GB/T 36257-2018
ActiveGeneral requirements for hybrid remote power controllers of aircraft
飞机混合式远程功率控制器通用要求
Application Summary AI generated
This standard specifies the general technical requirements, test methods, and acceptance criteria for hybrid remote power controllers used in aircraft electrical power systems. It applies to the design, manufacturing, and quality verification of these controllers, which combine solid-state and electromechanical switching to manage and protect electrical loads in both civil and military aircraft. The standard ensures reliable power distribution and fault isolation in airborne environments.
Related Standards
GB/Z 132-2025
Aerospace electrical requirements—Sleeves and moulded shapes—List of aircraft standards
GB/Z 37312.2-2025
Process management for avionics—Electronic components for aerospace, defence and high performance (ADHP) applications—Part 2：General requirements for passive components
GB/Z 126.1-2025
Process management for avionics—Electronics design—Part 1: Electrical signal properties, naming conventions and interface control document （ICD）
GB/T 13536-1992
Connectors for ground electrical supplies
GB/T 30110-2013
Measuring methods of parameters of HgCdTe epilayers used for space infrared detectors
GB/T 30215-2013
General requirements for electromagnetic relays and contactors of aircraft
GB/T 30205-2013
General requirements for solid remote power controller of aircraft
GB/T 30203-2013
Characteristics of aircraft electrical system
Transparency note: The application summary and key sentences on this page were automatically generated by AI from the standard's original text. This content has not been human-verified and should not be used for compliance or regulatory purposes. Always refer to the official standard document from the issuing authority.