Abstract: A method and apparatus of providing accelerated thermal fatigue testing of an engine component, comprising: (i) impinging one or more torch flames directly on a selected area of the test specimen (i.e. metallic engine cylinder head) to heat such area to a critical test temperature that exceeds the normal maximum loading temperature of the specimen in normal use by about 10-25%, and holding such temperature for a period of 0.01-2.0 minutes; (ii) at the end of the holding period (ie. Water jet water in head jacket, or air in ports) quenching the heated area of the test specimen to a temperature that is about 75% below that of the normal maximum loading temperature and holding such quenching temperature for about 1-3 minutes; and (iii) repeating steps (i) and (ii) until a crack is induced in the test specimen while recording the history of temperature and time involved in such repeated steps.

Abstract: A method for producing powder metal cylinder bore liners for an internal combustion engine includes the steps of loading a powder metal mixture into a die cavity of a die, compacting the powder metal mixture in the die cavity using uniaxial pressure from the die and forming the powder metal cylinder bore liner, and sintering the powder metal cylinder bore liner.

Abstract: A method for producing self lubricating powder metal cylinder bore liners for an internal combustion engine includes the steps of loading a powder metal mixture into a die cavity, compacting the powder metal mixture in the die cavity and forming the powder metal cylinder bore liner having a porous structure, sintering the powder metal cylinder bore liner, and impregnating the porous structure of the cylinder bore liner with lubricant.

Abstract: In a composite anode structure having a refractory metal portion with a graphite portion attached thereto, an intersparsed zirconium brazing layer is isolated from the graphite material by a thin layer of platinum to thereby prevent the formation of embrittling carbides when the combination is raised to operating temperatures. The platinum is mechanically bonded to the graphite, and the zirconium is diffusion bonded to both the molybdenum portion and the platinum layer to form a high-strength, lasting bond.