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 extruded bars, rods, wire, profiles, and tubing. These extrusions have been used typically for structural parts requiring high strength up to 500 degrees F (260 degrees C), but usage is not limited to such applications. May be welded in the specified condition but properties are improved by reheat treatment after welding. Reheat treatment after welding, however, may reduce resistance to stress-corrosion cracking.
Aluminum Alloy@ Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T8511) Solution Treated@ Stress Relief Stretched@ Straightened@ and Precipitation Heat Treated (UNS A92219)
This specification covers an aluminum or aluminum alloy in the form of sheet, laminated and edge bonded.
Aluminum Sheet, Laminated, Edge Bonded
This specification covers the specific requirements for 7075 aluminum alloy bar, rod, wire, and special shapes produced by rolling, drawing, or cold finishing.
Aluminum Alloy 7075, Bar, Rod, Wire, and Special Shapes; Rolled, Drawn, or Cold Finished
This specification covers treated aluminum core material for structural sandwich construction.
Core Material, Aluminum, for Sandwich Construction
Aluminum Alloy Plate 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T7651) Solution Heat Treated, Stress Relieved, and Overaged
This specification covers aluminum in the form of sheet and plate.
Aluminum Sheet and Plate (1060-0)
Aluminum Alloy, Plate 1.6Cu - 2.2Mg - 0.22Cr - 5.7Zn (7475-T7651) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated
This SAE Aerospace Information Report (AIR) is intended to be used as a process verification guide for evaluating implementation of key factors in repair of metal bond parts or assemblies in a repair shop environment. This guide is to be used in conjunction with a regulatory approved and substantiated repair, and is intended to promote consistency and reliability.
Guidelines for Repair Process Evaluation of Aluminum Bonded Structure
Aerospace series - Aluminium alloy AL-P7175 - T73511 - Extruded bar and section - a or D <= 150 mm; German and English version EN 4293:2014
This specification covers a dilute aluminum/TiB2 metal matrix composite in the form of investment castings.
Cast Aluminum Alloy Composite 4.6Cu - 3.4Ti - 1.4B - 0.75Ag - 0.27Mg (205.0/TiB2/3p-T7P) Investment Cast, Solution and Precipitation Heat Treated
Aerospace series. Aluminium alloy AL-P7175. T73511. Extruded bar and section. a or D
Aluminum Alloy, Coiled Sheet; 4.4Cu - 1.5Mg - 0.60Mn (2024-T4); Solution Treated
This specification specifies the engineering requirements for heat treatment, by part fabricators (users) or their vendors or subcontractors, of parts (See 8.8.1). It also covers heat treatment by warehouses or distributors converting raw material from one temper to another temper (See 1.3 and 8.5). It covers the following aluminum alloys: 1100, 2004, 2014, 2017, 2024, 2098, 2117, 2124, 2219, 2224, 3003, 5052, 6013, 6061, 6063, 6066, 6951, 7049, 7050, 7075, 7149, 7178, 7249, 7475
Heat Treatment of Wrought Aluminum Alloy Parts
This European Standard specifies the requirements relating to: Aluminium alloy AL-P7175-T73511 Extruded bar and section a or D 150 mm for aerospace applications.
Aerospce series - Aluminium alloy AL-P7175 - T73511 - Extruded bar and section - a or D 150 mm
This specification covers the specific requirements for 7075 aluminum alloy alclad one side plate and sheet; the general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy (7075) core with a thin layer of an aluminum alloy (7072) anodic to the core bonded to one surface.
Aluminum 7075, Plate and Sheet, Alclad One Side
This specification covers the specific requirements for aluminum alloy 2014 bar, rod, shapes, tube, and wire produced by extrusion.
Aluminum Alloy 2014, Bar, Rod, Shapes, Tube, and Wire, Extruded
This specification covers the specific requirements for 7178 aluminum alloy, 7011 alclad, plate and sheet; the general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable 7178 aluminum alloy core with thin layers of a 7011 aluminum alloy anodic to the core and of approximately equal thickness, bonded to both surfaces.
Aluminum Alloy, 7011 Alclad 7178 Plate and Sheet
This specification covers the specific requirements for 7178 aluminum alloy plate and sheet material; the general requirements are covered in AMS-QQ-A-250.
Aluminum Alloy 7178, Plate and Sheet
This specification covers the specific requirements for improved exfoliation resistant alclad aluminum alloy 7178-T76 sheet and -T7651plate. The general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy (7178) core with thin layers of an aluminum alloy (7072) anodix to the core and of approximately equal thickness, bonded to both surfaces.
Aluminum Alloy, 7178-T76, Alclad Plate and Sheet, Improved Exfoliation Resistant
This specification covers the specific requirements for improved exfoliation-resistant aluminum alloy, 7178-T76 sheet and 7178-T7651 plate.
Aluminum Alloy, 7178-T76, Plate and Sheet Improved Exfoliation Resistant
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