Device for attaching ring sectors around a turbine rotor of a turbomachine
View Patent ↗A device for attaching ring sectors around a turbine rotor in a turbomachine is disclosed. Each of the ring sectors includes at its upstream end a circumferential rim being able to be held on an annular casing rail by an annular locking member, and at its downstream end a pressing part that can press axially against a fixed element of the turbine to prevent the upstream rim of the ring sector from disengaging from the locking member in the event of considerable wear of the rail.
1. A device for attaching ring sectors around a turbine rotor in a turbomachine, each ring sector comprising:
a frustoconical wall that supports a block of abradable material attached to a radially inner surface of the frustoconical wall;
a circumferential rim disposed at an upstream end of the ring sector which is engaged in a radially inner annular groove of an annular casing rail and held radially in the groove by a C-section annular locking member that is engaged axially from upstream on the casing rail and on the circumferential rims of the ring sectors; and
a pressing part disposed at a downstream end of the ring sector that is fitted and attached to the radially inner surface of the frustoconical wall and to the block of abradable material of the ring sector,
wherein the part presses axially against a fixed element of the turbine to prevent the upstream circumferential rim from disengaging from the wall of the locking member, and
wherein the axial clearance between the pressing part and the fixed element is less than the axial length of a bearing surface of the upstream rim of the wall on the locking member.
2. The device as claimed in claim 1 , wherein a portion of the pressing part presses radially on the fixed element.
3. The device as claimed in claim 1 , wherein the pressing part is attached to the radially inner surface of the downstream end of the frustoconical wall and to the block of abradable material by brazing or welding.
4. The device as claimed in claim 1 , wherein an axial clearance between the pressing part and the fixed element is between 0.3 and 1.2 mm approximately.
5. The device as claimed in claim 1 , wherein the pressing part has an F-shaped section.
6. The device as claimed in claim 5 , wherein the pressing part comprises first and second rims in a portion of a cylinder that extend in the downstream direction, the first rim being attached to a radially inner surface of the wall of the ring sector and the second rim being able to press radially on a radially outer face of a cylindrical rim of the fixed element.
7. The device as claimed in claim 1 , wherein the fixed element forms part of a turbine guide vane element.
8. A turbomachine which comprises at least one device as claimed in claim 1 .
9. A turbomachine turbine, which comprises at least one device as claimed in claim 1 .
10. The device as claimed in claim 1 , wherein a radially inner surface of the pressing part presses against the fixed element of the turbine and a radially outer surface of the pressing part is fitted and attached to the radially inner surface of the frustoconical wall.
11. A ring sector for a turbomachine turbine, comprising:
a frustoconical wall that supports a block of abradable material attached to a radially inner surface of the frustoconical wall;
a rim disposed at an upstream end of the ring sector for coupling to a casing; and
an axial and radial pressing part disposed at a downstream end of the ring sector that is fitted and attached to the radially inner surface of the frustoconical wall and to the block of abradable material of the ring sector.
12. The ring sector as claimed in claim 11 , wherein the pressing part is attached by welding or brazing to the block of abradable material and to the radially inner surface of the downstream end of the frustoconical wall of the ring sector.