首页> 外国专利> HYSTERESIS-CONTROLLED DC-DC BOOST CONVERTER FOR AERIAL VEHICLES

HYSTERESIS-CONTROLLED DC-DC BOOST CONVERTER FOR AERIAL VEHICLES

机译:飞行器用滞环控制DC-DC升压变换器

摘要

A power conversion unit may include two or more power modules for providing high-voltage direct current power to electrical loads, such as one or more propulsion motors aboard an aerial vehicle. Each of the power modules may be controlled by hysteresis, and may include one or more pairs of transistors that are switched by a gate driver with respect to differences between a reference current and a sensed current passing through a boost inductor. The number, size and shape of the power modules may be selected to accommodate the electrical loads, and may be switched on or off, as necessary. The power conversion unit may feature at least one more power module than is required to meet all anticipated electrical loads, thereby ensuring that the power conversion unit may continue to provide power even in the event that one of the power modules experiences a fault of any kind.
机译:功率转换单元可包括两个或多个功率模块,用于向电气负载(例如飞行器上的一个或多个推进电机)提供高压直流电。每个功率模块可以由滞后控制,并且可以包括一对或多对晶体管,这些晶体管由栅极驱动器根据通过升压电感器的参考电流和感测电流之间的差异进行切换。可选择电源模块的数量、尺寸和形状以适应电气负载,并可根据需要打开或关闭电源模块。功率转换单元可以具有至少一个比满足所有预期电负载所需的功率模块多的功率模块,从而确保即使其中一个功率模块发生任何类型的故障,功率转换单元也可以继续提供功率。

著录项

  • 公开/公告号EP3619806B1

    专利类型

  • 公开/公告日2022-04-13

    原文格式PDF

  • 申请/专利权人 AMAZON TECHNOLOGIES INC.;

    申请/专利号EP20180723650

  • 发明设计人 TRAUBE JOSHUA WHITE;

    申请日2018-04-24

  • 分类号H02P7/29;H02P7/291;H02P31;H02M3/155;H02M3/156;B64C39/02;B64C29;

  • 国家 EP

  • 入库时间 2022-08-25 00:31:44

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