MIL-A-8861B (AMENDMENT 1)
作者:标准资料网 时间:2024-05-10 04:43:01 浏览:8792
来源:标准资料网
MIL-A-8861B (AMENDMENT 1), MILITARY SPECIFICATION: AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS (5 DEC 1994)., This amendment forms a part of MIL-A-886lB(AS), dated7 February 1986, and is approved for use within the Naval Air SystemsCommand, Department of the Navy, and is available for use by allDepartments and Agencies of the Department of Defense.
【英文标准名称】:Zincandzincalloys-Castings-Specifications;GermanversionEN12844:1998
【原文标准名称】:锌和锌合金.铸件.规范
【标准号】:EN12844-1998
【标准状态】:现行
【国别】:
【发布日期】:1999-01
【实施或试行日期】:
【发布单位】:欧洲标准学会(EN)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:锌合金;铸件;砂型铸造;规范;化学成分;冷型铸造;名称与符号;定义;作标记;规范(验收);锌
【英文主题词】:Castings;Chemicalcomposition;Chillcasting;Definition;Definitions;Designations;Die-castpart;Marking;Sandcasting;Specification;Specification(approval);Zinc;Zincalloys
【摘要】:
【中国标准分类号】:H62;J31
【国际标准分类号】:77_150_60
【页数】:10P.;A4
【正文语种】:英语
Product Code:SAE AS1701
Title:Lubricant, Solid Film
Issuing Committee:E-25 General Standards For Aerospace And Propulsion Systems
Scope:This document covers the performance requirements for solid dry film lubricants, air dried, or heat cured for use in aerospace applications. These lubricants are intended to prevent galling, and may be capable of remaining effective for extended periods of time after exposure to extreme environmental conditions.
