49.025.99 其他材料 标准查询与下载



共找到 1040 条与 其他材料 相关的标准,共 70

This specification covers a magnesium alloy in the form of sand castings. These castings have been used typically for parts requiring high yield strength up to 570 degrees F (299 degrees C) and excellent corrosion resistance, but usage is not limited to such applications.

Castings, Sand, Magnesium Alloy 5.1Y - 3.0Re - 0.70Zr (WE54 - T6) Solution and Precipitation Heat Treated

ICS
49.025.99
CCS
发布
2013-09-18
实施

This specification covers a magnesium alloy in the form of permanent mold castings.

Magnesium Alloy Castings, Permanent Mold, 9.0Al - 2.0Zn (AZ92A-T6), Solution and Precipitation Heat Treated

ICS
49.025.99
CCS
发布
2013-09-18
实施

This specification covers a magnesium alloy in the form of rolled plate. This product has been used typically for parts requiring a combination of light weight, high yield strength up to 480 °F (250 °C), relatively high corrosion resistance, and good flammability resistance for magnesium alloys,but usage is not limited to such applications.

Magnesium Alloy, Plate, 4.0Y - 2.25Nd - 0.5Zr (WE43C - T5), Precipitation Heat Treated

ICS
49.025.99
CCS
V16
发布
2013-08-12
实施

Aerospace series - Non-metallic materials - Glass transparencies - Test methods - Determination of modulus of rupture; German and English version EN 3864:2013

ICS
49.025.99
CCS
V13
发布
2013-08-01
实施

Aerospace series - Non-metallic materials - Glass transparencies - Material standard - Thermally tempered soda lime float glass

ICS
49.025.99
CCS
V13
发布
2013-07-26
实施
2013-07-26

Aerospace series - Non-metallic materials - Glass transparencies - Test methods - Determination of flatness

ICS
49.025.99
CCS
V13
发布
2013-07-12
实施
2013-07-12

Aerospace series - Non-metallic materials - Glass transparencies - Test methods - Determination of ream and surface ripple

ICS
49.025.99
CCS
V13
发布
2013-07-12
实施
2013-07-12

This European Standard defines the requirements for the determination of the modulus of rupture of glass transparencies for aircraft applications, whether in the annealed or chemically or thermally tempered condition.

Aerospace series - Non-metallic materials - Glass transparencies - Test methods - Determination of modulus of rupture

ICS
49.025.99
CCS
发布
2013-07-12
实施
2013-07-12

Aerospace series - Non-metallic materials - Glass transparencies - Material standard - Chemically tempered soda lime float glass

ICS
49.025.99
CCS
V13
发布
2013-07-12
实施
2013-07-12

This specification covers a corrosion and heat resistant nickel alloy in the form of welding wire. This wire has been used typically as filler metal for gas-tungsten-ar or gas-metal-arc welding of corrosion and heat resistant nickel alloys of similar composition where the weld area is required to have strength and corrosion resistance comparable to those of the base metal, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Welding Wire 50Ni 20Cr 20Co 5.9Mo 2.2Ti 0.45Al Consumable Electrode or Vacuum Induction Melted

ICS
49.025.99
CCS
V11
发布
2013-07-10
实施

Aerospace series. Non-metallic materials. Glass transparencies. Test methods. Determination of modulus of rupture

ICS
49.025.99
CCS
V13
发布
2013-06-30
实施
2013-06-30

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, extrusions, flash welded rings, and stock for forging or flash welded rings. These products have been used for parts requiring both corrosion and oxidation resistance up to 2000 degrees F (1093 degrees C) and where such parts may require welding during fabrication, but usage is not limited to such applications.

Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, Extrusions, and Rings 62Ni 21.5Cr 9.0Mo 3.65Cb (Nb) Annealed

ICS
49.025.99
CCS
V11
发布
2013-06-05
实施

This standard describes the accepted methods used for preparing aerospace sealant test specimens for qualification and quality conformance or acceptance testing. AS5127/1 and AS5127/2 are to be used in conjunction with this document and the applicable AMS specifications.

Aerospace Standard Test Methods for Aerospace Sealants Methods for Preparing Aerospace Sealant Test Specimens

ICS
49.025.99
CCS
V13
发布
2013-05-30
实施

This specification covers the engineering requirements for producing brazed joints in parts fabricated from steels, iron alloys, nickel alloys, cobalt alloys, and copper alloys by use of silver alloys, and the properties of such joints. This procedure has been used typically for joints requiring high strength up to 400 °F (204 °C), but usage is not limited to such applications.

Brazing, Silver For Use Up to 400°F (204°C)

ICS
49.025.99
CCS
J33
发布
2013-05-29
实施

This specification covers a columbium (niobum) alloy in the form of sheet, strip, and plate. This material has been used typically for parts requiring exposure at ultra-high temperatures, but usage is not limited to such applications. Applications in oxidizing atmospheres necessitate a protective coating.

Columbium (Niobium) Alloy Sheet, Strip, and Plate, 10Hf 1.0Ti

ICS
49.025.99
CCS
V11
发布
2013-05-23
实施

This specification cover as columbium alloy in the form of bars, rods, or wire. This material has been used typically for parts requiring exposure at ultra-high temperatures, but usage is not limited to such applications. Applications in oxidizing atmospheres necessitate a protective coating.

Columbium (Niobium) Alloy Bars, Rods, and Wire 10W 2.5Zr Recrystallized

ICS
49.025.99
CCS
V11
发布
2013-05-23
实施

This specification covers a columbium (niobium) alloy in the form of foil, sheet, strip, or plate. This material has been used typically for parts requiring exposure at ultra-high temperatures, but usage is not limited to such applications. Applications in oxidizing atmospheres necessitate a protective coating.

Columbium (Niobium) Alloy Foil, Sheet, Strip and Plate, 10W 2.5Zr Recrystallized

ICS
49.025.99
CCS
V11
发布
2013-05-23
实施

This specification covers the requirements for qualification, requalification, and certification of etch inspectors.

Qualification and Certification of Etch Inspectors

ICS
49.025.99
CCS
A18
发布
2013-05-09
实施

This European Standard defines the requirements for the determination of the modulus of rupture of glass transparencies for aircraft applications, whether in the annealed or chemically or thermally tempered condition.

Aerospace series - Non-metallic materials - Glass transparencies - Test methods - Determination of modulus of rupture

ICS
49.025.99
CCS
V13
发布
2013-05-01
实施
2013-05

Aerospace series - Sealants - Test methods - Determination of low-temperature flexibility; German and English version EN 3102:2013

ICS
49.025.99
CCS
V13
发布
2013-05
实施



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