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Dc-DC converter for controlling an aircraft fan inverter, and associated control method and fan

机译:用于控制飞机风扇逆变器的dc-dc转换器以及相关的控制方法和风扇

摘要

The invention relates to an electric DC-DC converter suitable for being supplied with power by a primary voltage source and for supplying control electronics of a three-phase inverter with power, said three-phase inverter being configured to control a fan of a ventilation system of an aircraft. The DC-DC converter is characterised in that it comprises a transformer (16), a primary circuit (12) comprising two loops forming a symmetrical assembly, at least one secondary circuit (14) comprising a secondary winding (LS), suitable for supplying, firstly, the inverter with an output voltage equal to twice the peak voltage at the terminals of the secondary winding (LS) and, secondly, a branch of the circuit suitable for supplying the inverter with an output voltage equal to the opposite of the peak voltage at the terminals of the secondary winding (LS), and in that the controllable transistors (M1, M2) are suitable for each being switched at zero voltage.
机译:DC-DC转换器技术领域本发明涉及一种DC-DC转换器,该DC-DC转换器适合于由主电压源供电,并且向三相逆变器的控制电子设备供电,所述三相逆变器被配置为控制通风系统的风扇。一架飞机。该DC-DC转换器的特征在于,它包括变压器( 16 ),一次电路( 12 ),一次电路包括形成对称组件的两个环路,至少一个二次电路( 14 )包括一个次级绕组(L S ),适合于首先为逆变器提供输出电压,该输出电压等于次级端子上峰值电压的两倍绕组(L S ),其次是适合于为逆变器提供输出电压的电路分支,该输出电压等于次级绕组端子(L S ),并且可控晶体管(M 1 ,M 2 )适用于在零电压下进行开关的情况。

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