Turbine nozzle for a turbomachine
View Patent ↗A turbine nozzle for a turbomachine, the nozzle including two coaxial platforms interconnected by radial vanes, an inner platform being connected to an annular partition that is festooned or crenellated and on which there is fastened an annular support carrying elements made of abradable material. The support is capable of sliding circumferentially over the partition between a mounting-and-dismounting position and a position for locking the support on the partition.
1. A turbine nozzle for a turbomachine, the nozzle being sectorized and comprising:
sectors placed end to end, and each sector comprising two annular platforms that are coaxial, respectively an inner platform and an outer platform, said two annular platforms are connected together by substantially radial vanes, the inner platform being connected to a substantially radial annular partition, wherein an inner periphery of the annular partition of each sector is festooned or crenellated and comprises radially extending solid portions alternating with hollow portions;
a non-sectorized annular support to which elements of abradable material are fastened, the annular support extending continuously over 360°; and
a fastener mechanism for fastening the annular support to the annular partitions of the sectors,
wherein the support is capable of sliding circumferentially over the partitions and being movable angularly between a mounting-and-dismounting position and a locking position in which the fastener mechanism co-operates with the solid portions of the annular partitions of the sectors to hold the support on the partition, and
wherein the fastener mechanism includes a radially extending flange which axially abuts a radially extending surface of the annular partition, and a radially extending rim which abuts a circumferential end of the solid portion of the annular partition in the locking position, and
wherein the support is substantially C-shaped and includes a radially annular wall connected to inner and outer cylindrical walls at inner and outer radial ends of the radially annular wall.
2. A nozzle according to claim 1 , wherein the support is in a form of a rail and is made of sheet metal.
3. A nozzle according to claim 1 , wherein the fastener mechanism defines annular groove portions that are open radially outwards and in which there are received the solid portions of the annular partitions of the sectors in the locking position.
4. A nozzle according to claim 3 , wherein each annular groove portion includes one circumferential end that is open for engaging the fastener mechanism on at least one solid portion of the partition.
5. A nozzle according to claim 1 , wherein the fastener mechanism presents a section that is substantially L or U-shaped, and is regularly distributed around a circumference of the support.
6. A nozzle according to claim 1 , wherein the fastener mechanism is made of sheet metal and fitted to the annular support and fastened, or brazed, or welded thereto.
7. A nozzle according to claim 6 , wherein the fastener mechanism includes a folded sheet metal.
8. A nozzle according to claim 1 , wherein the solid portions are formed at the circumferential ends of the partitions of the sectors of the nozzle.
9. A nozzle according to claim 8 , wherein the partition of each sector includes at each of its circumferential ends one fraction of a solid portion having its other fraction formed by a circumferential end of the partition of an adjacent sector of the nozzle.
10. A nozzle according to claim 1 , wherein the fastener mechanism presents an annular extent or dimension in a circumferential direction that is equal to or greater than a corresponding dimension of the solid portions of the partitions of the sectors.
11. A nozzle according to claim 1 , further comprising annular deflectors of sheet metal fastened or brazed to the partition.
12. A nozzle sector for a nozzle according claim 1 , the sector comprising:
two coaxial annular platforms, respectively an inner platform and an outer platform, that are connected together by substantially radial vanes, the inner platform being secured to a radially inner annular partition,
wherein the inner periphery of the partition is festooned or crenellated and comprises solid potions alternating with hollow portions.
13. A continuous annular support for a nozzle according to claim 1 , including a fastener mechanism regularly spaced apart around the axis of the support and defining annular grooved portions.
14. A continuous annular support according to claim 13 , made of sheet metal.
15. A nozzle according to claim 1 , wherein an axial end portion of the outer cylindrical wall of the support is folded inward so as to present a radial annular rim extending inward from the outer cylindrical wall.
16. A nozzle according to claim 1 , wherein the fastening mechanism includes a cylindrical flange, the radially extending flange of the fastening mechanism radially extends from an axial end of the cylindrical flange, and the radially extending rim of the fastening mechanism extends from a circumferential end of the cylindrical flange.
17. A nozzle according to claim 16 , wherein a radially outer face of the cylindrical flange of the fastening mechanism abuts the solid portion of the annular partition, and a radially inner face of the cylindrical flange of the fastening mechanism abuts the support.
18. A low pressure turbine for a turbomachine, the turbine comprising at least one nozzle according to claim 1 .
19. A turbomachine, an airplane turboprop, or a turbojet, comprising at least one nozzle according to claim 1 .