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- W2056998315 abstract "While manufacturing the stator/rotor assemblies of the aircraft power components, increased power losses are typically pronounced due to an imposed axial load onto the stack of magnetic laminates to increase the rigidity of the stack. An axial loader to enable core loss measurements to be made while the laminate stack is subjected to an axial load has been designed. The apparatus and multilayered slotted interface plates, allowing for the toroidal windings and simultaneous load application were used to evaluate the effect of compression up to 27.5 MPa on magnetic properties of commercially available Fe–Co based Hiperco® 50, Hiperco® 50 HS, and Hiperco® 27 alloys. For each composition, we tested two sets of samples: (1) completely insulated and (2) uninsulated. We report the increased losses due to an axial load and discuss the origin of these increased losses in terms of constant size anisotropy for completely insulated laminates." @default.
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- W2056998315 date "2003-05-09" @default.
- W2056998315 modified "2023-10-18" @default.
- W2056998315 title "Magnetic properties of FeCo laminates subjected to axial loading" @default.
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- W2056998315 doi "https://doi.org/10.1063/1.1556106" @default.
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