EP0903422A1

Coating parent bore metal of engine blocks

Abstract

A method of fluxing a cast light-weight metal substrate for thermally adhering sprayed metallic coatings thereto, comprising: (a) preparing the substrate to be clean of grease and oil and to have a uniform and homogeneous surface energy; (b) electrostatically depositing a dry flux powder coating onto such prepared surface; and © thermally depositing melted metal onto and across the flux coated surface to further thermally activate the flux if not already activated, for stripping away any substrate oxides and to thermally metallurgically bond the deposited molten metal to the substrate.

EP0903422A1, drawing sheet 1
Sheet 1 of 5

Term

Term ended

Projected expiry passed 31 December 2017, 8.7 years ago.

  1. Priority
  2. Filed
  3. Published
  4. Projected expiry
  5. Today

10 claims: 4 independent, 6 dependent

  1. 1
    A method of fluxing a thermally sprayed coating, comprising;(a) preparing a cast metallic substrate surface to be clean of oil and grease and to have a uniform surface tension;(b) electrostatically depositing a dry flux powder onto such prepared surface;and(c) thermally depositing melted metal onto and across said electrostatically fluxed surface to further thermally activate said flux, if not already activated, for stripping away any substrate oxides and for metallurgically bonding the sprayed metal as a coating to the cast substrate.
  2. 4
    A method as claimed in any one of claims 1 to 3, in which said thermally deposited metal in step (c) is comprised of a bonding metal selected from the group of nickel-aluminium, aluminium-bronze, and silicon bronze.
  3. 5
    A method as claimed in any one of the preceding claims, in which said thermal deposition is carried out by the use of wire arc, high velocity oxy-fuel, or powder plasma thermal spraying to provide superheated metal droplets at a temperature in excess of 1000°C.
  4. 7
    A method of coating adjacent cylinder bore surfaces of an aluminium engine block, the surfaces having a bridge wall separating the bore surfaces and having a preconditioned surface roughness of less than 50 microns Ra, comprising:(a) washing said surfaces with an aqueous solution of non-etching alkaline cleaning agent comprising borate, carboxylic acid and sodium gluconate, said agent being effective to increase and make homogeneous the surface energy of said preconditioned surface,(b) after drying said surfaces, electro-statically applying a dry dehumidified non-corrosive brazing flux that clings to said wash surfaces in a uniform coating thickness of 10 micrometers,(c) thermally spraying said adjacent bore surfaces at the same time with a transition bonding metal to simultaneously (i) thermally activate said electrostatically deposited dry flux to strip said surfaces of oxides, and (ii) metallurgically adhere said bonding metal to the stripped surfaces,(d) thermally spraying a top metal coat over said bonding metal in each bore to metallurgically adhere thereto said thermal spraying utilising propulsion and atomising air that is pumped through said bores to cool said block and avoid excessive engine block heating particularly at the bridge walls between said adjacent bores, and(e) removing a portion of said top coat to finish said coated surface to 0.1-0.4 micrometers Ra.