Rotor shaft with cooling bore inlets
The invention relates to a rotor shaft adapted to rotate about a rotor axis thereof. The rotor shaft includes a rotor cavity configured concentrically or quasi-concentrically to the rotor axis inside the rotor shaft, and a plurality of cooling bores extending radially or quasi-radially outward from the inside to an outside of the rotor shaft. Each cooling bore having a bore inlet location and a distal bore outlet portion, the respective bore inlet location being adapted to abut on the rotor cavity. At least one side or part-side of the cooling bore inlet location is provided with an asymmetric edge fillet in order to maximize the wall thickness between two adjacent cooling bores.
1. A rotor shaft adapted to rotate about a rotor axis of the rotor shaft, the rotor shaft comprising: a rotor cavity configured concentrically or quasi-concentrically to the rotor axis inside the rotor shaft, a plurality of cooling bores extending outward from the inside to an outside of the rotor shaft and towards a direction of rotation of the rotor shaft, each of the plurality of cooling bores having a bore inlet and a bore outlet, wherein the each of the plurality of cooling bores comprises a constant cooling bore diameter extending from the bore inlet to the bore outlet, the respective bore inlet being adapted to abut on the rotor cavity, and wherein at least one side or part-side of the circumferential area of the bore inlet is provided with an edge fillet in order to maximize a wall thickness downstream of the edge fillet between two adjacent cooling bores, and wherein the edge fillet of each of the plurality of cooling bores has a radius of 0.3 to 0.7 of the cooling bore diameter and an opposite side of the bore inlet is without an edge fillet, and wherein the edge fillet of each of the plurality of plurality of cooling bores is arranged on a front of the bore in the direction of rotation of the rotor shaft.
2. The rotor shaft according to claim 1 , wherein the edge fillet of the cooling bore is a milled edge fillet.
3. The rotor shaft according to claim 1 , wherein the rotor shaft is a member of a gas or steam turbine or a turbo-machinery.
4. The rotor shaft according to claim 1 , wherein the edge fillet has a depth and a width, and wherein the depth and the width of the edge fillet is 0.3 to 0.7 of the diameter of the cooling bore.
5. The rotor shaft according to claim 1 , wherein the wall thickness abutting the rotor cavity between the rounded edge fillet of each of the plurality of cooling bores and the cooling bore inlet that is without the edge fillet is less than the constant cooling bore diameter.
6. A rotor shaft adapted to rotate about a rotor axis of the rotor shaft, the rotor shaft comprising:
a rotor cavity configured concentrically or quasi-concentrically to the rotor axis inside the rotor shaft; and
a plurality of cooling bores extending outward from the inside to an outside of the rotor shaft and towards a direction of rotation of the rotor, each of the plurality of cooling bores having a cooling bore extending from a bore inlet to a bore outlet, the respective bore inlet being adapted to abut the rotor cavity, and wherein at least one side or part-side of the circumferential area of the bore inlet is provided with a rounded edge fillet having a radius of 0.3 to 0.7 of a diameter of the cooling bore and an opposite side of the bore inlet is without an edge fillet, and wherein the edge fillet of the each of the plurality of plurality of cooling bores is arranged on a front of the bore in the direction of rotation of the rotor.
7. The rotor shaft according to claim 6 , wherein the rounded edge fillet of the cooling bore is a milled round edge fillet.
8. The rotor shaft according to claim 6 , wherein the rotor shaft is a member of a gas or steam turbine or a turbo-machinery.
9. The rotor shaft according to claim 6 , wherein the rounded edge fillet has a depth and a width, and wherein the depth and the width of the rounded edge fillet is 0.3 to 0.7 of the diameter of the cooling bore.
10. The rotor shaft according to claim 6 , wherein the wall thickness abutting the rotor cavity between the rounded edge fillet of each of the plurality of cooling bores and the cooling bore inlet that is without the edge fillet is less than the cooling bore diameter.
11. A rotor shaft adapted to rotate about a rotor axis of the rotor shaft, the rotor shaft comprising: a rotor cavity configured concentrically or quasi-concentrically to the rotor axis inside the rotor shaft; and a plurality of cooling bores extending outward from the inside to an outside of the rotor shaft and towards a direction of rotation of the rotor shaft, each of the plurality of cooling bores extending from a bore inlet to a bore outlet, the respective bore inlet being adapted to abut the rotor cavity, and wherein at least one side or part-side of the circumferential area of the bore inlet is provided with a rounded edge fillet having a radius of 0.3 to 0.7 of a diameter of the cooling bore and an opposite side of the bore inlet is without an edge fillet, and the edge fillet of the each of the plurality of cooling bores being arranged on a front of the bore in a direction of rotation of the rotor, and wherein a wall thickness abutting the rotor cavity between the rounded edge fillet of each of the plurality of cooling bores and the cooling bore inlet that is without the edge fillet is less than the cooling bore diameter.
12. The rotor shaft according to claim 11 , wherein the rounded edge fillet of the cooling bore is a milled round edge fillet.
13. The rotor shaft according to claim 11 , wherein the rotor shaft is a member of a gas or steam turbine or a turbo-machinery.
14. The rotor shaft according to claim 11 , wherein the rounded edge fillet has a depth and a width, and wherein the depth and the width of the rounded edge fillet is 0.3 to 0.7 of the diameter of the cooling bore.