US2012210578A1PendingUtilityA1
Method Of Manufacturing An Engine Block
Est. expiryJul 3, 2028(~2 yrs left)· nominal 20-yr term from priority
B23P 6/04B23P 6/02Y10T29/49233Y10T29/49231
48
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Claims
Abstract
A method for manufacturing an engine block, such as for an internal combustion engine, includes a step of removing material from a top deck of the engine block surrounding a cylinder bore to create a first removal area. Material is also removed from the top deck of the engine block surrounding at least one fluid passage to create a second removal area. An insert is positioned within a recessed area defined by the first removal area and the second removal area.
Claims
exact text as granted — not AI-modified1 . A method for manufacturing an engine block, comprising:
removing material from a top deck of the engine block surrounding a cylinder bore to create a first removal area; removing material from the top deck of the engine block surrounding at least one fluid passage to create a second removal area; and positioning an insert within a recessed area defined by the first removal area and the second removal area.
2 . The method of claim 1 , wherein the second removing step includes removing material from the top deck of the engine block surrounding each of a plurality of fluid passages circumferentially spaced about the cylinder bore.
3 . The method of claim 1 , wherein at least one of the first removing step and the second removing step includes machining out a crack within the engine block.
4 . The method of claim 3 , wherein at least one of the first removing step and the second removing step further includes machining out the crack radiating from the cylinder bore.
5 . The method of claim 3 , wherein at least one of the first removing step and the second removing step further includes machining out the crack radiating from the at least one fluid passage.
6 . The method of claim 1 , wherein the positioning step includes press fitting the insert within the recessed area.
7 . The method of claim 6 , wherein the positioning step further includes aligning a keyed feature of the insert with a complementary keyed feature of the recessed area prior to the press fitting step.
8 . The method of claim 6 , further including machining the insert to a thickness greater than a depth of the recessed area.
9 . The method of claim 8 , further including planing the top deck of the engine block after the press fitting step.
10 . The method of claim 1 , wherein the first removing step and the second removing step include removing the material using a computer numerical control machining tool.Cited by (0)
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