초록 ▼

A segment of an abradable ring seal for a turbomachine, includes: a reinforcing support; a composite fabric including fibers impregnated with polymerized resin, and a track of abradable material. The composite fabric is interposed between the reinforcing support 71 and the track of abradable materia

A segment of an abradable ring seal for a turbomachine, includes: a reinforcing support; a composite fabric including fibers impregnated with polymerized resin, and a track of abradable material. The composite fabric is interposed between the reinforcing support 71 and the track of abradable material and is bonded to the reinforcing support, on the one side, and to the track of abradable material, on the other side. The segment of an abradable ring seal has a resistance to tearing in a direction perpendicular to the interface between the track of abradable material and the composite fabric, on the one hand, and between the composite fabric and the reinforcing support, on the other hand, greater than 5.106 newtons per square meter. A process for the manufacture of such a segment is also described.

대표청구항 ▼

1. A process for the manufacture of a segment (911) of an abradable ring seal (91) for a turbomachine, said process comprising the following steps: a. to arrange a piece (25) consisting of polymerized abradable material on at least part of the base (82) of a mold (81),b. to cover the piece (25) cons

1. A process for the manufacture of a segment (911) of an abradable ring seal (91) for a turbomachine, said process comprising the following steps: a. to arrange a piece (25) consisting of polymerized abradable material on at least part of the base (82) of a mold (81),b. to cover the piece (25) consisting of polymerized abradable material and a free part of the base (82) of the mold (81) with a composite fabric (61), the composite fabric (61) comprising fibres impregnated with thermosetting resin,c. to cover the composite fabric (61) with a reinforcing support (71), the reinforcing support (71) being placed in the mold (81),d. to submit the mold (81) to a temperature adapted to cause polymerisation of the thermosetting resin and the mutual adhesion of the piece (25) consisting of polymerized abradable material, the composite fabric (61) and the reinforcing support (71), ande. to eject, from the mold (81), a segment (911) of an abradable ring seal (91) for a turbomachine. 2. The process according to claim 1, wherein an additional step is carried out before step b: a′: the composite fabric (61) is preformed on a convex mold. 3. The process according to claim 1, wherein, prior to being arranged in the at least part of the base of the mold, the piece (25) consisting of polymerized abradable material has a curved shape. 4. The process according to claim 3, wherein, when ejected from the mold, the segment (911) of the abradable ring seal (91) is comprised of the reinforcing support (71), the composite fabric (61) with the fibres impregnated with the polymerised resin, and a track of abradable material (93) consisting of the polymerized abradable material, the composite fabric (61) being interposed between the reinforcing support (71) and the track of abradable material (93) and being bonded to the reinforcing support (71), on a first side, and to the track of abradable material (93), on an opposite, second other side, andthe segment (911) of the abradable ring seal (91) having a resistance to tearing in a direction perpendicular to an interface between the track of abradable material (93) and the composite fabric (61), and between the composite fabric (61) and the reinforcing support (71), greater than 5.106 newtons per square meter. 5. The process according to claim 1, wherein, prior to being arranged in the at least part of the base of the mold, the piece (25) consisting of polymerized abradable material has a curved shape and dimensions adapted to correspond to a receiver (97) provided for use in an inner surface (103) of a casing (100) of a fan (101) of a turbomachine. 6. The process according to claim 1, wherein, after step d., the reinforcing support (71) has a honeycomb structure and a density of less than 96 kilograms per cubic meter. 7. The process according to claim 1, wherein, the composite fabric (61) used in step b., comprises a weave based on glass fibres or carbon fibres and the thermosetting resin is an epoxy resin.