V18 冷加工工艺 标准查询与下载

SAE AMS2406L-2007 镀硬化沉积铬

This specification covers the engineering requirements for electrodeposited hard chromium plate and processing requirements. This plating has been used typically on parts for increasing abrasion resistance, increasing tool and die life, maintaining accuracy of gages, and reconditioning worn or undersized parts, but usage is not limited to such applications.

Plating, Chromium Hard Deposit

SAE AMS2451/9A-2007 低氢脆化锌镍电镀刷

This specification covers the engineering requirements and processes for brush plating of zinc-nickel by electrodeposition. This process has been used typically to improve corrosion resistance of steel parts operating under 500 °F (260 °C) asplated or under 250 °F (121 °C) when chromate treated, to repair zinc-nickel deposits and to repair damaged or worn parts, but usage is not limited to such applications.

Plating, Brush, Zinc-Nickel Low Hydrogen Embrittlement

SAE AMS2470M-2007 铬酸工艺对铝合金的阳极处理

This specification establishes the for anodic coatings on aluminum alloys. This process has been used typically to increase corrosion resistance and to provide surfaces which will promote adherence of paint and other organic finishes, and has been found useful for assemblies which have faying surfaces and/or which may trap electrolyte, but usage is not limited to such applications. This process is primarily applicable to aluminum and aluminum alloy parts which have nominal copper content not greater than 5% by weight or total nominal alloy content not greater than 7.5% by weight, AMS 2471 being recommended for parts having higher alloy content. Coating may be dyed if specified, but AMS 2472 is recommended where a colored finish is required.

Anodic Treatment of Aluminum Alloys, Chromic Acid Process

SAE AMS2412H-2007 银铜电镀后低温烘干

This specification covers the engineering requirements for silver deposited on metal parts with a copper strike between the basis metal and the silver deposit. This process has been used typically to provide a bearing surface and to prevent galling or seizing of metal surfaces of parts made of materials where a high baking temperature may be detrimental to the properties of the basic material.

Plating, Silver Copper Strike, Low Bake

SAE AMS2526C-2007 用浸渍薄润滑油膜的二硫化钼涂层

This specification covers a coating consisting of finely-powdered molybdenum disulfide in a heat-resistant inorganic binder applied to parts.

Molybdenum Disulfide Coating, Thin Lubricating Film Impingement Applied

SAE AMS2401H-2007 低氢含量沉积物的镀镉

This specification covers the engineering requirements for cadmium deposited on ferrous metals. This process has been used typically to provide corrosion resistance to steel parts heat treated to tensile strength of 180 ksi (1240 MPa) and higher and used at temperatures not higher than 450 °F (232 °C).

Plating, Cadmium Low Hydrogen Content Deposit

NAVY MIL-PRF-16173 E INT AMD 1-2006 冷应用稀释溶剂防腐化合物 取代NAVY MIL-PRF-16173 E INT AMD 1, NAVY MIL-PRF-16173 E, NAVY MIL-C-16173 D (2), NAVY MIL-C-16173 D (1), NAVY MIL-C-16173 D, NAVY MIL-C-16173 C, NAVY MIL-C-16173 B, NAV

This specification covers solvent-dispersed corrosion preventive compounds that deposit thin, easily removable films after evaporation of solvent.

CORROSION PREVENTIVE COMPOUND, SOLVENT CUTBACK, COLD-APPLICATION

SAE AMS2451/2A-2006 硬沉积低应力镍镀涂工艺

This specification covers the engineering requirements and process controls for brush plating of hard, low stress nickel by electrodeposition. This process has been used typically to provide wear resistance and to repair damaged, worn, or mismachined parts in applications requiring hardness, fatigue resistance, and service at temperatures up to 450°F (232°C) but usage is not limited to such applications.

Plating, Brush, Nickel Low Stress, Hard Deposit [Superseded: SAE AMS 2439A, SAE AMS 2439, SAE AMS 2439]

SAE AMS2451/8A-2006 镀层和涂刷的非氰化物银一般用途

This specification covers the engineering requirements and process for brush plating of non-cyanide silver by electrodeposition. It is used, in conjunction with AMS 2451, for silver deposits. This process has been used typically to provide low electrical contact resistance, prevent galling or seizing of surfaces of parts, and corrosion protection, but usage is not limited to such applications.

Plating, Brush, Non-Cyanide Silver General Purpose

SAE AMS2451/7A-2006 中等硬度沉积低应力镍镀涂工艺

This specification covers the engineering requirements and process for brush plating of medium-hardness, low stress nickel by electrodeposition. It should be used, in conjunction with AMS 2451, for medium-hardness, low stress nickel deposits. This process has been used typically to provide wear resistance and to repair damaged, worn, or mismachined parts in applications requiring hardness, fatigue resistance, and service temperatures up to 450 degrees F (232 degrees C), but usage is not limited to such applications.

