A number of variations may include a product comprising: a turbomachinery device comprising: an electric motor surrounding a portion of a shaft constructed and arranged to selectively drive the shaft in rotation about a rotational axis, wherein the electric motor further comprises a stator comprising a lamination stack; a housing surrounding the electric motor, wherein the housing includes a plurality of channels constructed and arranged to lubricate a first bearing; and wherein the lamination stack includes at least one retention component wherein the retention component is constructed and arranged to locking the stator in an axial direction while locking rotation of the stator about the rotational axis and wherein the retention component further comprises at least one conduit constructed and arranged to pass fluid through the electric motor to a second bearing.

An adjusting device for mechanically actuating a component may include a housing, which may include a first housing part and a second housing part that abut on one another along a dividing plane. The device may also include an electric motor for rotationally driving an actuator arranged on the second housing part and configured to couple to a component. The first housing part and the second housing part may be fastenable to one another via a plurality of first fastening elements disposed on the first housing part and a plurality of second fastening elements provided complementary thereto and disposed on the second housing part. The plurality of first fastening elements and the plurality of second fastening elements may be arranged evenly distributed in the circumferential direction such that the first housing part and the second housing part are fastenable in a plurality of different rotational positions.

An adjusting device for mechanically actuating a component may include a housing, which may include a first housing part and a second housing part that abut on one another along a dividing plane. The device may also include an electric motor for rotationally driving an actuator arranged on the second housing part and configured to couple to a component. The first housing part and the second housing part may be fastenable to one another via a plurality of first fastening elements disposed on the first housing part and a plurality of second fastening elements provided complementary thereto and disposed on the second housing part. The plurality of first fastening elements and the plurality of second fastening elements may be arranged evenly distributed in the circumferential direction such that the first housing part and the second housing part are fastenable in a plurality of different rotational positions.

An engine may include a plurality of cylinders generating driving torque by burning fuel; a first intake valve disposed in a first intake line in which intake air supplied to the cylinders flows; a second intake valve disposed in a second intake line in which intake air supplied to the cylinders flows; a first electric supercharger disposed in the first intake line; a second electric supercharger disposed in the second intake line; a bypass valve disposed in a bypass line connecting the first intake line and the second intake line; and a controller for controlling the first electric supercharger and the second electric supercharger to be operated in a single mode, a serial mode, or a parallel mode based on an operating region of the engine determined by driving information.

An acoustic damper includes an upstream wall with an inlet aperture and a downstream wall with an outlet aperture. The acoustic damper includes a first resonator that is supported by at least one of the upstream wall and the downstream wall. The acoustic damper also includes a second resonator that is supported by at least one of the upstream wall and the downstream wall. The first resonator and the second resonator are arranged in-parallel. Also, the first resonator and the second resonator are configured to cooperatively attenuate acoustic energy associated with a fluid flowing from the inlet aperture to the outlet aperture.

An acoustic damper includes an upstream wall with an inlet aperture and a downstream wall with an outlet aperture. The acoustic damper includes a first resonator that is supported by at least one of the upstream wall and the downstream wall. The acoustic damper also includes a second resonator that is supported by at least one of the upstream wall and the downstream wall. The first resonator and the second resonator are arranged in-parallel. Also, the first resonator and the second resonator are configured to cooperatively attenuate acoustic energy associated with a fluid flowing from the inlet aperture to the outlet aperture.

A compressor assembly can include a shaft sleeve that includes a bore that extends between a first end and a second end and an outer shoulder; a shaft received by the bore of the shaft sleeve where the shaft includes a compressor end; a compressor wheel disposed on the shaft; and a thrust collar disposed on the shaft and seated between the outer shoulder of the shaft sleeve and the compressor wheel where the thrust collar includes a stem portion and a cap portion that includes a sacrificial portion.

A compressor assembly can include a shaft sleeve that includes a bore that extends between a first end and a second end and an outer shoulder; a shaft received by the bore of the shaft sleeve where the shaft includes a compressor end; a compressor wheel disposed on the shaft; and a thrust collar disposed on the shaft and seated between the outer shoulder of the shaft sleeve and the compressor wheel where the thrust collar includes a stem portion and a cap portion that includes a sacrificial portion.

A device and method for imparting a negative pre-whirl to an airstream entering a compressor wheel of a turbocharger. Using a plurality of radially positioned vanes through which the airstream to the compressor wheel communicates, a negative pre-whirl is imparted to the airstream entering the compressor wheel from an intake passage. This pre-whirl is imparted by positioning the vanes radially within an engageable ring and curving the vanes in a direction opposite the direction of rotation of the compressor wheel. Performance is further enhanced by a hub centrally positioned with the vanes where the hub includes a cavity sized to encapsulate a compressor nut and eliminate air turbulence therefrom.

A device and method for imparting a negative pre-whirl to an airstream entering a compressor wheel of a turbocharger. Using a plurality of radially positioned vanes through which the airstream to the compressor wheel communicates, a negative pre-whirl is imparted to the airstream entering the compressor wheel from an intake passage. This pre-whirl is imparted by positioning the vanes radially within an engageable ring and curving the vanes in a direction opposite the direction of rotation of the compressor wheel. Performance is further enhanced by a hub centrally positioned with the vanes where the hub includes a cavity sized to encapsulate a compressor nut and eliminate air turbulence therefrom.