V11 航空与航天用金属铸锻材料 标准查询与下载

EN 966:2012/A1:2012 航空体育活动专用头盔

This European Standard specifies requirements and test methods for protective helmets used in paragliding, hang gliding and flying with ultra-light aeroplanes. Helmets for airborne sports are indicated in this European Standard as follows: category HPG: Helmets for paragliding and hang gliding; category UL: Helmets for flying with ultra-light aeroplanes. Requirements and the corresponding methods of test, where appropriate, are given for the following: construction including chin strap, fastening devices, field of vision, head mobility and eye protection; penetration resistance; shock-absorbing properties; retention system properties; marking and information for users. NOTE The requirements cover both categories. Special requirements are contained in the relevant clauses. This European Standard does not apply to other kinds of head protection used in airborne sports.

Helmets for airborne sports

DIN EN 3456:2012 航空航天系列. TI-P64001 (Ti-6Al-4V)型钛合金. 退火. 热轧板材和带材. <小于 => 6 mm; 德文和英文版本EN 3456-2012

Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Sheet and strip, hot rolled - a 6 mm; German and English version EN 3456:2012

BS EN 3464:2012 航天航空系列.钛合金(TI-6AI-4V).煅烧.板材.6 mm

SAE AMS6302J-2012 耐高温0.65Si 1.25Cr 0.50Mo 0.25V(0.28-0.33C)低合金钢筋,铸件和管件

This specification covers an aircraft-quality, low-alloy, heat-resistant steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts, such as shafts and fasteners, in service up to 1000 °F (538 °C), but usage is not limited to such applications.

Low-Alloy Steel, Heat-Resistant, Bars, Forgings, and Tubing 0.65Si 1.25Cr 0.50Mo 0.25V (0.28-0.33C)

SAE AMS4124E-2012 溶解热处理,拉伸和过旧进行应力消除的5.6Zn 2.5Mg 1.6Cu 0.23Cr (7075-T73, T7351)铝合金轧制或冷磨光棒材,杆材和线材

This specification covers an aluminum alloy in the form of rolled or cold finished bars, rods, and wire. These products have been used typically for machined parts subject to excessive warpage during machining due to residual stresses and for parts requiring high strength and resistance to stress-corrosion cracking and whose fabrication does not involve forming or welding, but usage is not limited to such applications.

Aluminum Alloy, Rolled or Cold Finished Bars, Rods, and Wire 5.6Zn 2.5Mg 1.6Cu 0.23Cr (7075-T73, T7351), Solution Heat Treated, Stress Relieved by Stretching, and Overaged

SAE AMS4979G-2012 溶解和沉淀热处理钛合金棒材,线材,锻件和环材6A1 6V 2Sn

This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts requiring high strength- to-weight ratio up to 750 °F (399 °C), 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, Bars, Wire, Forgings, and Rings 6A1 6V 2Sn Solution and Precipitation Heat Treated

SAE AMS4940B-2012 退火25.0 ksi屈服强度(172 MPa)工业纯钛金属片材,带板和板材

This specification covers one grade (Grade 1) of commercially-pure titanium in the form of sheet, strip, and plate up through a thickness of 1.000 inch (25.40 mm). This material has been used typically for parts requiring the properties of titanium and good formability but not high strength, but usage is not limited to such applications.

Titanium Sheet, Strip, and Plate Commercially Pure Annealed, 25.0 ksi (172 MPa) Yield Strength

SAE AMS4970J-2012 溶解和沉淀热处理7A1 4Mo钛合金棒材,线材和铸件

This specification covers a titanium alloy in the form of bars, wire, forgings, and forging stock. This alloy has been used typically for parts requiring strength up to 900 °F (482 °C), but usage is not limited to such application. 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 Bars, Wire, and Forgings 7A1 4Mo Solution and Precipitation Heat Treated

SAE AMS-A-22771C-2012 热处理铝合金锻件

This specification has previously been widely used and may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend this specification for future use in new designs. This specification covers the requirements for heat treated aluminum alloy die forgings, hand forgings, and ring forgings, produced under additional mechanical property control to ensure known mechanical properties for parts used in aerospace critical applications. This specification also covers the requirements for forgings furnished in the F or 01 conditions which will ultimately be used in the heat treated condition.

Aluminum Alloy Forgings, Heat Treated

SAE AMS4910P-2012 退火5Al 2.5Sn钛合金片材,带材和板材

This specification covers a titanium alloy in the form of sheet, strip, and plate. These products have been used typically for parts requiring strength up to 800 °F (427 °C) and where such parts may require welding during fabrication, 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 5Al 2.5Sn Annealed

SAE AMS6320N-2012 0.50Cr 0.55Ni 0.25Mo (0.33-0.38C) (8735)钢棒材,铸件和环材

This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts, 0.75 inch (19.0 mm) and under in nominal section thickness at the 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 proportionally lower hardness but usage is not limited to such applications.