Plating, Brush, Nickel Low Stress, Medium-Hardness Deposit

SAE AMS2451B-2006 镀层和涂刷一般要求

This specification and its supplementary detail specifications establish the requirements and process controls for electrodeposition of metals by brush plating. This process has been used typically to improve surface properties such as corrosion resistance, wear resistance, and brazeability or to repair damaged, worn, or mismachined parts, but usage is not limited to such applications. This process is particularly useful for plating localized areas on-site, especially on large parts or assemblies, and for minimizing masking.

Plating, Brush General Requirements

SAE AMS2451/5A-2006 硬化沉积三价铬镀涂工艺

This specification covers the engineering requirements and process controls for selective plating of hard chromium by electrodeposition. It should be used, in conjunction with AMS 2451, for cosmetic touch-up and for wear-resistant chromium deposits. This process has been used typically to provide a corrosion-resistant deposit with excellent wear resistance and to repair damaged, worn, or mismachined parts but usage is not limited to such applications.

Plating, Brush, Chromium Hard Deposit, Trivalent

SAE AMS2451/6A-2006 铜镀涂工艺的一般要求

This specification establishes the engineering requirements and process controls for brush plating of copper by electrodeposition. It should be used, in conjunction with AMS 2451, for general purpose copper deposits. This process is used typically to repair damaged, worn, or mismachined parts and as a stop-off in carburizing and nitriding but usage is not limited to such applications.

Plating, Brush, Copper General Purpose

HB 7786-2005 零件化学铣切精度和表面粗糙度的一般要求

本标准规定了零件化学铣切（以下简称“化铣”）精度和表面粗糙度的一般要求。 本标准适用于航空产品铝合金（含铝锂合金）、钛合金零件的化铣。

General requirements for precision and surface roughness of chemically milled parts

HB 7775-2005 复合材料制件工装建模要求

本标准规定了复合材料制件工装建模的通用要求。 本标准适用于基于CATIA软件进行复合材料制件专用工装的建模，基于UG等其它软件进行复合材料制件工装建模时可参考使用。

Modeling requirements of tooling for composite parts

HB 5067.1-2005 镀覆工艺氢脆试验 第1部分：机械方法

本部分规定了镀覆工艺氢脆试验机械方法的试验原理、试验设备、试样、试验步骤和结果评定。 本部分适用于镀覆工艺氢脆倾向和抗拉强度大于1050MPa 的钢制零件镀覆产品氢脆性能的评定，并用于镀覆工艺氢脆向及镀覆产品氢脆性能的仲裁鉴定。

Test methods for hydrogen embrittlement evaluation of plating processes--Part 1: Methanical method

HB 5067.2-2005 镀覆工艺氢脆试验 第2部分：测氢仪方法

本部分规定了测氢仪试验方法的试验原理、试验要求、试验步骤、试验结果的计算和试验结果的评定等。 本部分适用于松孔镀镉（低氢脆镀镉）、电镀镉-钛溶液氢脆倾向及其电镀产品氢脆性能的快速评定、不作为仲裁结果。

Test methods for hydrogen embrittlement evaluation of plating processes--Part 2: Hydrogen detection instrument method

HB 7787-2005 插齿退刀槽尺寸

本标准规定了插齿退刀槽的型式、尺寸和技术要求。 本标准适用于渐开线圆柱齿轮和渐开线花键。

Dimensions of slitting clearance groove

HB/Z 223.22-2005 飞机装配工艺 高抗剪铆钉铆接

本部分规定了使用高抗剪铆钉铆接的工艺过程、技术要求、工艺参数、铆接质量检查和排除故障方法以及安全要求。 本标准适用于飞机装配时的高抗剪铆钉铆接。

Aircraft assembling technology Riveting for high shearing strength rivets

BS X 38:2005 航空航天用热养护着色图.规范

This British Standard specifies requirements for the materials and performance of two types of heat curing paint for aerospace applications up to 220 ℃. Type A materials are intended for use either as a sealer/primer coat for magnesium alloy, pre-treated to BS M 93, or for ferrous and non-ferrous substrates as a primer coat, containing chromate pigment, which may be over-coated with type B if required. Type B materials are intended as a finish over type A. The heat curing paint is intended to give protection against corrosion and resistance to aircraft fluids. Information on application for type approval is provided in Annex A.

Heat curing paint scheme for aerospace purposes - Specification