2024電動(dòng)無人機(jī)高壓配電系統(tǒng)技術(shù)規(guī)范

Technicalspecificationforhighvoltagepowerdistributionsystemofelectric GB/T18384GB/T38909GB/T38924ASTMF2490-20飛機(jī)用電負(fù)荷與電源容量分析（AircraftElectricalLoadandPowerSourceCapacityAnalysis）ASTMF2639-18（DesignAlterationandCertificationofAircraftElectricalWiringSystems）ASTMF2696-14（StandardPracticeforInspectionofAirplaneElectricalWiringSystems）ASTMF2799-14（StandardPracticeforMaintenanceofAirplaneElectricalWiringSystems）ASTMF3239-22a（AircraftElectricPropulsionASTMF3316-19電動(dòng)或混合動(dòng)力推進(jìn)飛機(jī)的電氣系統(tǒng)（ElectricalSystemsforAircraftwithElectricorHybrid-ElectricPropulsion）EASASCE-19（Electric/HybridPropulsionRTCA/DO-160G（EnvironmentalConditionsandTestProceduresforAirborneEquipment）RTCA/D0-178C機(jī)載系統(tǒng)和設(shè)備合格審定中的軟件考慮(SoftwareConsiderationsinAirborneSystemsandEquipmentCertification)RTCA/D0-254機(jī)載電子設(shè)備硬件設(shè)計(jì)保證指南(DesignAssuranceGuidanceforAirborneElectronicHardware)SAEAIR7502（AircraftElectricalVoltageLevelSC-VTOL-01（VTOL）航空器（SpecialCondition：VerticalTake-OffandLanding(VTOL)Aircraft）高壓配電系統(tǒng)HighVoltagePowerDistribution高壓配電控制系統(tǒng)ControlSystemofHighVoltagePowerDistribution高壓匯流條開關(guān)保護(hù)裝置c）負(fù)載的運(yùn)行不應(yīng)對發(fā)電、配電和布線產(chǎn)生有害影響；g）電動(dòng)無人機(jī)高壓配電系統(tǒng)最大工作電壓應(yīng)大于60VDC，各主機(jī)廠可根據(jù)自身設(shè)計(jì)需求適當(dāng)調(diào)整工1電壓等級(jí)60-300432電壓等級(jí)300-600864電壓等級(jí)600-10001440電壓等級(jí)1000-15002160b）匯流條在流過電流并分流時(shí)，不應(yīng)產(chǎn)生有危害的高溫。b）對于飛行安全所必不可少的電路保護(hù)裝置，不應(yīng)用于保護(hù)其他電路；（“自動(dòng)斷路”裝置，其跳閘機(jī)構(gòu)不能由操縱器件來操控）應(yīng)設(shè)