V40 电气系统与设备 标准查询与下载

ARMY MIL-G-58083 A VALID NOTICE 2-2005 螺纹安装四极转速表发电机

MIL-G-58083A remains inactive for new design, however, the document is valid for use.

GENERATOR, TACHOMETER, FOUR POLE, SCREW MOUNTED

ARMY MS87015 REV A VALID NOTICE 3-2005 螺杆式四极转速表发电机

The activities above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at http://assist.daps.dla.mil

GENERATOR, TACHOMETER, FOUR-POLE, SCREW-MOUNTED

DLA A-A-59286 VALID NOTICE 1-2005 工具分解发电机

The activities above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at http://assist.daps.dla.mil

ELECTRICAL DISCHARGE MACHINE, TOOL DISINTEGRATING

NF L58-405-406*NF EN 3841-406:2005 航空航天系列.断路器.试验方法.第406部分:易燃性

Aerospace series - Circuits breakers - Test methods - Part 406 : flammability.

NF L58-405-404*NF EN 3841-404:2005 航空航天系列.断路器.试验方法.第404部分:防爆

Aerospace series - Circuits breakers - Test methods - Part 404 : explosion proofness.

BS EN 60952-1:2004 飞行器用蓄电池组.第1部分:一般试验要求和性能水平

This part of IEC 60952 defines test procedures for the evaluation, comparison and qualification of batteries and states minimum environmental performance levels for airworthiness. Where specific tests are defined with no pass/fail requirement (to establish performance capability), the manufacturer’s declared values, from qualification testing, will be used to establish minimum requirements for ongoing maintenance of approval for that design of battery. To provide representative examples, this standard utilises voltage and current values based upon an aircraft electrical system nominally rated at 28 V d.c. Additionally, the nominal values for cell voltage are assumed to be 1,2 V per cell for nickel-cadmium batteries and 2,0 V per cell for lead-acid batteries. It is important to note that when using this standard to evaluate products designed to operate on an aircraft electrical system other than the nominal 28 V d.c., or whose chemical properties are such that the individual cell voltage differs from that stated above, test values need to be adjusted accordingly. The specific topics addressed in this part of 60952 serve to establish acceptable quality standards required to qualify a battery as airworthy and are divided into 2 classes (class I and II) as defined in Clause 3 of this standard. – Most of the requirements of this Part 1 state the minimum performance level for class I applications which are also mandatory for class II applications. – Subclauses 5.6 and 6.6 state 2 different levels of performance for class I and II applications. – Clause 7 states special requirements for class II applications only. In cases where a specific application demands testing and/or requirements exceeding those detailed in this standard the purchaser will detail said requirements in the product specification and the method of establishing compliance.

Aircraft batteries - Part 1: General test requirements and performance levels

BS EN 60952-3:2004 飞行器用蓄电池组.第3部分:产品规范及设计与性能的声明(DDP)

This part of IEC 60952 defines requirements for the product specification as well as procedures for a Declaration of Design and Performance (DDP) for nickel-cadmium and lead-acid aircraft batteries containing vented or valve-regulated cells or monoblocs. The batteries are used for both general purposes and specific aerospace applications. The specific topics addressed in this part serve to establish acceptable quality standards required to qualify a battery as airworthy and are divided into two class (class I and II) as defined in Clause 3 of IEC 60952-1. This part defines the above requirements and procedures for both class I and class II types. The design construction and test requirements should conform to the requirements specified in IEC 60952-1 and IEC 60952-2.

Aircraft batteries - Part 3: Product specification and declaration of design and performance (DDP)

BS EN 60952-2:2004 飞行器用蓄电池组.第2部分:设计和制造要求

This part of IEC 60952 defines the physical design, construction and material requirements for nickel-cadmium and lead-acid aircraft batteries containing vented or valve-regulated cells or monoblocs. The batteries are used for both general purposes and specific aerospace applications. The specific topics addressed in this part serve to establish acceptable quality standards required to qualify a battery as airworthy and are divided into two classes (class I and II) as defined in Clause 3 of IEC 60952-1. A preferred range of aircraft batteries is specified in Annex A, but this part of IEC 60952 may be used for other battery sizes, arrangements and ratings. For particular applications, other design requirements may be stipulated. These will be in addition to the requirements of this part and will be covered by specific documents.

