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GB/Z 24837-2009 1100kV高压交流隔离开关和接地开关技术规范

作者:标准资料网 时间:2024-05-14 23:09:30  浏览:9669   来源:标准资料网
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基本信息
标准名称:1100kV高压交流隔离开关和接地开关技术规范
英文名称:Specification for 1100 kV alternating-current disconnectors and earthing switches
中标分类: 电工 >> 输变电设备 >> 高压开关设备
ICS分类: 电气工程 >> 输电网和配电网 >> 变电站、电涌放电器
发布部门:中华人民共和国国家质量监督检验检疫总局 中国国家标准化管理委员会
发布日期:2009-11-30
实施日期:2010-05-01
首发日期:2009-11-30
作废日期:
主管部门:中国电力企业联合会
归口单位:中国电力企业联合会
起草单位:国家电网公司、中国电力科学研究院、西安高压电器研究院、华东电网有限公司、清华大学、西安交通大学、西安西开高压电气股份有限公司等
出版社:中国标准出版社
出版日期:2010-05-01
页数:64页
计划单号:20076812-Z-524
适用范围

 本指导性技术文件规定了1100kV高压交流隔离开关和接地开关的使用条件、额定值、设计与结构、试验、选用导则、运输、储存、安装、运行和维护等要求。本指导性技术文件适用于设计安装在户外、额定电压1100 kV且运行频率50 Hz的交流隔离开关和接地开关。

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所属分类: 电工 输变电设备 高压开关设备 电气工程 输电网和配电网 变电站 电涌放电器
下载地址: 点击此处下载
MIL-HDBK-336-3, MILITARY HANDBOOK SURVIVABILITY, AIRCRAFT, NONNUCLEAR, GENERAL CRITERIA (VOLUME 3) (4 FEB 1983)., This is the first volume in a four-volume design handbook for nonnuclear survivability of military aircraft. Each volume is structured to be used in conjunction with the other three volumes, as needed, in the design process. The objective of Volume 3 is to provide a ready reference containing design information on military aircraft engine and propulsion system survivability. It contains data on design-techniques to reduce visual, infrared, radar, and aural detectability; and projectile and high-energy laser vulnerability of military aircraft engines and engine installations. The design techniques discussed ranged from combat- and test- proven systems, through development, laboratory, and breadboard equipment, to undeveloped concepts. Turbine engines are stressed, but piston engines are also presented. APPLICATION: The data contained in this design handbook have been arranged to support the development of both fixed and rotary wing military aircraft. Each has unique mission and performance characteristics that require specialized attention and design solutions. The subystem design categories have been established with these considerations in mind. For example, the power train and rotor blade subsystems deal primarily with military helicopter applications, while the launch/recovery systems deal with those subsystem elements for both fixed and rotary wing aircraft landing gear systems and for those systems related to the assisted takeoff (launching) and deceleration (recovery) methods most used by the Air Force and Navy fixed-wing aircraft.

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