Surface pre-treatment method for pre-coated heat-treatable, precipitation-hardenable stainless steel ferrous-alloy components and components coated thereby

a technology of precipitation hardening and stainless steel ferrous alloys, applied in the direction of superimposed coating process, transportation and packaging, synthetic resin layered products, etc., can solve the problems of not finding a single replacement coating or system that meets all engineering requirements, labor-intensive, time-consuming, and, consequently, very costly wet-sealant process, etc., to achieve the effect of improving compatibility or inter-relationship

Inactive Publication Date: 2004-08-26
THE BOEING CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0007] The present invention is related to the discovery that, by utilizing a particularly selected surface pre-treatment process for heat-treatable, precipitation-hardenable stainless steel ferrous-alloy components prior to applying a corrosion-inhibiting coating, a significantly improved, pre-determined, final coated condition can be achieved. This improved or enhanced final condition results from the improved compatibility or inter-relationship afforded by the pre-treatment process between the compositions of the subsequently applied protective coating and the component substrate yielding an improved pre-coated component.
[0008] More specifically, the present invention relates to the use, in a pre-treatment process, of a flash plating without a chromate seal as a surface treatment for a ferrous-alloy substrate prior to applying a corrosion-inhibiting coating to improve the overall corrosion protection of the pre-treatment process. Preferably the flash plating is either a cadmium flash plate or a zinc-nickel (Zn--Ni) alloy flash plate coating.

Problems solved by technology

These fasteners are often installed using a labor-intensive, time-consuming, and, consequently, very costly wet-sealant process.
However, cadmium is suspected of being a carcinogen and is a known toxic element.
Although several candidate coatings have been identified, no single replacement coating or system has been found that meets all of the engineering requirements.
However, it has been shown that, with respect to pre-coated components having different ferrous-alloy substrate materials, while the surrounding structural components are adequately protected to equivalent levels from corrosion attack, the coating itself that is applied to some of the components in known pre-coating processes may be adversely affected from an appearance standpoint and may interact to a degree that is visually perceptible.
Over a prolonged period of time, the possibility exists that the adverse effect of this interaction could not only manifest itself in the coating's visual appearance but may also have an effect on the coating's integrity, possibly leading to a compromised corrosion protection condition.

Method used

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  • Surface pre-treatment method for pre-coated heat-treatable, precipitation-hardenable stainless steel ferrous-alloy components and components coated thereby
  • Surface pre-treatment method for pre-coated heat-treatable, precipitation-hardenable stainless steel ferrous-alloy components and components coated thereby
  • Surface pre-treatment method for pre-coated heat-treatable, precipitation-hardenable stainless steel ferrous-alloy components and components coated thereby

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example

[0050] A comparative 2000 hour salt spray exposure test performed on A-286 stainless steel Hi-Set.RTM. fasteners having various surface preparation methods employed prior to the application of Hi-Kote.RTM. 1 aluminum pigmented coating. Hi-Kote.RTM. 1 is a phenolic resin-based aluminum coating as described above, and has been demonstrated to possess excellent corrosion protection when subjected to 2000-hour salt spray corrosion evaluations, as well as high temperature resistance (to 400.degree. F.), excellent resistance to fuel, hydraulic fluids, solvents when applied on a wide variety of metallic surfaces.

[0051] The salt spray evaluation testing was performed in accordance with ASTM B117 apparatus and standard test method procedures. Aluminum-alloy test speciment assemblies, each containing six fastener installations, were placed at a 15-degree angle to the horizontal inside the salt spray test chamber for a period of 2000 hours.

[0052] All fasteners used in the evaluation were selec...

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Abstract

The present invention relates to the use, in a pre-coating process, of a flash plating, without a subsequent chromate seal, as a surface pre-treatment for a ferrous-alloy substrate prior to applying a corrosion-inhibiting coating to improve the overall corrosion protection of the pre-treatment component. Preferably the ferrous alloy is a heat-treatable, precipitation-hardenable stainless steel and the pre-treatement is a cadmium flash plate or a zinc-nickel alloy flash plate.

Description

[0001] This invention relates to the preparation of pre-coated ferrous-alloy components. More particularly, the present invention relates to the use of a surface preparation as a preliminary step in a pre-coating process to improve the corrosion protection and other properties of coated ferrous-alloy components.[0002] Aircraft manufacturers use a variety of different ferrous and non-ferrous metals in the fabrication of aircraft components. Commonly assigned U.S. Pat. No. 5,614,037 discloses a method for pre-treating aluminum and aluminum-alloy articles to obviate the use of wet sealants and other coatings for protection against corrosion damage.[0003] Ferrous alloys such as carbon steels and aircraft-quality low-alloy stainless steels, such as, for example, Aermet 100, HY-TUF.TM., 300M, H-11, HP9-4-30, 52100, 1095, 4130, 4135, 4140, 4330V, 4340, 6150, 8740, 18-8, 17-4PH, 17-7PH, 15-5PH, PH 13-8Mo, PH 15-7Mo, A-286, etc. are often used as primary structural aircraft components. Typic...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): B05D3/02B05D7/14C21D6/00C23C26/00C23C28/00C25D5/48
CPCB05D3/0254B05D7/14B05D2350/65C21D6/004C23C26/00Y10T428/12799C25D5/48Y02T50/67Y10T428/12785Y10T428/12549Y10T428/12569C23C28/00Y10T428/31688Y10T428/31678Y02T50/60
Inventor KEENER, STEVEN G.MENDOZA, MICHAEL A.
Owner THE BOEING CO
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