Aircraft batteries - Part 2: Design and construction requirements

GJB/Z 219-2005 飞机/悬挂物电气连接系统应用手册

本手册向武器系统设计者提供了在当前的和未来的飞机和悬挂物中，实施GJB 1188A-1999规定的标准电气连接系统所必需的信息。这些信息包括但不限于： a)对GJB 1188A-1999规定的要求的详尽理解； b)对设计范畴内可能影响接口相容性问题的判定； c)对实施GJB 1188A-1999也许有用的设计技术、组成和设计实践的说明； d)供GJB 1188A-1999的用户在未来应用中使用的实践指南和相关原理。 本手册适用于作为在考虑和选择与飞机悬挂物挂点上包括标准接口能力、在运载悬挂物和任务悬挂物上提供通用电气接口有关的设计和方案的指南。

Application Handbook for Aircraft/store Electrical Interconnection System

NAVY MS3155 REV C VALID NOTICE 2-2005 符合尾部零件设计标准的电气连接件

MIL-DTL-22442/27C, dated 1 April 2000, has been reviewed and determined to be valid for use in acquisition

CONNECTOR, ELECTRIC, REAR ACCESSORY DESIGN STANDARD

AECMA PREN 2591-223-2005 航空航天系列.光电连接元件　试验方法.第223部分:同轴电缆连接器或者触点阻抗特性的测量

This standard specifies a method to determine the longitudinal dimensional stability of the outer sheath/jacket and secondary coating or buffer of a fibre optic cable or fibre. It shall be used together with EN 3745-100.

Aerospace series Elements of electrical and optical connection Test methods Part 223: Measurement of characteristic impedance of a coaxial connector or contact Edition P 1

AECMA PREN 2591-224-2005 航空航天系列.光电连接元件　试验方法.第224部分:射频泄露

This standard specifies a method of assessing the effects of a controlled salt laden atmosphere on optical connection elements and fibre optic couplers.

Aerospace series Elements of electrical and optical connection Test methods Part 224: RF leakage Edition P 1

AECMA PREN 2591-225-2005 航空航天系列.光电连接元件　试验方法.第225部分:耐射频高电位

This standard specifies the characteristics of elbow, 37°in titanium alloy intended for use in aircraft fluid system pipe lines.

Aerospace series Elements of electrical and optical connection Test methods Part 225: high potential withstanding voltage Edition P 1

AECMA PREN 2591-226-2005 航空航天系列.光电连接元件　试验方法.第226部分:电离化电压

This draft is now available for public comment and your views and technical comments on it muld be appreciated. Ifyou have no specific comments to make but fmd it generally acceptable it muld be helpfu! if you mould notify us accordingly Suggestions entailing revision of the text should indicate the preferred wording. Please quote the relevant clause number against any comment.

Aerospace series Elements of electrical and optical connection Test methods Part 226: Corona level Edition P 1

SAE AS85049/120-2005 4B类90?自锁紧应力消除电气连接器附件(MIL-DTL-5015弯曲 、MIL-DTL-26482 系列2、 AS81703 系列3和 MIL-DTL-83723 系列III 连接器)

CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, 90 DEGREES SELF-LOCKING, CATEGORY 4B (FOR MIL-DTL-5015 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS) FSC 5935;FIGURE 1 - DIMENSION AND CONFIGURATION;TABLE 1 - MATERIAL AND FINISH;

CONNECTOR ACCESSORIES, ELECTRICAL, STRAIN RELIEF, 90 DEGREES SELF-LOCKING, CATEGORY 4B (FOR MIL-DTL-5015 CRIMP, MIL-DTL-26482 SERIES 2, AS81703 SERIES 3, AND MIL-DTL-83723 SERIES III CONNECTORS) FSC 5935

SAE AMS-S-8802B-2005 高粘性整体燃料箱和燃料电池盒的耐热密封剂

This specification covers temperature resistant, two component synthetic rubber compounds of the polysulfide type for sealing and repairing integral fuel tanks and fuel cell cavities, for continuous service use from -65 to +250 degrees F (-54 to 121 degrees C).

