Turbine-blade retaining structure and rotary machine having the same
View Patent ↗A turbine-blade retaining structure in which deformation of end portions of locking pieces exposed through an insertion window portion in the axial direction is prevented, and the occurrence of a crack in a welded portion is prevented. At least one of the end portions of adjacent locking pieces exposed through the insertion window portion is provided with a thick-plate portion that expands in the disc-thickness direction so as to be inside the insertion window portion.
1. A turbine-blade retaining structure comprising:
blade grooves that extend through a rotor disc in a disc-thickness direction so as to receive blade roots of turbine blades arranged in a circumferential direction;
a protruding portion that protrudes, as a whole, outwards in the disc-thickness direction such that an outer circumferential end is located at an inner side of an inner circumferential end of the blade grooves in the radial direction;
a ring-shaped locking groove that is formed in a circumferential edge portion of the protruding portion along the circumferential direction so as to open towards an outer side in the radial direction;
a step portion that protrudes outwards in the disc-thickness direction in a circumferential edge portion on an inner circumferential side of the blade root so as to face the locking groove; and
plate-like locking pieces arranged in the circumferential direction and received in the ring-shaped locking groove, the locking pieces being fitted between the locking groove and the step portion;
wherein the circumferential edge portion of the protruding portion is provided with, along the circumferential direction, at least one insertion window portion that is cut out in the disc-thickness direction such that an inner circumferential surface thereof is flush with an inner circumferential surface of the locking groove, and
end portions of adjacent locking pieces, exposed through the insertion window portion, are joined to each other by means of welding; and
at least one of the end portions of the adjacent locking pieces exposed through the insertion window portion is provided with a thick-plate portion expanding in the disc-thickness direction so as to be inside the insertion window portion.
2. A turbine-blade retaining structure according to claim 1 , wherein the thick-plate portion is provided from one end of the locking piece that is joined by means of welding, towards a side at the other end.
3. A turbine-blade retaining structure according to claim 2 , wherein a recessed groove is provided in a central portion of the thick-plate portion in the width direction so as to extend from the one end of the locking piece, which is joined by means of welding, towards the side at the other end and so as to open at the one end.
4. A turbine-blade retaining structure according to claim 1 , wherein the thick-plate portion is provided on end portion of the locking piece on a leading side in a rotation direction of the rotor disc.
5. A turbine-blade retaining structure according to claim 1 , wherein a sloped portion is provided so as to be formed to have a plate thickness that increases gradually from one end of the locking piece, which is joined by means of welding, towards a side at the other end.
6. A rotary machine comprising the turbine-blade retaining structure according to claim 1 .
7. A turbine-blade retaining structure comprising:
blade grooves that extend through a rotor disc in a disc-thickness direction so as to receive blade roots of turbine blades arranged in a circumferential direction;
a protruding portion that protrudes, as a whole, outwards in the disc-thickness direction such that an outer circumferential end is located at an inner side of an inner circumferential end of the blade grooves in the radial direction;
a ring-shaped locking groove that is formed in a circumferential edge portion of the protruding portion along the circumferential direction so as to open towards an outer side in the radial direction;
a step portion that protrudes outwards in the disc-thickness direction in a circumferential edge portion on an inner circumferential side of the blade root so as to face the locking groove; and
plate-like locking pieces received in the ring-shaped locking groove and fitted between the locking groove and the step portion;
wherein the circumferential edge portion of the protruding portion is provided with, along the circumferential direction, at least one insertion window portion that is cut out in the disc-thickness direction such that an inner circumferential surface thereof is flush with an inner circumferential surface of the locking groove, and
end portions of adjacent locking pieces are exposed through the insertion window portion and are joined to each other by means of welding; and
at least one of the end portions of the locking pieces is provided with a thick-plate portion expanding in the disc-thickness direction.
8. A turbine-blade retaining structure according to claim 7 , wherein the thick-plate portion is provided from one end of the locking piece that is joined by means of welding, towards a side at the other end.
9. A turbine-blade retaining structure according to claim 8 , wherein a recessed groove is provided in a central portion of the thick-plate portion in the width direction so as to extend from the one end of the locking piece, which is joined by means of welding, towards the side at the other end and so as to open at the one end.
10. A turbine-blade retaining structure according to claim 7 , wherein the thick-plate portion is provided on end portion of the locking piece on a leading side in a rotation direction of the rotor disc.
11. A turbine-blade retaining structure according to claim 7 , wherein a sloped portion is provided so as to be formed to have a plate thickness that increases gradually from one end of the locking piece, which is joined by means of welding, towards a side at the other end.
12. A rotary machine comprising the turbine-blade retaining structure according to claim 7 .