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An improved flight assembly for an elevator used with a wheel tractor scraper is provided. The flight assembly comprises a support member made of one type of material and an edge plate made of a second type of material that is harder and less flexible than the support member material. The edge plate

An improved flight assembly for an elevator used with a wheel tractor scraper is provided. The flight assembly comprises a support member made of one type of material and an edge plate made of a second type of material that is harder and less flexible than the support member material. The edge plate is mounted to the support member and includes the cutting/digging edge of the flight assembly. In one embodiment the support member is made of a rolled steel material having a hardness of about 205 BHN and the edge plate is made of a hardened, heat treated steel material having a hardness of between about 360 BHN and about 440 BHN.

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1. A bimaterial flight assembly for an elevator used to carry material upwardly and rearwardly into a bowl of a wheel tractor scraper, the bimaterial flight assembly having a contact edge that cuts into the material and is susceptible to wear, the flight assembly comprising: a support member compris

1. A bimaterial flight assembly for an elevator used to carry material upwardly and rearwardly into a bowl of a wheel tractor scraper, the bimaterial flight assembly having a contact edge that cuts into the material and is susceptible to wear, the flight assembly comprising: a support member comprising an elongated body portion having an asymmetrical U-shaped side profile, the support member made of a first material, wherein said support member includes left and right hand bracket members affixed to opposing ends; andan edge plate mounted to the support member, the edge plate including an elongated, substantially planar upper portion and an elongated substantially planar lower portion including the contact edge of the flight assembly, joined along a longitudinal bend and defining an obtuse included angle, the edge plate being made of a second material that is harder and less flexible than the first material. 2. The bimaterial flight assembly of claim 1 wherein: said edge plate includes a narrow section that is partially separated from a wide section by a pair of horizontal slots formed in said edge plate;wherein said slots are configured to receive the bracket members when said flight assembly is assembled. 3. The bimaterial flight assembly of claim 1 wherein: the support member is made of a first steel material; andthe edge plate is made of a second steel material that is harder and less flexible than the first steel material. 4. The bimaterial flight assembly of claim 3 wherein: the support member is made of a rolled steel material; andthe edge plate is made of a hardened, tempered quenched steel material that is harder and less flexible than the support member steel material. 5. The bimaterial flight assembly of claim 4 wherein: the edge plate is made of hardened, tempered quenched steel with a hardness of between about 360 BHN and 440 BHN and a compressive yield strength of between about 900 MPa and 1100 MPa; andthe support member is made of rolled steel with a hardness of about 205 BHN and a compressive yield strength of about 500 MPa. 6. The bimaterial flight assembly of claim 4 wherein: the support member comprises an elongated body portion having an asymmetrical, U-shaped side profile, the body portion comprising a substantially flat, elongated top section and a substantially flat, elongated bottom section connected along a curved rear edge;the edge plate comprises an elongated body having opposing ends, a top edge, a cutting edge, a front side and a rear side. 7. The bimaterial flight assembly of claim 6 wherein: the top section of the support member extends from a front edge to the curved rear edge and the bottom section of the support member extends from a forward edge to the curved rear edge; andthe edge plate further comprises an elongated, substantially planar upper portion and an elongated, substantially planar lower portion joined along a longitudinal bend. 8. The bimaterial flight assembly of claim 7 wherein: the rear side of the edge plate is positioned against the support member so that the upper portion of the edge plate abuts the front edge of the top section of the support member and the lower portion of the edge plate abuts at least part of the forward edge of the bottom section of the support member. 9. The bimaterial flight assembly of claim 7 wherein: the edge plate is welded to the support member along the support member's front edge and forward edge. 10. A method of making a work tool for an off-highway machine comprising the steps of: providing a carrying component comprising an elongated body portion having an asymmetrical U-shaped side profile, the carrying component made of a first steel material;providing a working component having an elongated, substantially planar upper portion and an elongated substantially planar lower portion including a cutting edge and joined along a longitudinal bend and defining an obtuse included angle, the working component made of a second steel material that is harder and less flexible than the first steel material; andaffixing the working component to the carrying component. 11. The method of claim 10 wherein: the first steel material is rolled steel; andthe second steel material is hardened, heat treated steel. 12. The method of claim 10 wherein: the off-highway machine is a wheel tractor scraper;the work tool is a flight assembly for an elevator;the working component is an edge plate; andthe carrying component is a support member on which the edge plate is mounted.