GB/T 43376-2023 航空航天 可熱處理強(qiáng)化不銹鋼零件表面清理

Surface cleaning of aerospace heat-treatable stainless steel parts

GB/T 38825-2020 民用飛機(jī)復(fù)合材料制件鉚接要求

本標(biāo)準(zhǔn)規(guī)定了復(fù)合材料制件錦接的一般要求`.工藝控制和質(zhì)量控制。本標(biāo)準(zhǔn)適用于民用飛機(jī)復(fù)合材料層壓板制件的實(shí)心錦釘錦接和抽芯鉀釘鉀接。

Requirements of riveting connection in civil aircraft of composite parts

GB/T 38929-2020 民用飛機(jī)蒙皮鏡像銑削工藝通用要求

本標(biāo)準(zhǔn)規(guī)定了蒙皮類(lèi)零件鏡像銑削的一般要求、特征定義與分類(lèi)、編程方法.工藝流程.質(zhì)量控制。本標(biāo)準(zhǔn)適用于民用飛機(jī)金屬蒙皮零件的鏡像銑削加工,其他產(chǎn)品可參照?qǐng)?zhí)行。

General requirements of mirror milling process for civil aircraft skin parts

QJ 1722A-2014 線(xiàn)扎制作工藝技術(shù)要求

本標(biāo)準(zhǔn)規(guī)定了航天電子電氣產(chǎn)品線(xiàn)扎制作的技術(shù)要求、工藝方法和檢驗(yàn)要求。 本標(biāo)準(zhǔn)適用于航天電子電氣產(chǎn)品線(xiàn)扎的制作和檢驗(yàn)。其他產(chǎn)品亦可參照?qǐng)?zhí)行。

Technical requirement for binding manufacturing

HB/Z 20019-2014 鈦合金鉚釘鉚接工藝

本指導(dǎo)性技術(shù)文件規(guī)定了鈦合金鉚釘鉚接工藝的一般要求、施工、工藝試驗(yàn)、人員和技術(shù)安全等。 本指導(dǎo)性技術(shù)文件適用于金屬結(jié)構(gòu)、復(fù)合材料結(jié)構(gòu)及混合夾層結(jié)構(gòu)的鈦合金實(shí)心鉚釘?shù)你T接。

Process for riveting for titanium alloy rivet

HB/Z 20025-2014 柔性多點(diǎn)模具蒙皮拉形工藝

本指導(dǎo)性技術(shù)文件規(guī)定了柔性多點(diǎn)模具蒙皮拉形的人員、環(huán)境、材料、設(shè)備與工裝、柔性多點(diǎn)模具的工藝性鑒定、工藝參數(shù)選擇與確定、工藝參數(shù)的重新確定、工藝控制、質(zhì)量控制以及安全要求等。本指導(dǎo)性技術(shù)文件適用于壁厚不大于5mm的鋁合金、鋁鋰合金常溫柔性多點(diǎn)模具蒙皮拉形。其他材料或厚度的板材常溫柔性多點(diǎn)模具蒙皮拉形可參照本指導(dǎo)性技術(shù)文件。采用上壓模式的常溫柔性多點(diǎn)模具蒙皮拉形也可參照本指導(dǎo)性技術(shù)文件。

Process of skin stretch forming with flexible multi-point die

HB/Z 408-2013 鋁合金小彎曲半徑管的內(nèi)壓推彎成形工藝

Internal pressure push-bending forming process of aluminum alloy tube with small bending radius

HB/Z 412-2013 鈦合金零件化學(xué)銑切工藝

Chemical Milling Technology of Titanium Alloy Parts

HB/Z 406-2013 鋁合金零件噴丸成形工藝

Shot peening process of aluminum alloy parts

HB/Z 407.2-2013 鋁合金零件壓彎成形與校形工藝 第2部分：型材類(lèi)零件

Aluminum Alloy Parts Press-bending and Shaping Technology Part 2: Profile Parts

HB 8406-2013 飛機(jī)裝配工裝設(shè)計(jì)要求

Aircraft Assembly Tooling Design Requirements

SAE AMS2470N-2013 鉻酸法鋁合金的陽(yáng)極處理

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

Anodic Treatment of Aluminum Alloys, Chromic Acid Process

SAE AMS2405D-2013 無(wú)電極低磷鍍鎳

Electroless Nickel Plating Low Phosphorus

SAE AMS2580A-2013 超音速驅(qū)動(dòng)的噴丸加工

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

HB/Z 407.1-2013 鋁合金零件壓彎成形與校形工藝 第1部分：壁板類(lèi)零件

Aluminum Alloy Parts Press-bending and Shaping Technology Part 1: Panel Parts

SAE AMS2460A-2013 鍍鉻

This specification covers the requirements for electrodeposited chromium plating.

Plating, Chromium

SAE AMS2401J-2013 低氫含量沉積鍍鎘

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

SAE AMS2400X-2013 電鍍鎘

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

SAE AS107E-2013 表面拋光(RMS)

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)

SAE AMS2451/9B-2012 低氫脆性鋅-鎳電鍍刷

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