Method for the assembly of a radial turbine and radial turbine

A method for the assembly of a counter-rotating radial turbine, comprising:

• preparing a central case;
• pre-assembling a first turbine unit comprising:
• a first half-case delimiting a first housing;
• a first rotating unit comprising a first shaft housed and rotatably supported in the first housing and that is free to rotate about a first axis of rotation with respect to said first housing;
• a first rotor disc joined to and overhanging a distal end of the first shaft and having a front bladed face facing the opposite side with respect to the first half-case;
• wherein pre-assembling the first turbine unit comprises:
• preparing the first half-case delimiting the first housing;
• preparing the first rotating unit comprising a first support sleeve and the first shaft rotatably housed in the first support sleeve;
• housing the first rotating unit in the first housing and fixing the first support sleeve to the first half-case;
• pre-assembling a second turbine unit comprising:
• a second half-case delimiting a second housing;
• a second rotating unit comprising a second shaft housed and rotatably supported in the second housing and that is free to rotate about a second axis of rotation with respect to said second housing;
• a second rotor disc joined to and overhanging a distal end of the second shaft and having a front bladed face facing the opposite side with respect to the second half-case;
• wherein pre-assembling the second turbine unit comprises:
• preparing the second half-case delimiting the second housing;
• preparing the second rotating unit comprising a second support sleeve and the second shaft rotatably housed in the second support sleeve;
• housing the second rotating unit in the second housing and fixing the second support sleeve to the second half-case;
• coupling the first pre-assembled turbine unit and the second pre-assembled turbine unit to the central case so as to arrange the front bladed face of the first rotor disc in front of the front bladed face of the second rotor disc, wherein, following the coupling process, the first half-case and the second half-case laterally close the central case;
• wherein pre-assembling the first turbine unit comprises:
• coupling first pipes to the first half-case, said first pipes being configured to set a working space delimited between the first rotor disc and the second rotor disc in fluid communication with the exterior;
• wherein pre-assembling the second turbine unit comprises:
• coupling second pipes to the second half-case, said second pipes being configured to set said working space in fluid communication with the exterior;
• and
• further comprising:
• pre-assembling a first set comprising the first pipes joined to each other and applying the first set of first pipes en bloc to the first half-case by means of a relative axial translational movement;
• pre-assembling a second set comprising the second pipes joined to each other and applying the second set of second pipes en bloc to the second half-case by means of a relative translational movement.