V11 航空与航天用金属铸锻材料 标准查询与下载

EN 4266:2013 航空航天系列 金属对金属的球面滑动轴承，耐腐蚀钢，镀镉 宽系列 尺寸和载荷 英制系列

This European Standard specifies the characteristics of spherical plain bearings, metal to metal, in corrosion resisting steel, cadmium plated and chromated, wide series, inch series for aerospace applications. They are intended for use in fixed or moving parts of the aircraft structure and their control mechanisms. They shall be used in the temperature range - 54 °C to 150 °C. As they are lubricated by means of the following greases: Code A: Grease as per MIL-PRF-23827C, operating temperature range - 73 °C to 121 °C; Code B: Grease as per MIL-PRF-81322G, operating temperature range - 54 °C to 177 °C. The range of application for bearings lubricated with grease per code A is limited to 121 °C. In both cases the spherical surface of the outer or inner ring have to be provided with a dry-film lubricant as per MIL-PRF-46010G or equivalent (anti-seizing protection). The slide hole treatment either at the outer ring or inner ring.

Aerospace series - Bearing spherical plain, metal to metal, in corrosion resisting steel, cadmium plated - Wide series - Dimensions and loads - Inch series

SAE AMS6349D-2013 标准化的钢棒0.95Cr 0.20Mo (0.38-0.43C) (SAE 4140标准)

This specification covers an aircraft-quality, low-alloy steel in the form of bars. These bars have been used typically for parts 0.50 inch (12.7 mm) and under in section thickness at time of heat treatment requiring a through-hardening steel capable of developing hardness as high as 50 HRC when properly hardened and tempered and also for parts of greater thickness requiring proportionately lower hardness, but usage is not limited to such applications.

Steel Bars 0.95Cr 0.20Mo (0.38-0.43C) (SAE 4140) Normalized

SAE AMS6381H-2013 机械钢管0.95Cr 0.20Mo(0.38-0.43C)(SAE 4140标准)

This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing. This tubing has been used typically for parts, 0.500 inch (12.70 mm) and under in section thickness at the time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 50 HRC when properly hardened and tempered and also parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.

Steel, Mechanical Tubing 0.95Cr 0.20Mo (0.38-0.43C) (SAE 4140)

SAE AMS6371K-2013 0.95Cr 0.20Mo(0.28-0.33C)机制钢管(SAE 4130标准)

This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing. This tubing has been used typically for parts, 0.375 inch (9.52 mm) and under in nominal thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 40 HRC when properly hardened and tempered and for parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.

Steel, Mechanical Tubing 0.95Cr 0.20Mo (0.28-0.33C) (SAE 4130)

SAE AMS4966P-2013 屈服强度为110 ksi(758 MPa)的退火钛合金锻件5Al 2.5Sn

This specification covers a titanium alloy in the form of forgings and forging stock. These forgings have been used typically for parts requiring strength up to 800 °F (427 °C) and which may be welded during fabrication, but usage is not limited to such applications.

Titanium Alloy, Forgings 5Al 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength

SAE AMS4939B-2013 经溶液热处理的钛合金3Al 8V 6Cr 4Mo 4Zr薄板材、带材和厚板材

This specification covers a titanium alloy in the form of sheet, strip, and plate through 4.000 inches (101.60 mm).. This material has been used typically for parts to be formed or machined in the solution heat treated condition and subsequently precipitation heat treated requiring high strength-to-weight ratio and stability up to 550 °F (288 °C) in the precipitation heat treatment condition, but usage is not limited to such applications. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.

Titanium Alloy Sheet, Strip, and Plate 3Al 8V 6Cr 4Mo 4Zr Solution Heat treated

SAE AMS4915L-2013 单退火8Al 1V 1Mo钛合金薄板材、带材和厚板材

This specification covers a titanium alloy in the form of sheet, strip, and plate up through 4.000 inches (101.60 mm). These products have been used typically for parts requiring strength up to 800 °F (427 °C) where fracture toughness is not critical. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.

Titanium Alloy Sheet, Strip, and Plate 8Al 1V 1Mo Single Annealed

DIN EN 3528:2013 航空航天系列. X2NiCoMo18-8-5 (1.6359) 型钢. 真空感应熔炼和真空电弧再熔. 溶液处理和沉淀处理. 棒材. a/D ≤ 150 mm-1750 Mpa ≤ Rm ≤ 2 000 Mpa; 德文和英文版本EN 3528-2013

Aerospace series - Steel X2NiCoMo18-8-5 (1.6359) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Bar - a or D 150 mm - 1 750 MPa Rm 2 000 MPa; German and English version

SAE AMS6372M-2013 机械钢管0.95Cr 0.20Mo (0.33-0.38C) (SAE 4135)

This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing. This tubing has been used typically for parts, 0.75 inch (19 mm) and under in nominal wall thickness at time of heat treatment requiring a through-hardening steel capable of developing hardness as high as 40 HRC when properly hardened and tempered and for parts of greater wall thickness but requiring proportionately lower hardness, but usage is not limited to such applications.

