V11 航空与航天用金属铸锻材料 标准查询与下载

SAE AMS5396E-2013 耐热和耐腐蚀镍合金熔模铸件65Ni-28Mo-5.5Fe-0.4V(N-12MV)

Nickel Alloy, Corrosion and Heat Resistant, Investment Castings, 65Ni - 28Mo - 5.5Fe - 0.4V (N-12MV), As-Cast

SAE AMS6492A-2013 航空器质量1.0Cr - 3.25Ni - 0.40Mo (0.17 - 0.22C)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. These products have been used typically for carburized parts requiring high minimum core hardness with a narrow range, reduced distortion and subject to magnetic particle inspection standards, but usage is not limited to such applications.

Steel Bars, Forgings, and Tubing, 1.0Cr - 3.25Ni - 0.40Mo (0.17 - 0.22C) Aircraft Quality

NF L17-018*NF EN 4526:2013 航空航天系列.金属材料.试验方法.片材和带材的锐边缺口拉伸试验

Aerospace series - Metallic materials - Test methods - Sharp edge-notch tensile testing for sheet and strip

BS EN 3983:2013 航空航天系列. AL-P7050型铝合金. T7651. 厚板材. 6 mm < a ≤ 60 mm

Aerospace series. Aluminium alloy AL-P7050. T7651. Plate - 6 mm a 60 mm

DIN EN 2043:2013 航空航天系列. 金属材料. 半成品资格的一般要求(锻件和铸件除外); 德文和英文版本EN 2043-2013

Aerospace series - Metallic materials - General requirements for semi-finished product qualification (excluding forgings and castings); German and English version EN 2043:2013

EN 3983:2013 航空航天系列.AL-P7050铝合金.T7651.板材.6 mm< a = 160 mm

This European Standard specifies the requirements relating to: Aluminium alloy AL-P7050 - T7651 Plate 6 mm < a 160 mm for aerospace applications.

Aerospace series - Aluminium alloy AL-P7050- - T7651 - Plate - 6 mm < a ��160 mm

BS EN 4262:2013 航空航天系列.耐热合金FE-PA4901(X12CrNiCoMoW21-20).铸造.锻坯.a或D 200 mm.690 MPa Rm 880 MPa

Aerospace series. Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20). As forged. Forging stock. a or D 200 mm - 690 MPa Rm 880MPa

BS EN 2043:2013 航空航天系列.金属材料.半成品合格的通用要求(锻件和铸件除外)

Aerospace series. Metallic materials. General requirements for semi-finished product qualification (excluding forgings and castings)

BS EN 4263:2013 航空航天系列. FE-PA4901 (X12CrNiCoMoW21-20) 型耐热合金. 锻造的. 锻坯. a或D ≤ 200 mm - 690 MPa≤ Rm ≤ 960 MPa

Aerospace series. Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20). As forged. Forging stock. a or D 200 mm - 690 MPa Rm 960MPa

SAE AMS6557-2013 热均衡加压粉末冶金制品9 V â 5.25 Cr â 1.3 Mo (1.80 â 1.95C)钢筋,钢线和锻件

This specification covers a premium aircraft-quality, high-alloy tool 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 to such applications.

Steel, Bars, Wire, and Forgings, 9 V â 5.25 Cr â 1.3 Mo (1.80 â 1.95C), Powder Metallurgy Product, Hot Isostatically Pressed

SAE AMS5659/H1025A-2013 消耗再融化,溶解和沉积热处理15Cr â 4.5Ni â 0.30Cb (Nb) â 3.5Cu耐腐蚀钢筋,钢线,锻件,环材和挤压制品(H1025)

This specification covers a corrosion-resistant steel product in the solution and precipitation heat treated (H1025) condition. The aged product may be supplied directly by a mill or by a producer other than the mill. The latter would be accomplished by precipitation heat treatment of solution treated material previously certified to AMS5659. The entity assuming responsibility for the aging operation is designated the producer of AMS5659/H1025.

Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions, 15Cr â 4.5Ni â 0.30Cb (Nb) â 3.5Cu, Consumable Remelted, Solution and Precipitation Heat Treated (H1025)

SAE AMS4271A-2013 溶液热处理和冷加工以及人工老化铝合金片材和板材4.4Cu 1.5Mg 0.60Mn (2024-T861)

This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification covers an aluminum alloy in the form of sheet and plate supplied in the -T861 temper. These products have been used typically for structural parts requiring a combination of high strength and good corrosion resistant and whose fabrication does not involve welding; but usage is not limited to such applications.

