STRUCTURAL MODULE HAVING FRANGIBLE EXTENSION MEMBER
20230356572 · 2023-11-09
Inventors
Cpc classification
B60J5/0418
PERFORMING OPERATIONS; TRANSPORTING
B60J5/0461
PERFORMING OPERATIONS; TRANSPORTING
B60J5/0455
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A structural door module for a motor vehicle door includes a carrier plate with a dryside and wetside surface configured for mounting components thereto. The carrier plate includes an extension member projecting inwardly toward the vehicle interior. A frangible connection seam is disposed at least partially around the interface between the extension member and the carrier plate. In response to a side impact load, the carrier plate moves inwardly, and the frangible connection seam at least partially severs. The carrier plate moves inwardly relative to the extension member, limiting intrusion of the extension member into the passenger compartment.
Claims
1. A structural door module for a motor vehicle closure panel, comprising, a carrier plate including a dryside surface facing an interior of the motor vehicle and an opposed wetside surface facing an exterior of the motor vehicle; a frangible connection seam extending across at least a portion of the carrier plate; wherein the frangible connection seam severs relative to the carrier plate in response to an impact load exerted on the carrier plate.
2. The structural door module of claim 1, wherein the structural door module further comprises an extension member integrally formed with the carrier plate and projecting away from the carrier plate, wherein the frangible connection seam extends at least partially around an interface between the extension member and the carrier plate.
3. The structural door module of claim 2, wherein the connection seam extends fully around the interface, and the extension member separates fully from the carrier plate in response to the impact load.
4. The structural door module of claim 2, wherein the connection seam extends partially around the interface, and a retaining section of the interface extends between opposite ends of the connection seam, and the extension member separates partially from the carrier plate and pivots about the retaining section relative to the carrier plate in response to the impact load.
5. The structural door module of claim 2, wherein the connection seam is defined by a reduced material thickness relative to the carrier plate.
6. The structural door module of claim 2, wherein the connection seam defines a flat interface that is orthogonal to the impact load when the impact load is directed toward the interior of the vehicle.
7. The structural door module of claim 4, wherein the retaining section is disposed along an upper edge of the extension member and the connections seam extends along a bottom edge and lateral edges of the extension member.
8. The structural door module of claim 4, wherein the connection seam has a reduced material thickness relative to the retaining section.
9. The structural door module of claim 2, wherein the extension member includes two arm rest supports each having the connection seam.
10. The structural door module of claim 2, wherein the extension member is configured to retain its shape in response to severing the connection seam, wherein the carrier plate moves inwardly relative to the retained shape of the extension member in response to the impact load.
11. A method of limiting inward intrusion by a structural module of a vehicle closure panel during a side impact, the method including the steps of: providing a structural module having an extension member integrally formed with and projecting from a carrier plate; providing a frangible connection seam disposed around at least a portion of an interface between the carrier plate and the extension member; receiving an impact load at the carrier plate directed inwardly; in response to receiving the impact load, shifting the carrier plate inwardly and at least partially severing the frangible connection seam.
12. The method of claim 11, further comprising maintaining a connection between the extension member and the carrier plate along a retaining section therebetween in response to shifting the carrier plate inwardly.
13. The method of claim 12, wherein the frangible connection seam extends around the interface and includes first and second ends, wherein the retaining section extends between the first and second ends, wherein the extension member bends relative to the carrier plate about the retaining section in response to the carrier plate shifting inwardly.
14. The method of claim 11, wherein the frangible connection seam defines a closed loop around the interface, the method including fully severing the extension member relative to the carrier plate in response to shifting the carrier plate inwardly.
15. The method of claim 11, wherein at least a portion of the extension member remains attached to an interior trim component in response to the carrier plate shifting inwardly.
16. The method of claim 11, wherein the carrier plate defines an aperture, wherein the extension member encloses the aperture prior to receiving the impact load, wherein at least a portion of the extension member translates through the aperture in response to receiving the impact load.
17. The method of claim 11, further comprising severing a reduced material thickness along the connection seam in response to receiving the impact load, wherein the extension member shifts relative to the carrier plate in areas corresponding to the reduced material thickness.
18. A structural door module for a motor vehicle closure panel, comprising: a carrier plate including a dryside surface facing an interior of the motor vehicle and an opposed wetside surface facing an exterior of the motor vehicle; an extension member integrally formed with the carrier plate and projecting outwardly from the carrier plate and toward a passenger compartment of the motor vehicle; an aperture formed in the carrier plate and enclosed by the extension member along an interface between the extension member and the carrier plate; wherein at least a portion of the interface has a reduced material thickness relative to the carrier plate; wherein the extension member severs relative to the carrier plate along the reduced material thickness of the interface in response to an inwardly directed impact load exerted on the carrier plate.
19. The structural door module of claim 18, wherein the reduced material thickness extends fully around the interface to define a closed loop, wherein the extension member fully severs relative to the carrier plate.
