【英文标准名称】:Thermalsolarsystemsandcomponents-Custombuiltsystems-Part3:Performancetestmethodsforsolarwaterheaterstores;GermanversionEN12977-3:2012
【原文标准名称】:太阳热能设备和部件.定制设备.第3部分:太阳蓄水加热器的性能试验方法
【标准号】:DINEN12977-3-2012
【标准状态】:现行
【国别】:德国
【发布日期】:2012-06-01
【实施或试行日期】:
【发布单位】:德国标准化学会(DE-DIN)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:
【英文主题词】:Classification;Components;Definitions;Durability;Efficiency;Evaluations;Hotwaterpreparationplants;Installations;Interpretations;Outputdetermination;Performance;Plant;Potablewater;Ratingtests;Reliability;Residentialareas;Safetyrequirements;Solarheating;Solarpower;Solar-powereddevices;Specification(approval);Storagewaterheaters;Stores;Testset-ups;Testing;Thermal;Thermalefficiency;Thermaltesting;Volumeflowrate;Water;Waterheating;Water-heatingplants
【摘要】:
【中国标准分类号】:F12
【国际标准分类号】:27_160
【页数】:54P;A4
【正文语种】:德语
基本信息
| 标准名称： | 锡锌合金镀层技术条件 |
| 中标分类： |
|
| ICS分类： |
航空器和航天器工程 >>
有关航空航天制造用涂覆与有关工艺
|
| 发布日期： | 1996-08-13 |
| 实施日期： | 1996-12-31 |
| 首发日期： | |
| 作废日期： | |
| 出版日期： | |
| 页数： | 7页 |
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： 航空器和航天器工程 有关航空航天制造用涂覆与有关工艺
Product Code:SAE AIR1083
Title:Airborne Hydraulic and Control System Survivability for Military Aircraft
Issuing Committee:A-6a2 Military Aircraft Committee
Scope: This SAE Aerospace Information Report (AIR) provides the hydraulic system designer with the various design options and techniques currently available to enhance the survivability of hydraulic systems. A comprehensive knowledge of the hostile environment to which the air vehicle will be exposed will form form the basis upon which the overall design philosophy is formulated. The designer should strive to achieve at the absolute minimum acceptable flying quality level to complete the operational mission for which the aircraft is designed; i.e., the aircraft can be controlled and the mission terminated safely, including landing. This AIR will attempt to address the following threats: a. typical small arms fire (5,56, 7.62, 12.7 and 14.5 mm AP); b. cannon (20, 30, and 40 mm API/HEI);c. NBC/EMI/EMP/beamed particle; and d. chemical/biological. Protection against missiles is beyond the scope of this AIR. Except for electronic counter-measures or evasive maneuvers, no practice technology exists which allows a hydraulic system to survive a direct hit by a missile or large caliber anti-aircraft projectile. The AIR addresses the following major topics: a. design concepts and architecture; b. Design implementation; c. Subsystem mechanization; and d. Component design. gy exists which allows a hydraulic system to survive a direct hit by a missile or large caliber anti-aircraft projectile. The AIR addresses the following major topics: a. design concepts and architecture; b. Design implementation; c. Subsystem mechanization; and d. Component design.
Rationale: This SAE Aerospace Information Report (AIR) provides the hydraulic system designer with the various design options and techniques currently available to enhance the survivability of hydraulic systems. A comprehensive knowledge of the hostile environment to which the air vehicle will be exposed will form form the basis upon which the overall design philosophy is formulated. The designer should strive to achieve at the absolute minimum acceptable flying quality level to complete the operational mission for which the aircraft is designed; i.e., the aircraft can be controlled and the mission terminated safely, including landing. This AIR will attempt to address the following threats: a. typical small arms fire (5,56, 7.62, 12.7 and 14.5 mm AP); b. cannon (20, 30, and 40 mm API/HEI);c. NBC/EMI/EMP/beamed particle; and d. chemical/biological. Protection against missiles is beyond the scope of this AIR. Except for electronic counter-measures or evasive maneuvers, no practice technology exists which allows a hydraulic system to survive a direct hit by a missile or large caliber anti-aircraft projectile. The AIR addresses the following major topics: a. design concepts and architecture; b. Design implementation; c. Subsystem mechanization; and d. Component design. gy exists which allows a hydraulic system to survive a direct hit by a missile or large caliber anti-aircraft projectile. The AIR addresses the following major topics: a. design concepts and architecture; b. Design implementation; c. Subsystem mechanization; and d. Component design.