ASME SEC III D1 APP A2003-2003 更改摘要

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【英文标准名称】:Rubbercompoundingingredients-Abbreviations.
【原文标准名称】:橡胶配合剂.缩略语
【标准号】:NFT40-107-2006
【标准状态】:作废
【国别】:法国
【发布日期】:2006-02-01
【实施或试行日期】:2006-02-20
【发布单位】:法国标准化协会(FR-AFNOR)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:缩写;名称与符号;配料;混合物;橡胶;符号
【英文主题词】:Abbreviations;Designations;Ingredients;Mixtures;Rubber;Symbols
【摘要】:
【中国标准分类号】:G34
【国际标准分类号】:83_040_20
【页数】:21P.;A4
【正文语种】:其他


Product Code:SAE AIR4253
Title:Description of Actuation Systems for Aircraft With Fly-By-Wire Flight Control Systems
Issuing Committee:A-6a3 Flight Control Systems Committee
Scope: This information report (AIR) provides design information of various contemporary aircraft fly-by-wire flight control actuation systems that may be useful in the design of future actuation systems for similar applications. This AIR provides a description of representative state-of-the-art, fly-by-wire (FBW) actuation systems used in flight control systems of manned aircraft. It presents the basic characteristics, hardware descriptions, redundancy concepts, functional schematics, and discussions of the servo controls, failure monitoring, and fault tolerance. All existing FBW actuation systems are not described herein; however, those most representing the latest designs are included. While this AIR is intended as a reference source of information for future aircraft actuation system designs, the exclusion or omission of any other appropriate actuation system or subsystem should not limit consideration of their use on future aircraft.
Rationale: This information report (AIR) provides design information of various contemporary aircraft fly-by-wire flight control actuation systems that may be useful in the design of future actuation systems for similar applications. This AIR provides a description of representative state-of-the-art, fly-by-wire (FBW) actuation systems used in flight control systems of manned aircraft. It presents the basic characteristics, hardware descriptions, redundancy concepts, functional schematics, and discussions of the servo controls, failure monitoring, and fault tolerance. All existing FBW actuation systems are not described herein; however, those most representing the latest designs are included. While this AIR is intended as a reference source of information for future aircraft actuation system designs, the exclusion or omission of any other appropriate actuation system or subsystem should not limit consideration of their use on future aircraft.