V11 航空与航天用金属铸锻材料 标准查询与下载

HB 20096-2012 高强度钢热损伤巴克豪森检测

本标准规定了高强度铁磁性钢制零件热损伤的巴克豪森的一般要求和详细要求。本标准适用于高强度钢磨削后以及对涂/镀层磨削后所产生的基体金属热损伤的检测,也可用于在役产生的热损伤的检测。本标准不适用于有镀镍层的高强度钢制零件热损伤的检测。

Barkhausen inspection for thermal damage of high-strength steel

HB 5448-2012 钛及钛合金熔模精密铸件规范

本规范规定了钛及钛合金熔模精密铸件的要求、质量保证规定、交货准备等。本规范适用于航空用钛及钛合金熔模精密铸件。

Specificatiaon for titanium and titanium alloy investment castings

HB 20082-2012 航空用高温合金轴锻件规范

本规范规定了航空用GH2901、GH4169、GH 4500高温合金轴锻件的要求、质量保证规定和交货准备等。本规范适用于航空用高温合金轴锻件(以下简称锻件)。

Specification for superalloy shaft forgings for aviation

SAE AMS4459A-2013 伸长1至3%和老化的溶解热处理,应力消除镁合金挤制加工2.7Cu 1.8Li 0.7Zn 0.3Mn 0.3Mg 0.08Zr (2099-T81)

This specification covers an aluminum alloy in the form of extruded bars, rods, and profiles (shapes) produced with cross sectional area of 22.5 square inches (145 cm2) maximum and a circumscribing circle diameter (circle size) of 17.4 inches (44.2 cm) maximum.

Aluminum Alloy, Extrusion 2.7Cu 1.8Li 0.7Zn 0.3Mn 0.3Mg 0.08Zr (2099-T81) Solution Heat Treated, Stress Relived by Stretching 1 to 3% and Aged

SAE AMS6408D-2013 电渣再熔化(ESR)或自耗电极真空电弧再熔化(VAR)退火钢制热加工用具,钢棒和钢锻件5.2Cr 1.5Mo 1.0V (0.35-0.45C) (H-13)

This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. These products have been used typically for hotwork tooling or for parts requiring a steel capable of through-hardening to a minimum hardness of 50 HRC in section thicknesses up to 12 inches (305 mm) with relatively high levels of strength, fatigue resistance, ductility, and thermal stability for use in service from -100 to +1000 °F (-73 to 538 °C) and where such parts may require welding, but usage is not limited to such applications.

Steel, Hotwork Tool, Bars and Forgings 5.2Cr 1.5Mo 1.0V (0.35-0.45C) (H-13) Electroslag Remelted (ESR) or Consumable Electrode Vacuum Arc Remelted (VAR) Annealed

SAE AMS6547-2013 飞机-质量等级1.0Cr 3.2Ni 0.2Mo (0.12 - 1.17C)钢筋,锻件和管件

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 1.0Cr 3.2Ni 0.2Mo (0.12 - 1.17C) Aircraft-Quality

SAE AMS5582F-2013 溶解热处理,沉淀硬化至155 ksi (1069 MPa)抗张强度的镍合金耐蚀和耐热无缝管,72Ni 15.5Cr 0.95Cb (Nb) 2.5Ti 0.70Al 7.0Fe

This specification covers a precipitation hardenable, corrosion and heat resistant nickel alloy in the form of seamless tubing. This tubing has been used typically for fluid lines requiring high strength up to 1300 degrees F (704 degrees C) and oxidation resistance up to 1800 degrees F (980 degrees C), but usage is not limited to such applications. Parts may be formed and then heat treated to improve strength at elevated temperatures.

Nickel Alloy, Corrosion and Heat Resistant, Seamless Tubing, 72Ni 15.5Cr 0.95Cb (Nb) 2.5Ti 0.70Al 7.0Fe, Solution Heat Treated, Precipitation Hardenable to 155 ksi (1069 MPa) Tensile Strength

SAE AMS7488F-2013 闪焊铝和铝合金环材

This specification covers flash welded rings made of aluminum and aluminum alloys. These products have been used typically for parts such as flangers and rings, but usage is not limited to such applications.

