V18 冷加工工艺 标准查询与下载

HB/Z 5071-2004 化学镀镍工艺及质量检验

本指导性技术文件制订了钢铁零件、铜及铜合金零件化学镀镍的通用工艺方法。 　　化学镀镍适用于形状复杂的用镀铬方法不能满足要求的零件，也适用于防腐蚀及有耐磨要求的啮合零件以及导磁要求好的零件。

Process and quality inspection for electroless nickel plating

HB/Z 5005-2004 铝合金零、部件涂漆工艺

本技术文件规定了H06-2锌黄环氧酯底漆、H06-2锌黄环氧酯底漆—H04-2各色环氧硝基磁漆和H06-2锌黄环氧酯底漆—H04-10各色环氧硝基无光磁漆三种涂层和涂层系统，作为飞机内部一般铝合金零、部件涂漆的基本规则。

Painting process for aluminium alloys components

AECMA PREN 4101-2003 航空航天系列铝合金AL-2024-T4薄板和带材改良的拉升成型能力0,4mm小于或等于a小于或等于6mm

The text of this standard , whick exists in thress equivalent versions has been drawn up under the responsibility of AECMA and has been circulated to Official Services. Any reservations expressed by Official Services and not resolved in this issue, have been incorporated in the history sheet which has accompanied this prEN to CEN.

Aerospace Series Aluminium Alloy AL-P2024-T4 Sheet and Strip with Improved Stretch Forming Capability 0,4 mm Less Than or Equal to a Less Than or Equal to 6 mm Edition P 2

AECMA PREN 4100-2003 航空航天系列铝合金 AL-P2219-T62　薄板和带材0,5mm小于或等于a小于或等于6mm

This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-2.

Aerospace Series Aluminium Alloy AL-P2219-T6 or T62 Sheet and Strip 0,5 mm Less Than or Equal to a Less Than or Equal to 6 mm Edition P 2

AECMA PREN 4099-2003 航空航天系列AL-P2219-T6 或T62覆层薄板和带材0,5mm小于或等于a小于或等于6mm

This standard specifies the required characteristics for lamp, code 682, used on-board aircraft. It shall be used together with EN 2756.

Aerospace Series Aluminium Alloy AL-P2219-T6 or T62 Clad Sheet and Strip 0,5 mm Less Than or Equal to a Less Than or Equal to 6 mm Edition P 2

AECMA PREN 4102-2003 航空航天系列.铝合金AL-P2219-T81金属薄片和0,5mm小于或等于a小于或等于6mm .P2版

This standard specifies a method for testing the resistance of an optical cable to scrape abrasion.

Aerospace Series Aluminium Alloy AL-P2219-T81 Clad Sheet and Strip 0,5 mm Less Than or Equal to a Less Than or Equal to 6 mm Edition P 2

AECMA PREN 2732-2003 航空和航天系列镁合金MG-C46001 T6冷硬铸造

This standard is initially published on green paper for the needs of AECMA-Members (Association Europeenne des Constructeurs de Matdriel Adrospatial). it has been technically approved by the experts of the concerned AECMA Commission following comment by the manufacturers of the Member countries.

Aerospace Series Magnesium Alloy MG-C46001 T6 Chill Castings Issue P 2

AECMA PREN 3342-2003 航空航天系列.铝合金AL-P6061-T4 或 T42冷拉或挤压棒和型材a或直径D小于或等于150 mm

This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-2.

Aerospace Series Aluminium Alloy AL-P6061-T4 or T42 Drawn or Extruded Bar and Section a or D Less Than or Equal to 150 mm Edition P 3

SAE AMS2485J-2002 黑色氧化物覆层

This specification covers the engineering requirements for producing black oxide coatings on parts and the properties of such coatings. This coating has been used typically to improve the anti-chafing and anti-friction properties of carbon and low-alloy steel parts, particularly sliding or bearing surfaces, by providing a finish coating which will retain an oil film, but usage is not limited to such applications.

Coating, Black Oxide

SAE AMS2422E-2002 (R)镀金

1.1 Form:This specification covers the engineering requirements for electrodeposition of gold and theproperties of the deposit.1.2 Application:This plating has been used typically to improve the solderability, electrical conductivity, corrosionresistance, performance, and appearance of electronic and electrical parts, but usage is not limited to such applications.1.3 Safety - Hazardous Materials:While the materials, methods, applications, and processes described or referenced in thisspecification may involve the use of hazardous materials, this specification does not address thehazards which may be involved in such use. It is the sole responsibility of the user to ensurefamiliarity with the safe and proper use of any hazardous materials and to take necessaryprecautionary measures to ensure the health and safety of all personnel involved.

