Claims
- 1. Method for manufacturing a composite bimetal wearing part including inserts having two longitudinal sides made of a first metal alloy with high resistance to wear and a cast support made from a second more ductile metal alloy resistant to mechanical stresses comprising the steps of:
- providing said inserts with at least one protruding rib on the longitudinal sides of said inserts;
- disposing said inserts one against another and against an axially symmetrical mould circumference in a manner such that adjacent inserts are separated by a spacing defined by said protruding ribs on said longitudinal sides of said inserts; and
- casting said second more ductile metal in said mould so as to fill the hollow space of said mould forming a radial fin between two adjacent inserts whereby said casting is carried out in such a way as to establish only a mechanical bonding between said inserts and said support being purely mechanical due an appropriate geometrical shape of said inserts.
- 2. Method for manufacturing a composite bimetal wearing part according to claim 1 wherein said mould is a cylinder.
- 3. Method for manufacturing a composite bimetal wearing part according to claim 1 wherein said mould is a truncated cone.
- 4. Method for manufacturing a composite bimetal wearing part according to claim 1 wherein said mould is an annulus.
- 5. Method according to claim 1 wherein the inserts are prepared by a heat treatment, a refractory or a ceramic coating treatment before the second metal is cast.
- 6. In a method for manufacturing a composite bimetal wearing part including cross-sectionally tapered inserts having defined root and wear surfaces, each insert made of a high wear-resistant first metal alloy, and a support which is cast of a second metal alloy more ductile than said first and mechanically stress resistant, an improvement for maximizing total insert wearing surface of the part characterized by the shape of:
- providing each insert a longitudinally elongate shape having an essentially orthogonal cross-sectional taper, which taper increases towards said defined wear surface, while further providing longitudinally thereon at least one protruding rib having at least one nonlinear feature;
- disposing the inserts adjacently, while contacting one another, along the circumference of an axially symmetrical mould so that said inserts wear surfaces are directed radially outward and spacing between adjacent inserts is defined by at least one protruding rib of an insert, and further providing therebetween, by said disposing, a plurality of narrow elongate voids for investment therein of said second alloy, whereby a high insert dispositioning rate is attained along said circumference; and
- casting the second alloy in said mould and filling thereby all spaces and voids thus forming a radial fin in each said narrow elongate investment void and effecting the mechanical bonding of each insert to the mould by capturing therein said nonlinear feature of each rib, whereby realizing the wearing part by the aforesaid steps, particularly attaining said high, contacting insert dispositioning, effects a maximizing of total wear surfaces of said part.
Priority Claims (1)
Number |
Date |
Country |
Kind |
09000895 |
Sep 1990 |
BEX |
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Parent Case Info
This application is a continuation-in-part of application Ser. No. 761,429, filed Sep. 17, 1991, now abandoned.
US Referenced Citations (5)
Foreign Referenced Citations (1)
Number |
Date |
Country |
2182875 |
May 1987 |
GBX |
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
761429 |
Sep 1991 |
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