V11 航空与航天用金属铸锻材料 标准查询与下载
共找到 5951 条与 航空与航天用金属铸锻材料 相关的标准，共 397 页
This specification covers steel in the form of laminated sheet. This material has been used typically for shims in which thickness is adjusted by removal of laminations as required, but usage is not limited to such applications.
Steel, Carbon, Laminated Sheet, Surface Bonded
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2013-02-07
- 实施
This specification covers a corrosion and heat-resistant, work strengthened and aged cobalt-nickel-chromium alloy in the form of bars 2 inches (50.8 mm) and under in nominal diameter. These bars have been used typically for parts, such as fasteners, requiring a room temperature minimum tensile strength of 170 ksi (1172 MPa) for use up to 850 °F (454 °C) in applications requiring high ductility to promote toughness and resistance to cracking under shock loading conditions, but usage is not limited to such applications. This alloy exhibits exceptionally good resistance to corrosion, crevice corrosion, and stress-corrosion cracking.
Cobalt-Nickel Alloy, Corrosion and Heat-Resistant, Round Bars 19Cr 36Co 25Ni 7.0Mo 0.50Cb (Nb) 2.9Ti 0.20Al 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated, Work Strengthened and Aged, Modified Strength
- ICS
- 49.025.99
- CCS
- V11
- 发布
- 2013-02-07
- 实施
This specification covers a corrosion and heat-resistant, work strengthened cobalt-nickel-chromium alloy in the form of bars 2 inches (50.8 mm) and under in nominal diameter. These bars have been used typically for parts, such as fasteners, requiring a room temperature minimum tensile strength of 170 ksi (1172 MPa) for use up to 850 °F (454 °C) in applications requiring high ductility to promote toughness and resistance to cracking under shock loading conditions, but usage is not limited to such applications. This alloy exhibits exceptionally good resistance to corrosion, crevice corrosion, and stress-corrosion cracking.
Cobalt-Nickel Alloy, Corrosion and Heat-Resistant, Round Bars 19Cr 36Co 25Ni 7.0Mo 0.50Cb (Nb) 2.9Ti 0.20Al 9.0Fe Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated and Work Strengthened, Modificed Strength
- ICS
- 49.025.99
- CCS
- V11
- 发布
- 2013-02-07
- 实施
This specification covers a copper-beryllium alloy in the form of bars and rods. These products have been used typically for parts requiring a combination of high strength, wear resistance, and corrosion resistance, and where thermal conductivity, electrical conductivity and low magnetic susceptibility may be important, but usage is not limited to such applications.
Copper-Beryllium Alloy, Bars and Rods 98Cu 1.9Be Solution Heat Treated, Cold Worked, and Precipitation Heat Treated (TH04, formerly HT)
- ICS
- 49.025.99
- CCS
- V11
- 发布
- 2013-02-07
- 实施
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Steel Bars, Forgings and Tubing 1.75 Cr 4.0 Ni 0.5 Mo (0.35-0.40 C) Premium Aircraft Quality Consumable Electrode Vacuum Remelted
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2013-02-07
- 实施
This specification covers an aluminum alloy in the form of die forgings, hand forgings, rolled rings, and forging stock. These products have been used typically for rotating parts operating in service up to 450 °F (232 °C) and other parts operating up to 600 °F (316 °C) at low stresses, but usage is not limited to such applications.
Aluminum Alloy, Die and Hand Forgings, Rolled Rings, and Forging Stock 2.3Cu 1.6Mg 1.1Fe 1.0Ni 0.18Si 0.07Ti (2618-T61) Solution and Precipitation Heat Treated
- ICS
- 49.025.20
- CCS
- V11
- 发布
- 2013-02-07
- 实施
This specification covers one type of copper-beryllium alloy in the form of bars, rods, forgings, and forging stock. These products have been used typically for parts requiring a combination of high strength, good wear resistance, and corrosion resistance and where electrical conductivity or low magnetic susceptibility may be important, but usage is not limited to such applications.
