Crusher rotor
A rotor for a comminution apparatus that is arranged to launch material to be comminuted towards a surface, such as an anvil or an autogenous layer of crushed material. The rotor includes a frame including an upper plate, a lower plate and wall elements extending between the upper plate and the lower plate. The rotor further includes an inlet opening in the upper plate and an outlet located between the upper plate and the lower plate. An uppermost surface of the frame and a lowermost surface of the frame have a greater hardness than the rest of the frame such that additional wear protection elements may be omitted at those uppermost and lowermost surfaces.
1 . Rotor for a comminution apparatus, said rotor being arranged to launch material to be comminuted towards a surface, said rotor comprising a frame including an upper plate, a lower plate and wall elements extending between said upper plate and said lower plate, the rotor further comprising an inlet opening in said upper plate and an outlet located between the upper plate and the lower plate, wherein the upper plate and the lower plate has a greater hardness than the wall elements such that an uppermost surface of the frame and a lowermost surface of the frame has a greater hardness than the rest of the frame such that additional wear protection elements can be omitted at those upper most and lowermost surfaces.
2 . Rotor in accordance with claim 1 , wherein the frame is provided in the form of a weldment.
3 . Rotor in accordance with claim 1 , wherein the frame is balanced about its intended rotational axis.
4 . Rotor in accordance with claim 1 , wherein a ratio of the hardness of at least one of the upper plate and the lower plate to the hardness of at least one of the wall elements lies in a range of 1.3 to 5.3.
5 . Rotor in accordance with claim 1 , wherein a ratio of the hardness of at least one of the upper plate and the lower plate to the hardness of at least one of the wall elements lies in a range of 2.5 to 3.
6 . Rotor in accordance with claim 1 , wherein a ratio of the tensile strength of at least one of the upper plate and the lower plate to the tensile strength of at least one of the wall elements lies in a range of 1.5 to 3.8.
7 . Rotor in accordance with claim 1 , wherein a ratio of the tensile strength of at least one of the upper plate and the lower plate to the tensile strength of at least one of the wall elements lies in a range of 2.2 to 2.6.
8 . Rotor in accordance with claim 1 , wherein the frame is configured to receive replaceable wear protection elements at exposed areas thereof.
9 . Rotor in accordance with claim 8 , wherein the replaceable wear protection elements are weight matched to reduce imbalance.
10 . Rotor in accordance with claim 8 , wherein the replaceable wear protection elements comprise one or more of the following: cavity wear plates; trail plates; rotor tips; distribution plate arranged at the lower plate, downstream from the inlet.
11 . Rotor in accordance with claim 1 , wherein a circumference of the upper plate and the lower plate have a generally circular shape.
12 . Rotor in accordance with claim 11 , wherein the upper plate and the lower plate have local recesses deviating from the circular shape.
13 . Method for manufacturing a rotor for a comminution apparatus, said rotor being arranged launch material to be comminuted towards a surface, said method comprising the following steps
providing rotor an upper plate having an inlet opening therein, a lower plate and wall elements;
connecting said wall elements such that they extend between said upper plate and said lower plate and such that one or more outlets are created between the upper plate and the lower plate,
wherein the upper plate and the lower plate has a greater hardness than the wall elements such that an uppermost surface of the upper plate and a lowermost surface of the lower plate has a greater hardness than the rest of the rotor such that additional wear protection elements may be omitted at those surfaces.
14 . Comminution apparatus comprising a rotor in accordance with claim 1 .