20. The structural door module of claim 18, wherein the reduced material thickness extends along a first portion of the interface, and a retaining section extends along a second portion of the interface, wherein the second portion of the interface has a greater thickness than the first portion of the interface, wherein the first portion severs and the second portion retains the extension member to the carrier plate in response to the impact load.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0030] Preferred embodiments of the present invention will now be described, by way of example only, with reference to the attached Figures, wherein:
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DETAILED DESCRIPTION OF THE INVENTION
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[0052] Carrier plate 22 may include a number of integrally formed or molded components. Integrally formed components on carrier plate 22, as shown in
[0053] Carrier plate 22 is preferably manufactured from a composite material and molded into the desired shape. In the preferred embodiment, carrier plate 22 is manufactured using a 30% polypropylene matrix with glass reinforcement fibers. Other matrix materials will occur to those of skill in the art. Other reinforcement fibers contemplated include Kevlar, carbon fibers, and hemp, and other reinforcement materials will occur to those of skill in the art. As used herein, portions and/or features described as being integral with the carrier plate are formed as part of the molding process, which is to be distinguished from separate components that are then later fixed or attached to the formed/molded carrier plate 22. Put another way, the integral components may be part of a one-piece or single piece structure. Such a one-piece structure may be homogenous, or may be in the form of multi-shot molding where different materials are molded and formed together to define a generally fixed structure. For instance while the arm rest 15 may be attached and fixedly secured to the carrier plate 20, these components are not “integral.” The arm rest supports 34 projecting from the carrier plate 20, however, are “integral.” However, as discussed further, even with an integrally formed component, portions of the component could separate in response to an impact of other force applied to the integrally formed structure. This ability for a portion to separate is distinguishable from separately attached components that are designed to be formed separately and then attached together.
[0054] The support ribs 33 are a series of integrally formed ridges that traverse portions of the dryside and wetside surfaces of carrier plate 22, thereby reinforcing carrier plate 22. The inherent material strength of the composite material used in carrier plate 22 combined with support ribs 33 reinforces door module 20, and thus strengthens the motor vehicle door body when mounted thereto.
[0055] Referring additionally to
[0056] During a side-impact collision, arm rest support 34 is designed to be frangible relative to the carrier plate 22. Put another way, the arm rest support 34 is configured to sever or break from the carrier plate 22, at least partially, such that the carrier plate 22 may shift inwardly relative to the vehicle door 10 (having the arm rest 34 support attached for example with a fastener or the like) while the arm rest support 34 does not substantially intrude into the passenger compartment. The arm rest 15 and the supports 34 may instead remain generally in place while the outer components move inwardly.
[0057] As can be seen clearly in
[0058] In one aspect, the seam 54 may have a thickness of 1.0 mm, and the remainder of the flat area (or directly adjacent areas) may be 2 mm. Other relative thicknesses may be chosen depending on the size and arrangement of the carrier plate 22 and the arrangement of the arm rest 15 or trim that is supported by the arm rest support 34. The thickness of the seam 54 may be chosen such that the arm rest support 34 may sufficiently support the arm rest and be resistant to downward forces (from the weight of the arm, for example) during normal vehicle use, but still thin enough that during increased stress and loading caused by a crash event, such as a side impact event, the seam 54 will break or sever relative to the carrier plate 22, which itself receives the force of impact and shifts inwardly.
[0059] The flat interface 55 may be entirely comprised of the seam 54, such that the carrier plate 22 and the arm rest support 34 transition directly into the seam 54. Put another way, a curved transition portion of the arm rest support 34 may extend into the seam 54, and the seam 54 may then transition into a curved transition portion of the carrier plate 22. In another aspect, the curved transitions on either side of the seam 54 may transition into a straight or flat section on one or both sides of the seam 54. These curved transitions, whether leading directly to the seam 54 or leading to a flat portion on either side of the seam 54, may have a greater thickness that the seam as described above, thereby defining a reduced thickness along the seam that provides less resistance to an impact force and that thereby will sever or break in response to such a force while the surrounding structure remains thick enough to withstand such force.
[0060] The arrangement of the seam 54 is such that the seam 54 is part of the flat area that is orthogonal to the load direction during a side impact. Accordingly, the side impact load direction will have a reduced counter-acting reaction force vector from the arm rest support 34. However, it will be appreciated that the seam 54 will inherently provide a modicum of resistance opposite the inwardly directed force vector during a crash impact. Due to the reduced thickness of the seam 54 and the reduction or lack of a substantial reaction force at the location of the seam 54, the seam 54 will break or sever prior to a substantial loading of the arm rest support 34 or the surrounding area, such that after the seam 54 breaks, the arm rest support 34 will no longer receive a load (or will receive a reduced load) from the carrier plate 22 as the carrier plate is being impacted, and the arm rest support 34 will thereby be limited from intruding inwardly into the passenger compartment.
