49.025.20 铝 标准查询与下载

DS/EN 4001:2007 航空航天系列 铝合金 AL-P2024-T351 具有改进的化学铣削能力的复合板材和钢带 1,6 mm <= a <= 6 mm

This standard specifies the requirements relating to:Aluminium alloy AL-P2024-T351 - Clad sheet and strip with improved chemical milling capability 1,6 mm

Aerospace series - Aluminium alloy AL-P2024-T351 - Clad sheet and strip with improved chemical milling capability 1,6 mm <= a <= 6 mm

DS/EN 4006:2007 航空航天系列 铝合金 AL-P6082-T4 或 T42 板材和带材 0.4 mm <= a <= 6 mm

This standard specifies the requirements relating to:Aluminium alloy AL-P6082-T4 or T42 - Sheet and strip 0,4 mm

Aerospace series - Aluminium alloy AL-P6082-T4 or T42 - Sheet and strip 0,4 mm <= a <= 6 mm

DS/EN 4005:2007 航空航天系列 铝合金 AL-P5052-O 板材和带材 0,3 mm <= a <= 6 mm

This standard specifies the requirements relating to:Aluminium alloy AL-P5052-O - Sheet and strip 0,3 mm

Aerospace series - Aluminium alloy AL-P5052-O - Sheet and strip 0,3 mm <= a <= 6 mm

DS/EN 3998:2007 航空航天系列 铝合金 AL-P2024-T4 或 T42 板材和带材 0,3 mm <= a <= 6 mm

This standard specifies the requirements relating to:Aluminium alloy AL-P2024-T4 or T42 - Sheet and strip 0,3 mm

Aerospace series - Aluminium alloy AL-P2024-T4 or T42 - Sheet and strip 0,3 mm <= a <= 6 mm

DS/EN 4004:2007 航空航天系列 铝合金 AL-P3103-H16 板材和带材 0,4 mm <= a <= 6 mm

This standard specifies the requirements relating to:Aluminium alloy AL-P3103-H16 Sheet and strip 0,4 mm

Aerospace series - Aluminium alloy AL-P3103-H16 - Sheet and strip 0,4 mm <= a <= 6 mm

LST EN 3339-2007 航天系列 铝合金 AL-P7010-T76 模锻件

Aerospace series - Aluminium alloy AL-P7010-T76 - Die forgings - a ? 200 mm

DS/EN 3997:2007 航空航天系列 铝合金 AL-P2024-T3 板材和带材 0,4 mm < a < 6 mm

This standard specifies the requirements relating to:Aluminium alloy AL-P2024-T3 - Sheet and strip 0,4 mm < a < 6 mm for aerospace application.

Aerospace series - Aluminium alloy AL-P2024-T3 - Sheet and strip 0,4 mm < a < 6 mm

SAE AMS4013F-2007 表面粘结的叠层铝薄板

This specification covers aluminum and aluminum alloy foil in the form of laminated sheet. This product has been used typically for shims in which thickness is to be adjusted by removal of laminations as required, but usage is not limited to such applications.

Aluminum Sheet, Laminated Surface Bonded

SAE AMS4306B-2007 老化、应力释放和溶解热处理的6.4Zn 2.4Mg 2.2Cu 0.12Zr铝合金板材(7150 - T6151)

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 moderate resistance to exfoliation corrosion, but usage is not limited to such applications. Certain design and processing may cause this plate to become susceptible to stress-corrosion cracking: ARP 823 recommends practices to minimize such conditions.

Aluminum Alloy, Plate 6.4Zn - 2.4Mg - 2.2Cu - 0.12Zr (7150-T6151) Solution Heat Treated, Stress Relieved, and Aged UNS A97150

SAE AMS4157D-2007 7.7Zn 2.4Mg 1.6Cu 0.16Cr (7049-T73511)溶解热处理、应力释放和过度老化的铝合金挤压品

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, shapes, and tubing. These products have been used typically for parts in structural applications requiring a combination of high strength and good stress-corrosion resistance, but usage is not limited to such applications.

Aluminum Alloy Extrusions 7.7Zn - 2.4Mg - 1.6Cu - 0.16Cr (7049-T73511) Solution Heat Treated, Stress Relieved, and Overaged UNS A97049

SAE AMS4406-2007 溶解和沉淀热处理的热均衡压力下5.6Zn 2.5Mg 1.6Cu 0.23Cr (709.0-T61)离心铝合金铸件

This specification covers an aluminum alloy in the form of centrifugal castings. These products have been used typically for applications requiring high strength in light-to-medium sections and where dimensional stability is required during machining, but usage is not limited to such applications. Certain design and processing procedures may cause these castings to become susceptible to stress-corrosion cracking.

