초록 ▼

An engine block mold package includes a barrel crankcase core having a plurality of barrels on an integral crankcase region and one or more locator surfaces on the crankcase region. The barrels are formed by a barrel-forming tool element of a core box. The barrel-forming tool element is configured t

An engine block mold package includes a barrel crankcase core having a plurality of barrels on an integral crankcase region and one or more locator surfaces on the crankcase region. The barrels are formed by a barrel-forming tool element of a core box. The barrel-forming tool element is configured to also form the locator surface(s) on the crankcase region such that the locator surface(s) is/are accurately positioned relative to the barrels and thus the cylinders formed in the engine block cast in the mold package. The locator surface(s) can be used to locate the engine block casting in subsequent aligning and machining operations without the need to reference a curved surface of a cylinder bore liner.

대표청구항 ▼

1. A method of making a barrel crankcase core, comprising forming a plurality of barrels on an integral crankcase region using a barrel-forming tool element in a core box and forming one or more locator surfaces on said crankcase region using said barrel-forming tool element. 2. The method of claim

1. A method of making a barrel crankcase core, comprising forming a plurality of barrels on an integral crankcase region using a barrel-forming tool element in a core box and forming one or more locator surfaces on said crankcase region using said barrel-forming tool element. 2. The method of claim 1 wherein said barrel-forming tool element forms a primary locator surface and secondary locator surface on said crankcase region. 3. A method of making a barrel crankcase core, comprising forming first and second banks of a plurality of barrels on an integral crankcase region using respective first and second barrel-forming tool elements in a core box and forming one or more locator surfaces on said crankcase region using at least one of said barrel-forming tool elements. 4. The method of claim 3 wherein said first and second barrel-forming tool elements form three primary locator surfaces and two secondary locator surfaces on said crankcase region. 5. The method of claim 4 including forming a third locator surface on said crankcase region.