Rotor assembly with a composite sleeve that is optimized for press-fit installation
A rotor for an electric machine includes a magnetic core configured for arrangement on a shaft. An end ring is arranged on opposite axial ends of the magnetic core. A composite sleeve includes an annular body including an inner surface and an outer surface, and a polymer matrix encapsulating circumferentially oriented fibers. The composite sleeve includes a first tapered portion on the inner surface arranged adjacent to an axial end thereof and configured to facilitate press-fitting of the composite sleeve onto the rotor.
1 . A rotor for an electric machine, comprising:
a magnetic core configured for arrangement on a shaft;
an end ring arranged on opposite axial ends of the magnetic core, the end ring having an axial thickness; and
a composite sleeve comprising an annular body including an inner surface and an outer surface, and a polymer matrix encapsulating circumferentially oriented fibers,
wherein the composite sleeve includes a first tapered portion on the inner surface arranged adjacent to an axial end thereof and configured to facilitate press-fitting of the composite sleeve onto the rotor,
wherein the end ring includes a second tapered portion configured to bias the first tapered portion to facilitate press-fitting of the composite sleeve onto the rotor,
wherein the second tapered portion extends in an axial direction from a flat portion arranged parallel to an axial direction,
wherein the second tapered portion of the end ring extends 75% to 95% of the axial thickness of the end ring and terminates at the flat portion, and
wherein the flat portion has a diameter greater than or equal to a diameter of the magnetic core.
2 . The rotor of claim 1 , wherein a taper angle of the first tapered portion and the second tapered portion is in a range from 0.1° to 5°.
3 . The rotor of claim 1 , wherein the composite sleeve has a diameter in a range from 0.5 to 5 mm after grinding.
4 . The rotor of claim 1 , wherein the annular body comprises:
an outer layer including greater than or equal to 50% axial fibers oriented at an angle greater than 45° of a circumferential direction;
a middle layer comprising greater than or equal to 80% circumferential fibers oriented at an angle less than or equal to 5° of the circumferential direction; and
an inner layer including greater than 50% axial fibers oriented at an angle greater than 45° of a circumferential direction.
5 . The rotor of claim 4 , further comprising a physical vapor deposition coating on the inner surface of the composite sleeve.
6 . The rotor of claim 4 , wherein the middle layer comprises more than 80% of a thickness of the composite sleeve after grinding.
7 . The rotor of claim 4 , wherein the inner layer further includes a filler configured to reduce friction of the inner layer when press-fitting the composite sleeve onto the rotor.
8 . The rotor of claim 7 , wherein the filler is selected from a group consisting of silicon dioxide (SiO 2 ), calcium carbonate (CaCO 3 ), aluminum oxide (Al 2 O 3 ), titanium dioxide (TiO 2 ), graphene and graphene nanoplatelets, zirconium dioxide (ZrO 2 ), and molybdenum disulfide (MoS 2 ), and combinations thereof.
9 . A rotor of an electric machine, comprising:
a magnetic core configured for arrangement on a shaft;
an end ring arranged on opposite axial ends of the magnetic core, the end ring having an axial thickness; and
a composite sleeve comprising an annular body including an inner surface, an outer surface, reinforcing fibers embedded in a polymer matrix, and a first tapered portion formed on an axial end of the inner surface and configured to facilitate press-fitting of the composite sleeve onto the rotor,
wherein the end ring includes a second tapered portion configured to bias the first tapered portion to facilitate press-fitting of the composite sleeve onto the rotor,
wherein the second tapered portion extends in an axial direction from a flat portion arranged parallel to an axial direction,
wherein the second tapered portion of the end ring extends 75% to 95% of the axial thickness of the end ring and terminates at the flat portion, and
wherein the flat portion has a diameter greater than or equal to a diameter of the magnetic core.
10 . The rotor of claim 9 , wherein a taper angle of the first tapered portion is in a range from 0.1° to 5°.
11 . The rotor of claim 9 , wherein the composite sleeve has a diameter in a range from 0.5 to 5 mm.
12 . The rotor of claim 9 , further comprising a ring attached to the outer surface of a pressed end of the composite sleeve.
13 . The rotor of claim 9 , wherein, prior to grinding, the annular body comprises:
an outer layer including greater than or equal to 50% axial fibers oriented at an angle greater than 45° of a circumferential direction;
a middle layer comprising greater than or equal to 80% circumferential fibers oriented at an angle less than or equal to 5° of the circumferential direction; and
an inner layer including greater than 50% axial fibers oriented at an angle greater than 45° of a circumferential direction.
14 . The rotor of claim 13 , wherein the inner layer further includes a filler configured to reduce friction of the inner layer when press-fitting the composite sleeve onto the rotor.
15 . The rotor of claim 14 , wherein the filler is selected from a group consisting of silicon dioxide (SiO 2 ), calcium carbonate (CaCO 3 ), aluminum oxide (Al 2 O 3 ), titanium dioxide (TiO 2 ), graphene and graphene nanoplatelets, zirconium dioxide (ZrO 2 ), and molybdenum disulfide (MoS 2 ), and combinations thereof.
16 . The rotor of claim 14 , wherein the filler comprises nano-sized particles.
17 . The rotor of claim 14 , wherein the filler comprises 1 to 10 wt % of the inner layer.
18 . The rotor of claim 14 , wherein the middle layer comprises more than 80% of a thickness of the composite sleeve after grinding.
19 . A rotor of an electric machine, comprising:
a magnetic core configured for arrangement on a shaft;
an end ring arranged on opposite axial ends of the magnetic core, the end ring having an axial thickness; and
a composite sleeve comprising an annular body including an inner surface, an outer surface, a polymer matrix having fibers embedded therein, and a first tapered portion formed on an axial end of the inner surface and configured to facilitate press-fitting of the composite sleeve onto the rotor,
the end ring including a flat portion arranged parallel to an axial direction and a second tapered portion configured to bias the first tapered portion, the second tapered portion extending in the axial direction from the flat portion,
wherein the second tapered portion of the end ring extends at least 75% of the axial thickness of the end ring, and terminates at the flat portion and an end of the first tapered portion of the composite sleeve, and
wherein the flat portion has a diameter greater than or equal to a diameter of the magnetic core.
20 . The rotor of claim 19 , wherein a taper angle of the first tapered portion and the second tapered portion is in a range from 0.1° to 5°.