Patent ID: 11913473
Assignee: GARRETT TRANSPORTATION I INC.
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  H | IPC F  H

Claim 10:
11. The compressor device of claim 1, wherein the axial end of the motor case is comprised of a first axial end and a second axial end, the axial portion of the coolant jacket is a first axial end portion that spans in the radial direction across the first axial end of the motor case; wherein the coolant jacket includes a second axial end portion that spans in the radial direction across the second axial end of the motor case; wherein the plurality of flow passages includes a first junction that fluidly connects the radial portion of the coolant jacket and the first axial end portion, and wherein the plurality of flow passages includes a second junction that fluidly connects the radial portion of the coolant jacket and the second axial end portion.