The present disclosure is generally directed to leaf springs and particularly directed to composite leaf springs and methods of making the leaf springs for applications, such as automotive systems.
Vehicle manufacturers have long sought to reduce weight of vehicles for the purposes of improving fuel economy, increasing payload capacity, and enhancing the ride and handling characteristics of automobiles, trucks, utility vehicles, and recreational vehicles. Moreover, automotive companies also desire ways to cost effectively reduce vehicle weight in order to meet federally mandated fuel economy requirements.
A large proportion of vehicles employ steel leaf springs as load carrying and energy storage devices in their suspension systems. While an advantage of steel leaf springs is that they can be used as attaching linkages and/or structural members in addition to their capacity as an energy storage device, they are substantially less efficient than other types of springs in terms of energy storage capacity per unit of mass, thereby also reducing fuel economy. Steel leaf springs are heavy by nature, noisy, and subject to corrosion. This weight requires additional consideration with respect to mounting requirements, as well as damping requirements. For instance, shock absorbers are often necessary with the use of steel leaf springs in order to control the mass of the leaf spring under operating conditions.
Accordingly, what is needed is an alternative leaf spring that can provide a lighter weight assembly construction thereby increasing vehicle fuel economy.
According to aspects illustrated herein, there is provided a composite leaf spring comprising a thermoset matrix material reinforced with fibers embedded in the matrix of the composite leaf spring.
According to further aspects illustrated herein, there is provided a method of making a composite leaf spring. The method comprises forming a plurality of layers of composite material comprising a fiber reinforced thermoset polymeric material to form a plurality of precut and shaped blanks. The method further comprises inserting and stacking the blanks in a gluing fixture; and gluing the blanks to form the composite leaf spring.
The inventors have determined that the composite leaf springs disclosed herein comprised of fiber reinforced thermoset polymeric (FRTP) materials can provide a much lighter assembly than, e.g., traditional steel leaf springs, and thereby increase fuel economy of a vehicle, such as an automobile, light truck, and so forth. In addition, the fiber reinforced composite leaf springs and assemblies disclosed herein transmit less noise than steel leaf springs, and require less damping force than steel leaf springs to maintain control under operating conditions.
The composite leaf springs disclosed herein, according to embodiments, comprise overload springs, often referred to as second stage load leafs. According to embodiments, a composite leaf spring comprises a thermoset matrix material reinforced with fibers embedded in the matrix of the composite leaf spring. The polymer matrix from which the composite leaf spring and/or composite layers thereof are manufactured comprises any suitable thermoset polymeric matrix material, according to embodiments. Non-limiting examples of suitable thermoset matrix materials include phenolics, polyesters, epoxides, combinations thereof, and so forth.
Particles or fibers that are embedded in the polymer matrix material to form the thermoset composite material can include, but are not limited to, carbon, glass, Kevlar® fiber, aramid fibers, combinations of the foregoing, and the like that are embedded in the polymer matrix material to form the polymer composite material. In addition to the above-described particles and fibers, iron particles can also be incorporated into the composite material disclosed herein. It is noted that the fibers can be continuous and/or non-continuous fibers.
According to embodiments, fiber reinforced thermoset composite leaf springs may generally be comprised of a combination of thermoset polymeric matrix materials, high strength reinforcing fibers and other reinforcing materials.
Thermoset polymer loading by weight can vary widely depending on physical property requirements of the intended use of the product sheet. A composite material may contain about 50 to about 15 wt % thermoset matrix, more preferably about 40 to about 20 wt % and most preferably, about 30 to about 25 wt % of thermoset matrix material, by weight of thermoset matrix material plus fibers.