Steel Bars, Forgings, and Rings, 0.50Cr 0.55Ni 0.25Mo (0.33-0.38C) (8735)

SAE AMS4598A-2012 固溶退火和旋接线硬化(TX 00)77Cu 15Ni 8Sn铜镍矿锡合金机械管

This specification covers a copper-nickel-tin alloy in the form of mechanical tube. These products have been used typically for parts requiring high strength, wear resistance, and corrosion resistance at moderate temperatures, but usage is not limited to such applications.

Copper Nickel Tin alloy, Mechanical Tube 77Cu 15Ni 8Sn Solution Annealed and Spinodal Hardened (TX 00)

SAE AMS6265N-2012 真空再熔化自耗电极1.2Cr 3.25Ni 0.12Mo (0.07 0.13C)(9310)钢制棒材,锻件和管材

This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for critical carburized parts requiring high minimum core hardness with a narrow range and subject to very rigid magnetic particle inspection standards, but usage is not limited to such applications.

Steel, Bars, Forgings, and Tubing 1.2Cr 3.25Ni 0.12Mo (0.07 0.13C) (9310) Vacuum Consumable Electrode Remelted

SAE AMS2728C-2012 熟铜铍合金零件热处理

This specification establishes the requirements for heat treatment of wrought copper beryllium parts by users or by their vendors or subcontractors. This specification is applicable to parts made from the following alloys: UNS C17000, UNS C17200, UNS C17300, UNS C17500, and UNS C17510.

Heat Treatment of Wrought Copper Beryllium Alloy Parts

SAE AMS4439G-2012 4.2Zn 1.2稀土族镁合金铸件.O.7Zr (ZE41A-T5)沉淀热处理

This specification covers a magnesium alloy in the form of sand castings. These castings have been used typically for components requiring uniform medium strength up to 320 °F (160 °C), pressure tightness, good fatigue and creep characteristics, and which may require welding during fabrication, but usage is not limited to such applications.

Magnesium Alloy Castings 4.2Zn 1.2 Rare Earths - O.7Zr (ZE41A-T5) Precipitation Heat Treated

SAE AMS6430H-2012 0.75Mn 0.78Cr 1.8Ni 0.35Mo 0.20V (0.32-0.38C) (4335改良)钢制棒材,锻件,管材和环材

This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for heat treated parts, which may be welded during fabrication, requiring through-hardening to high strength levels, and which may be used at operational stress levels approaching the yield strength, but usage is not limited to such applications.

Steel Bars, Forgings, Tubing, and Rings, 0.75Mn 0.78Cr 1.8Ni 0.35Mo 0.20V (0.32-0.38C) (4335 Modified)

SAE AMS4975L-2012 溶解和沉淀热处理6.0Al 2.0Sn 4.0Zr 2.0Mo 0.08Si钛合金棒材,线材和环材

This specification covers a titanium alloy in the form of bars, wire, flash welded rings, and stock for flash welded rings. These products have been used typically for parts requiring high strength and toughness and good creep resistance up to 1000 °F (538 °C), 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. ARP 982 recommends practices to minimize such conditions.

Titanium Alloy, Bars, Wire and Rings, 6.0Al 2.0Sn 4.0Zr 2.0Mo 0.08Si, Solution and Precipitation Heat Treated

SAE AMS4976H-2012 溶解和沉淀热处理6.0Al 2.0Sn 4.0Zr 2.0Mo钛合金铸件

This specification covers a titanium alloy in the form of forgings and forging stock. These products have been used typically for parts requiring high strength and toughness and good creep resistance up to 1000 ° F (538 °C), but usage is not limited to such applications. Certain processing procedure and service conditions may cause these forgings to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.

Titanium Alloy, Forgings 6.0Al 2.0Sn 4.0Zr 2.0Mo Solution and Precipitation Heat Treated

SAE AMS4981F-2012 融解和沉积热处理6.0Al 2.0Sn 4.0Zr 6.0Mo钛合金棒材,线材和铸件

This specification covers a titanium alloy in the form of bars, wire, forgings, and forging stock. This alloy has been used typically for parts requiring high strength up to 1000 °F (538 °C), 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 Bars, Wire, and Forgings 6.0Al 2.0Sn 4.0Zr 6.0Mo Solution and Precipitation Heat Treated

SAE AMS2643E-2012 钛合金结构检查,化学腐蚀检查规程

This specification covers a procedure for revealing the macrostructure and microstructure of titanium alloys. This inspection procedure has been used typically for detecting defects and segregation in titanium alloys. This procedure should not be used on finished parts.

Structural Examination of Titanium Alloys, Chemical Etch Inspection Procedure