-carrier ( 14 ).
9. A brake according to claim 1 , wherein the strap ( 37 ) closes off a reception space in the actuator carrier ( 14 ) for the actuator ( 15 ) and is operative to secure the actuator ( 15 ) to the actuator-carrier ( 14 ).