Rings, Flash Welded Aluminum and Aluminum Alloys

SAE AMS6548-2013 高级航空品质电渣再熔化或自耗电极真空电弧再熔化钢棒,钢锻件和钢管1.0Cr 3.2Ni 0.2Mo (0.12 - 0.17C)

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

Steel Bars, Forgings, and Tubing 1.0Cr 3.2Ni 0.2Mo (0.12 - 0.17C) Premium Aircraft-Quality Electroslag Remelted or Consumable Electrode Vacuum Remelted

SAE AMS4016M-2013 应变硬化四分之一硬度和稳定的镁合金薄板和板材,2.5Mg 0.25Cr (5052-H32)

This specification covers an aluminum alloy in the form of sheet and plate. These products have been used typically for parts requiring moderate strength, good formability, good welding and resistance spot welding characteristics, and good resistance to corrosion, but usage is not limited to such applications.

Aluminum Alloy, Sheet and Plate, 2.5Mg 0.25Cr (5052-H32), Strain Hardened, Quarter-Hard, and Stabilized

SAE AMS5583E-2013 沉积可硬化拉伸强度至170 ksi (1172 MPa)真空融解热处理72Ni 15.5Cr 0.95Cb (Nb) 2.5Ti 0.70Al 7.0Fe,耐腐蚀耐高温镍合金无缝管件

This specification covers a corrosion and heat resistant nickel alloy in the form of seamless tubing. This tubing has been used typically for fluid-conducting lines requiring high strength up to 1100 degrees F (593 degrees C), but usage is not limited to such applications. Parts may be formed and then heat treated to improve strength at elevated temperatures.

Nickel Alloy, Corrosion and Heat Resistant, Seamless Tubing 72Ni 15.5Cr 0.95Cb (Nb) 2.5Ti 0.70Al 7.0Fe, Vacuum Melted Solution Heat Treated, Precipitation Hardenable to 170 ksi (1172 MPa) Tensile Strength

ASTM E192-13 航天设备蜡模钢铸件的标准参考放射线照片

1.1 The reference radiographs provided in the adjunct to this standard illustrate various types and degrees of discontinuities occurring in thin-wall steel investment castings.2 Use of this standard for the specification or grading of castings requires procurement of the adjunct reference radiographs which illustrate the discontinuity types and severity levels. They are intended to provide the following: 1.1.1 A guide enabling recognition of thin-wall steel casting discontinuities and their differentiation both as to type and degree through radiographic examination. 1.1.2 Example radiographic illustrations of discontinuities and a nomenclature for reference in acceptance standards, specifications and drawings. 1.2 Two illustration categories are covered as follows: 1.2.1 Graded—Six common discontinuity types each illustrated in eight degrees of progressively increasing severity. 1.2.2 Ungraded—Twelve single illustrations of additional discontinuity types and of patterns and imperfections not generally regarded as discontinuities. 1.3 The reference radiographs were developed for casting sections up to 1 in. (25.4 mm) in thickness. 1.4 This document may be used where there is no other applicable document existing or for other material thicknesses for which it is found to be applicable and for which agreement has been reached between the purchaser and manufacturer. Note 1—The set of reference radiographs, produced with X-rays in the range from 130 to 250 kVp, consist of 16 plates (81/2 by 11 in. (216 by 279 mm)) in a 93/4 by 111/2-in. (248 by 292-mm) ring binder. 1.5 These film reference radiographs are not intended to illustrate the types and degrees of discontinuities found in aerospace investment castings when performing digital X-ray imaging. When performing digital X-ray imaging of these castings, refer to Digital Reference Image Standard E2660. 1.6 The values stated in inch-pound units are to be regarded as the standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard. 1.7 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Reference Radiographs of Investment Steel Castings for Aerospace Applications

EN 2030:2013 航空航天系列 钢 X105CrMo17（1.3544） 淬火和回火 棒材 De = 150 mm

This European Standard specifies the requirements relating to: Steel X105CrMo17 (1.3544) Hardened and tempered Bars De 150 mm for aerospace applications. NOTE Other common designation: UNS: S44004, AISI: 440C, XDBD.

