V11 航空与航天用金属铸锻材料 标准查询与下载

SAE AMS4172F-2013 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T4511 or T4510)溶解热处理和通过拉伸进行应力消除的铝合金挤压制品

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing.

Aluminum Alloy, Extrusions 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T4511 or T4510) Solution Heat Treated and Stress Relieved by Stretching

SAE AMS4150M-2013 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T6)溶解热处理和沉淀热处理的铝合金挤压制品和环

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing, flash welded rings fabricated from extruded stock, and stock for flash welded rings.

Aluminum Alloy, Extrusions and Rings 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T6) Solution and Precipitation Heat Treated

SAE AMS4161H-2013 溶解热处理和自然老化铝合金挤压制品1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T4)

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing.

Aluminum Alloy, Extrusions 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T4) Solution Heat Treated and Naturally Aged

SAE AMS4173F-2013 溶解热处理，并通过拉伸、校直和沉淀热处理消除压力的铝合金挤压制品1.0Mg 0.60Si 0.30Cu 0.20Cr (6061-T6511 pr T6510)

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

Aluminum Alloy, Extrusions 1.0Mg 0.60Si 0.30Cu 0.20Cr (6061-T6511 pr T6510) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Precipitation Heat Treated

SAE AMS5899B-2013 热等静压成型粉末冶金制品耐腐蚀钢棒材、线材和锻件17Cr 0.52Mo (0.95-1.20C)

This specification covers a corrosion-resistant steel, consolidated by hot isostatic pressing (HIP) product from prealloyed powder, in the form of bars, wire, forgings, and forging stock. These products have been used typically for parts requiring minimum hardness of 58 HRC and resistance to wear, corrosion, and oxidation, but usage is not limited to such applications.

Steel, Corrosion-Resistant, Bars, Wire, and Forgings 17Cr 0.52Mo (0.95 - 1.20C) Powder Metallurgy Product, Hot Isostatically Pressed

SAE AMS5555E-2013 镍线和镍带的99镍

This specification covers nickel in the form of round wire and rectangular ribbon. These products have been used typically as weldable leads for electronic component parts or as filler wire for welding, but usage is not limited to such applications.

Nickel Wire and Ribbon 99Ni

SAE AMS5782G-2013 20.5Cr 9.0Ni 0.50Mo 1.5W 1.2Cb 0.20Ti真空感应融化耐高温耐腐蚀钢制焊丝

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-metal-arc or gas-tungsten-arc welding of steels of similar composition requiring joints with strength and corrosion resistance comparable to those of the basis metal, but usage is not limited to such applications.

Steel, Corrosion and Heat-Resistant, Welding Wire 20.5Cr 9.0Ni 0.50Mo 1.5W 1.2Cb 0.20Ti Vacuum Induction Melted

DIN EN 3354:2013 航空航天系列.钛合金Ti-6Al-4V.退火.超塑性成形片材.a < kleiner => 6 mm.德文和英文版本EN 3354-2013

Aerospace series - Titanium alloy Ti-6Al-4V - Annealed - Sheet for superplastic forming - a 6 mm; German and English version EN 3354:2013

DIN EN 3813:2013 航空航天系列.钛合金TI-P64001(Ti-6Al-4V).退火.锻造紧固件的棒材和线材.D_e 50 mm.德文和英文版本EN 3813-2013

Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar and wire for forged fasteners - D_e 50 mm; German and English version EN 3813:2013

DIN EN 2089:2013 航空航天系列. AL-P2014A-T6或T62铝合金. 薄板材和带材. 0.4 ≤ a ≤ 6 mm; 德文和英文版本EN 2089-2005

Aerospace series - Aluminium alloy AL-P2014A-T6 or T62 - Sheet and strip - 0,4 mm a 6 mm; German and English version EN 2089:2005

BS EN 4631:2013 航空航天系列.X4CrNiMo16-5-1 (1.4418)型钢.空气熔炼.硬化和回火.棒材.De≤200 mm.900 MPa≤Rm≤1050 MPa

Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De 200 mm. 900 MPa Rm 1050 MPa

BS EN 4629:2013 航空航天系列.X4CrNiMo16-5-1 (1.4418)钢.空气融化.软化.锻坯.De 300 mm

Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Softened. Forging stock. De 300 mm

BS EN 4628:2013 航空航天系列.FE-PM 3504(X4CrNiMo16-5-1)型钢.空气熔炼.回火和淬火.棒材.De≤150 mm.1100 MPa≤Rm≤1300 MPa

Aerospace series. Steel X4CrNiMo16-5-1 (1.4418). Air melted. Hardened and tempered. Bar. De 200 mm. 1150 MPa Rm 1300 MPa

SAE AMS4778K-2013 1800至1900℉固相线-液相线范围的镍合金钎料92Ni 4.5Si 3.1B

This specification covers a nickel alloy in the form of wire, rod, strip, foil, and powder and a viscous mixture (paste) of the powder in a suitable binder and procured in inch/pound units. This filler metal has been used typically for joining corrosion and heat resistant steels and alloys requiring corrosion and oxidation resistant joints with good strength at elevated temperatures, but usage is not limited to such applications. Also may be used as a corrosion and oxidation resistant hard coating.

Nickel Alloy, Brazing Filler Metal 92Ni 4.5Si 3.1B, 1800 to 1900°F Solidus-Liquidus Range

SAE AMS5574F-2013 溶液热处理耐腐蚀和耐热无缝钢管23Cr 13.5Ni (309S)

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 for parts requiring oxidation resistance up to 2000 degrees F (1093 degrees C) though useful at that temperature only when stresses are low, but usage is not limited to such applications.

Steel, Corrosion and Heat Resistant, Seamless Tubing 23Cr 13.5Ni (309S) Solution Heat Treated

SAE AMS5575P-2013 溶解热处理的耐腐蚀和耐高温焊接钢管18Cr 10.5Ni 0.70Cb(Nb)(347)

This specification covers a corrosion and heat resistant steel in the form of welded tubing. This tubing has been used typically for parts requiring both corrosion and heat resistance, especially when subjected to welding, brazing, or other exposure at temperatures over 800 °F (427 °C) during fabrication but usage is not limited to such applications. Also has been used for parts requiring oxidation resistance up to 1500 °F (816 °C) but useful at that temperature only when stresses are low, but usage is not limited to such applications.

Steel, Corrosion and Heat Resistant, Welded Tubing 18Cr 10.5Ni 0.70Cb(Nb) (347) Solution Heat Treated

SAE AMS4998E-2013 6Al 4V钛合金粉末

This specification covers a titanium alloy in the for of prealloyed powder. This powder has been used typically for compaction into net or near net shapes and into forgings stock in the form of billets or preforms, but usage is not limited to such applications.

Titanium Alloy Powder 6Al 4V

NF L14-648*NF EN 3351:2013 航空航天系列.钛合金Ti-4Al-4Mo-2Sn.溶液处理和老化.锻件. De 150 mm

Aerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De < ou = 150 mm

SAE AMS5880E-2013 轴承用耐腐蚀钢棒材、锻件及线材17Cr 0.52Mo (0.95-1.20C) (SAE 51440C标准)

AMS5880E rescinds the previous cancellation and supersession, and at the same tim estabilizes the document becasue it still has use in the bearing industry. For historical reference, revision D of AMS5880 cancelled the document and superseded it with AMD 5618 AMS5880E has been declared ""STABILIZED"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability of technical requirements. New technology may exist. The last technical update of this document occured in May, 2006. Users of this document should refer any certification issues (e.g. exceptions listed on the certification

Steel, Corrosion and Resistant, Bars, Forgings, and Wire 17Cr 0.52Mo (0.95-1.20C) (SAE 51440C) For Bearing Applications

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)