Abstract:
A rotor housing for a rotary internal combustion engine is disclosed having a wear-resistant coating system characterized by high temperature hardness stability and controlled porosity to improve the lubricating characteristics of the surface-to-surface engagement with the rotary apex seals. The coating system comprises a self-fused composite of martensitic stainless steel powder and an equally hard powder consisting of a nickel-based alloy. Powder particle size is controlled to render a smoother machined surface and sub-surface porosity. An intermediate transition coating may be used consisting of a composition selected from nickel aluminide, arc sprayed nickel, molybdenum, all effective to operate as a bonding intermediate to a supporting aluminum structure. A method of producing the wear-resistant coating system for a rotor housing is disclosed, comprising preparation of an aluminum casting having a supporting epitrochoid end wall, machining a reference, embedment of thermally resistant plugs about certain openings in the end wall, removing a uniform layer of said casting end wall to a predetermined depth, soft grit blasting of the removed surface, coating of the margins about ports in the end wall with an anti-bond material flame spraying the entire end wall with a mixture of martensitic stainless steel and a nickelbased alloy, immersing said coated casting in oil for a predetermined period of time immediately after coating, and grinding off a portion of said coating to the depth of said reference.
Abstract:
A rotary internal combustion engine is disclosed having a rotor housing presenting an internal epitrochoid surface which is electrolytically coated with a composite of nickel and a carbide of silicon. A rotor piston is mounted for planetary movement within the rotor housing and carries a plurality of apex seal strips each comprised of a distinct wear-resistant portion and a distinct supporting portion. The wear-resistant portion is constituted of a sintered powder compact principally of iron and titanium carbide. The supporting portion is constituted of a sintered powder compact of high strength aluminum having a higher coefficient of thermal expansion than said wear-resistant portion. Both portions are mechanically keyed together to resist loads transverse to the strip and to make a mechanical joint as said portions differentially expand. The supporting portion is constituted of a material having a lower specific gravity than the wear-resistant portion; the wear-resistant portion has higher wear and antigalling properties as well as a lower dynamic coefficient of friction than the supporting portion.
Abstract:
An improved wear-resistant surface preparation is used on the inner side walls of the combustion chamber of a rotary piston engine. The improvement comprises deposition of two distinct but admixed metallic powders of generally equal hardness; one of the powders contains fluxing agents which enable the deposited powders to self-sinter if deposited in a semiplastic condition. The powders are deposited on a previously undercut cast iron side-housing. The resulting coating composition is characterized by minimum hardness value of Rc 30 at elevated operating temperatures of 400*F. The composition retains a stable hardness at elevated temperature levels up to 1100*F. The coating may have a porosity of 3-9%, but particle size is controlled to limit the porosity to 5% which is compatible with lubricating requirements of a rotary engine. The coating composition is deposited across the entire area circumscribed by the path of the outer most side point of the apex seals carried by the rotary piston; the path is substantially commensurate or approaches the entire shape of the epitrochoid chamber. The coating is compatible with the composition of the rotor side seals, oil seals and corner seals bearing thereagainst. The rotor side seals are comprised of cast iron, the oil seals are cast iron coated with limited chromium, the corner seals are prepared from cast iron, and the apex seals are strips of metal coated with an alloy of iron and titanium carbide with graphite. A method is disclosed comprising: (1) machining a cast side housing structure to a depth sufficient to accommodate a slightly oversized finish coating. The cast structure is undercut, grit blasted and preheated to 200*F., (2) a coating of admixed martensitic stainless steel and an equally hard nickel-based alloy is flame sprayed upon the machined area including approximately three-eights of an inch margin beyond the undercut area, the spraying being conducted by rotating the surface to be sprayed along with radial and rotative movement of the spray gun arranged to direct the spray perpendicular to the surface, (3) soaking the flame sprayed coating immediately after deposition with oil, and (4) grinding the surface finish to a predetermined reference thickness.
Abstract:
A rotary internal combustion engine and particularly an improved rotor construction for such engine and method of making is disclosed. A coating system is applied at least to the flank surfaces of the rotor which face the variable volume combustion chambers of the engine, the system serving to reduce heat flow to the oil lubrication system within the rotor and to quench heat build-up on the above surfaces to prevent pre-ignition. The engine is permitted to run at a somewhat higher operating temperature resulting in increased efficiency, better fuel comsumption and reduction of emissions.
Abstract:
A method (and resulting product) is disclosed for making rotor housings useful in a rotary internal combustion engine. The housing is preferably sand cast; the internal epitrochoid surface is flame-spray coated with a thin layer of nickel-aluminide, flame-spray coated with a thicker layer of plain carbon steel, and then plated with chromium. The resulting casting-coating composite provides enhanced wearability, increased dimensional stability, and reduced internal stress of the coatings.
Abstract:
A side wall coating system is disclosed for use in a rotary internal combustion engine having a narrow chamber bounded by a pair of flat side walls and an epitrochoidally-shaped end wall joining the side walls. A rotor is mounted for planetary movement in the chamber and in close spacing with each of said side walls, the rotor carries annular seals sliding against said side walls to define a shifting oil chamber in the spacing between the rotor and each of said side walls. The coating system comprises a selffused particle coating across the entire area of each of said side walls and is comprised of an admixture of stainless steel and nickel-based alloy powders of generally equal hardness. A resin is impregnated in said coating effective to close the pores substantially below the surface of said coating but the pores adjacent the surface are devoid of such resin as a result of decomposition under engine operating conditions. The decomposition of the resin insures limited porosity for retention of a controlled amount of oil to facilitate an oil film between the scraping seals and the side housing wall and also assure a deposit of carbon acting as a dry lubricant to further facilitate the metallic contact therebetween.