The present invention relates to structural enhancement of a composite intake manifold.
Intake manifolds coupled to engines, e.g., engines used in the propulsion of vehicles, may be composed at least partially of composite materials including plastics, resins, and/or polymer materials. Such composite intake manifolds are generally not as strong or stiff as manifolds made from metal or ceramic materials, for example. Thus sections of outer walls of such composite intake manifolds may lack sufficient structural support, e.g., to withstand significant internal pressures and accommodate components which may be mounted on the manifold. A section of an outer wall of a composite intake manifold lacking sufficient structural support may contribute to NVH (noise, vibration, harshness), durability, and/or strength problems of the intake manifold. Increasing thickness of the outer walls of a composite manifold or introducing additional structural elements within the hollow body of a composite intake manifold are examples of approaches aimed at enhancing structural integrity of composite intake manifolds.
However, the inventors herein have recognized issues with such approaches. For example, increasing the thickness of the outer walls of a composite intake manifold may increase the weight of the manifold, especially depending on the location of the increased thickness. Such increased weight may then lead to lower fuel efficiency in an engine used to propel a vehicle. Additionally, introducing structural elements within the hollow body of a composite intake manifold may increase part cost and degrade the air flow performance of the intake manifold.
To at least partially address these issues, a system for a V-engine, is provided. The system comprises, a composite intake manifold having an upper outer wall positioned opposite a plurality of air outlets of the manifold; and a supporting member overmolded in the upper outer wall. In some examples, the composite intake manifold may be substantially composed of a first material and the supporting member may be substantially composed of a second material, where the second material has a greater tensile strength than the first material.
In this way, the structural integrity of a composite intake manifold may be enhanced without increasing the thickness of the outer walls or introducing structural elements within the hollow body of the manifold. Such a manifold may have increased air flow performance, lower material and part cost, and lower weight. Note that the wall thickness may be increased in addition to the overmolded support, if desired.
It should be understood that the background and summary above is provided to introduce in simplified form a selection of concepts that are further described in the detailed description. It is not meant to identify key or essential features of the claimed subject matter, the scope of which is defined uniquely by the claims that follow the detailed description. Furthermore, the claimed subject matter is not limited to implementations that solve any disadvantages noted above or in any part of this disclosure.
The following description relates to composite intake manifolds composed at least partially of plastic or polymer materials. A composite intake manifold may be coupled to cylinder heads of an engine, for example as shown approximately to scale in
Sections of outer walls of a composite intake manifold may lack sufficient structural support, e.g., to withstand significant internal pressures and accommodated components which may be mounted on the manifold. For example, an upper outer wall of the manifold may lack sufficient structural support in a region positioned above and between cylinder heads in a V-engine. Sections of outer walls of the manifold lacking sufficient structural support may contribute to NVH (noise, vibration, harshness), durability, and/or strength problems of the intake manifold.
In order to enhance the structural integrity of a composite intake manifold in an unsupported region of an outer wall of a manifold, a supporting member may be overmolded in said region.
By overmolding a supporting member in an unsupported region of an outer wall of a composite intake manifold, e.g., in an upper outer wall of the manifold between cylinder heads of a V-engine, the structural integrity of the manifold may be enhanced without increasing the thickness of the outer walls or introducing additional structural elements within the hollow body of the manifold. Such a composite intake manifold may have increased air flow performance, lower material and part cost, and lower weight. For example, it may be desirable to minimize a weight of the air intake manifold in order to reduce the weight of a vehicle to thereby increase fuel efficiency.
Turning now to the figures, a composite intake manifold 10 is shown coupled to a first cylinder head 12 and a second cylinder head 14 of a V-engine 15. The first cylinder head is coupled to a first cylinder block 17 of engine 15 and the second cylinder head is coupled to a second cylinder block 19 of engine 15. Intake manifold 10 is positioned on a top side of the engine (labeled “TOP” in
The first and second cylinder blocks and heads form a valley 16 in the V-engine. The valley 16 is an open space beneath the intake manifold which, in some examples, may be used for various engine components, such as air, exhaust, and/or engine coolant conduits. Additionally, open space in the valley may assist in cooling of the engine.
Though not shown in the figures, each cylinder block of the engine includes a plurality of combustion chambers (i.e., cylinders). Each cylinder may include a piston coupled to a crankshaft so that reciprocating motion of the piston is translated into rotational motion of the crankshaft. The crankshaft may be coupled to at least one drive wheel of a vehicle via an intermediate transmission system, for example.
Each cylinder may receive intake air from intake manifold 10 via an intake port located on the cylinder head and may exhaust combustion gases via an exhaust port located on the cylinder head. Thus each cylinder head includes a plurality of exhaust ports and a plurality of intake ports. The exhaust ports are positioned on sides of the cylinders heads opposing the valley 16 in an outbound configuration. For example, outbound exhaust manifolds leading to a tail pipe may be coupled to the exhaust ports on cylinder heads of the banks. A plurality of exhaust ports 18 on cylinder head 14 can be seen in
Composite intake manifold 10 is a generally hollow structure with a hollow body formed at least partially from plastic, resin, and/or polymer materials, e.g., nylon 6, nylon 6/6, or any suitable polyamide. In some examples, intake manifold 10 may be formed at least partially from resin impregnated with a matrix material such a carbon fiber cloth.
