SAE AS4694 Fitting Assembly, Cap, Hollow End, Acorn, Short Flareless

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【英文标准名称】:Aerospace;studswithMJthread,ringlocked,steel;nominaltensilestrength900MPa,fortemperaturesupto235°C
【原文标准名称】:航空航天.公称抗张强度900Mpa.使用温度235℃以下的钢制环锁紧的MJ螺纹螺柱.
【标准号】:DIN65395-1989
【标准状态】:现行
【国别】:德国
【发布日期】:1989-01
【实施或试行日期】:
【发布单位】:德国标准化学会(DIN)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:形状;螺纹形状;航空航天运输;钢;航天运输;螺柱;材料;设计;作标记;尺寸;热稳定性;质量(物质);额定值;弹簧固定环;紧固件;螺纹;螺钉;表面处理;航空运输;抗拉强度
【英文主题词】:mass;materials;threads;steels;fasteners;screws(bolts);design;aerospacetransport;studs(fasteners);dimensions;surfacetreatment;spacetransport;thermalstability;shape;tensilestrength;marking;airtr
【摘要】:
【中国标准分类号】:V20
【国际标准分类号】:49_030_20
【页数】:5P;A4
【正文语种】:德语


Product Code:SAE ARP5764
Title:Aerospace Active Inceptor Systems for Aircraft Flight and Engine Controls, General Specification For
Issuing Committee:A-6a3 Flight Control Systems Committee
Scope: The purpose of this document will be to develop an ARP for active inceptor systems. The ARP will develop technical material that describes the key characteristics of an active inceptor system and clearly identifies the capabilities and limitations of this type of system. Where appropriate, the effects of platform specific requirements e.g. single axis/dual, single seat/dual seat axis, civil/military, rotary aircraft/conventional aircraft, etc. will be clearly identified. The material developed will serve as a reference guide for a) Aircraft Manufacturers who want to understand AIS technology and develop their own set of requirements, b) Equipment Suppliers who want to develop AIS equipment and c) Regulatory Authorities who will be involved in the certification of these types of systems.
Rationale: The purpose of this document will be to develop an ARP for active inceptor systems. The ARP will develop technical material that describes the key characteristics of an active inceptor system and clearly identifies the capabilities and limitations of this type of system. Where appropriate, the effects of platform specific requirements e.g. single axis/dual, single seat/dual seat axis, civil/military, rotary aircraft/conventional aircraft, etc. will be clearly identified. The material developed will serve as a reference guide for a) Aircraft Manufacturers who want to understand AIS technology and develop their own set of requirements, b) Equipment Suppliers who want to develop AIS equipment and c) Regulatory Authorities who will be involved in the certification of these types of systems.