Variable turbine geometry component wear mitigation in radial turbomachines with divided volutes by aerodynamic force optimization at all vanes or only vane(s) adjacent to volute tongue(s)

An entryway system comprising:

• a divided volute turbocharger for receiving exhaust gas from an internal combustion engine and for delivering compressed air to the internal combustion engine, the internal combustion engine including a first group of cylinders and a second group of cylinders, said divided volute turbocharger comprising:
• a turbine housing comprising a turbine housing interior adapted to receive a turbine wheel having a plurality of equally spaced turbine blades,
• a first volute adapted for fluid communication with the internal combustion engine and said turbine housing interior for delivering exhaust gas from the first group of cylinders to said turbine housing interior,
• a second volute adapted for fluid communication with the internal combustion engine and said turbine housing interior for delivering exhaust gas from the second group of cylinders to said turbine housing interior independently of said first volute,
• a turbine housing outlet in fluid communication with said turbine housing interior, and
• a wall separating said first volute from said second volute and including a first tongue and a second tongue spaced from said first tongue;
• and
• a vane ring disposed in said turbine housing interior between said first and second volutes and around said turbine wheel, said vane ring comprising an annular disk including a vane ring surface disposed between an inner circumferential ring and an outer circumferential ring with said inner circumferential ring defining an orifice for receiving said turbine wheel, said vane ring surface defining a plurality of openings extending between an upper surface and an opposing lower surface, said vane ring comprising a plurality of vanes dividing said vane ring surface into a first arcuate region and a second arcuate region, with one of said plurality of vanes disposed within a respective one of said openings in said vane ring, wherein at least two of said plurality of vanes are moveable between an open and a closed position about a pivot axis with each of said plurality of vanes comprising:
• a lower shaft received in one opening of said plurality of openings of said vane ring,
• an upper shaft, with a length of said upper shaft axially aligned with a length of said lower shaft so as to define said pivot axis, and
• a vane blade coupled to each of said lower shaft and said upper shaft and extending in length between a leading edge and a trailing edge with a length of each vane blade of said plurality of vanes measured between said leading edge and said trailing edge being equal,
• wherein a first distance between said leading edge and said pivot axis of said vane blade of one of said plurality of vanes is different than a second distance between said trailing edge and said pivot axis of said vane blade of said one of said plurality of vanes, and
• wherein said plurality of vanes includes a first tongue vane positioned adjacent to said first tongue and a second tongue vane positioned adjacent to said second tongue, and wherein the entryway system further comprises:
• a first spacer positioned on said vane ring surface of said annular disk adjacent to said outer circumferential ring with said first spacer aligned along an axis with and extending from said first tongue vane, and
• a second spacer positioned on said vane ring surface of said annular disk adjacent to said outer circumferential ring with said second spacer aligned along an axis with said second tongue vane.

An entryway system comprising:

• a divided volute turbocharger for receiving exhaust gas from an internal combustion engine and for delivering compressed air to the internal combustion engine, the internal combustion engine including a first group of cylinders and a second group of cylinders, said divided volute turbocharger comprising:
• a turbine housing comprising a turbine housing interior adapted to receive a turbine wheel having a plurality of equally spaced turbine blades,
• a first volute adapted for fluid communication with the internal combustion engine and said turbine housing interior for delivering exhaust gas from the first group of cylinders to said turbine housing interior,
• a second volute adapted for fluid communication with the internal combustion engine and said turbine housing interior for delivering exhaust gas from the second group of cylinders to said turbine housing interior independently of said first volute,
• a turbine housing outlet in fluid communication with said turbine housing interior, and
• a wall separating said first volute from said second volute and including a first tongue and a second tongue spaced from said first tongue;
• and
• a vane ring disposed in said turbine housing interior between said first and second volutes and around said turbine wheel, said vane ring comprising an annular disk including a vane ring surface disposed between an inner circumferential ring and an outer circumferential ring with said inner circumferential ring defining an orifice for receiving said turbine wheel, said vane ring surface defining a plurality of openings extending between an upper surface and an opposing lower surface, said vane ring comprising a plurality of vanes dividing said vane ring surface into a first arcuate region and a second arcuate region, with one of said plurality of vanes disposed within a respective one of said openings in said vane ring, wherein at least two of said plurality of vanes are moveable between an open and a closed position about a pivot axis with each of said plurality of vanes comprising:
• a lower shaft received in one opening of said plurality of openings of said vane ring,
• an upper shaft, with a length of said upper shaft axially aligned with a length of said lower shaft so as to define said pivot axis, and
• a vane blade coupled to each of said lower shaft and said upper shaft and extending in length between a leading edge and a trailing edge with a length of each vane blade of said plurality of vanes measured between said leading edge and said trailing edge being equal,
• wherein a first distance between said leading edge and said pivot axis of said vane blade of one of said plurality of vanes is different than a second distance between said trailing edge and said pivot axis of said vane blade of said one of said plurality of vanes, and
• wherein a gap defined between said leading edge of one vane blade of said plurality of vane blades and said trailing edge of an adjacent one vane blade of a first adjacent pair of said plurality of vane blades in said closed position is different in length than a gap defined between said leading edge of one vane blade of said plurality of vane blades and said trailing edge of an adjacent one vane blade of a second adjacent pair of said plurality of vane blades in said closed position.