Balancing system for turbomachine rotor
View Patent ↗The present invention relates to a turbomachine rotor balancing system comprising a balancing flange ( 52 ) provided with through-passageways ( 78 ), the system further comprising balance weights ( 54 ) each mounted fixedly on the flange ( 52 ) by means of a first and a second screw/nut assembly ( 56 a, 56 b ) having a first and a second screw ( 84, 84 ) passing through a first and a second passageway ( 78, 78 ). According to the invention, said first screw is pressing against a first tangential end side ( 116 ) of the first through-passageway, and at a distance from a second tangential end side, and the second screw is pressing against a second tangential end side ( 118 ) of the second through-passageway, and at a distance from the first tangential end side.
1. A turbomachine rotor balancing system comprising a balancing flange provided with a plurality of through-passageways, said system also comprising a plurality of balance weights each mounted fixedly onto said balancing flange by means of a first and a second screw/nut assembly having respectively a first screw and a second screw passing respectively through a first and a second directly consecutive passageway, each of said passageways having a first and a second tangential end side situated on either side of the screw of said associated screw/nut assembly, said second tangential end side being offset tangentially from the first tangential end side in a first direction and said first through-passageway being offset tangentially from said second through-passageway in a second direction opposite to the first direction,
wherein said first screw is pressing against said first tangential end side of said first through-passageway and at a distance from said second tangential end side, and wherein said second screw is pressing against said second tangential end side of said second through-passageway and at a distance from said first tangential end side.
2. The balancing system as claimed in claim 1 , wherein, in cross section of the flange passing through said through-passageways, for each of said through-passageways, a maximum distance (D) in the tangential direction between the two tangential end sides is greater than a maximum length (d) of said screw in this same tangential direction, so that the ratio D/d lies between 1.2 and 2.
3. The balancing system as claimed in claim 2 , wherein, in cross section of the flange passing through said through-passageways, each of said through-passageways has an axis of symmetry extending radially, and wherein a screw axis of said screw passing through said passageway is offset tangentially from said axis of symmetry.
4. The balancing system as claimed in claim 1 , wherein, in cross section of the flange passing through said through-passageways, each of said through-passageways has an axis of symmetry extending radially, and wherein a screw axis of said screw passing through said passageway is offset tangentially from said axis of symmetry.
5. The balancing system as claimed in of claims 1 - 4 or 3 , wherein, in cross section of the flange passing through said through-passageways, each of said through-passageways has a radial end portion consisting of an arc of a circle with a radius (R 1 ) on either side of which are respectively two arcs of a circle with a radius (R 2 ) less than the radius (R 1 ).
6. The balancing system as claimed in claim 5 , wherein said radius (R 2 ) is substantially identical to the radius of said screw passing through said passageway.
7. The balancing system as claimed in claim 6 , wherein each through-passageway takes the form of a scallop or a hole.
8. A turbomachine module which comprises at least one balancing system as claimed in claim 6 .
9. The turbomachine module as claimed in claim 8 , which is a turbine or a turbomachine compressor.
10. The balancing system as claimed in claim 5 , wherein each through-passageway takes the form of a scallop or a hole.
11. A turbomachine module which comprises at least one balancing system as claimed in claim 5 .
12. The turbomachine module as claimed in claim 11 , which is a turbine or a turbomachine compressor.
13. The balancing system as claimed in of claims 1 - 4 , wherein each through-passageway takes the form of a scallop or a hole.
14. A turbomachine module which comprises at least one balancing system as claimed in claim 13 .
15. The turbomachine module as claimed in claim 14 , which is a turbine or a turbomachine compressor.
16. A turbomachine module which comprises at least one balancing system as claimed in any of claims 1 - 4 .
17. The turbomachine module as claimed in claim 16 , which is a turbine or a turbomachine compressor.
18. A turbomachine comprising at least one module as claimed in claim 16 .