Sealing Compound, Temperature Resistant, Integral Fuel Tanks and Fuel Cell Cavities, High Adhesion

SAE AS4851A-2005 绝缘电线的相对热时效和温度指数

This test method provides performance data on candidate insulation systems as a function of time and temperature. These data give engineering information on the wire insulation candidate relative to the performance of materials already in use with a backlog of experience. These tests expose candidate insulation systems to a wide range of temperatures for short and long periods of time, while measuring the degradation of its physical properties. For aerospace use, end-point proof tests include mandrel bend, water soak, and dielectric integrity. The thermal rating of an insulation system describes the quantitative relation of life of an insulation system to the temperature and time of exposure. The end of life is defined by the mechanical/electrical loss of integrity of the insulation system after exposure. A Temperature Index (TI) is then assigned based on temperatures and times recorded during the test. It should be noted that the Index is based upon the time at which 50% of the samples have failed. A related quantity is Relative Temperature Index (RTI) and is obtained when a candidate insulation system is simultaneously tested with a known insulation system using identical conditions (e.g., same temperatures, time intervals, and oven). RTI has been found to be more meaningful than TI since it is less affected by the variations in test conditions and procedures. Also included in this document is an extensive appendix to assist the user in performing and interpreting this test. Included in the appendix is an example which provides greater detail for those who have not previously run this test. This type of detail is not included in any of the referenced documents. This test method serves several purposes. Initial qualification of new aerospace wires to specifications for both commercial and military users may be established by using the TI and RTI. Also, it provides engineering information data for assigning operating or rating temperatures for a specific insulated wire. The high temperature test may be used to statistically compare the thermal performance data of a lot of wire with the original test data. The high temperature test is not recommended for use in continuing production quality control procedures until empirical evidence shows that the high temperature test or another analytical procedure, such as a thermogravemetric test, can accurately provide quality control testing information. This test method is primarily based on the degradation of the wire insulation, which tends to follow the Arrhenius relationship with respect to time and temperature. This test method, however, does not address, in and of itself, all mechanisms which may occur to degrade the insulation, nor does it imply that all degradation follow this relationship.

Relative Thermal Life and Temperature Index for Insulated Electric Wire

SAE ARP5637-2005 飞行器外部照明塑料透镜的设计和维修依据

The information in this document is intented to apply to commercial jet transport category airplanes that incorporate plastic (polycarbonate or acrylic) lenses on exterior light assemblies, or are being considered for such an application. Exterior lighting applications include position light assemblies, anticollision light asemblies, and landing light assemblies. However, much of the material provided herein is general in nature and is directly applicable to many aircraft categories including, but not limited to, helicopters, general aviation aircraft, and military aircraft.

Design and Maintenance Considerations For Aircraft Exterior Lighting Plastic Lenses

BS EN 3841-511:2005 航空航天系列.断路器.试验方法.组合试验:温度、高度和振动

This standard specifies a method for a combined test of temperature, altitude and vibration of circuit breakers. It shall be used together with EN 3841-100.

Aerospace series - Circuit breakers - Test methods - Combined test: temperature, altitude and vibration

BS EN 3841-510:2005 航空航天系列.断路器.试验方法.信号接线柱强度

This standard specifies a method of verifying the strength of signal contact terminals of circuit breakers. It shall be used together with EN 3841-100.

Aerospace series - Circuit breakers - Test methods - Strength of signal contact terminals