The reinforcing fibers used may include, but are not limited to, glass fibers (such as E-glass and S-glass), aramid fibers (KEVLAR®), carbon fibers, and other high strength fibers and combinations thereof. Other fibers may also be incorporated, preferably in combination with E-glass and/or S-glass, but optionally instead of E- and/or S-glass. Such other fibers include ECR, A and C glass, as well as other glass fibers; fibers formed from quartz, magnesia alumuninosilicate, non-alkaline aluminoborosilicate, soda borosilicate, soda silicate, soda lime-aluminosilicate, lead silicate, non-alkaline lead boroalumina, non-alkaline barium boroalumina, non-alkaline zinc boroalumina, non-alkaline iron aluminosilicate, cadmium borate, alumina fibers, asbestos, boron, silicone carbide, graphite and carbon such as those derived from the carbonization of polyethylene, polyvinylalcohol, saran, aramid, polyamide, polybenzimidazole, polyoxadiazole, polyphenylene, PPR, petroleum and coal pitches (isotropic), mesophase pitch, cellulose and polyacrylonitrile, ceramic fibers, metal fibers as for example steel, aluminum metal alloys, and the like.
Where high performance is required and cost justified, high strength organic polymer fibers formed from an aramid exemplified by Kevlar may be used. Other preferred high performance, unidirectional fiber bundles generally have a tensile strength greater than 7 grams per denier. These bundled high-performance fibers may be more preferably any one of, or a combination of, aramid, extended chain ultra-high molecular weight polyethylene (UHMWPE), poly [p-phenylene-2,6-benzobisoxazole] (PBO), and poly[diimidazo pyridinylene (dihydroxy) phenylene].
In addition, materials such as metals, e.g., aluminum, steel, and other ferrous and/or non ferrous metals, plastics, epoxies, composites, and/or other suitable materials may be used as reinforcements, additives or inserts to impart specific mechanical, dimensional or other physical properties either uniformly throughout the spring, or in specific regions of the spring.
It is noted that an exemplary, non-limiting combination of materials for a composite leaf spring, according to embodiments, is an epoxy matrix reinforced with E-glass fibers.
Various constructions and configurations of leaf springs and assemblies, according to embodiments, are set forth below. It is noted that advantageously with respect to the following descriptions and embodiments, any or all of the components of the leaf spring and/or assemblies can be made of the afore-described fiber reinforced thermoset polymeric (FRTP) composite materials and optional additional reinforcements, and in any combination of materials thereof. Moreover, it is noted that like reference numerals set forth in the Figures refer to like elements and descriptions, accordingly.
With reference to
At least one layer of composite material generally, but not limited to, having an elastic modulus lower than the material of the primary leaf 12, is disposed substantially parallel to and bonded to one of the tension surface 14 and the compression surface 16 of the primary leaf 12, according to embodiments. The at least one layer of composite material is preferably formed from a plurality of substantially parallel fibers embedded in a polymeric matrix. As shown in
The hybrid leaf spring 10 is typically fabricated by bonding the first layer of composite material 20 and the second layer of composite material 22 to the primary leaf 12 and placing the assembled components in a press employing a heated die having a shape conforming to the desired unloaded shape of the finished hybrid leaf spring. The components are then pressed together and through the combination of heat and pressure hybrid leaf springs of consistent repeatable shape can be formed. However, the present invention is not limited in this regard as other fabrication techniques known to those skilled in the pertinent art, such as molding, may be employed.
A clamping means 24 is employed to couple the leaf spring 10 in a three-point configuration to an axle 26 of a vehicle, according to embodiments. In the illustrated embodiment, the clamping means 24 includes a pair of U-bolts 28 extending around the axle 26 with the leaf spring 10 being received between the U-bolts. A locking plate 30 defining two pairs of apertures 32 for receiving ends 34 of the U-bolts 28 is positioned adjacent to the second layer of composite material 22 and fasteners 36 are threadably engaged with the ends of the U-bolts for releasably clamping the U-bolts and the leaf spring 10 onto the axle 26. In addition, a load leaf 38 for enhancing the load carrying capacity of the leaf spring 10 in the area of highest stress is interposed between the second layer of composite material 22 and the locking plate 30.
A load leaf (overload spring) 38 can be bonded to the second layer of composite material 22 or it can be retained in contact with the second layer of composite material by the clamping means 24. The load leaf (overload spring) 38 can be either curved or flat, and may or may not vary in cross-section and be constructed of, e.g., the afore-described fiber reinforced thermoset polymeric (FRTP) material.
