49.040 有关航空航天制造用镀涂和有关工艺 标准查询与下载
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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 has been declared ""CANCELLED"" by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been ""CANCELLED"". This specification covers a zinc chromate primer in the form of a liquid. This product has been used typically as a protective coating on metals and
Primer, Zinc Chromate
- ICS
- 49.040
- CCS
- 发布
- 2013-07-22
- 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 has been declared ""CANCELLED"" by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been ""CANCELLED"".
Paint Vehicle, Glyceryl Phthalate
- ICS
- 49.040
- CCS
- 发布
- 2013-07-22
- 实施
This specification covers a coating consisting of finely-powdered graphite in a heat-resistant inorganic binder. This coating has been used typically on metal parts and selected nonmetallic materials requiring a coating less than 0.0001 inch (2.5 um) thick for reducing wear or minimizing galling, but usage is not limited to such applications.
Graphite Coating, Thin Lubricating Film Impingement Applied
- ICS
- 49.040
- CCS
- V13
- 发布
- 2013-07-10
- 实施
This specification establishes the for anodic coatings on aluminum alloys. This process has been used typically to increase corrosion resistance and to provide surfaces which will promote adherence of paint and other organic finishes, and has been found useful for assemblies which have faying surfaces and/or which may trap electrolyte, but usage is not limited to such applications. This process is primarily applicable to aluminum and aluminum alloy parts which have nominal copper content not greater than 5% by weight or total nominal alloy content not greater than 7.5% by weight, AMS 2471 being recommended for parts having higher alloy content. Coating may
Anodic Treatment of Aluminum Alloys, Chromic Acid Process
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-07-09
- 实施
Electroless Nickel Plating Low Phosphorus
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-06-21
- 实施
This specification covers the requirements for inducing compressive residual stresses on the surface of metal parts using ultrasonically activated shot peening. Ultrasonically activated shot peening is typically used to induce compressive residual stresses on the surface layer of metallic parts to a depth up to 0.040 inch (1 mm). The shape and depth of the compressive residual stress distribution depend on the properties of the part and the ultrasonically activated shot peening process parameters. The residual stresses produced increase fatigue performance, resistance to stress-corrosion cracking, corrosion fatigue, and fretting fatigue, but its usage is no
Shot Peening, Ultrasonically Activated
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-06-11
- 实施
This specification establishes the engineering requirements for producing thick coatings of polytetrafluoroethylene (PTFE) resin on parts and the properties of such coatings. Primarily to provide dry lubrication, high heat stability, and corrosion protection on parts which operate at not higher than 527 degrees F (275 degrees C) for limited periods or not higher than 473 degrees F (245 degrees C) for extended periods. This coating is usually smoother than that of AMS 2515. This coating may also be used as a release film for molds.
Polytetrafluoroethylene (PTFE) Resin Coating, High Build, 698-752°F (370-400°C) Fusion
- ICS
- 49.040
- CCS
- V13
- 发布
- 2013-03-21
- 实施
This specification covers the requirements for electrodeposited chromium plating.
Plating, Chromium
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-03-12
- 实施
Aerospace series - Tartaric-Sulphuric-Acid anodizing of aluminium and aluminium wrought alloys for corrosion protection and paint pre-treatment (TSA)
- ICS
- 49.040
- CCS
- V13
- 发布
- 2013-03-06
- 实施
- 2013-03-06
Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Subsonic erosion resistance; German and English version EN 4595:2013
- ICS
- 49.040
- CCS
- V13
- 发布
- 2013-03
- 实施
Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Supersonic erosion resistance; German and English version EN 4594:2013
- ICS
- 49.040
- CCS
- V13
- 发布
- 2013-03
- 实施
This specification covers the requirements for electrodeposition of zinc plating. This process has been used typically to provide corrosion resistance to metal parts, but usage is not limited to such applications. Unless otherwise stated on the engineering drawing, high strength steel parts having a hardness of 45 HRC or greater shall not be electroplated to this document.
Plating, Zinc
- ICS
- 49.040
- CCS
- V11
- 发布
- 2013-02-20
- 实施
Surface treatments - Codes for standard item part numbers and use
- ICS
- 49.040
- CCS
- V22
- 发布
- 2013-02-16
- 实施
- 2013-02-16
Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Supersonic erosion resistance
- ICS
- 49.040
- CCS
- 发布
- 2013-02-15
- 实施
- 2013-02-15
Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Subsonic erosion resistance
- ICS
- 49.040
- CCS
- 发布
- 2013-02-15
- 实施
- 2013-02-15
This specification covers the engineering requirements for cadmium deposited on ferrous metals. This process has been used typically to provide corrosion resistance to steel parts heat treated to tensile strength of 180 ksi (1240 MPa) and higher and used at temperatures not higher than 450 °F (232 °C), but usage is not limited to such applications.
Plating, Cadmium, Low Hydrogen Content Deposit
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-02-15
- 实施
This standard specifies the requirements for a two component polyurethane, topcoat, with a medium degree ofresistance to erosion by the effects of rain, available in a range of colours and levels of gloss, to be appliedover a primer for aerospace applicat
Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Subsonic erosion resistance
- ICS
- 49.040
- CCS
- 发布
- 2013-02-15
- 实施
- 2013-02-15
This standard specifies the requirements for a two component polyurethane, topcoat, with a medium degree ofresistance to erosion by the effects of rain, available in a range of colours and levels of gloss, to be appliedover a primer for aerospace applicat
Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Supersonic erosion resistance
- ICS
- 49.040
- CCS
- 发布
- 2013-02-15
- 实施
- 2013-02-15
This specification covers the requirements for electrodeposited cadmium on metal parts. This process has been used typically to provide corrosion resistance to metal parts, but usage is not limited to such applications.
Plating, Cadmium
- ICS
- 49.040
- CCS
- V18
- 发布
- 2013-02-11
- 实施
The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification, AMS 2431.
Peening Media, Ceramic Shot
- ICS
- 49.040
- CCS
- V13
- 发布
- 2013-02-07
- 实施
