V16 热加工工艺 标准查询与下载

HB 459-2004 航空用结构钢焊条规范

本规范规定了结构钢焊条的要求、质量保证规定和交货准备等。 本规范适用于航空用结构钢焊条 HTJ-LHT]一Z、HT]一3、H丁] 一4、H丁] 一5和 HTJ 一6的生产及 检验。

Specification for coverd electrodes of structure steel for aviation

HB/Z 140-2004 航空用高温合金热处理工艺

本说明书规定了航空用高温合金管材、丝材、板金件、焊接组合件、棒材、锻件、盘形锻件、铸件及其半成品、成品的热处理工艺规范、设备控制、工艺控制、质量控制以及检验的有关要求。 　　本说明书作为航空工业部部标准，是指导部内工厂航空用高温合金及其制件热处理的主要技术文件

Heat treatment of superalloy for aviation

HB/Z 190-2004 聚酰胺1010注塑成型工艺

本规范规定了聚??010（简称PA1010）注射成型时的原料和设备要求、工艺程序及参数等内容。 　　本标准适用于聚??010制件的注射成型。

Injecting moulding technology for polyamide 1010 plastics

BS EN 14612:2003 焊接和相关工艺.金属焊接工艺的定义

This specification defines the basic requirements for the verification and approval of automatic machine wave soldering for use in spacecraft hardware. The process requirements for wave soldering of double-sided and multilayer boards are also defined.

Space product assurance - Verification and approval of automatic machine wave soldering

BS EN 14612:2004 航天产品保险.自动机械波焊的检定和验收

Space product assurance - Verification and approval of automatic machine wave soldering

NAVY MIL-PRF-2819 G-2004 热绝缘块

This specification establishes the requirements for thermal insulation block for use on machinery and equipment at surface temperatures up to the limits for the classes specified.

INSULATION BLOCK, THERMAL

QJ 3196-2004 焊前准备及焊后处理要求

Pre-weld preparation and post-weld treatment requirements

SAE AMS4243B-2003 UNS A87050经溶液热处理和沉淀的6.2Zn-2.3Cu-2.2Mg-0.12Zr(Alclad 7050-T76)铝合金铝包片材

This specification covers an aluminum alloy in the form of sheet. This sheet has been used typically for applications requiring a high level of mechanical properties and good resistance to exfoliation corrosion, but usage is not limited to such applications.

Aluminum Alloy, Alclad Sheet 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (Alclad 7050-T76) Solution Heat Treated and Overaged UNS A87050

SAE AMS4426A-2003 UNS M18410经溶液和沉淀热处理的镁合金5.1Y-3.0Re-0.70Zr(WE54- T6)砂铸件

This specification covers a magnesium alloy in the form of sand castings. These castings have been used typically for parts requiring high yield strength up to 570 degrees F (299 degrees C) and excellent corrosion resistance, but usage is not limited to such applications.

Castings, Sand, Magnesium Alloy 5.1Y - 3.0Re - 0.70Zr (WE54 - T6) Solution and Precipitation Heat Treated UNS M18410

SAE AMS4293-2003 经溶液热处理,压力释放,校直和沉淀的7.9Zn-1.6Cu-2.2Mg-0.16Cr(7249-T76511)铝合金挤压件

This specification covers an aluminum alloy procured in the form of extruded bars, rods, wire, profiles (shapes) and tubing. These extrusions have been used typically for structural applications requiring a combination of high tensile strength and good corrosion resistance where intergranular attack is unacceptable, but usage is not limited to such applications.

Aluminum Alloy Extrusions 7.9Zn-1.6Cu-2.2Mg-0.16Cr (7249-T76511) Solution Heat Treated, Stress-Relieved, Straightened, and Overaged

SAE AMS4205C-2003 UNS 97010 固溶处理以及消除应力和沉淀热处理的6.2Zn-1.8Cu-2.4Mg-0.13Zr(7010-T73651)或(7010-T7451)铝合金板材

This specification covers an aluminum alloy in the form of plate. This plate has been used typically for parts requiring higher tensile strength than SAE AMS 4203 (7010-T7351) and good resistance to stress-corrosion cracking, exfoliation corrosion, and fracture toughness, but usage is not limited to such applications.

