Patent Application
20190210101
The present disclosure relates to methods of casting parts, and more particularly to casting components within an engine block.
The statements in this section merely provide background information related to the present disclosure and may not constitute prior art. Throughout the present disclosure, metallurgical bonds and molecular bonds are nearly synonymous.
Generally, the structure of an aluminum engine block is reinforced to achieve a high-power density, low-displacement engine. Often, pre-fabricated ferrous-based engine block inserts are used to transmit loads from an engine head deck to a crankshaft. The engine block inserts are usually cast into the engine block in a single operation, such as those disclosed in U.S. Pat. No. 9,719,461, which is commonly assigned with the present application and the contents of which are incorporated herein by reference in their entirety.
Unfortunately, dissimilar metals (e.g. aluminum and iron) rarely bond to one another during casting (e.g., High Pressure Die Casting (HPDC) or sand casting), and thus a bond is not created between the block insert and the parent assembly when casting an engine block. The lack of a bond between the engine block insert (iron) and the engine block alloy (aluminum) metal enables cracks to initiate at the aluminum-iron interfaces. Unfortunately, these cracks to grow during normal operating conditions, which could cause permanent damage and thus reduce the service life.
When loads are not transmitted efficiently, equally, or uniformly through engine components, including the insert and engine block, this may also lead to a reduced service life because the engine components undergo greater fatigue cycling. Therefore, reduced load-carrying capacity may result in reduced engine block fatigue life.
The present disclosure addresses issues related to dissimilar materials within engine blocks, their load-carrying and load-transferring capabilities, and other issues related to casting dissimilar metals.
In one form of the present disclosure, a method of forming an assembly is provided. The method comprises forming an insert, coating the insert with a bond material and placing the insert within a casting mold or die. The casting mold or die is purged with an inert gas and the casting mold or die is filled with molten metal to encapsulate the insert. The encapsulated insert is diffusion bonded to the molten metal to form a diffusion bonded insert, which is placed within a cavity of a secondary casting mold or die. The secondary casting mold or die is filled with molten metal to form a composite casting assembly. After or during the casting, the composite casting assembly is heat treated.
In a variation of one method of the present disclosure, the insert is a material selected from the group consisting of a ferrous alloy, a nickel-based alloy, a super alloy, and a nonferrous alloy. With additional variants, at least one external area of the insert is texturized and oxide-cleansed prior to coating with the bond material, the bond material is one of a copper material or a nickel material, and the bond material is applied by a process selected from the group consisting of electroforming, electroless coating, chemical vapor deposition (CVD), plasma vapor deposition (PVD), thermal spray, cold spray, and plasma spray.
In one form, the cast part is an engine block, the bond material is applied in a thickness less than or equal to 1 mm, and the molten metal is aluminum and applied in a thickness up to 10 mm.
In other variants, the molten metal is aluminum, the insert is completely encapsulated by the molten metal, the diffusion bonding step includes processing the inserts in a furnace, the step of heating the diffusion bonded insert and the cast part is carried out according to a heat treatment, a high pressure die casting (HPDC) method is used in the step of filling the casting mold or die with molten metal to encapsulate the insert, a sand casting method is used in the step of filling the casting mold or die with molten metal to encapsulate the insert, and an engine block is manufactured according to the various methods disclosed herein.
In another form of the present disclosure, a method of forming an assembly is provided. The method comprises bonding a coating around a steel insert to form a bonded insert, encapsulating the bonded insert with a layer of aluminum material to form an encapsulated diffusion bonded insert, and placing the encapsulated diffusion bonded insert within a cavity of an aluminum cast part. Then the encapsulated diffusion bonded insert and the aluminum cast part are heated together to form a composite casting assembly.
In variants of this method, the coating is one of a copper material or a nickel material. In another method of the present disclosure, the coating defines a thickness less than or equal to 1 mm, the aluminum material defines a thickness up to 10 mm, and at least a portion of exterior surfaces of the insert are texturized prior to bonding the coating.