In order to properly position the leaf spring 10 along the axle 26, a positioner 40 is engaged with the axle 26, according to embodiments, and in the illustrated embodiment of
Advantageously, the inventors have herein determined that one or all of the components of the leaf spring 10 of
As shown in
Another embodiment is shown in
Accordingly, composite leaf springs in accordance with embodiments herein, may utilize a single leaf design, as shown in, e.g.,
Typically, however, the leaf spring 110 functions as a second stage leaf (overload spring 110), e.g., within, on or under, a stack of other leafs, and comprising the afore-described fiber reinforced thermoset polymeric (FRTP) composite material.
The overload spring 110 of
A cut away section 111 is also shown in
A positioner 120 is also depicted in
Also depicted in
It is further noted that the embodiment of
The inventors have also determined that in addition to employing the afore-referenced fiber reinforced thermoset polymeric (FRTP) composite material, the weight of the resultant structures and assemblies can be even further reduced by varying, e.g., increasing the section modulus of the composite leaf spring (e.g., overload spring) 110 thus eliminating width.
Accordingly, as shown in, e.g., the embodiments of
In the embodiment depicted in
It is further noted that while individual stacked layers 116 are described above in various embodiments of the composite leaf spring 110 (e.g., overload spring 110), embodiments could be machined/molded, e.g., without such layering and in the resultant configurations disclosed herein, such as in a one piece configuration with, e.g., open channels 124 and with inserts 126 integrally formed therein.
With regard to the methods of manufacturing, it is noted that the composite leaf springs, assemblies and so forth, according to embodiments, can be manufactured by combining the afore-described fiber reinforced thermoset polymeric (FRTP) material including the reinforcing fibers and other appropriate materials in the presence of heat and/or pressure, usually in a mold or other device that imparts a desired shape to the assembly. The heating and consolidating can typically be performed at, e.g., between about 400° F. and about 600° F., including between about 450° F. and about 550° F., and at a pressure of, e.g., up to about 300 psi for construction.
Also, according to embodiments, bar stock of desired material, e.g., comprising the afore-referenced fiber reinforced thermoset polymeric (FRTP) composite material of desired thickness, such as. e.g., about 0.5 inches, can be slit to a desired width. The material is then cut to the appropriate length, including end tapers if desired. The precut and shaped bar stock blanks are placed in a gluing (adhesive) fixture employing a suitable glue/adhesive, along with appropriate glued or pinned spacers. Accordingly, possible design/manufacturing modifications include stacking and gluing/pining the, e.g, 0.5 inch shaped composite bar stock to the desired width; utilization of spacers including, e.g, composite, metal, plastic, and so forth, stacked and glued/pinned to the load shaped bearing composite bar stock lineals to achieve the desired with; and stacking and gluing/pinning of the, e.g., 0.5 inch bar stock to the desired width and then machining out the channels or slots. It is further noted at a bar stock of about 0.5 inches is advantageously able to achieve a faster cure time than, e.g, much thicker stocks. However, the invention is not limited to this particular thickness and any suitable dimensions/configurations may be employed. A further advantage of embodiments disclosed herein is that hybrid constructions are disclosed herein where, e.g, composites can be employed in the load bearing structure and the same, or even alternative materials can be employed in mounting sections where, e.g, abrasion or compressive properties are needed and can be addressed with use of suitable materials having the desired properties therefore.
The final strength and stiffness, as well as other desirable properties, depends upon the thermoset material(s) used, as well as the type, size, and orientation of the reinforcements and other materials used. In addition, the strength and stillness of the final product is also dependent upon the overall dimensional shape of the composite leaf spring, including length, width, thickness, and cross-sectional areas.
In some embodiments, the shape of the composite leaf spring may be developed by buildup of layers of pre-impregnated (prepreg) reinforcing materials. This buildup of layers is usually inserted into a shaped tool or mold, where heat and/or pressure may be applied to consolidate the materials.
Although this invention has been shown and described with respect to the detailed embodiments thereof, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiments disclosed in the above detailed description, but that the invention will include all embodiments falling within the scope of the appended claims.
This patent application claims priority benefit under 35 U.S.C. §119(e) of copending, commonly owned U.S. Provisional Patent Application Ser. No. 61/788,199, filed on Mar. 15, 2013, the contents of which is incorporated by reference herein in its entirety.
Number | Date | Country | |
---|---|---|---|
61788199 | Mar 2013 | US |