The subject invention relates to a shock tower that includes at least one overmolded bracket that is made from a continuous fiber reinforced polymer composite (CFRP) material, for example.
Vehicles utilize many different suspension systems and components to absorb vibrations from road load inputs to improve vehicle control and passenger comfort. One such suspension component is a shock tower that is used to facilitate mounting of a damping component between a vehicle fixed structure and a suspension component for a vehicle wheel. Traditionally, shock towers have been formed from stamped steel components that are welded together to form a final assembly. These steel shock towers are heavy, time consuming to assemble, and adversely affect fuel economy. Die cast aluminum and magnesium shock towers provide for weight savings over traditional steel shock towers; however, these solutions have a cost premium that is only suitable for certain applications.
In one exemplary embodiment, a method of making a shock tower assembly includes forming a bracket from continuous fiber reinforced thermoplastic, where the bracket has a load bearing portion an overmolded portion. The method further includes placing the bracket in an injection tool, injecting a polymer composite material into the injection tool to surround the overmolded portion of the bracket, and removing a finished component from the injection tool, wherein the finished component comprises the load bearing portion of the bracket extending outwardly from the finished component and the overmolded portion of the bracket that is surrounded by the polymer composite material.
In a further embodiment of the above, the method includes thermoforming the bracket from an organo sheet to a predetermined shape.
In a further embodiment of any of the above, the method includes providing at least one location feature in the injection tool, inserting the bracket into the location feature, and applying pressure to opposing sides of the bracket to hold the bracket in place.
In a further embodiment of any of the above, the method includes at least one attachment feature in the load bearing portion of the bracket and inserting the load bearing portion of the bracket into the location feature such that the attachment feature is protected from the polymer composite material during injection molding.
In another exemplary embodiment, a shock tower assembly includes a shock tower body composed of a polymer composite material, and at least one bracket composed of a continuous fiber reinforced thermoplastic, the bracket having a load bearing portion extending outwardly from the shock tower body and an overmolded portion that is attached to the shock tower body at an overmolding interface.
In a further embodiment of any of the above, at least one attachment feature is formed in the load bearing portion of the bracket, wherein the attachment feature is configured to be attached to load bearing component.
In a further embodiment of any of the above, the overmolded portion of the bracket includes a transversely extending lip or flange that is overmolded with the polymer composite material.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
As shown in
As shown in
In one example configuration, a load bearing bracket 30 (
A method of making a component 38 with the bracket 30 is shown in
In one example, the bracket 30 is thermoformed from an organo sheet to a predetermined shape. Once in the required shape, the bracket 30 can then be trimmed and drilled/machined to include one or more attachment features as needed. In one example, the attachment feature comprises at least one attachment hole 44 that facilitates mechanical bonding with the polymer composite material during injection. In another example, the attachment feature comprises at least one flange 46 formed at one end of the bracket 30 to facilitate mechanical bonding with the polymer composite material during injection. Other types of attachment features could also be incorporated in the bracket 30 to interface with the polymer composite material during injection to increase bonding of the bracket 30 to the component body 40.
In one example, the bracket 30 is heated to improve adhesion during injection. A heat source 48, such as an electric heater or heating element for example, can be used to heat the bracket 30 before being placed into the tool 34 or during the injection process.
In one example, at least one attachment feature 50 is formed in the load bearing portion 32 of the bracket 30. The attachment feature 50 can comprise a mounting hole with or without a metallic insert, flange, etc. that is configured for attachment to a load bearing component. In one example, the attachment feature 50 is machined into the bracket 30 prior to being inserted into the tool 34.
In one example, at least one location feature 52 is made in the injection tool 34. The bracket 30 is inserted into the location feature 52 and pressure is applied to opposing sides of the bracket 30 to hold the bracket in place during injection. The load bearing portion 32 of the bracket 30 is inserted into the location feature 52 such that the attachment feature 50 is protected from the polymer composite material during injection. In one example, the location feature 52 comprises a groove and the attachment feature 50 comprises at least one hole.
In one example, a first slide 60 is used to apply pressure against a first side 62 of the bracket 30 and a second slide 64 is used to apply pressure against a second side 66 of the bracket 30, opposite the first side 62, such that the bracket 30 is securely clamped between the first 60 and second 64 slides during injection of the polymer composite material. The slides 60, 64 also keep the bracket 30 in place during closing of the tool 34 (
In one example, the component body 40 defines a planar surface 70 that surrounds the bracket 30 at the overmold interface 42. The load bearing portion 32 of the bracket 30 extends outwardly away from the planar surface 70 to a second end 82 that is configured for attachment via at least one fastener 74 to a load bearing component 76 (
The bracket 30 extends from a first end 80 to the second end 82 to define a bracket length that can vary per various design parameters The bracket has a thickness defined between the opposing sides 62, 66 that is limited by the CFRP thermoforming process.