Steel, Mechanical Tubing 0.95Cr 0.20Mo (0.33-0.38C) (SAE 4135)

SAE AMS2402K-2013 镀锌

This specification covers the requirements for electrodeposition of zinc plating. This process has been used typically to provide corrosion resistance to metal parts, but usage is not limited to such applications. Unless otherwise stated on the engineering drawing, high strength steel parts having a hardness of 45 HRC or greater shall not be electroplated to this document.

Plating, Zinc

SAE AMS4469-2013 溶解热处理,并通过拉伸和老化应力消除无缝拉伸1.8 Cu 1.0 Mg 0.8 Si 0.20 Cr铝合金管件(2013-T4511)

This specification covers an aluminum alloy in the form of seamless, drawn tubing.

Aluminum Alloy Tubing, Seamless, Drawn 1.8 Cu 1.0 Mg 0.8 Si 0.20 Cr Solution Heat Treated, Stress Relieved by Stretching, and Aged (2013-T4511)

SAE AMS6560-2013 轴承应用件惰性气体原子化和热均衡等压加固用溢价飞行器质量10 Co 7 Mo 6 V 6 W 4 Cr (2.2 - 2.4C)钢筋,钢丝和锻件

This specification covers a premium aircraft-quality, high-alloy steel in the form of bars, wire, forgings, and forging stock. These products have been used typically for critical parts, such as bearings operating under heavy loads and high speeds at moderate temperatures and subject to very rigid inspection standards, but usage is not limited such applications.

Steel Bars, Wire and Forgings 10 Co 7 Mo 6 V 6 W 4 Cr (2.2 - 2.4C) Premium Aircraft-Quality for Bearing Applications Inert Gas Atomized and Hot Isostatically Pressed Consolidated

SAE AMS5570Q-2013 溶解热处理耐腐蚀和耐热无缝钢管18Cr 11Ni 0.40Ti (321)

This specification covers a corrosion and heat resistant steel in the form of seamless tubing. This tubing has been used typically for parts requiring both corrosion and heat resistance, especially when such parts are welded during fabrication, and also for parts requiring oxidation resistance up to 1500 degrees F (816 degrees C) but useful at that temperature only when stresses are low; usage is not limited to such applications.

Steel, Corrosion and Heat Resistant, Seamless Tubing 18Cr 11Ni 0.40Ti (321) Solution Heat Treated

SAE AMS5804H-2013 耐蚀和耐热钢制焊丝15Cr 25.5 Ni 1.3Mo 2.2Ti 0.006B 0.30V

This specification covers a corrosion and heat resistant steel in the form of welding wire. This wire has been used typically as filler metal for gas-tungsten-arc or gas-metal-arc welding of precipitation-hardenable, corrosion and heat resistant steels of similar composition, but usage is not limited to such applications.

Steel, Corrosion and Heat Resistant, Welding Wire 15Cr 25.5 Ni 1.3Mo 2.2Ti 0.006B 0.30V

SAE AMS4236C-2013 溶解热处理和天然老化4.6Cu 0.35Mn 0.25Mg 0.22Ti (A206.0-T4)铝合金铸件

This specification covers an aluminum alloy in the form of sand, investment, permanent mold, and composite mold castings. Primarily for components requiring high strength combined with good ductility and impact strength. Certain design and processing procedures may cause these castings to become susceptible to stress-corrosion cracking.

Aluminum Alloy Castings 4.6Cu 0.35Mn 0.25Mg 0.22Ti (A206.0-T4) Solution Heat Treated and Naturally Aged

SAE AMS2315G-2013 铁素体含量测定

This specification covers two methods for determining the percentage of delta ferrite in steels and other iron alloys. When applicable, this specification will be invoked by the material specification.

Determination of Delta Ferrite Content

SAE AMS2771E-2013 铝合金铸件的热处理

The specification covers the engineering requirements for heat treatment of aluminum alloy castings and for parts machined from castings.

Heat Treatment of Aluminum Alloy Castings

SAE AMS2675H-2013 铜焊镍合金填充金属

This specification covers the requirements for producing brazed joints in parts made of steels, iron alloys, nickel alloys, and cobalt alloys by use of nickel alloy filler metal. This process has been used typically for joints requiring high strength and corrosion and oxidation resistance up to 1200 degrees F (649 degrees C), but usage is not limited to such applications.

Brazing, Nickel Alloy Filler Metal

SAE AMS6539-2013 航空品质钢棒材,铸件和钢管1.7Cr 3.8Ni 0.3Mo (0.32 - 0.38 C)

This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.

Steel Bars, Forgings, and Tubing 1.7Cr 3.8Ni 0.3Mo (0.32 - 0.38 C) Aircraft-Quality

SAE AMS6387B-2013 表面结合层压板碳素钢

This specification covers steel in the form of laminated sheet. This material has been used typically for shims in which thickness is adjusted by removal of laminations as required, but usage is not limited to such applications.

Steel, Carbon, Laminated Sheet, Surface Bonded