【英文标准名称】:Graphicalsymbolsforuseonequipment-Part2:symbolsoriginals.
【原文标准名称】:设备用图形符号.第2部分:符号源
【标准号】:NFC03-417-2-2000
【标准状态】:作废
【国别】:法国
【发布日期】:2000-09-01
【实施或试行日期】:2000-09-05
【发布单位】:法国标准化协会(AFNOR)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:多语种的;作标记;使用;法语;电驱动装置;仪器;英语;符号;图形符号;电气工程
【英文主题词】:marking;graphicsymbols;instruments;applications;englishlanguage;multilingual;frenchlanguage;symbols;electricappliances;electricalengineering;electrically-operateddevices
【摘要】:
【中国标准分类号】:K04
【国际标准分类号】:33_020;29_020;01_080_20
【页数】:275P;A4
【正文语种】:其他


Product Code:SAE AIR6139
Title:Ways of Dealing with Power Regeneration onto an Aircraft Electrical Power System Bus
Issuing Committee:Ae-7c Systems
Scope: This AIR considers the issue of power regeneration onto the Electrical Power system of an aircraft. A series of options for dealing with this regenerative power are considered and arranged in categories. Advantages and disadvantages of each solution, including the existing solution, are included. Validated simulation results from representative Electrical Power systems are presented in order to demonstrate how some of the solutions may operate in practice and how power quality can be maintained during regeneration. The impact on changes to the electrical generation system are also highlighted in this AIR, as these changes may have an impact on the solution deployed and the wider impact on the design of engines and auxiliaries. This AIR reviews concepts and excludes detailed discussions on power system design. These concepts relate to the More Electric Aircraft, cover both AC and DC systems and can be applied to both normal operating conditions or as fault mitigation.
Rationale: This AIR considers the issue of power regeneration onto the Electrical Power system of an aircraft. A series of options for dealing with this regenerative power are considered and arranged in categories. Advantages and disadvantages of each solution, including the existing solution, are included. Validated simulation results from representative Electrical Power systems are presented in order to demonstrate how some of the solutions may operate in practice and how power quality can be maintained during regeneration. The impact on changes to the electrical generation system are also highlighted in this AIR, as these changes may have an impact on the solution deployed and the wider impact on the design of engines and auxiliaries. This AIR reviews concepts and excludes detailed discussions on power system design. These concepts relate to the More Electric Aircraft, cover both AC and DC systems and can be applied to both normal operating conditions or as fault mitigation.