Aluminum Alloy, Sheet and Plate 4.4Cu 1.5Mg 0.60Mn; (2024-T861) Solution Heat Treated and Cold Worked and Artificially Aged

SAE AMS6559-2013 热等静压成型粉末冶金产品钢棒材、线材和锻件9.75 V 5.25 Cr 1.3 Mo (2.40-2.55 C)

This specification covers a premium aircraft-quality, high-alloy tool steel in the form of bars, wire, forgings, and forging stock.

Steel, Bars, Wire, and Forgings 9.75 V 5.25 Cr 1.3 Mo (2.40 - 2.55 C) Powder Metallurgy Product Hot Isostatically Pressed

SAE AMS4478-2013 溶液热处理、冷却处理以及人工老化的铝合金片材和板材铝衣合金4.4Cu 1.5Mg 0.60Mn (铝衣合金2024、-T81片材、-T851板材)

This specification covers an aluminum alloy in the form of Alclad sheet and plate supplied in the -T81/-T851 temper.

Aluminum Alloy, Sheet and Plate, Alclad 4.4Cu 1.5Mg 0.60Mn (Alclad 2024, -T81 Sheet, -T851 Plate) Solution Heat Treated, Cold Worked and Artificially Aged

NF L10-034-3*NF EN 4050-3:2013 航空航天系列 - 金属材料试验方法 - 棒材, 板材, 锻坯和锻件的超声波检查 - 第3部分: 对比试块

Aerospace series - Test method for metallic materials - Ultrasonic inspection of bars, plates, forging stock and forgings - Part 3: reference blocks

SAE AMS5966B-2013 自耗电极或真空感应熔炼的耐腐蚀耐热性镍合金焊制线材50Ni 20Cr 20Co 5.9Mo 2.2Ti 0.45Al

This specification covers a corrosion and heat resistant nickel alloy in the form of welding wire. This wire has been used typically as filler metal for gas-tungsten-ar or gas-metal-arc welding of corrosion and heat resistant nickel alloys of similar composition where the weld area is required to have strength and corrosion resistance comparable to those of the base metal, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Welding Wire 50Ni 20Cr 20Co 5.9Mo 2.2Ti 0.45Al Consumable Electrode or Vacuum Induction Melted

SAE AMS5565L-2013 溶液热处理的耐腐蚀钢焊接管19Cr 9.5Ni(304)

This specification covers a corrosion-resistant steel in the form of welded tubing. This tubing has been used typically for parts, such as fluid-conducting lines not subjected to high pressure, requiring good corrosion resistance, but usage is not limited to such applications. Welding, brazing, or other exposure to temperatures over 800 degrees F (427 degrees C) during fabrication may impair corrosion resistance.

Steel, Corrosion Resistant, Welded Tubing 19Cr 9.5Ni (304) Solution Heat Treated

EN 4262:2013 航空航天系列.FE-PA4901 (X12CrNiCoMoW21-20) 耐高温合金.锻造的.锻坯.a或D = 200 mm - 690 MPa = Rm = 880MPa

This European Standard specifies the requirements relating to: Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) As forged Forging stock a or D 200 mm 690 MPa < Rm < 880 MPa for aerospace applications.

Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D ��200 mm - 690 MPa ��Rm ��880MPa

EN 4263:2013 航空航天系列.FE-PA4901 (X12CrNiCoMoW21-20)耐高温合金.锻造的.锻坯.a或D 200 mm - 690 MPa R _m 960 MPa.

This European Standard specifies the requirements relating to: Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) As forged Forging stock a or D 200 mm 690 MPa Rm 960 MPa for aerospace applications.

Aerospace series - Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) - As forged - Forging stock - a or D ��200 mm - 690 MPa ��Rm ��960MPa

SAE AMS6475K-2013 钢制渗氮棒材、锻件和管材1.1Cr 3.5Ni 0.25Mo 1.2Al (0.21-0.26C)

This specification covers a nitriding grade of aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for nitrided parts requiring highest surface hardness, high core hardness, resistance to heat, and less distortion than parts made from steel requiring quenching to case harden, but usage is not limited to such applications.

Steel, Nitriding, Bars, Forgings, and Tubing 1.1Cr 3.5Ni 0.25Mo 1.2Al (0.21-0.26C)