Aluminum Alloy, Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T73651) or (7010-T7451) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated UNS 97010

SAE AMS4331-2003 经溶液热处理,压力释放和沉淀热处理的7.8Zn-2.6Mg-2.0Cu-0.10Zr -(7068-T6511)铝合金挤压件

This specification covers an aluminum alloy in the form of extruded bars, rods, shapes (profiles), and tubing. These extrusions have been used typically for structural parts requiring a combination of high tensile strength and moderate fatigue strength, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy Extrusions 7.8Zn - 2.6Mg - 2.0Cu - 0.10Zr - (7068-T6511) Solution Heat Treated, Stress Relieved, and Precipitation Heat Treated

HB/Z 346-2002 熔模铸造钢铸件补焊工艺及检验

本指导性技术文件规定了对结构钢 ，不锈钢及耐热钢熔模铸造钢铸件缺陷补焊的补焊铸件确定、补 焊前准备、补焊、补焊后的清理、补焊后的热处理、补焊质量检验质量控制及技术安全。 本指导性技术文件适用于航空产品熔模铸造钢铸件铸造缺陷及其在机械加工过程中出现的缺陷采 用手工钨极氨弧焊和焊条电弧焊进行的补焊。

Process and inspection of repair welding for investment castings of stssl

HB/Z 345-2002 铝合金铸件补焊工艺及检验

本指导性技术文件规定了对铝合金铸件在铸造及机械加工过程中产生的缺陷进行补焊时补焊铸件 的确定、补焊前的准备、补焊前的预热.补焊 .铸件补焊后的清理、铸件补焊后的热处理，铸件补焊后的检 验和质量控制。 本指导性技术文件适用于采用手工金极氨弧焊和氧- 乙焊进行航空用铝合金链件缺陷的补焊。

Process and inspection of repair welding for aluminium alloy castings

SAE AMS2426D-2002 镉真空镀层

This specification covers the engineering requirements for vacuum deposition of cadmium and the properties of the deposit. This process has been used typically to provide a corrosion resistant coating for high strength ferrous parts operating at not higher than 450 degrees F (232 degrees C) and requiring freedom from hydrogen embrittlement, but usage is not limited to such applications. Deposits are "line-of-sight" and may not be applicable to some internal surfaces.

Coating, Cadmium Vacuum Deposition

DIN EN 4250:2002 航空航天系列.镍基合金NI-B41001 (NiSr19Si7B).硬钎焊填充金属.非晶态箔

The document specifies the requirements relating to filler metal for brazing, amorphous foil in nickel base alloy NI-B41001 for aerospace applications.#,,#

Aerospace series - Nickel base alloy NI-B41001 (NiSr19Si7B) - Filler metal for brazing, amorphous foil; German version EN 4250:2001

DIN EN 4085:2002 航空航天系列.镍基合金NI-B40002 (NiSi4B2).硬钎焊填充金属.非晶态箔

The document specifies requirements relating to Nickel base alloy NI-B40002 (NiSi4B2) filler metal for brazing, amorphous foil, for aerospace applications.

Aerospace series - Nickel base alloy NI-B40002 (NiSi4B2) - Filler metal for brazing; Amorphous foil; German version EN 4085:2001

DIN EN 4059:2002 航空航天系列.钢焊接用焊条和焊丝.直径0.5-5.0mm.尺寸

The document specifies the dimensions and tolerances of filler rods and filler wires for welding, in steel, diameter 0,5 mm D 5,0 mm for aerospace applications.

Aerospace series - Filler rods and filler wires for welding in steel - Diameter 0,5 mm D 5,0 mm; Dimensions; German and English version EN 4059:2001

QJ 3131-2001 热处理常用槽液技术条件

Specification for the pot bath and quenching medium for heat treatment

BS EN 3689:2001 航空航天系列.焊接管用钛合金制T环形填充物.28000kPa公称压力

This standard specifies the characteristics for T-ring fillers in titanium alloy for welding pipes, for aerospace applications. Nominal pressure: up to 28 000 kPa

Aerospace series - T-ring fillers in titanium alloy for welding pipes - 28000 kPa nominal pressure