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SAE J17 Latex Foam Rubbers

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Product Code:SAE J17
Title:Latex Foam Rubbers
Issuing Committee:Committee On Automotive Rubber Specs
Scope:These specifications and methods of testing apply to cellular-rubber products known as latex foam rubbers but do not apply to sponge and expanded rubbers. The base material used in their manufacture may be natural rubber, reclaimed rubber, synthetic rubber, or rubberlike materials, alone or in combination. In case of conflict between the provisions of these general specifications and those of detailed specifications or methods of test for a particular product, the latter shall take precedence. Reference to methods for testing cellular-rubber products should specifically state the particular test or tests desired. The SAE Committee on Automotive Rubber Specifications has concluded, that in light of the fact that SAE J17 is a mirror image of ASTM D 1055, SAE J17 will be eliminated in the year 2005.
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【英文标准名称】:Non-activesurgicalimplants-Jointreplacementimplants-Particularrequirements
【原文标准名称】:非活性外科植入物.关节替代用植入物.特殊要求
【标准号】:ISO21534-2002
【标准状态】:作废
【国别】:国际
【发布日期】:2002-11
【实施或试行日期】:
【发布单位】:国际标准化组织(ISO)
【起草单位】:ISO/TC150
【标准类型】:()
【标准水平】:()
【中文主题词】:金属;功能;定义;医疗设备;生产;塑料;铰链;材料;精整;试验;规范(验收);作标记;骨接合术;制造日期;关节;钝性的;设计;陶瓷;外科学;连接;外科植入物;外科植入物;包装件
【英文主题词】:
【摘要】:ThisEuropeanStandardspecifiesparticularrequirementsfortotalandpartialjointreplacementimplants,artificialligamentsandbonecement,hereafterreferredtoasimplants.Forthepurposesofthisstandard,artificialligamentsandtheirassociatedfixingdevicesareincludedinthetermimplant,hereinafterreferredtoasimplants.Itspecifiesrequirementsforintendedperformance,designattributes,materials,designevaluation,manufacturing,sterilization,packagingandinformationtobesuppliedbythemanufacturer.Sometestsrequiredtodemonstratecompliancewiththisstandardarecontainedinorreferencedinlevel3standards.
【中国标准分类号】:C35
【国际标准分类号】:11_040_40
【页数】:12P;A4
【正文语种】:英语


MIL-HDBK-1797, DEPARTMENT OF DEFENSE HANDBOOK: FLYING QUALITIES OF PILOTED AIRCRAFT (19 DEC 1997) (S/S BY MIL-STD-1797A)., This standard is intended for use with fixed-wing aircraft supported primarily by aerodynamic force rather than engine thrust. It also covers the handling characteristics of aircraft under piloted control on the ground, and may be used with powered-lift aircraft in aerodynamic flight (above the conversion speed, Vcon). This standard also applies to piloted transatmospheric flight when flight depends upon aerodynamic lift and/or air breathing propulsion systems. Flying qualities of military rotorcraft are specified in MIL-H- 8501. while flying qualities in V/STOL flight are the subject of MIL-F-83300. NOTE: MIL-STD-1797A has been redesignated as a handbook, and is to be used for guidance purposes only. This document is no longer to be cited as a requirement. For administrative expediency, the only physical change from MIL-STD-1797A is this cover page. However, this document is no longer to be cited as a requirement. If cited as a requirement, contractors may disregard the requirements of this document and interpret its contents only as guidance. For further background information, see Appendix C.