US20140080036A1 - Vehicle Component and Component Assembly Comprising Elastic Averaging Features - Google Patents
Vehicle Component and Component Assembly Comprising Elastic Averaging Features Download PDFInfo
- Publication number
- US20140080036A1 US20140080036A1 US14/086,018 US201314086018A US2014080036A1 US 20140080036 A1 US20140080036 A1 US 20140080036A1 US 201314086018 A US201314086018 A US 201314086018A US 2014080036 A1 US2014080036 A1 US 2014080036A1
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- Prior art keywords
- elastically deformable
- compression
- shape
- deformable protrusions
- face
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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Classifications
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- H01M2/1083—
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K1/00—Arrangement or mounting of electrical propulsion units
- B60K1/04—Arrangement or mounting of electrical propulsion units of the electric storage means for propulsion
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/24—Grouping of fuel cells, e.g. stacking of fuel cells
- H01M8/2465—Details of groupings of fuel cells
- H01M8/247—Arrangements for tightening a stack, for accommodation of a stack in a tank or for assembling different tanks
- H01M8/2475—Enclosures, casings or containers of fuel cell stacks
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/218—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by the material
- H01M50/22—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by the material of the casings or racks
- H01M50/227—Organic material
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
- H01M50/233—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by physical properties of casings or racks, e.g. dimensions
- H01M50/24—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders characterised by physical properties of casings or racks, e.g. dimensions adapted for protecting batteries from their environment, e.g. from corrosion
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/50—Fuel cells
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49622—Vehicular structural member making
Definitions
- the invention generally relates to an article of manufacture for a vehicle and an assembly that incorporates the article, and more specifically to an article of manufacture that incorporates elastically deformable features to secure and align the article to other articles, including other identical articles.
- the various different vehicular assemblies in which a first member must be precisely aligned with a second member may include, but are not limited to, multiple plates of a battery pack for an electric vehicle, multiple plates of a fuel cell pack for a hydrogen fuel cell, one or more components of a dashboard assembly relative to each other or a support structure, a body panel relative to the support structure, or a trim panel relative to the body panel.
- the different members may be aligned with a datum reference structure, in which one or more surfaces of the different members are pressed against the datum reference structure to remove the various degrees of movement between the different members.
- locating features may be machined into or otherwise attached to the different members.
- a certain amount of clearance must be designed into the locating features, which decreases the precision of the alignment.
- a vehicle member in an embodiment, includes a first face and a second opposing face, the vehicle member defining a cavity that extends inward into the second face.
- a first set and a second set of a plurality of elastically deformable protrusions extend outward from an outer surface of the first face.
- a first set and a second set of a plurality of compression features are disposed within the cavity. The respective first sets and the respective second sets of the plurality of elastically deformable protrusions and the plurality of compression features are spaced apart from each other.
- the respective first sets and the respective second sets of the plurality of elastically deformable protrusions and the plurality of compression features are geometrically distributed relative to each other such that when the first surface of a first of the vehicle member is matingly engaged face-to-face adjacent with the second surface of a second of the vehicle member, each of the plurality of elastically deformable protrusions press fit engage with respective ones of the plurality of compression features with an averaged elastic deformation between all of the plurality of elastically deformable protrusions of the first vehicle member and all of the plurality of compression features of the second vehicle member that precisely aligns the first and second vehicle members along a longitudinal central axis of at least one of the plurality of elastically deformable protrusions.
- an assembly in an embodiment, includes a plurality of members, each of the plurality of members having a first face and a second opposing face, each member of the plurality of members defining a cavity that extends inward into the second face.
- a first set and a second set of a plurality of elastically deformable protrusions extend outward from an outer surface of the first face.
- a first set and a second set of a plurality of compression features are disposed within the cavity. The respective first sets and the respective second sets of the plurality of elastically deformable protrusions and the plurality of compression features are spaced apart from each other.
- the first surface of a first of the plurality of members is matingly engaged face-to-face adjacent with the second surface of a second of the plurality of members, the respective first sets and the respective second sets of the plurality of elastically deformable protrusions and the plurality of compression features being geometrically distributed relative to each other such that each of the plurality of elastically deformable protrusions press fit engage with respective ones of the plurality of compression features with an averaged elastic deformation between all of the plurality of elastically deformable protrusions of the first member and all of the plurality of compression features of the second member that precisely aligns the first and second members along a longitudinal axis of the assembly.
- an interference fit engagement between locating protrusions of a first member and compression features of a second member secure the first member and the second member together during manufacture of the assembly.
