Connecting module between a drive shaft of an engine fan and a rolling-element bearing
View Patent ↗A connecting module interposed between a drive shaft of an aircraft engine fan and a rolling-element bearing, wherein the module includes an inner structure attached to the shaft and including a bonnet, and an outer structure attached to the bearing, which is radially supported on a mechanism installed on the inner structure and delimiting a raceway which is complementary to the bonnet so as to form a ball-joint connection kept in a blocked state by a blocking device installed on the inner structure and protruding radially from the bonnet, wherein a mechanism forming a mechanical fuse provides a junction between the device and the bonnet, such that the ball-joint connection is released following fracture of this mechanism forming a mechanical fuse. The radial support mechanism is added to the device.
1. A connecting module configured to be interposed between a drive shaft of a rotor of a fan of an aircraft engine, and a rolling-element bearing configured to transmit radial and axial forces, the module comprising:
an inner annular structure configured to be attached to the drive shaft, and including a bonnet; and
an outer annular structure configured to be fixed relative to an inner ring of the rolling-element bearing,
wherein the outer structure, radially supported on radial support means installed on the inner structure, delimits a raceway having a shape complementary to a shape of the bonnet, so as to form jointly a ball joint connection kept in a blocked state by a blocking system including a blocking device installed on the inner structure,
wherein the blocking device projects radially towards an exterior from the bonnet, and penetrates into the outer structure,
wherein the module further comprises means forming a mechanical fuse and providing a junction between the blocking device and the bonnet, such that the ball joint connection is released following fracture of the means forming a mechanical fuse, and
wherein the radial support means is provided on the blocking device.
2. The module according to claim 1 , wherein the blocking device also axially retains the inner annular structure relative to the outer annular structure.
3. The module according to claim 1 , wherein the blocking device also retains the inner annular structure relative to the outer annular structure, in a tangential direction.
4. The module according to claim 1 , wherein the blocking device is a ring.
5. The module according to claim 4 , wherein the ring includes through-passages which are circumferentially spaced relative to one another.
6. The module according to claim 5 , wherein the blocking device is fitted in a recess of the outer structure, and the blocking system also includes retaining tabs which are securely attached to the outer structure, fitted in the recess, and traversing the passages made in the ring.
7. The module according to claim 1 , wherein the radial support means includes one or more cylindrical raceways.
8. The module according to claim 1 , wherein the means forming a mechanical fuse includes a narrowed section.
9. An aircraft engine comprising a module according to claim 1 .
10. An engine according to claim 9 , further comprising three rolling-element bearings interposed between the drive shaft of the rotor of the fan and a stator of the engine,
wherein the three bearings are spaced axially relative to one another, and include a forward rolling-element bearing associated with a bearing bracket connected to the stator of the engine by a fusible mechanical link, together with an intermediate rolling-element bearing installed on the drive shaft of the fan rotor by the module.