Methods and systems for engine block thermal conductivity
AssigneeFord Global Technologies, LLC
InventorsCarsten Weber, Paul Turner, Urban Morawitz, Clemens Maria Verpoort
Life of this patent
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Abstract
Methods and systems are provided for coatings of a portion of an engine block shaping a combustion chamber. In one example, the engine block includes a first coating with a thermal conductivity higher than a conductivity of the engine block arranged in an upper region of the combustion chamber and a second coating with a thermal conductivity lower than the conductivity of the engine block arranged in a lower region of the combustion chamber, and where the second coating touches the first coating.
Claims20
An engine block comprising:
- a first coating arranged on interior surfaces of a cylinder near a top-dead center position of a piston and a second coating arranged on the interior surfaces near a bottom-dead center position of the piston, the first coating comprising a hypereutectic aluminum-silicon alloy and the second coating comprising an iron-based alloy with a thermal conductivity lower than a thermal conductivity of the first coating and a thermal conductivity of the interior surfaces.
A system comprising:
- a combustion chamber shaped between surfaces of an engine head, an engine block, and a piston, the piston shaped to oscillate along a longitudinal axis passing through its center;
- a first coating arranged on surfaces of the engine block corresponding to interior surfaces of the combustion chamber adjacent to the engine head and a top-dead center position of the piston, and where a first coating thermal conductivity is higher than an interior surfaces thermal conductivity, and where the first coating is an aluminum-silicon alloy comprising greater than 12% silicon;
- and
- a second coating arranged on surfaces of the engine block corresponding to interior surfaces of the combustion chamber distal to the engine head and adjacent to a bottom-dead center position of the piston, and where a second coating thermal conductivity is lower than the interior surfaces thermal conductivity, and where the second coating is an iron-alloy with a nanocomposite material.
A method comprising:
- applying a first coating with a first thermal conductivity to interior surfaces of an upper region of a combustion chamber, wherein the first coating is an aluminum-silicon alloy comprising greater than or equal to 12% silicon;
- and
- applying a second coating with a second thermal conductivity less than the first thermal conductivity to interior surfaces of a lower region of the combustion chamber during a cooling process of the first coating to generate a weld-metallurgical bond therebetween;
- wherein
- the upper region extends from a top of a portion of the combustion chamber shaped in an engine block down to a portion of the combustion chamber equal to between 20 to 40% of its total length, and where the lower region extends from the upper region to a bottom of a portion of the combustion chamber shaped in the engine block.
Dependencies are inferred from the claim text.