- a plurality of elastically deformable locating protrusions and a plurality of elastically deformable compression features define multiple points of contact between the first member and the second member. The average of the elastic deformation between the locating protrusions and the compression features provides a precise and highly repeatable alignment of the first member relative to the second member, thereby precisely positioning the first member relative to the second member without the need of expensive datum alignment tools.
- the multiple contacts also increase the structural stiffness of the connection.
- FIG. 1 is a schematic perspective view of an assembly for a vehicle, wherein the assembly includes an energy storage device manufactured from a plurality of members.
- FIG. 2 is a schematic plan view of a first face of one of the members of the energy storage device shown in FIG. 1 .
- FIG. 3 is a schematic plan view of a second face of one of the members of the energy storage device shown in FIG. 1 .
- FIG. 4 is a schematic side view of a portion of one of the members of the energy storage device taken along cut line 4 - 4 shown in FIG. 2 , with some hidden line detail removed for clarity.
- FIG. 5 is an enlarged schematic plan view of a portion of one of the members of the energy storage device shown in FIG. 2 showing a plurality of locating protrusions.
- FIG. 6 is an enlarged schematic plan view of a portion of one of the members of the energy storage device shown in FIG. 3 showing a plurality of compression features.
- FIG. 7 is a schematic plan view of a first alternative shape of one of the locating protrusions.
- FIG. 8 is a schematic plan view of a second alternative shape of one of the locating protrusions.
- FIG. 9 is a schematic plan view of a third alternative shape of one of the locating protrusions.
- FIG. 10 is a schematic plan view of a fourth alternative shape of one of the locating protrusions.
- FIG. 11 is an enlarged schematic side view of one of the plurality of the locating protrusions manufactured from an active material, and shown in an initial and/or final shape.
- an assembly for a vehicle is shown generally at 20 .
- the assembly 20 includes an energy storage device 22 , such as but not limited to a battery pack or a fuel cell pack.
- the assembly 20 may include some other vehicular assembly 20 not shown or described herein, including but not limited to a dashboard assembly 20 or a body panel assembly 20 .
- the invention disclosed herein is described incorporated into the energy storage device 22 , it should be appreciated that the invention may be incorporated into other vehicular assemblies 20 , and that the energy storage device 22 is simply described as an exemplary embodiment of a vehicular assembly 20 including the invention.
- the energy storage device 22 includes a plurality of generally planar members 24 .
- Each of the members includes a first face 26 , shown in FIG. 2 , and a second face 28 , shown in FIG. 3 .
- the first face 26 and the second face 28 of the plurality of planar members 24 are defined by opposing, i.e., opposite, surfaces of each of the planar members 24 .
- the plurality of planar members 24 are arranged face-to-face adjacent each other along a longitudinal axis 30 to define a continuous stack 32 of planar members 24 . Accordingly, each first face 26 of one of the planar members 24 is disposed adjacent a second face 28 of another of the planar members 24 .
- the stack 32 of planar members 24 may include any number of planar members 24 .
- the energy storage device 22 may include several hundred of the planar members 24 . It should be appreciated that the exposed face of the end members of the stack 32 are not disposed adjacent other planar members 24 .
- the plurality of planar members 24 is described herein in terms of a first member 34 , shown in FIG. 2 , and a second member 36 , shown in FIG. 3 .
- the stack 32 of planar members 24 may include, but is not required to include, more than the first member 34 and the second member 36 , and that the description of the first member 34 and the second member 36 is applicable to all of the plurality of planar members 24 .
- each of the first member 34 and the second member 36 may include a plurality of elastically deformable locating protrusions 38 (depicted in groups 38 . 1 , 38 . 2 and 38 . 3 , for example, in FIG. 2 ) extending outward from an outer surface of the first face 26 .
- the locating protrusions 38 on the first member 34 and the second member 36 extend outward from the first face 26 of each member along a central axis 40 of each of the locating protrusions 38 respectively.
- Each of the locating protrusions 38 includes a cross sectional shape perpendicular to their respective central axis 40 .
- the cross sectional shape of the locating protrusions 38 may define, but is not limited to, one of a circular shape shown in FIG. 4 , a heptagon shape shown in FIG. 7 , an octagon shape shown in FIG. 8 , a decagon shape shown in FIG. 9 , or a dodecagon shape shown in FIG. 10 .
- the various locating protrusions 38 may also be of different sizes or varying scales within the same assembly 20 and or members 24 , incorporating both a coarse and fine locating sequence.
- Each of the first member 34 and the second member 36 may define a cavity 42 extending inward into the second face 28 of the first member 34 and the second member 36 respectively.