(R) Plating, Gold

SAE AS7117-2002 国家航空航天和国防合同方授信项目喷丸,喷丸成型和玻璃丸喷丸要求

This Aerospace Standard (AS) establishes the requirements for suppliers of Shot Peening Services to be accredited by the National Aerospace and Defense Contractors Accreditation Program (NADCAP). NADCAP accreditation is granted in accordance with SAE AS7003 after demonstration of compliance with the requirements herein. The requirements may be supplemented by additional requirements specified by the NADCAP Nonconventional Machining and Surface Enhancement (NMSE) Task Group. Using the corresponding Audit Criteria (PRI AC7117) will ensure that accredited Shot Peening suppliers meet all of the requirements in this standard and all applicable supplementary standards. The purpose of this audit program is to assess a suppliers ability to consistently provide a product or service that conforms to the technical specifications and customer requirements. The corresponding audit criteria are also structured to obtain information relevant to management practices and processes that directly or indirectly affect the product or service. This information will be used in the determination of accreditation status and may be used by the supplier to guide improvements in the product or service and the associated processes.

NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM REQUIREMENTS FOR SHOT PEENING, PEEN FORMING, GLASS BEAD PEENING

AECMA PREN 4103-2001 航空航天系列.铜焊硼化物.P2版镍合金NI-B40002填充金属取代.P1版,1994年1月 被取代EN 4103

This standard specifies the required characteristics for lamp, code 31 1, used on-board aircraft. It shall be used together with EN 2756.

Aerospace Series Nickel Base Alloy NI-B40002 Filler Metal for Brazing Borided Foil Edition P2; Supersedes Edtion P 1: January 1994

SAE AMS2435G-2001 碳化钨-钴涂覆爆轰处理的涂层

This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of June, 2007. It is recommended, therefore, that this specification not be specified for new designs. "NONCURRENT" refers to those specifications which have previously been widely used and which may be required on some existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. This specification covers the engineering requirements for applying tungsten carbide/cobalt coatings to metal parts by the detonation process and the properties of such coatings. This coating has been used typically to provide a hard, wear resistant surface on metal parts which do not operate in service higher than 1000 °F (538 °C) but usage is not limited to such applications. These coatings are not recommended for surfaces with deep vee-shaped grooves, blind cavities, narrow holes or sharp corners, or where deformation of the base metal may be expected. Higher cobalt content provides increased ductility for applications where impact or fretting wear is involved.

Coating, Tungsten Carbide-Cobalt Coating Detonation Process

SAE ARP2654-2001 超声测厚去毛刺

To provide general instructions for accomplishing ultrasonic thickness measurements. Measurements can be made from one side of a material when access to the opposite side is restricted. This Recommended Practice is intended for, but not limited to use at maintenance and overhaul facilities to inspect aerospace structures and hardware for material loss or remaining thickness after rework or fabrication processes. Due to the number of variables which can affect the reliability of ultrasonic thickness measurements, it is only recommended for use when mechanical methods of measurement are not practical.

Ultrasonic Thickness Testing

SAE ARP1925B-2001 自动刷式去毛刺

This recommended practice establishes procedures for the application of long string abrasive fibers to machined aircraft structures for the purpose of removing burrs produced during the machining operations. This procedure is applicable to aluminum, titanium, and steel, but usage is not limited to such applications. The process is applicable to the removal of light machining burrs but will not remove burrs that have been extruded by dull cutting tools. The process described responds to an automated brush deburring method that would lend itself to machine automation and robotic applications and be applicable to a wide range of part geometry variables.

Automated Brush Deburring

ARINC 628P7 ITEM 3.0-2001 飞机冷却系统

Airplane Cooling Systems

Airplane Cooling Systems

ARINC 628P7 ITEM 2.0-2001 IFE设备冷却等级

Classes of IFE Equipment Cooling

Classes of IFE Equipment Cooling

AECMA PREN 2726-2001 航空和航天系列铝合金AL-C42201 T6冷硬铸造a小于或等于20mm

This specification defines the process applicable to the lubrication of threaded bolts, nuts, lock bolt pins and collars with cetyl alcohol. It defines the product application methods and the relevant quality assurance requirements for the lubrication of the commonly used fastener materials: Aluminium alloys, alloy steels, stainless steels, titanium alloys and nickel base alloys.

Aerospace Series Aluminium Alloy AL-C42201 T6 Sand Casting a Less Than or Equal to 20 mm Issue P 2

SAE AMS3146-2000 涂覆,内部飞行器舱低热和烟雾释放

This specification covers interior aircraft cabin coatings, which when tested under specified conditions exhibit low heat release and smoke release properties.

Coating, Interior Aircraft Cabin Low Heat and Smoke Release

NAVY MIL-HDBK-1133-1999 用于船的冷铁架和用于岸上设备的能量预算和水消耗

ESTIMATING ENERGY AND WATER CONSUMPTION FOR SHORE FACILITIES AND COLD IRON SUPPORT FOR SHIPS [Superseded: NAVY NAV MO-303]

ESTIMATING ENERGY AND WATER CONSUMPTION FOR SHORE FACILITIES AND COLD IRON SUPPORT FOR SHIPS [Superseded: NAVY NAV MO-303]