V16 热加工工艺 标准查询与下载

BS EN 3688:2001 航空航天系列.焊接管用钛合金制T环形填充物.14000kPa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 14 000 kPa

Aerospace series - T-ring fillers in titanium alloy for welded pipes - 14000 kPa nominal pressure

BS EN 3893:2001 航空航天系列.钛合金TI-W19001.焊接用填充金属

This standard specifies the requirements relating to: Titanium alloy TI-W 19001 Filler metal for welding for aerospace applications.

Aerospace series - Titanium alloy TI-W19001 - Filler metal for welding

BS EN 4104:2001 航空航天系列.NI-B40002镍基合金.硬钎焊用填充金属.粉末或糊料

This standard specifies the requirements relating to: Nickel base alloy NI-B40002 Filler metal for brazing Powder or paste for aerospace applications.

Aerospace series - Nickel base alloy NI-B40002 - Filler metal for brazing - Powder or paste

SAE AMS2759/7A-2001 渗碳级钢部件的渗碳和热处理

This specification, in conjunction with the general requirements for steel heat treatment covered in AMS 2759, establishes the requirements and procedures for three classes of gas, vacuum and liquid carburizing and related heat treatment of parts fabricated from carburizing grade steels. It does not cover pack carburizing.

Carburizing and Heat Treatment of Carburizing Grade Steel Parts

SAE AMS4140H-2001 UNS A92018 固溶及沉淀热处理的4.0Cu-2.0Ni-0.68Mg(2018-T61)铝合金型锻

This specification covers an aluminum alloy in the form of die forgings and forging stock. This product has been used typically for parts for aircraft engines, but usage is not limited to such applications. Certain design and processing procedures may cause these forgings to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

Aluminum Alloy Die Forgings 4.0Cu - 2.0Ni - 0.68Mg (2018-T61) Solution and Precipitation Heat Treated UNS A92018

SAE AMS4232A-2001 UNS A92090经溶液热处理以及冷却和沉淀热处理的2.7Cu-2.2Li-0.12Zr(2090-T86)铝合金挤压件

This specification covers an aluminum alloy in the form of extruded bars, rods, and shapes. These extrusions have been used typically for parts in structural applications requiring strength similar to 7050-T6 with good exfoliation resistance and with a lower density of approximately 7.8%, but usage is not limited to such applications.

Aluminum Alloy Extrusions 2.7Cu - 2.2Li - 0.12Zr (2090-T86) Solution Heat Treated, Cold Worked, and Precipitation Heat Treated UNS A92090

SAE AMS2672F-2001 钎焊,铝火焰或熔炉

1.1 Purpose:This specification covers the engineering requirements for producing brazed joints on aluminum and aluminum alloys by torch or furnace brazing.1.2 Application:This process has been used typically for joining aluminum and selected aluminum alloys.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.

Brazing, Aluminum Torch or Furnace

SAE AMS4259A-2001 固溶及沉淀热处理(未再结晶化)的2.4Li-1.3Cu-0.95Mg-0.10Zr(8090-T6)铝合金片材

This specification covers an aluminum alloy in the form of sheet. This sheet has been used typically for structural parts requiring the strength of 2024-T3 and lower density, but usage is not limited to such applications.

Aluminum Alloy, Sheet 2.4Li - 1.3Cu - 0.95Mg - 0.10Zr (8090-T6) Solution and Precipitation Heat Treated (Unrecrystallized)

SAE AMS4289-2001 沉淀热处理的7.0Si-0.55Mg-0.12Ti(F357.0-T6)铝合金铸件

This specification covers an aluminum alloy in the form of castings. These castings have been used typically for structural components requiring high strength, but usage is not limited to such applications.

Aluminum Alloy Castings 7.0Si - 0.55Mg - 0.12Ti (F357.0-T6) and Precipitation Heat Treated

QJ 1993A-2001 钛及钛合金的热处理

Heat Treatment of Titanium and Titanium Alloys

SAE AMS4288-2001 经溶液和沉淀热处理的7.0Si-0.58Mg-0.15Ti(E357.0-T6)铝合金铸件

This specification covers an aluminum alloy in the form of castings. These castings have been used typically for structural aircraft components, but usage is not limited to such applications.

Aluminum Alloy Castings 7.0Si - 0.58Mg - 0.15Ti (E357.0-T6) Solution and Precipitation Heat Treated

SAE AMS4335-2001 经热处理的铝合金2xxx和7xxx锻件成品特性:短横截面拉伸性能和断裂韧性

This specification establishes requirements for 2xxx-series and 7xxx- series aluminum alloy forgings of any shape or form from which finished parts are to be made. These forgings are used typically in the manufacture of high-performance parts when control of short-transverse tensile properties and fracture toughness is required, but usage is not limited to such applications.

Forgings, Aluminum Alloys 2xxx and 7xxx, Heat-Treated, Finished-Part Properties: Short-Transverse Tensile Properties and Fracture Toughness

NF L06-395:2000 航空航天系列.航天结构的焊接和钎焊.激光束焊金属材料的焊缝.焊接质量

Aerospace series - Weldments and brazements for aerospace structures - Joints of metallic materials by laser beam welding - Quality of weldments.

DLA A-A-50179 A-2000 热保温桌和冷食品柜

This commercial item description covers, US standard gage, stainless steel, pans, non-perforated and perforated, rectangular, 12 inch by 20 inch series and pan covers, of various sizes, soup tureens and round insets for use in hot food tables and cold food counters. The perforated pans may also be used in steam cookers.

PANS, WITH OR WITHOUT COVERS, FOOD SERVING, RECTANGULAR, SOUP TUREEN AND ROUND INSETS FOR HOT FOOD TABLES AND COLD FOOD COUNTERS

SAE AMS2759/5C-1999 热处理马氏耐蚀钢件

This specification, in conjunction with the general requirements for steel heat treament covered in AMS 2795,establishes the requirements for heat treatment of martensitic corrosion-resistant steel parts.parts are defined in AMD 2759.

Heat Treatment Martensitic Corrosion Resistant Steel Parts

SAE AMS-C-8837-1999 镉真空镀层

This specification covers the requirements for three types and three classes for vacuum deposited cadmium coating.

Coating, Cadmium (Vacuum Deposited) AREA MFFP; Should Be Used Instead of MIL-C-8837B, Which Was Cancelled on 10 September 1999

QJ 176A-1999 地面设备熔焊技术条件

Ground equipment fusion welding technical conditions

QJ 3092-1999 半导体集成电路 HCT与门、与非门详细规范

Detailed specification for semiconductor integrated circuits HCT AND gates and NAND gates

QJ 3099-1999 航天产品焊接质量控制通用要求

General requirements for welding quality control of aerospace products

NF L06-394:1999 航空工业.航空航天结构的焊接件和钎焊件. 用TIG法焊接的金属材料组件.焊接件质量

Aircraft industrie. Weldments and brazements for aerospace structures. Assembly of metallic materials welded by TIG method. Quality of weldments.