- the cavity 42 extends inward a depth 44 that is equal to or greater than a length 46 of the locating protrusions 38 .
- Each of the first member 34 and the second member 36 may further include a plurality of compression features 48 , 50 , 52 (depicted in groups: 48 . 1 , 50 . 1 , 52 . 1 ; 48 . 2 , 50 . 2 , 52 . 3 ; and 48 . 3 , 50 . 3 , 52 . 3 , for example, in FIG. 3 ) disposed within the cavity 42 of the first member 34 and the second member 36 respectively.
- the plurality of compression features 48 , 50 , 52 may include but are not limited to a combination of at least one compression protrusion 48 , at least one compression rib 50 , and at least one compression ridge 52 .
- Each compression protrusion 48 is a generally cylindrical shaft that extends along an axis that is parallel with the central axis 40 of each of the locating protrusions 38 respectively.
- Each compression rib 50 is an intermediate or interior wall that extends between opposing side walls of the first member 34 and the second member 36 respectively, and that extends along plane that is parallel with the central axis 40 of each of the locating protrusions 38 respectively.
- Each compression ridge 52 is a ridge of material disposed peripherally about the side walls of the first member 34 and the second member 36 respectively, and that extend along a line parallel with the central axis 40 of each of the locating protrusions 38 respectively inward toward a center of the cavity 42 .
- the compression protrusions 48 , the compression ribs 50 and the compression ridges 52 are all spaced from each other to define at least one region therebetween that is substantially equal to yet slightly smaller than one of the locating protrusions 38 . Accordingly, insertion of the locating protrusions 38 into the region between the various compression features 48 , 50 , 52 forces the locating protrusion 38 and/or at least one of the compression features 48 , 50 , 52 to compress.
- each of the first member 34 and the second member 36 are preferably identical, with each of the first member 34 and the second member 36 including a plurality of elastically deformable locating protrusions 38 , and each of the first member 34 and the second member 36 defining a cavity 42 and including a plurality of elastically deformable compression features 48 , 50 , 52 disposed within their respective cavities.
- the locating protrusions 38 and the compression features 48 , 50 , 52 include and are manufactured from an elastically deformable material.
- the locating protrusions 38 and the compression features 48 , 50 , 52 may include and be manufactured from a polymer material, including but not limited to a plastic.
- the locating protrusions 38 may include, but are not required to include, an active material capable of changing between a first shape and a second shape in response to a signal, such as but not limited to an electrical signal or a thermal signal.
- a signal such as but not limited to an electrical signal or a thermal signal.
- the active material forming the locating protrusions 38 changes from a non-energized shape into a temporary, energized shape, i.e., the first shape.
- the active material changes back to the non-energized shape, e.g., the second shape.
- Each adjacent pair of members i.e., the first member 34 and the second member 36 , includes the locating protrusions 38 of the first member 34 disposed within the cavity 42 of the second member 36 .
- the locating protrusions 38 of the first member 34 are disposed within the cavity 42 of the second member 36 in press fit engagement with the compression features 48 , 50 , 52 of the second member 36 . Insertion of the locating protrusions 38 into the cavity 42 elastically deforms one of the locating protrusions 38 and/or at least one of the compression features 48 , 50 , 52 .
- the elastic deformation between each of the locating protrusions 38 and at least one of the compression features 48 , 50 , 52 secures the first member 34 and the second member 36 together, relative to each other.
- the average of the elastic deformation between all of the locating protrusions 38 of the first member 34 and all of the compression features 48 , 50 , 52 of the second member 36 precisely and consistently aligns the first member 34 relative to the second member 36 along the longitudinal axis 30 of the stack 32 .
- the assembly 20 may include each of the generally planar members 24 defining one of the locating features 38 and the compression features 48 , 50 , 52 , with an elongated member 56 defining the other of the locating features 38 and the compression features 48 , 50 , 52 .
- the generally planar members 24 define the compression features 48 , 50 , 52 , with the elongated member 56 defining the locating protrusions 38 .
- the elongated member 56 spans a length 54 of the stack 32 of planar members 24 , thereby securing the generally planar members 24 together and positioning the generally planar members 24 relative to each other.
- a method of manufacturing the assembly 20 is provided. While the method is described relative to the exemplary energy storage device 22 shown in the drawings, it should be appreciated that the scope of the method is not limited to the manufacture of the energy storage device 22 , but is also applicable to the manufacture of other assemblies 20 .
- the method includes forming the first member 34 to include the plurality of elastically deformable locating protrusions 38 .
- the first member 34 is formed such that the locating protrusions 38 extend outward from the exterior surface, i.e., the first face 26 , of the first member 34 .