Aluminum Alloy, Centrifugal Castings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (709.0-T61) Hot Isostatically Pressed, Solution and Precipitation Heat Treated

SAE AMS4100D-2007 5.7Zn 2.2Mg 1.6Cu 0.22Cr(硬铝合金7475-T761)溶解热处理和沉淀热处理的镀铝合金薄板材

This specification covers an aluminum alloy in the form of alclad sheet. This sheet has been used typically for structural applications requiring material with high strength and resistance to exfoliation-corrosion, moderate fatigue strength, and high fracture toughness, but usage is not limited to such applications.

Aluminum Alloy, Alclad, Sheet 5.7Zn 2.2Mg 1.6Cu 0.22Cr (Alclad 7475-T761) Solution and Precipitation Heat Treated

SAE AMS4408-2007 铝合金厚板材(7140-T7651)

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 moderate resistance to stress-corrosion cracking, but usage is not limited to such applications.

Aluminum Alloy, Plate (7140-T7651) 6.6Zn - 1.8Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved, and Overaged UNS A97140

SAE AMS4045J-2007 5.6Zn 2.5Mg 1.6Cu 0.23Cr 7075(-T6薄板材、-T651厚板材)溶解和沉淀热处理的铝合金薄板材和厚板材

This specification covers an aluminum alloy in the form of sheet and plate. These products have been used typically for structural components, including machined parts subject to excessive warpage during maching, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

Aluminum Alloy Sheet and Plate 5.6Zn 2.5Mg 1.6Cu 0.23Cr 7075: (-T6Sheet, -T651 Plate) Solution and Precipitation Heat Treated

SAE AMS2772D-2007 铝合金原料的热处理

This specification covers requirements and recommendations for the heat treatment of wrought aluminum alloy raw materials by producers. It supersedes AMS-H-6088 and replaces MIL-H-6088. Aluminum alloy tempers are described in SAE AS1990 and ANSI H35.1 This specification may be used for alloys other than those specified herein providing temperatures, times, and quenchant are specified.

Heat Treatment of Aluminum Alloy Raw Materials

BS EN 3998:2007 航空航天系列.AL-P2024-T4或T42型铝合金.薄板材和带材.0.3mm≤a≤6mm

This standard specifies the requirements relating to: Aluminium alloy AL-P2024-T4 or T42 — Sheet and strip 0,3 mm ≤ a ≤ 6 mm for aerospace application.

Aerospace series - Aluminium alloy AL-P2024-T4 or T42 - Sheet and strip - 0,3 mm a 6 mm

BS EN 3997:2007 航空航天系列.AL-P2024-T3型铝合金.薄板材和带材.0.4mm≤a≤6mm

This standard specifies the requirements relating to: Aluminium alloy AL-P2024-T3 — Sheet and strip 0,4 mm ≤ a ≤ 6 mm for aerospace application.

Aerospace series - Aluminium alloy AL-P2024-T3 - Sheet and strip 0,4 mm $3Q a $3Q 6 mm

BS EN 4004:2007 航空航天系列.AL-P3103-H16型铝合金.薄板材和带材.0.4mm≤a≤6mm

This standard specifies the requirements relating to: Aluminium alloy AL-P3103-H16 — Sheet and strip 0,4 mm ≤ a ≤ 6 mm for aerospace applications.

Aerospace series - Aluminium alloy AL-P3103-H16 - Sheet and strip - 0,4 mm a 6 mm

SAE AMS4303B-2007 溶液热处理, 冷加工和老化的2.7Cu - 2.2Li - 0.12Zr (2090-T81) 铝合金板

This specification covers an aluminum alloy in the form of plate.

Aluminum Alloy Plate, 2.7Cu - 2.2Li - 0.12Zr (2090-T81), Solution Heat Treated, Cold Worked, and Aged

SAE AMS-QQ-A-200/14A-2007 耐改性剥蚀的7178-T76挤压制的铝合金棒材, 杆材, 型材以及线材

This specification covers the specific requirements for aluminum alloy 7178-T76 bar, rod, shapes, and wire produced by extrusion.

Aluminum Alloy, Bar, Rod, Shapes, and Wire, Extruded, 7178-T76, Improved Exfoliation Resistance