【英文标准名称】:Petroleumproductsandlubricants;determinationofflashpoint;Pensky-Martensclosedcupmethod
【原文标准名称】:石油产品和润滑剂.闪点的测定.潘斯基--马丁斯(Pensky-Martens)闭杯法
【标准号】:ISO2719-1988
【标准状态】:作废
【国别】:国际
【发布日期】:1988-12
【实施或试行日期】:1988-12-01
【发布单位】:国际标准化组织(ISO)
【起草单位】:ISO/TC28
【标准类型】:()
【标准水平】:()
【中文主题词】:试验;试验设备;石油产品;测定;潘斯基-马丁斯仪;闪点;润滑剂
【英文主题词】:combustibleliquids;tests;pensky-martensapparatus;crucibles(laboratory);lubricatingoils;flashpoint;determination;lubricants;flametest;liquids;petroleumproducts;testequipment;testing
【摘要】:
【中国标准分类号】:E30
【国际标准分类号】:75_080
【页数】:11P;A4
【正文语种】:英语
基本信息
| 标准名称： | 固体火箭发动机静止试验程序 |
| 中标分类： |
航空、航天 >>
航天器及其附件 >>
航天器动力系统 |
| ICS分类： |
航空器和航天器工程 >>
航空航天发动机和推进系统
|
| 替代情况： | QJ 1004-1994 |
| 发布日期： | |
| 实施日期： | 2004-12-01 |
| 首发日期： | |
| 作废日期： | |
| 出版日期： | |
适用范围
没有内容
前言
没有内容
目录
没有内容
引用标准
没有内容
所属分类： 航空 航天 航天器及其附件 航天器动力系统 航空器和航天器工程 航空航天发动机和推进系统
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.