V18 冷加工工艺 标准查询与下载
共找到 335 条与 冷加工工艺 相关的标准，共 23 页
Surface cleaning of aerospace heat-treatable stainless steel parts
- ICS
- CCS
- V18
- 发布
- 2023-11-27
- 实施
- 2024-03-01
本标准规定了复合材料制件锦接的一般要求`.工艺控制和质量控制。本标准适用于民用飞机复合材料层压板制件的实心锦钉锦接和抽芯钾钉钾接。
Requirements of riveting connection in civil aircraft of composite parts
- ICS
- 49.040
- CCS
- V18
- 发布
- 2020-06-02
- 实施
- 2021-01-01 00:00:00.0
本标准规定了蒙皮类零件镜像铣削的一般要求、特征定义与分类、编程方法.工艺流程.质量控制。本标准适用于民用飞机金属蒙皮零件的镜像铣削加工,其他产品可参照执行。
General requirements of mirror milling process for civil aircraft skin parts
- ICS
- 49.040
- CCS
- V18
- 发布
- 2020-06-02
- 实施
- 2021-01-01 00:00:00.0
本标准规定了航天电子电气产品线扎制作的技术要求、工艺方法和检验要求。 本标准适用于航天电子电气产品线扎的制作和检验。其他产品亦可参照执行。
Technical requirement for binding manufacturing
- ICS
- CCS
- V18
- 发布
- 2014-11-20
- 实施
- 2015-02-20
本指导性技术文件规定了钛合金铆钉铆接工艺的一般要求、施工、工艺试验、人员和技术安全等。 本指导性技术文件适用于金属结构、复合材料结构及混合夹层结构的钛合金实心铆钉的铆接。
Process for riveting for titanium alloy rivet
- ICS
- CCS
- V18
- 发布
- 2014-11-17
- 实施
- 2015-02-01
本指导性技术文件规定了柔性多点模具蒙皮拉形的人员、环境、材料、设备与工装、柔性多点模具的工艺性鉴定、工艺参数选择与确定、工艺参数的重新确定、工艺控制、质量控制以及安全要求等。本指导性技术文件适用于壁厚不大于5mm的铝合金、铝锂合金常温柔性多点模具蒙皮拉形。其他材料或厚度的板材常温柔性多点模具蒙皮拉形可参照本指导性技术文件。采用上压模式的常温柔性多点模具蒙皮拉形也可参照本指导性技术文件。
Process of skin stretch forming with flexible multi-point die
- ICS
- CCS
- V18
- 发布
- 2014-11-17
- 实施
- 2015-02-01
Internal pressure push-bending forming process of aluminum alloy tube with small bending radius
- ICS
- CCS
- V18
- 发布
- 2013-09-01
- 实施
- 2013-09-01
Chemical Milling Technology of Titanium Alloy Parts
- ICS
- CCS
- V18
- 发布
- 2013-09-01
- 实施
- 2013-09-01
Shot peening process of aluminum alloy parts
- ICS
- CCS
- V18
- 发布
- 2013-09-01
- 实施
- 2013-09-01
Aluminum Alloy Parts Press-bending and Shaping Technology Part 2: Profile Parts
- ICS
- CCS
- V18
- 发布
- 2013-09-01
- 实施
- 2013-09-01
Aircraft Assembly Tooling Design Requirements
- ICS
- CCS
- V18
- 发布
- 2013-09-01
- 实施
- 2013-09-01
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
Anodic Treatment of Aluminum Alloys, Chromic Acid Process
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-07-09
- 实施
Electroless Nickel Plating Low Phosphorus
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-06-21
- 实施
This specification covers the requirements for inducing compressive residual stresses on the surface of metal parts using ultrasonically activated shot peening. Ultrasonically activated shot peening is typically used to induce compressive residual stresses on the surface layer of metallic parts to a depth up to 0.040 inch (1 mm). The shape and depth of the compressive residual stress distribution depend on the properties of the part and the ultrasonically activated shot peening process parameters. The residual stresses produced increase fatigue performance, resistance to stress-corrosion cracking, corrosion fatigue, and fretting fatigue, but its usage is no
Shot Peening, Ultrasonically Activated
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-06-11
- 实施
Aluminum Alloy Parts Press-bending and Shaping Technology Part 1: Panel Parts
- ICS
- CCS
- V18
- 发布
- 2013-04-25
- 实施
- 2013-09-01
This specification covers the requirements for electrodeposited chromium plating.
Plating, Chromium
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-03-12
- 实施
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), but usage is not limited to such applications.
Plating, Cadmium, Low Hydrogen Content Deposit
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-02-15
- 实施
This specification covers the requirements for electrodeposited cadmium on metal parts. This process has been used typically to provide corrosion resistance to metal parts, but usage is not limited to such applications.
Plating, Cadmium
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-02-11
- 实施
This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This standard provides a method for the application of surface finish control primarily to aircraft engine and propeller parts. Recommendations for a Surface Roughness Standard are contained in A.S.A. publication B46 and this S.A.E. Aeronautical Standard contains a summary of information therein plus other information which has been compiled from current manufacturing practice.
Surface Finish (RMS)
- ICS
- 49.040;49.050
- CCS
- V18
- 发布
- 2013-01-04
- 实施
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
- ICS
- 49.040
- CCS
- V18
- 发布
- 2012-09-20
- 实施
