Turbomachine rotor arrangement
View Patent ↗In a succession of rotor disks, only the end disks are connected to a main structure by bolted extensions and the intermediate disks are suspended from rigid spacer pieces by centering and anti-rotation connections. The end disks are interconnected to clamp the assembly in the axial direction. There is no bolted connection between the successive disks. Assembly is very easy. The disks and the spacer pieces are stacked together in alternately, and the assembly is torsionally very rigid because of the use of a high number of claw-coupling teeth formed by protruding ends of the blade roots forming teeth that engage in spacer piece end rims.
1. A rotor arrangement comprising a succession of disks carrying blades and joined by spacer pieces, wherein two of the disks, at opposite ends of the succession, are provided with extensions, wherein the extensions are tapered to meet at joined flanges, wherein said succession comprises at least one intermediary disk between said two disks, said at least one intermediary disk being suspended from at least one of said spacer pieces.
2. The arrangement as claimed in claim 1 , wherein the extensions are joined by an array of claw-coupling teeth and recesses for said extension teeth.
3. The arrangement as claimed in claim 1 , wherein each disk is provided with axially spaced annular ledges.
4. The arrangement as claimed in claim 3 , wherein the spacer pieces comprise axially spaced annular rims.
5. The arrangement as claimed in claim 4 , wherein one of the spacer pieces comprises a claw coupling to just one of the rims.
6. The arrangement as claimed in claim 4 , wherein the rims on the spacer pieces extend radially inwardly, and a shell ring extends between each adjacent pair of rings, concentric with the associated spacer piece, and each shell ring and the associated spacer piece form a ventilation chamber into which the slots of the associated disks open.
7. The arrangement as claimed in claim 4 , wherein the rims of each spacer piece extend one radially inwardly and the other radially outwardly.
8. The arrangement as claimed in claim 4 , wherein each rim engages an associated ledge.
9. The arrangement as claimed in claim 8 , wherein the disks and the rims comprise co-operating arrays of claw-coupling teeth and recesses for receiving said teeth and extending around the rims.
10. The arrangement as claimed in claim 9 , wherein blade roots are engaged in individual slots in the disks and pass through the disks, the teeth being formed by ends of the blade roots protruding from the slots.
11. The arrangement as claimed in claim 1 , wherein said succession comprises a plurality of intermediary disks between said two disks, each of said intermediary disks being suspended from at least one of said spacer pieces.
12. The arrangement as claimed in claim 11 , wherein each of said intermediary disks is suspended from two of said spacer pieces.
13. The arrangement according to claim 1 , wherein the spacer pieces comprise axially spaced annular rims, blade roots are engaged in individual slots in the disks and pass through the disks, and a shell ring forms a ventilation chamber together with at least one of the spacer pieces and a disk slot.
14. The arrangement as claimed in claim 13 , wherein the rims on the spacer pieces extend radially inwardly.
15. The arrangement as claimed in claim 13 , wherein said shell ring extends between each adjacent pair of rings.
16. The arrangement as claimed in claim 15 , wherein said shell ring is concentric with the associated spacer piece.
17. The arrangement as claimed in claim 16 , wherein the slots of the associated disks open into said ventilation chamber.
18. The arrangement according to claim 1 , wherein the spacer pieces comprise axially spaced annular rims, and wherein at least one of said rims extends radially outwardly.
19. The arrangement as claimed in claim 18 , wherein another of said rims extends radially inwardly.
20. A rotor arrangement comprising a succession of disks carrying blades and joined by spacer pieces, wherein two of the disks, at opposite ends of the succession, are provided with extensions, the extensions are tapered to meet at joined flanges, each disk is provided with axially spaced annular ledges, the spacer pieces comprise axially spaced annular rims, each rim engaging an associated ledge, the disks and the rims comprise co-operating arrays of claw-coupling teeth and recesses for receiving said teeth and extending around the rims, and the rims of each spacer piece extend one radially inwardly and the other radially outwardly.
21. A rotor arrangement comprising a succession of disks carrying blades and joined by spacer pieces, wherein two of the disks, at opposite ends of the succession, are provided with extensions, the extensions are tapered to meet at joined flanges, each disk being provided with axially spaced annular ledges, the spacer pieces comprise axially spaced annular rims, each rim engaging an associated ledge, the disks and the rims comprise co-operating arrays of claw-coupling teeth and recesses for receiving said teeth and extending around the rims, blade roots are engaged in individual slots in the disks and pass through the disks, the teeth being formed by ends of the blade roots protruding from the slots, the rims on the spacer pieces extend radially inwardly, a shell ring extends between each adjacent pair of rings, concentric with the associated spacer piece, and each shell ring and the associated spacer piece form a ventilation chamber into which the slots of the associated disks open.