The composite intake manifold may be formed as one piece or as multiple pieces joined together in a post-process. For example, one or more pieces of the manifold may be formed using injection molding or blow-molding processes. The one or more pieces of the manifold may be joined together by a suitable welding process, e.g., using a vibration welding technique, and/or by using bolts, gaskets, or other suitable hardware.
For example, composite intake manifold 10 shown in
The hollow body of intake manifold 10 defines a plurality of passages in fluid communication with the manifold. The plurality of passages includes an air intake conduit 22 which is a conduit integrally coupled to the front side of the intake manifold to supply air, e.g., atmospheric air, to the manifold. For example, the upper outer wall and the lower outer wall may form the air intake conduit. Air intake conduit 22 may be positioned in a direction perpendicular to the plurality of air outlets in the lower outer wall of the manifold.
The plurality of passages also includes a plurality of air outlets of the manifold positioned opposite the upper outer wall. For example, the plurality of air outlet may be formed in lower outer wall 25 adjacent to the edge of the manifold. Each air outlet in the plurality of outlets may be coupled to a corresponding intake port on the cylinder heads.
The plurality of air outlets of the manifold includes a first plurality of outlets 28 in the lower outer wall 25 adjacent to a first portion of the edge and coupled to first cylinder head 12 and a second plurality of outlets 29 in the lower outer wall 25 adjacent to a second portion of the edge opposite the first portion, and coupled to the second cylinder head. The first plurality of outlets 28 and the second plurality of outlets 29 can be seen in
Each air outlet in the plurality of air outlets may be flanked by support columns adjacent to the edge of intake manifold 10. For example, the intake manifold may include a first plurality of columns 30 integrally coupled to the upper and lower outer walls and flanking air outlets in the first plurality of outlets 28 and a second plurality of columns 43 integrally coupled to the upper and lower outer walls and flanking outlets in the second plurality of outlets. The columns may be cylindrically shaped and substantially hollow to provide structural support to regions of the intake manifold adjacent to the edge of the intake manifold. In some examples, the columns may be integrally molded with upper outer wall 23 of manifold 10. The columns may then be integrally coupled to the lower outer wall using a welding process, for example as described above. The substantially hollow columns may also assist in cooling of air delivered to the cylinders.
Each outlet in the first plurality of outlets 28 may be coupled to a corresponding intake port on the first cylinder head and each outlet in the second plurality of outlets 29 may be coupled to a corresponding intake port on the second cylinder head. In some examples, each outlet in the first plurality of outlets 28 may be offset from the corresponding intake port in a direction toward the intake conduit 22 and each outlet in the second plurality of outlets 29 may be offset from the corresponding intake port in a direction opposing the air intake conduit 22. For example, with reference to
Intake manifold 10 may be mechanically coupled to the intake ports on the cylinder heads using mechanical fasteners. For example, intake manifold 10 may be attached to the cylinder heads by a plurality of attachments 32 located adjacent to outer edges of intake manifold 10. The manifold outlets 28 may be coupled to the corresponding cylinder intake ports using one or more of compression gaskets, flanges, mechanical fasteners, or the like.
Intake manifold 10 may further include various mounting components, outlets, etc. which may be coupled to various engine sensors, serve as a mounts for engine components, or secure the intake manifold to the engine. For example, a carburetor, throttle body, coolant cross over, fuel injectors and/or other components of the engine may be fastened to the outer walls of intake manifold 10, e.g., via mounting components 34, 36, 38, and 40. As another example, a manifold absolute pressure (MAP) sensor, a mass air flow (MAF) sensor, an air/fuel sensor, and/or other engine diagnostic devices may be coupled to intake manifold 10, e.g., via outlets 42, 44, and 46.
The upper outer wall 23 may have an undulating or curved shaped. For example, with reference to
Composite intake manifolds may have lighter weight, be less costly to produce, provide more insulation, and provide more design freedom than intake manifolds made from metal or ceramic materials. For example, intake manifolds made from metal, such as aluminum, steel, etc. may be costly to produce because of both material costs of the metal as well as production costs associated with casting and milling operations used to produce the metal intake manifold.
However, composite or plastic materials are generally not as strong or stiff as metal or ceramic materials. Thus composite manifolds may have NVH (noise, vibration, harshness), durability, and/or strength problems due to lack of sufficient structure in unsupported sections of the manifold's outer walls; for example, in areas where the manifold spans the cylinder heads of an engine.
In some examples, a framework 48 may be integrally molded onto at least a portion of the outer surface of intake manifold 10. Framework 48 may include a plurality of ribs, trusses, or a skeleton covering the manifold and made of the same material as the manifold. For example, the framework may be integrally molded to outer surfaces of the upper and lower outer walls of the manifold. In this way, structural support of the composite intake manifold may be enhanced.