[0061] The above description of the seam 54 includes a seam 54 that extends fully around the base of the arm rest support 34, such that the arm rest support may be completely frangible from the carrier plate 22 when the carrier plate 22 receives a side impact. However, even with the seam 34 defining a full closed loop, the direction and/or force of the impact may still result in partial severing or breaking, such that a portion of the support 34 remains integral with the carrier plate 22. In another aspect, the arm rest support 34 is only partially surrounded by a frangible section. In such an arrangement, the seam 54 does not form an entire closed loop. Rather, the seam 54 may be formed to leave a thicker portion to define hinge-type structure, for example a U-shape. The thicker portion may simply be the same material thickness as the surrounding structure, or may be only a slightly reduced thickness, with the seam 34 being defined by the U-shape having the full reduced thickness that is thinner than the slightly reduced thickness. Thus, the full reduced thickness along the U-shape will sever or break prior to the hinge-portion, and a bending or pivoting movement of the carrier plate about the hinge portion may occur, with the arm rest support 34 again remaining generally stationary. This type of arrangement is described in further detail below with reference to
[0062] With reference to
[0063] As shown, the retaining section 154a is at the top of the arm rest support 34, such that the arm rest support 34 will move downwardly. However, the retaining section 154a could also be disposed on a lateral side or the bottom of the arm rest support 34, with corresponding pivoting movement. The selection of the location of the retaining section 154a may be made in accordance with the desired controlled pivoting movement of the arm rest support 34 (or the carrier plate 22 relative to the arm rest support 34) during a side impact event.
[0064] Due to the bending that occurs at the retaining section 154a, the retaining section 154a may also be considered or referred to as a living hinge. In this aspect, the retaining section 154a may have a thickness that is greater than the seam 154, but still less than the surrounding carrier plate structure, such that the arm rest support 34 and the carrier plate 22 may still bend relative to each other in a controlled manner in response to the thinner connection seam 154 breaking.
[0065] With reference to
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[0069] The opening between the carrier plate 22 and the arm rest support 34 that occurs in response to at least partially severing the connection therebetween may be referred to as an aperture 38 defined by the carrier plate 22. Accordingly, the arm rest support 34 extends inwardly from the aperture 38, and is configured to move at least partially into the aperture in response to an impact event, or to translate at least partially through the aperture. The arm rest support 34 moves into the aperture 38 whether complete or partial severance occurs, as illustrated in
[0070] The arm rest support 34, being an extension relative to the carrier plate 22 toward the vehicle interior, may also be referred to as an extension member. Indeed, the concepts described above are applicable to other support structure, and are not limited to arm rest supports. Other support structures that extend inwardly toward the vehicle relative to the carrier plate 22 or other similar structure may therefore also have a similar seam extending around at least a portion of the base of such an extension member, to allow for controlled severing between the extension member and the carrier plate 22. The seam may be a pre-formed area in the body of the carrier plate 22, such as an indentation, a fold, a bend, an area of reduced strength, and area of reduced weakness, a partially perforated area, as non-limiting examples, to facilitate severing first along the seam, before severing of the adjacent body of the carrier plate 22, as may occur when a crash load is applied to the carrier 22. The shape of the base of the extension member may also vary relative to the illustrated arm rest support 34. For example, the arm rest support 34 is shown to generally include four main sides. However, other support structures with fewer sides, such as a triangular base, or a greater number of sides, may be used. The selection of which portions of the interface between the base of the extension member, and the module from which it extends, may be selected to control the areas of the interface that sever and the relative movement that occurs between the module and the extension member during a side impact event.
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[0072] Method 200 includes the steps of: at step 202, Providing a module having an extension member; at step 204, Providing a frangible connection between the module and the extension member; and, at step 206, configuring the frangible connection to break, separating at least in part the module from the extension member.
[0073] Method 300 includes the steps of: at step 302, Providing a module having an aperture; at step 304, Providing an extension member extending from the module and aligned with the aperture; and, at step 306, Configuring at least part of the extension member to pass through the aperture in response to at least a partial separation of the extension member from the module.
[0074] Method 400 includes the steps of: at step 402, Providing a module having an extension member; and, at step 404, Configuring the extension member to at least partially disconnect from the module to allow the extension member to move relative to the module in a crash condition.
[0075] Method 500 includes the steps of: at step 502, providing a structural module having an extension member projecting from a carrier plate; at step 504, providing a frangible connection seam disposed around at least a portion an interface between the carrier plate and the extension member; at step 506, receiving an impact load at the carrier plate directed inwardly; and, at step 508, in response to receiving the impact load, shifting the carrier plate inwardly and at least partially severing the frangible connection seam.
[0076] The above-described embodiments of the invention are intended to be examples of the present invention and alterations and modifications may be effected thereto, by those of skill in the art, without departing from the spirit of the invention.