In yet another form of the present disclosure, a method of forming an insert for use in an assembly is provided. The method comprises forming an insert from a steel alloy, texturizing at least a portion of the exterior surfaces of the insert, and coating the insert with a copper bond material. The coated insert is placed within a casting mold or die and the casting mold or die is purged with an inert gas. The casting mold or die is filled with molten aluminum metal to encapsulate the insert, which is heated to diffusion bond the molten aluminum metal to the insert to form a diffusion bonded insert. The diffusion bonded insert is placed within a cavity of an aluminum cast part and both are heated together to form a composite casting assembly. An engine block is also provided that is manufactured according to this method.
Further areas of applicability will become apparent from the description provided herein. It should be understood that the description and specific examples are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
In order that the disclosure may be well understood, there will now be described various forms thereof, given by way of example, reference being made to the accompanying drawings, in which:
The drawings described herein are for illustration purposes only and are not intended to limit the scope of the present disclosure in any way.
The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses. It should be understood that throughout the drawings, corresponding reference numerals indicate like or corresponding parts and features.
Generally, the present disclosure provides a method that creates a molecular bond between dissimilar metals that are cast, such as between an insert and a parent alloy housing material. The molecular bond improves load transmission and distribution between the dissimilar cast metals, which reduces overall mass and also eliminates certain features used in known inserts to improve bond strength. The improved load transmission and distribution enhances the application of multi-material products using aluminum and ferrous alloys. The present disclosure inhibits the formation of intermetallic phases that negatively impact the quality of the molecular bond.
The method that creates a molecular bond between the parent material (material α) and the insert (material β), by diffusion bonding an intermediary layer (bond material) between the parent material and the insert. In general, the intermediary layer is a material that diffusion bonds well with both the parent material (material α) and the insert (material β).
A form of the present disclosure provides a method for forming bulkhead inserts for castings, which in one form are engine blocks. The method creates molecular bonds that provide distributive load-bearing characteristics, thus providing a composite casting assembly that acts as a homogeneous material under loads. The method is applicable to both High Pressure Die Casting (HPDC) and sand casting processes, among others. Further, the method enables the use of multi-material products using mixed ferrous with aluminum alloys. The method does not require plasma temperatures to melt both interfacing contacting topologies or to merge (stir) the contacting topologies together at an atomic level when one component is a ferrous alloy and one component is an aluminum alloy
The present disclosure provides a diffusion-based bonding process between dissimilar materials to create and stabilize a metallurgical bond between the dissimilar materials. Particularly, the metallurgical bond between an insert and an engine block. In general, any thin metallic material can be used that will bond readily with both the insert metal and the engine block metal. The method of the present disclosure has a reduced cost as compared to plasma processes. The method overcomes the bond strength issues experienced during solidification and reduces fatigue loading under cyclic engine loading events of an internal combustion engine.
Referring to
The casting interface 34 is relatively thin and provides a mechanical connection between the insert 10 and the engine block 30. Due to the thin casting interface 34, the serrations 14 provide the requisite mechanical coupling between the insert 10 and the engine block 30.
Referring now to
In an example of the present disclosure, insert 50 is ferrous (insert material 51), the engine block 30 is aluminum (first casting material 33), with the interfacial casting area 52 between the ferrous insert 50 and the aluminum engine block 30. In one form, the coating material 54 is copper, the second casting material 56 is aluminum, the first coating interface 58 is electroformed, second coating interface 60 is diffusion bonded, wherein the second casting interface 62 bonds well with the aluminum engine block 30 as both materials are aluminum.
As described in greater detail below, the insert 50 is coated with the coating material 54 and placed within a mold or die. The mold or die is then purged with an inert gas and filled with a molten metal. Heat is then applied to diffusion bond the molten metal to the coated insert to form a diffusion bonded insert. The heating and filling with molten metal may be concurrent processes, or they may be separate sequential steps. The diffusion bonded insert is then placed into a secondary casting mold or die (a different casting mold or die), which contains a parent component such as the engine block 30, and the secondary casting mold or die is filled with molten metal, encapsulating the diffusion bonded insert and forming a composite casting assembly. The composite casting assembly is also heated to stabilize its structure and properties.
