共找到 1417 条与 铝 相关的标准,共 95 页
This specification covers an aluminum alloy in the form of sheet.This sheet has been used typically for structural parts requiring the strength of 2024-T3 and lower density, but usage is not limited to such applications.
Aluminum Alloy, Sheet 2.4Li - 1.3Cu - 0.95Mg - 0.10Zr (8090-T6) Solution and Precipitation Heat Treated (Unrecrystallized)
This specification covers the specific requirements for 2024 aluminum alloy plate and sheet; the general requirements are covered in AMS-QQ-A-250.
Aluminum Alloy 2024, Plate and Sheet
This specification covers an aluminum alloy in the form of hand forgings up to 6 inches (152 mm) inclusive, in nominal as-forged thickness and having a cross-sectional area of not more than 156 square inches (1006 cm2) (See 8.6).
Aluminum Alloy@ Hand Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7452) Solution Heat Treated@ Stress Relieved@ and Precipitation Heat Treated (UNS A97075)
This specification covers an aluminum alloy in the form of plate up to 5.500 inches (139.70 mm), inclusive in thickness (See 8.4).
Aluminum Alloy@ Plate 6.2Zn - 1.8Cu - 2.4Mg - 0.13Zr (7010-T7451) Solution Heat Treated@ Stress Relieved@ and Precipitation Heat Treated (UNS 97010)
Aerospace series - Aluminium alloy AL-P2024 - Al Cu4Mg1 - T351 - Plate - 6 mm < a <= 150 mm; German and English version EN 4725:2014
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing with a nominal diameter or least thickness (wall thickness of tubing) up to 5.000 inches, inclusive.
Aluminum Alloy@ Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7049-T76511) Solution Heat Treated@ Stress Relieved@ Straightened@ and Overaged (UNS A97049)
This specification covers aluminum-beryllium powders consolidated by hot isostatic pressing (HIP) into the form of bar, rod, tubing, and shapes.
Aluminum Beryllium@ Preforms Hot Isostatic Pressed and Heat Treated 38Al - 62Be
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing up to 32 square inches (206 square cm) in area.
Aluminum Alloy@ Extrusions 4.5Cu - 0.85Si - 0.80Mn - 0.50Mg (2014-T6) Solution and Precipitation Heat Treated (UNS A92014)
This specification covers an aluminum alloy in the form of extruded profiles such as angles, channels, tees, zees, I-beams, and H-beams.These products have been used typically for parts requiring moderate strength, especially where such parts require brazing or welding during fabrication, but usage is not limited to such applications.
Aluminum Alloy@ Extruded Profiles 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-T6) Solution and Precipitation Heat Treated (UNS A96061)
This specification covers an aluminum alloy in the form of sheet from 0.020 to 0.249 inch (0.51 to 6.32 mm), inclusive, in thickness (See 8.5).
Aluminum Alloy Sheet 1.0Mg - 0.8Si - 0.8Cu - 0.5Mn (6013-T4) Solution Heat Treated and Naturally Aged (UNS A96013)
This specification covers an aluminum alloy in the form of die forgings, hand forgings, and forging stock.
Aluminum Alloy Forgings 7.7Zn - 2.5Mg - 1.5Cu - 0.16Cr (7049-T73) Solution and Precipitation Heat Treated (UNS A97049)
This specification covers an aluminum alloy in the form of die forgings and forging stock ordered to inch/pound units. These forgings have been used typically for parts requiring good resistance to stress-corrosion cracking but with lower strength than AMS4126, but usage is not limited to such applications.
Aluminum Alloy Die Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T73) Solution and Precipitation Heat Treated (UNS A97075)
This specification covers an aluminum alloy in the form of plate. This plate has been used typically for parts requiring a high level of mechanical properties and good resistance to stress-corrosion cracking, but usage is not limited to such applications.
Aluminum Alloy@ Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7451) Solution Heat Treated@ Stress Relieved@ and Overaged (UNS A97050)
Aerospace series - Aluminium alloy AL-P7175 - T7351 - Plate - 6 mm < a <= 100 mm; German and English version EN 2512:2014
Aerospace series. Aluminium alloy AL-P2024- Al Cu4Mg1. T351. Plate. 6 mm $2J a
This specification covers an aluminum alloy in the form of sheet and plate.
Aluminum Alloy@ Sheet and Plate 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061-O) Annealed (UNS A96061)
This European Standard specifies the requirements relating to: Aluminium alloy AL-P2024- Al Cu4Mg1 T351 Plate 6 mm < a
Aerospace series - Aluminium alloy AL-P2024- Al Cu4Mg1 - T351 - Plate - 6 mm < a ��150 mm
Aerospace series. Aluminium alloy AL-P7175. T7351. Plate. 6mm a
This specification covers the specific requirements for aluminum alloy 7075 bar, rod, shapes, tube, and wire produced by extrusion. AMS-QQ-A-200/11A has been declared "STABILIZED" by AMS Committee D. This document will no longer be updated and may no longer represent standard industry practice. This document was stabilized because it contains requirements that are no longer state of the art and are also contained in alternate documents that contain equivalent requirements. Previously this document was reaffirmed. AMS Committee D has never performed a technical update of this document. Users of this document should refer to the cognizant engineering organization for disposition of any issues with reports/certifications to this specification; including exceptions listed on the certification. NOTE: In many cases, the purchaser may represent a sub tier supplier and not the cognizant engineering organization.
Aluminum Alloy 7075, Bar, Rod, Shapes, Tube, and Wire, Extruded
This European Standard specifies the requirements relating to: Aluminium alloy AL-P7175-T7351 Plate 6 mm < a
Aerospace series - Aluminium alloy AL-P7175 - T7351 - Plate - 6mm < a ��100 mm
Copyright ©2007-2022 ANTPEDIA, All Rights Reserved
京ICP备07018254号 京公网安备1101085018 电信与信息服务业务经营许可证:京ICP证110310号