Aerospace series - Steel X105CrMo17 (1.3544) - Hardened and tempered - Bars - De = 150 mm

SAE AMS6427L-2012 0.88Cr 1.8Ni 0.42Mo 0.08V(0.28-0.33C)(4330 Mod)钢制棒材、煅件和管材

Steel Bars, Forgings, and Tubing 0.88Cr 1.8Ni 0.42Mo 0.08V (0.25-0.33C) (4330 Mod)

SAE AMS6411H-2012 0.88Cr 1.8Ni 0.42Mo 0.08V (0.28-0.33C) (4330 Mod)自耗电极再熔炼钢制棒材、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 parts requiring high tensile strength and good ductility with relatively high impact strength, superior transverse properties, and hardness, but usage is not limited to these applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment. SAE ARP 1110 recommends practices to minimize such conditions.

Steel Bars, Forgings, and Tubing 0.88Cr 1.8Ni 0.42Mo 0.08V (0.28-0.33C) (4330 Mod) Consumable Electrode Remelted

SAE AMS5354F-2012 硬化和回火洛氏硬度(HRC)32-38的熔模铸件13Cr 2.0Ni 3.0W耐腐蚀和耐热钢

This specification covers a corrosion and moderate heat resistant steel in the form of investment castings. These castings have been used typically for parts, such as compressor blades and vanes, housings, and valves, for use up to 1000 degrees F (538 degrees C), but usage is not limited to such applications.

Steel, Corrosion and Heat Resistant, Investment Castings 13Cr 2.0Ni 3.0W Hardened and Tempered to 32 - 38 HRC

SAE AMS4413A-2012 3.5Cu 1.0Li 0.40Mg 0.35Mn 0.45Ag 0.12Zr (2050-T84)溶液热处理、应力释放和人工老化的铝合金厚板材

This specification covers an aluminum-lithium alloy in the form of plate. This plate has been used typically for parts where low density is needed in combination with a high level of mechanical properties and very good resistance to stress-corrosion cracking, but usage is not limited to such applications.

Aluminum Alloy, Plate 3.5 Cu 1.0Li 0.40Mg 0.35Mn 0.45Ag 0.12Zr (2050-T84) Solution Heat Treated, Stress Relieved, and Artificially Aged

SAE AMS5536N-2012 47.5Ni 22Cr 1.5Co 9.0Mo 0.60W 18.5Fe溶液热处理的耐腐蚀和耐热镍合金片材、带材和板材

This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in inch/pound units. These products have been used typically for parts requiring oxidation resistance up to 2200 °F and relatively high strength up to 1500 °F, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 47.5Ni 22Cr 1.5Co 9.0Mo 0.60W 18.5Fe, Solution Heat Treated

SAE AMS4485-2012 沉淀热处理的挤压制4.0Y 2.25Nd 0.5Zr(WE43C-T5)镁合金

This specification covers a magnesium alloy in the form of extruded bars, rods, wire, tubing, and profiles.

Magnesium Alloy, Extrusions 4.0Y 2.25Nd 0.5Zr (WE43C-T5) Precipitation Heat Treated

SAE AMS4470A-2012 经过热溶解处理、消除应力和过老化的的7.5Zn 1.6Cu 1.5Mg 0.12Zr铝合金板材(7085-T7451)

This specification covers an aluminum alloy in the form of plate. This product may be used in aerospace applications requiring a high level of mechanical properties and fracture toughness, good resistance to stress-corrosion cracking and resistance to exfoliation corrosion, but usage is not limited to such applications.

Aluminum Alloy, Plate (7085-T7451) 7.5Zn 1.6Cu 1.5Mg 0.12Zr Solution Heat Treated, Stress-Relieved, and Overaged