Aircraft variable frequency alternator anti-parallel control circuit

By simplifying the LACTR hardwired interlock logic and interlock wiring design, the problem of accidental parallel connection caused by errors in the aircraft variable frequency AC motor parallel controller is solved, improving the safety and reliability of the system, preventing parallel connection of AC sources, and protecting the motor and electrical equipment.

CN122418818APending Publication Date: 2026-07-17COMMERCIAL AIRCRAFT CORP OF CHINA LTD +1
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
COMMERCIAL AIRCRAFT CORP OF CHINA LTD
Filing Date
2026-04-28
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In existing technologies, when aircraft variable frequency AC motors are connected to the grid in parallel, controller errors or unexpected program issues can cause contactors to be connected in parallel unexpectedly, which may damage the motors and affect electrical equipment. Furthermore, the hard-wired interlock design is prone to failure, reducing system reliability.

Method used

Design a parallel control circuit for an aircraft variable frequency AC generator. By simplifying the LACTR hard-wired interlocking logic, hard-wired interlocking is achieved using interlocking connections, reducing the number of hard wires and auxiliary contacts, and improving system reliability.

Benefits of technology

Without affecting the power grid control logic, it significantly improves the safety and reliability of the system, prevents accidental parallel connection of AC sources, and enhances the protection of motors and electrical equipment.

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Abstract

本公开的一方面涉及一种用于飞机电源系统的互锁控制电路,飞机电源系统包括第一发电机和第二发电机、外电源、辅助发电机,所述互锁控制电路包括用于控制第一和第二发电机进入或退出电网的第一和第二投网接触器;用于控制外电源和辅助发电机进入或退出电网的第三和第四投网接触器;用于将第一与第三投网接触器互连的第一互连接触器;用于将第二与四投网接触器互连的第二互连接触器;以及用于将第一互连接触器与第二互连接触器互连的第三互连接触器,其中每个接触器均包括辅助触点,其中每个辅助触点包括常闭触点和常开触点,其中第一互连接触器与第一投网接触器的常闭触点连接,并通过第一发电机控制单元接地。
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