Claims
- 1. A pattern and insert assembly comprising an insert having opposite ends, and an evaporable foam pattern assembly surrounding said insert, being formed by a plurality of sections joined together around said insert, and including an interior wall having thereon a plurality of spaced projections supporting said insert, spacing said insert from said wall so as to form between said insert and said wall a cavity, and affording filling of said cavity with sand when said pattern and insert assembly is utilized in a lost foam casting process, both of said opposite ends of said insert being spaced from said pattern assembly such that sand can flow into said cavity at both of said ends of said insert.
- 2. An assembly as set forth in claim 1 wherein each of said projections has a generally circular cross section.
- 3. An assembly as set forth in claim 1 wherein said pattern sections are joined together with a glue.
- 4. A method for casting an engine block assembly for a two-cycle engine, said assembly including a cylinder block having a cylinder bore, an exhaust port communicating with said cylinder bore, and an interior passage which communicates with said exhaust port and which is defined by a wall which has thereon a plurality of projections, and an exhaust passageway liner surrounded by said cylinder block and supported in said interior passage by said projections and in inwardly spaced relation to said interior passage wall so as to form between said exhaust passageway liner and said interior passage wall an exhaust gas insulating cavity, said method comprising the steps of providing said exhaust passageway liner, providing a plurality of evaporative foam pattern sections respectively including at least one projection extending from a wall, engaging the exhaust passageway liner, and spacing the exhaust passageway liner from the interior passage wall, assembling said pattern sections around said exhaust passageway liner to form a pattern and liner assembly with said projections in spaced relation to afford filling of the space between the interior passage wall and the exhaust passageway liner with molding sand during embedding of the pattern and liner assembly in molding sand, joining said pattern sections together, and utilizing said pattern and liner assembly in a lost foam casting process wherein said pattern is replaced by a molten material to form said engine block assembly.
- 5. A method as set forth in claim 4 wherein said cylinder block is fabricated of a first material and said exhaust passageway liner is fabricated of a second material having a melting temperature higher than the melting temperature of said first material.
- 6. A method as set forth in claim 4 wherein said cylinder block has first and second cylinder bores and first and second exhaust ports respectively communicating with said first and second cylinder bores, wherein said interior passage communicates with both of said exhaust ports, and wherein said liner has therein first and second exhaust port openings respectively communicating with said first and second exhaust ports, and has an outlet opening spaced from said first and second exhaust port openings.
- 7. A method as set forth in claim 6 wherein said liner is spaced from said pattern sections at each of said first and second exhaust port openings and said outlet opening of said insert such that sand can flow between the interior passage wall and the exhaust passageway liner at, each of said first and second exhaust port openings and said outlet opening.
- 8. A pattern and insert assembly comprising an insert having a longitudinal axis, and an evaporable foam pattern assembly surrounding said insert, being formed by a plurality of sections joined together at a parting line and around said insert, and including an interior wall having thereon spaced projections supporting said insert, spacing said insert from said wall so as to form between said insert and said wall a cavity, and affording filling of said cavity with sand when said pattern and insert assembly is utilized in a lost foam casting process, and said projections including a plurality thereof being located in a single plane perpendicular to said longitudinal axis and being parallel and perpendicular to said parting line.
- 9. An assembly as set forth in claim 8 wherein said insert has opposite ends, and wherein both of said opposite ends of said insert are spaced from said pattern assembly such that sand can flow into said cavity at both of said ends of said insert.
- 10. An assembly as set forth in claim 8 wherein each of said projections has a generally circular cross section.
- 11. An assembly as set forth in claim 8 wherein said pattern sections are joined together with a glue.
Parent Case Info
This is a continuation of co-pending application Ser. No. 694,953, filed May 1, 1991 now abandoned.
US Referenced Citations (22)
Foreign Referenced Citations (6)
Number |
Date |
Country |
2643578 |
Aug 1990 |
FRX |
0305653 |
May 1988 |
DEX |
0133161 |
May 1990 |
JPX |
2187251 |
Jul 1990 |
JPX |
219331 |
Feb 1988 |
GBX |
PCTUS7800134 |
Nov 1978 |
WOX |
Continuations (1)
|
Number |
Date |
Country |
Parent |
694953 |
May 1991 |
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