- the locating protrusions 38 may be formed in any desirable area of the first face 26 .
- the locating protrusions 38 are formed in areas having a critical alignment requirement, including but not limited to cooling channels, side profiles, tie rod holes, battery cells, seal areas, etc.
- Forming the first member 34 may include forming the plurality of locating protrusions 38 integrally with the first member 34 from a common material.
- the first member 34 and the locating protrusions 38 may be formed through a plastic injection molding process or the like from a polymer, i.e., plastic material.
- the first member 34 and the locating protrusions 38 may be machined into the first member 34 through conventional machining processes.
- forming the first member 34 to include the plurality of locating protrusions 38 may include forming the locating protrusions 38 separately from the first member 34 .
- the separate and distinct locating protrusions 38 may be formed from the same material used for the first member 34 , or alternatively, may be formed from a different material than used to form the first member 34 , such as but not limited to an active material. If the locating protrusions 38 are formed separately from the first member 34 , then forming the first member 34 to include the plurality of locating protrusions 38 includes mounting the locating protrusions 38 to the pre-formed first member 34 .
- the locating protrusions 38 may be mounted in any suitable manner, such as but not limited to fasteners, chemical bonding, welding, or over molding. For example, if the locating protrusions 38 are formed separately from the first member 34 , then, forming the locating protrusions 38 separately from the first member 34 may include over molding the plurality of locating protrusions 38 onto the pre-formed first member 34 .
- the method further includes forming the second member 36 to define a cavity 42 , and to include the plurality of elastically deformable compression features 48 , 50 , 52 disposed within the cavity 42 .
- each member may include both the locating protrusions 38 on the first face 26 and the cavity 42 with the compression features 48 , 50 , 52 therein on the second face 28 , or may alternatively include separate members, such as the elongated member 56 described above.
- the cavity 42 with the compression features 48 , 50 , 52 are formed in positions along the second member that generally correspond to and align with the locating projections 38 of the first member 34 .
- Forming the second member 36 may include forming the plurality of compression features 48 , 50 , 52 integrally with the second member 36 from a common material.
- the second member 36 and the compression features 48 , 50 , 52 may be formed through a plastic injection molding process or the like from a polymer, i.e., plastic material.
- the second member 36 and the compression features 48 , 50 , 52 may be machined into the second member 36 through conventional machining processes.
- the method further includes inserting the locating protrusions 38 of the first member 34 into the cavity 42 of the second member 36 in press fit engagement with the plurality of compression features 48 , 50 , 52 .
- Inserting the plurality of locating protrusions 38 into the cavity 42 in press fit engagement includes elastically deforming the locating protrusions 38 and/or at least one of the compression features 48 , 50 , 52 .
- the elastic deformation of the locating protrusion 38 and/or at least one of the compression features 48 , 50 , 52 secures the first member 34 and the second member 36 relative to each other.
- the average of the elastic deformation between all of the plurality of locating protrusions 38 and all of the plurality of compression features 48 , 50 , 52 precisely and repeatably aligns the first member 34 relative to the second member 36 .
- the method further includes energizing the locating protrusions 38 to cause each of the plurality of locating protrusions 38 to change into the first shape prior to inserting the plurality of locating protrusions 38 into the cavity 42 .
- the method further includes de-energizing the locating protrusions 38 to cause each of the locating protrusions 38 to change into the second shape after the plurality of locating protrusions 38 are inserted into the cavity 42 .
- the second shape is an initial and/or final shape
- the first shape is a temporary installation shape
- energizing the locating protrusions 38 causes the shape of the locating protrusions 38 to change from the initial shape, i.e., the second shape, into the temporary installation shape, i.e., the first shape.
- the locating protrusions 38 may be de-energized to cause the locating protrusions 38 to thereby change back into the initial and/or final shape.
- the first shape e.g. the temporary installation shape
- the second shape e.g., the initial and/or final shape
- the inverted taper of the locating protrusions 38 may wedge into or otherwise more firmly grasp the compression features 48 , 50 , 52 to better secure the locating protrusions 38 within the cavity 42 .
- the method may further include fixing the first member 34 and the second member 36 together.
- Fixing the first member 34 and the second member 36 may include permanently attaching the first member 34 and the second member 36 together.
- the first member 34 and the second member 36 may be permanently attached in any suitable manner specific to the type of assembly 20 being manufactured.
- fixing the first member 34 and the second member 36 together may include but is not limited to fastening the first member 34 and the second member 36 together with a fastener, welding the first member 34 and the second member 36 together, or bonding the first member 34 and the second member 36 together with a chemical adhesive.
