Device for connecting two rotating shafts, in particular in a turbomachine
View Patent ↗Device for connecting two rotating shafts ( 10, 12 ), one driving and the other driven, comprising rectilinear splines ( 20 ) formed on the driving shaft ( 10 ) and engaged in complementary rectilinear splines ( 22 ) of the driven shaft ( 12 ), the splined region of the driven shaft having, in the vicinity of one of its longitudinal ends, at least one cylindrical portion ( 26 ) having a greater torsional flexibility.
1. A turbomachine comprising two rotating shafts, wherein one of said two rotating shafts is a driving shaft and the other of said two rotating shafts is a driven shaft configured to be driven by said driving shaft, wherein the driving shaft has rectilinear splines engaged in a driven spline portion of the driven shaft having rectilinear splines complementing the rectilinear splines of the driving shaft, wherein the driven shaft comprises at least one cylindrical portion devoid of splines located within the driven splined portion, and wherein said cylindrical portion has a torsional flexibility that is greater than a torsional flexibility of said driven spline portion.
2. The turbomachine as claimed in claim 1 , wherein the driving shaft, has a cylindrical portion corresponding to the cylindrical portion of the driven shaft, wherein said cylindrical portion of the driving shaft is devoid of splines.
3. The turbomachine as claimed in claim 2 , wherein the cylindrical portions of the driven and driving shafts are in the vicinity of downstream ends of the splines of the shafts.
4. The turbomachine as claimed in claim 2 , wherein the cylindrical portions of the driven and driving shafts are in the vicinity of upstream ends of the splines of the shafts.
5. The turbomachine as claimed in claim 1 , wherein, in the cylindrical portion, the splines of the driven shaft and of the driving shaft are configured to eliminate any contact between the splines.
6. The turbomachine as claimed in claim 1 , wherein the cylindrical portion has a radius that is less than a radius of said driven spline portion.
7. The turbomachine as claimed in claim 1 , wherein the cylindrical portion, defines drilled holes.
8. The turbomachine as claimed in claim 1 , wherein the length of the cylindrical portion is approximately 15 to 30% of the total length of that the driven spline portion.
9. The turbomachine of claim 1 , comprising a compressor with said driven shaft, and further comprising a turbine with said driving shaft.
10. The turbomachine as claimed in claim 1 , wherein the cylindrical portion has a thickness that is less than a thickness of said driven spline portion.
11. The turbomachine as claimed in claim 1 , wherein said splines of said driving and driven shafts are uniformly distributed around a longitudinal axis of said turbomachine.
12. The turbomachine as claimed in claim 11 , wherein said cylindrical portion is free of spline and extends around the longitudinal axis of said turbomachine.
13. The turbomachine as claimed in claim 12 , wherein said cylindrical portion defines holes aligned in a row that extends around the longitudinal axis of said turbomachine.
14. The turbomachine as claimed in claim 12 , wherein said cylindrical portion defines holes aligned in two parallel rows that extend around the longitudinal axis of said turbomachine.