As used herein, the term “encapsulate,” “encapsulated,” and “encapsulating” should be construed to mean covering at least a portion of the insert 50 with the coating material 54 and not necessarily covering all exterior surfaces of the insert 50. Although one form of the present disclosure involves complete encapsulation of all exterior surfaces of the insert 50 (“completely encapsulated”), it should be understood that only select exterior surfaces may be coated with the coating material 54 and still be “encapsulated” according to the teachings of the present disclosure.
The methods of the present disclosure are at least applicable to engine blocks, cylinder heads, or any part that employs a load-bearing cast-in insert. Example applications include, but are not limited to: (1) bulkhead reinforcement inserts of ferrous metal cast into an aluminum engine block main bearing web region; (2) cylinder liners; (3) cylinder blocks using a bedplate with ferrous metal insert to improve structural stiffness; (4) head bolt inserts in cylinder blocks; and (5) valve seat inserts in cylinder heads.
Referring to
In a variation of this method, the insert includes ferrous alloys, nickel-based alloys, super alloys, and nonferrous alloys. In additional variations, at least one external area of the insert is texturized and oxide-cleansed prior to coating with the bond material, the bond material is one of a copper material or a nickel material, the bond material is applied by a process that includes electroforming, electroless coating, chemical vapor deposition (CVD), plasma vapor deposition (PVD), thermal spray, cold spray, and plasma spray, the cast part is an engine block, the bond material is applied in a thickness less than or equal to 1 mm, and the molten metal is aluminum and applied in a thickness up to 10 mm, the molten metal is aluminum, the insert is completely encapsulated by the molten metal, the diffusion bonding step includes processing the inserts in a furnace, the step of heating the diffusion bonded insert and the cast part is carried out according to a heat treatment, a high pressure die casting (HPDC) method is used in the step of filling the casting mold or die with molten metal to encapsulate the insert, and a sand casting method is used in the step of filling the casting mold or die with molten metal to encapsulate the insert. The present disclosure also provides an engine block manufactured according to the teachings of the present disclosure.
Referring to
In a variation of this method, the coating is one of a copper material or a nickel material. In another method of the present disclosure, the coating defines a thickness less than or equal to 1 mm. In further variations of this method, the aluminum material defines a thickness up to 10 mm, and at least a portion of exterior surfaces of the insert are texturized prior to bonding the coating.
Referring to
In an exemplary method of forming a part by diffusion bonding the insert 50 to the engine block 30, where compacted graphite iron (CGI) is the insert material and a nickel-based alloy is the diffusion-bonding material, the following steps are employed:
1. Creating a steel alloy block insert using one or more standard manufacturing techniques such as casting, powder metallurgy, forging, and/or machining.
2. Performing an optional grit blasting operation on insert to texturize external surfaces and performing an optional oxide-cleaning which promotes adhesion during the electroforming process.
3. Coating the insert with a thin (0.5-1.5 nm or 5-15 angstroms (Å)) copper layer using an electroforming process. Copper is chosen in one form of the present disclosure as copper will diffusion bond well with both iron and aluminum.
4. Placing the coated block insert into a HPDC casting die. The casting die is closed and an inert gas (e.g. Argon or Nitrogen gas) is used to flood the casting die and displace the oxygen-containing atmosphere. The inert gas reduces or negates oxidation of the coated block insert during the HPDC casting.
5. Injecting molten aluminum into the casting die using a standard HPDC process. In one form, the inserts are completely encapsulated by an aluminum layer up to 10 mm in thickness. The high pressures associated with HPDC promotes solidification of the aluminum alloy in direct contact with the CGI insert.
6. Removing the encapsulated insert from the HPDC casting die.
7. Placing the encapsulated insert into a furnace to diffusion bond the aluminum to the encapsulated insert, thus creating a diffusion bonded insert.
8. Placing the diffusion bonded insert into an engine block casting die and using conventional HPDC processes to cast aluminum around the diffusion bonded insert, creating a composite casting assembly.
9. Transferring the composite casting assembly to a furnace and heat treating the composite casting assembly to achieve a T5 heat treatment. This heat treatment also operates as an artificial aging process improves the strength of the composite casting assembly.
The description of the disclosure is merely exemplary in nature and, thus, variations that do not depart from the substance of the disclosure are intended to be within the scope of the disclosure. Such variations are not to be regarded as a departure from the spirit and scope of the disclosure.