However, even with framework 48, sections of outer walls of a composite intake manifold may lack sufficient structural support. In order to enhance the structural integrity of the composite manifold in regions of the manifold which lack sufficient structural support, a supporting member 50 may be overmolded in an outer wall, e.g., in upper outer wall 23, of the intake manifold such as shown in
The overmolded supporting member 50 may be composed of a material which has a greater tensile strength than the material that the composite manifold is made of. For example, if the intake manifold is composed of a first material, then the supporting member is composed of a second material, where the second material has a greater tensile strength than the first material. In some examples, the supporting member may be a plate made of metal, e.g., aluminum, magnesium, stainless steel, alloys, etc. In other examples, the supporting member may be a composite plate of a material more rigid, e.g., with greater tensile strength, than the base substrate comprising the intake manifold.
Overmolding the supporting member into the composite manifold may include inserting the supporting member substantially within an outer wall of the manifold, e.g., within upper outer wall 23 traversing from opposite the plurality of air outlets to the edge 27. For example, the supporting member may be fully overmolded in the upper outer wall of the composite intake manifold during the molding process used to produce the manifold. For example, supporting member 50 may be integrally sandwiched between two layers of upper outer wall 23 as shown in
Supporting member 50 may extend from a back side 37 of edge 27 toward the front of the manifold opposite the plurality of air outlets in the lower outer wall of the manifold. For example, the supporting member may extend from a side of the manifold opposing the air intake conduit 22 toward the air intake conduit. Additionally, the supporting member may be positioned between the first and second plurality of columns and the first plurality of outlets 28 and the second plurality of outlets 29.
In some examples, a region of the supporting member adjacent to the edge 27 opposite the air intake conduit 22, e.g., region 35 shown in
Further, the supporting member 50 may include a plurality of holes 54 or anchor points which may be used to further secure the supporting member to the intake manifold; thereby increasing the tensile strength conferred by the supporting member to the outer walls of the intake manifold. In some examples, the supporting member may be a lattice or truss type structure in order to decrease weight while still providing structural enhancement.
Supporting member 50 may substantially conform to the shape of the region of the composite intake manifold which includes the supporting member. Thus the supporting member may have a curved or undulating shape. For example, a region of the supporting member adjacent to the edge opposite the air intake conduit, e.g., region 61 shown in
In some examples, a dimension of the supporting member, e.g., the length, width, and/or thickness of the supporting member, may depend on a variety of physical properties of the intake manifold and/or engine. Such physical properties may include the span of the manifold (e.g., the distance between the cylinder heads), choice of material used in producing the intake manifold, engine type (e.g., size, number of cylinders, etc.), and/or other components surrounding and/or attached to the intake manifold.
Additionally, a width 52 of the supporting member may decrease or taper from the back of the supporting member to the front of the supporting member. For example, a width of the supporting member may decreases from a region of the edge 27 opposite the air intake conduit 22 toward the air intake conduit 22. The thickness 56 of the supporting member may be constant, throughout, e.g., the supporting member may be 3 mm thick. However, in some examples, the thickness 56 of the supporting member may vary, e.g., the thickness may decrease from back to front of the supporting member. Additionally, the width of the supporting member may be greater than the thickness of the supporting member by a threshold value. For example, the width may be at least five times the thickness.
By overmolding such a supporting member in the outer walls of a composite intake manifold, the structural integrity of the composite intake manifold may be enhanced without increasing thickness of the outer walls of the manifold or introducing structural elements within the hollow body of the manifold. Such a composite manifold may have increased air flow performance, reduced vibrations, lower material and part cost, and lower weight.
It will be appreciated that the configurations and routines disclosed herein are exemplary in nature, and that these specific embodiments are not to be considered in a limiting sense, because numerous variations are possible. For example, the above technology can be applied to V-6, I-4, I-6, V-12, opposed 4, and other engine types.
The subject matter of the present disclosure includes all novel and nonobvious combinations and subcombinations of the various systems and configurations, and other features, functions, and/or properties disclosed herein.
The following claims particularly point out certain combinations and subcombinations regarded as novel and nonobvious. These claims may refer to “an” element or “a first” element or the equivalent thereof. Such claims should be understood to include incorporation of one or more such elements, neither requiring nor excluding two or more such elements. Other combinations and subcombinations of the disclosed features, functions, elements, and/or properties may be claimed through amendment of the present claims or through presentation of new claims in this or a related application. Such claims, whether broader, narrower, equal, or different in scope to the original claims, also are regarded as included within the subject matter of the present disclosure.
The present application is a continuation of U.S. patent application Ser. No. 12/759,989 filed Apr. 14, 2010, now U.S. Pat. No. 8,360,025 issued Jan. 29, 2013, the entire contents of which are incorporated herein by reference for all purposes.
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Number | Date | Country | |
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20130139777 A1 | Jun 2013 | US |
Number | Date | Country | |
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Parent | 12759989 | Apr 2010 | US |
Child | 13753383 | US |