发明名称 Stator section for an axial flux electric machine with liquid cooling system
摘要 In a stator section of an axial flux electric machine with liquid cooling system, a toroidal core having an inside cylindrical surface and an outside cylindrical surface coaxial with each other along a reference axis, is provided along its annular center line with a plurality of electrical conductor coils spaced from each other and each placed around the core and having a first, a second, a third and a fourth face. Each cooling duct section produces a movement of the liquid coolant from a first to a second base surface of the core and is located between faces of two consecutive coils. At least a face of each coil is adjacent to and in contact with at least one cooling duct section.
申请公布号 US8963383(B2) 申请公布日期 2015.02.24
申请号 US200913130157 申请日期 2009.11.25
申请人 发明人 Lucchi Fabio
分类号 H02K3/24;H02K3/46;H02K9/19 主分类号 H02K3/24
代理机构 Pearne & Gordon LLP 代理人 Pearne & Gordon LLP
主权项 1. A stator section for an axial flux electric machine with liquid cooling system, comprising: a toroidal core having an inside cylindrical surface and an outside cylindrical surface coaxial with each other along a reference axis that is to be made coincide with the axis of rotation of a rotor section of an axial flux electric machine; liquid cooling means; a plurality of electrical conductor coils spaced from each other and distributed along the annular centre line of the core;where: each coil: has the shape of a solid with a hole passing through it, can be divided into four consecutive sides running round the through hole, is placed around the core with a first side of it lying on the outside cylindrical surface, a second side of it lying on the inside cylindrical surface and a third and fourth side of it lying transversally to the first and second sides, wherein the liquid cooling means comprise a plurality of cooling duct sections through which a liquid coolant can flow;each cooling duct section is in one of the two following, alternative conditions: either it is interposed between the first sides of two consecutive coils along the annular centre line of the core at a radial distance from the reference axis greater than or equal to the radius of the outside cylindrical surface, or it is interposed between the second sides of two consecutive coils along the annular centre line of the core at a radial distance from the reference axis less than or equal to the radius of the inside cylindrical surface;each cooling duct section produces a movement of the liquid coolant from a first to a second reference plane, both perpendicular to the reference axis, spaced from each other along the reference axis and corresponding, respectively, to at least one portion of a first base surface of the core and at least one portion of a second base surface of the core;at least the first or the second side of each coil is adjacent to and in contact with at least one respective cooling duct section of the plurality of cooling duct sections, wherein each coil is an individual coil for which the first, second, third and fourth side extend along lines lying on a same plane, and wherein the toroidal core has a cylindrical outside lateral surface and a cylindrical inside lateral surface, coaxial with each other along an axis that coincides with the axis of rotation of the rotor section, and is made by a metal strip wound spirally on itself around said axis.
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