Development of High Power, High Voltage Magnetic Components and Encapsulated Inductor for Power Propulsion Unit

S. Lorenzen, L. Gregersen, M. Simpson
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Abstract

As electrical power propulsion units (PPU) have become a major part for the space industry the need for higher power components at higher voltages has increased. This digest is based on an European Space Agency (ESA) development contract: “Planar and encapsulated SMD inductive electronic component qualification”, contract number: “4000122089/17/ NL/CRS”. There are two design and development objectives of this project. First, high power high voltage (HPHV) components for the PPU and second being encapsulated inductive components. The project underwent four phases such as component specification, component design, production and verification testing. Firstly, a 5 kW case study of PPU technology was made to create a specification for the PPU inductive components. Thereafter, the electrical design was completed. This was followed by the production of the PPU components. The PPU components were manufactured and finalized by verification testing consisting of power burn-in, mechanical shock, vibration, and temperature loaded stress tests. The PPU components have been designed using the planar ferrite cores, which enables a high power component with a relatively low build height. The disadvantage of the planar core is the lack of bobbin, therefore aircoil winding technology has been utilized which gives a large design freedom. The transformer was designed and manufactured with a coil consisting of flat wire windings stacked on top of each other, while the inductor was designed and manufactured using copper foil windings. In order to develop encapsulated magnetics a collaboration with the company Sintex A/S was established. Sintex A/S specializes in making high precision custom shapes in metal and soft magnetic composite materials. In this collaboration, Sintex A/S is providing expertise and manufacturing of the ferrite component of the encapsulated inductor. Both the HPHV components and the encapsulated inductor have been designed, manufactured and verified by testing.
动力推进装置大功率高压磁性元件及封装电感器的研制
随着电力推进装置(PPU)成为航天工业的重要组成部分,对高电压、高功率元件的需求也在增加。本摘要基于欧洲航天局(ESA)的一项开发合同:“平面和封装SMD感应电子元件鉴定”,合同编号:“4000122089/17/ NL/CRS”。这个项目有两个设计和开发目标。首先是用于PPU的高功率高压(HPHV)组件,其次是封装的电感组件。该项目经历了组件规格、组件设计、生产和验证测试四个阶段。首先,对一个5kw的PPU技术案例进行了研究,以创建PPU电感元件的规范。此后,电气设计完成。接下来是PPU组件的生产。PPU组件的制造和最终确定通过验证测试,包括功率老化,机械冲击,振动和温度加载应力测试。PPU组件采用平面铁氧体铁芯设计,这使得组件具有相对较低的构建高度。平面铁芯的缺点是没有筒子,因此采用了气圈绕线技术,使设计自由度大。变压器的设计和制造是用一个由扁线绕组堆叠在一起的线圈组成的,而电感的设计和制造是用铜箔绕组。为了开发封装磁性材料,与Sintex a /S公司建立了合作关系。Sintex A/S专门从事金属和软磁复合材料的高精度定制形状。在此次合作中,Sintex A/S提供封装电感的铁氧体组件的专业知识和制造。HPHV组件和封装电感都经过了设计、制造和测试验证。
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