In one example, the overmolded portion 42 includes a transversely extending lip or flange 46 with the first end 80 that is overmolded with the polymer composite material. This further increases the attachment strength of the bracket 30 to the component body 40. Optionally, metallic parts can be attached to the bracket 30 by riveting, fastening, etc., or during injection molding to further increase load bearing capabilities.
The subject invention provides a CFRP bracket 30 overmolded into a main component body structure, such as a shock tower structure for example, which results in significant weight and cost reduction when compared to traditional steel and aluminum component structures. The subject invention provides an out-of-plane bracket that supports loading of an integrated componeont body where the overmolded interface of the bracket is sufficiently strong to provide an attachment interface to other load bearing components. In addition to being used in shock towers, the subject invention could be applied to other parts made by injection or compression molding and that require brackets out of the main plane of the part with load bearing capabilities and without draft angle.
Although a preferred embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.
Number | Name | Date | Kind |
---|---|---|---|
2730772 | Jones | Jan 1956 | A |
3875661 | Lidstrom | Apr 1975 | A |
5217800 | Pentecost | Jun 1993 | A |
5226695 | Flint | Jul 1993 | A |
5358302 | Schoen | Oct 1994 | A |
5358779 | McGarry | Oct 1994 | A |
6174482 | Reames | Jan 2001 | B1 |
6202778 | Mistry | Mar 2001 | B1 |
6305733 | Rahmstorf | Oct 2001 | B1 |
6345706 | Oliver | Feb 2002 | B1 |
8556281 | Lee et al. | Oct 2013 | B2 |
8974224 | Stanley | Mar 2015 | B2 |
9371094 | Ferauche | Jun 2016 | B1 |
9542685 | Proud | Jan 2017 | B2 |
9580107 | Ranga | Feb 2017 | B1 |
9701250 | Ranga | Jul 2017 | B1 |
20030020202 | Ueno | Jan 2003 | A1 |
20040028858 | Schnell | Feb 2004 | A1 |
20050062308 | Pfister | Mar 2005 | A1 |
20050150087 | Lydan | Jul 2005 | A1 |
20050241259 | Rijsbergen | Nov 2005 | A1 |
20060061008 | Karner | Mar 2006 | A1 |
20060138038 | Proulx | Jun 2006 | A1 |
20070124912 | De Traglia Amancio Filho | Jun 2007 | A1 |
20070138835 | Kapadia | Jun 2007 | A1 |
20070295453 | Koelman | Dec 2007 | A1 |
20090202761 | Malek | Aug 2009 | A1 |
20090252908 | Angenheister | Oct 2009 | A1 |
20100028113 | Tohyama | Feb 2010 | A1 |
20110111176 | Chiu | May 2011 | A1 |
20110266785 | Mildner | Nov 2011 | A1 |
20110290980 | Bradshaw | Dec 2011 | A1 |
20120027983 | Elia | Feb 2012 | A1 |
20120028062 | Elia | Feb 2012 | A1 |
20120040169 | Boursier | Feb 2012 | A1 |
20120248821 | Schmied | Oct 2012 | A1 |
20130056466 | York | Mar 2013 | A1 |
20130057018 | Reese | Mar 2013 | A1 |
20130136529 | Py | May 2013 | A1 |
20130241108 | Zynda | Sep 2013 | A1 |
20130309435 | Boursier | Nov 2013 | A1 |
20130320742 | Murolo | Dec 2013 | A1 |
20140159425 | Kim | Jun 2014 | A1 |
20140252796 | Huber | Sep 2014 | A1 |
20140291894 | Kannengiesser | Oct 2014 | A1 |
20150068352 | Heitz | Mar 2015 | A1 |
20150093186 | Nabuurs | Apr 2015 | A1 |
20150130224 | Donabedian | May 2015 | A1 |
20160244103 | Amemiya | Aug 2016 | A1 |
20160304130 | Shin et al. | Oct 2016 | A1 |
20170100996 | Husek | Apr 2017 | A1 |
20170144504 | Al-Dahhan | May 2017 | A1 |
20170203798 | Bhosale | Jul 2017 | A1 |
20170305476 | Kulkarni | Oct 2017 | A1 |
20170313030 | Song | Nov 2017 | A1 |
20170320278 | Meeks | Nov 2017 | A1 |
20170370671 | Tucker | Dec 2017 | A1 |
20180056871 | Karner | Mar 2018 | A1 |
20180194277 | Lobo | Jul 2018 | A1 |
20180244215 | Husek | Aug 2018 | A1 |
20190106070 | Busuioc | Apr 2019 | A1 |
20190161126 | Dettling | May 2019 | A1 |
20190232578 | Kneveler | Aug 2019 | A1 |
Number | Date | Country |
---|---|---|
102011014849 | Sep 2012 | DE |
2967965 | Jun 2012 | FR |
Entry |
---|
Great Britain Search Report for Application No. GB 1900233.6 completed 21, Jun. 2019. |
Number | Date | Country | |
---|---|---|---|
20190210655 A1 | Jul 2019 | US |