Unducted fan for turbine engine
View Patent ↗An unducted fan of variable-pitch blades including roots engaged from outside in respective radial housings of an annular rotor element and guided to turn about their respective axes by pairs of rolling bearings, one of which is carried by an annular segment of a cylindrical skirt mounted in a groove of the annular body and by a locknut screwed onto the cylindrical skit. The bearing is covered externally by a ring including outer dog-clutch teeth co-operating with inner dog-clutch teeth of the housing to hold the ring axially in the housing. A blocking mechanism is engaged between the teeth of the housing and the teeth of the ring preventing the ring from turning and preventing the ring from being withdrawn axially from the housing.
1. An unducted fan for a turbine engine, comprising:
fan blades mounted to turn about their respective axes in radial housings of an annular rotor element, each blade including a root with a cylindrical body engaged from outside in a radial housing and guided to turn about its axis in the housing by first and second rolling bearings,
wherein the first bearing is carried by an annular rim of the radial inner end of the housing,
the second bearing is carried by an annular segment of a cylindrical skirt mounted in a groove of the cylindrical body and by a locknut screwed onto the cylindrical skirt of the segment and forming a spacer bearing against the first bearing, the second bearing being covered on the outside by a ring surrounding the cylindrical body of the blade root and including outer dog-clutch teeth co-operating with inner dog-clutch teeth of the housing to retain the ring axially in the housing, and
blocking means are engaged between the dog-clutch teeth of the housing and between the dog-clutch teeth of the ring to prevent the ring from turning and being extracted axially from the housing.
2. A fan according to claim 1 , further comprising an annular cover surrounding the blade root screwed onto the outer end of the housing to prevent the blocking means from being withdrawn axially.
3. A fan according to claim 1 , wherein the annular segment comprises two portions mounted end to end in the groove of the blade body.
4. A fan according to claim 3 , wherein the cylindrical skirt of the annular segment includes at least one axially-projecting tooth engaged in a setback of the cylindrical body and leading into the annular groove to prevent the segment from turning on the cylindrical body.
5. A fan according to claim 1 , further comprising a lockwasher interposed between the nut and the annular segment and that co-operates by interfitting shapes with the nut and with the segment to prevent the nut from turning on the blade root.
6. A fan according to claim 1 , wherein the ring includes three dog-clutch teeth regularly distributed about its axis, each having an angular extent of about 60°.
7. A fan according to claim 1 , wherein the blocking means comprises spacers in a form of sectors of a cylinder engaged by moving in axial translation from outside between the dog-clutch teeth of the ring and the dog-clutch teeth of the housing.
8. A fan according to claim 2 , further comprising a lockwasher interposed between the cover and the ring and that co-operates by interfitting shapes with the cover and with the ring to secure the cover in rotation with the ring.
9. A fan according to claim 1 , wherein the blade root is hollow and includes metal reinforcements fastened on its inner and outer faces by adhesive.
10. A fan according to claim 9 , wherein a wall of the blade root is of substantially constant thickness and includes undulations co-operating with complementary undulations of the reinforcements.
11. A turbine engine, or an airplane turbojet, or turboprop, comprising at least one fan according to claim 1 .