Copper-Beryllium Alloy, Bars, Rods, Shapes, and Forgings 98Cu 1.9Be Solution Heat Treated TB00 (A)
- ICS
- 49.025.99
- CCS
- V11
- 发布
- 2013-02-07
- 实施
Aerospace series - Welded and brazed assemblies for aerospace construction - Joints of metallic materials by electron beam welding - Part 001: quality of welded assemblies
- ICS
- 25.160.40;49.035
- CCS
- V11
- 发布
- 2013-02-02
- 实施
- 2013-02-02
This European Standard specifies the requirements relating to: Steel X4CrNiMo16-5-1 (1.4418) Air melted Hardened and tempered Bar De
Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ��200 mm - 1 150 MPa ��Rm ��1 300 MPa
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2013-02-01
- 实施
- 2013-02-01
This European Standard specifies the requirements relating to: Steel X4CrNiMo16-5-1 (1.4418) Air melted Softened Forging stock De
Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Softened - Forging stock - De ��300 mm
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2013-02-01
- 实施
- 2013-02-01
This European Standard specifies the requirements relating to: Steel X4CrNiMo16-5-1 (1.4418) Air melted Hardened and tempered Bar De
Aerospace series - Steel X4CrNiMo16-5-1 (1.4418) - Air melted - Hardened and tempered - Bar - De ��200 mm - 900 MPa ��Rm ��1 050 MPa
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2013-02-01
- 实施
- 2013-02-01
Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Bar and wire for forged fasteners. De
- ICS
- 49.025.30
- CCS
- V11
- 发布
- 2013-01-31
- 实施
- 2013-01-31
Aerospace series. Metallic materials. Test methods. Sharp edge-notch tensile testing for sheet and strip
- ICS
- 49.025.05;49.025.15
- CCS
- V11
- 发布
- 2013-01-31
- 实施
- 2013-01-31
Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Bar. a or D
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2013-01-31
- 实施
- 2013-01-31
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Steel Bars, Forgings, and Tubing 1.0Cr 3.2Ni 0.2Mo (0.12 - 0.17C) Premium Aircraft-Quality Double Vacuum Melted
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2013-01-22
- 实施
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 establishes maximum permissible limits for elements not normally specified but which may occur in trace amounts in wrought nickel, cobalt, and iron alloy products. Control provided by this specification has been used typically for highly-stressed rotating parts, such as turbine discs, where control of trace elements is required to maitain elevated-temperature tensile, stress-rupture, creep, and low-cycle
Trace Element Control Nickel Alloy, Cobalt Alloy, and Iron Alloy Wrought Products for High-Temperature, High-Stressed Applications
- ICS
- 49.025.99
- CCS
- V11
- 发布
- 2013-01-17
- 实施
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock
Steel, Corrosion-Resistant, Bars, Wire, and Forgings 10Cr 12Ni 2Mo 1.45Al 1.15Ti Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated, Precipitation Hardenable
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2013-01-10
- 实施
本标准规定了高强度铁磁性钢制零件热损伤的巴克豪森的一般要求和详细要求。本标准适用于高强度钢磨削后以及对涂/镀层磨削后所产生的基体金属热损伤的检测,也可用于在役产生的热损伤的检测。本标准不适用于有镀镍层的高强度钢制零件热损伤的检测。
Barkhausen inspection for thermal damage of high-strength steel
- ICS
- CCS
- V11
- 发布
- 2013-01-04
- 实施
- 2013-05-01
本规范规定了航空用GH2901、GH4169、GH 4500高温合金轴锻件的要求、质量保证规定和交货准备等。本规范适用于航空用高温合金轴锻件(以下简称锻件)。
Specification for superalloy shaft forgings for aviation
- ICS
- CCS
- V11
- 发布
- 2013-01-04
- 实施
- 2013-05-01
本规范规定了钛及钛合金熔模精密铸件的要求、质量保证规定、交货准备等。本规范适用于航空用钛及钛合金熔模精密铸件。
Specificatiaon for titanium and titanium alloy investment castings
- ICS
- CCS
- V11
- 发布
- 2013-01-04
- 实施
- 2013-05-01