- the press-fit engagement between the locating protrusions 38 of the first member 34 and the compression features 48 , 50 , 52 of the second member 36 are only intended to be a temporary alignment and attachment, with the final and permanent attachment being achieved through other fixing processes.
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Abstract
Description
- This application is a continuation and claims the benefit of U.S. patent application Ser. No. 13/229,926, filed on Sep. 12, 2011, which claims the benefit of U.S. Provisional Patent Application Ser. No. 61/411,614, filed on Nov. 9, 2010, the disclosures of which are hereby incorporated by reference herein in their entirety.
- The invention generally relates to an article of manufacture for a vehicle and an assembly that incorporates the article, and more specifically to an article of manufacture that incorporates elastically deformable features to secure and align the article to other articles, including other identical articles.
- When manufacturing various different assemblies for a vehicle, it is often very important to precisely align a first member relative to a second member to align stacked assemblies or to achieve small, uniform gaps for function or appearance. The various different vehicular assemblies in which a first member must be precisely aligned with a second member may include, but are not limited to, multiple plates of a battery pack for an electric vehicle, multiple plates of a fuel cell pack for a hydrogen fuel cell, one or more components of a dashboard assembly relative to each other or a support structure, a body panel relative to the support structure, or a trim panel relative to the body panel.
- The different members may be aligned with a datum reference structure, in which one or more surfaces of the different members are pressed against the datum reference structure to remove the various degrees of movement between the different members. Alternatively, locating features may be machined into or otherwise attached to the different members. However, in order to account for the part variations between the locating features, a certain amount of clearance must be designed into the locating features, which decreases the precision of the alignment.
- In an embodiment, a vehicle member includes a first face and a second opposing face, the vehicle member defining a cavity that extends inward into the second face. A first set and a second set of a plurality of elastically deformable protrusions extend outward from an outer surface of the first face. A first set and a second set of a plurality of compression features are disposed within the cavity. The respective first sets and the respective second sets of the plurality of elastically deformable protrusions and the plurality of compression features are spaced apart from each other. The respective first sets and the respective second sets of the plurality of elastically deformable protrusions and the plurality of compression features are geometrically distributed relative to each other such that when the first surface of a first of the vehicle member is matingly engaged face-to-face adjacent with the second surface of a second of the vehicle member, each of the plurality of elastically deformable protrusions press fit engage with respective ones of the plurality of compression features with an averaged elastic deformation between all of the plurality of elastically deformable protrusions of the first vehicle member and all of the plurality of compression features of the second vehicle member that precisely aligns the first and second vehicle members along a longitudinal central axis of at least one of the plurality of elastically deformable protrusions.
- In an embodiment, an assembly includes a plurality of members, each of the plurality of members having a first face and a second opposing face, each member of the plurality of members defining a cavity that extends inward into the second face. A first set and a second set of a plurality of elastically deformable protrusions extend outward from an outer surface of the first face. A first set and a second set of a plurality of compression features are disposed within the cavity. The respective first sets and the respective second sets of the plurality of elastically deformable protrusions and the plurality of compression features are spaced apart from each other. The first surface of a first of the plurality of members is matingly engaged face-to-face adjacent with the second surface of a second of the plurality of members, the respective first sets and the respective second sets of the plurality of elastically deformable protrusions and the plurality of compression features being geometrically distributed relative to each other such that each of the plurality of elastically deformable protrusions press fit engage with respective ones of the plurality of compression features with an averaged elastic deformation between all of the plurality of elastically deformable protrusions of the first member and all of the plurality of compression features of the second member that precisely aligns the first and second members along a longitudinal axis of the assembly.
- In an embodiment, an interference fit engagement between locating protrusions of a first member and compression features of a second member secure the first member and the second member together during manufacture of the assembly. A plurality of elastically deformable locating protrusions and a plurality of elastically deformable compression features define multiple points of contact between the first member and the second member. The average of the elastic deformation between the locating protrusions and the compression features provides a precise and highly repeatable alignment of the first member relative to the second member, thereby precisely positioning the first member relative to the second member without the need of expensive datum alignment tools. The multiple contacts also increase the structural stiffness of the connection.
- The above features and advantages and other features and advantages of the present invention are readily apparent from the following detailed description of the best modes for carrying out the invention when taken in connection with the accompanying drawings.
-
FIG. 1 is a schematic perspective view of an assembly for a vehicle, wherein the assembly includes an energy storage device manufactured from a plurality of members. -
FIG. 2 is a schematic plan view of a first face of one of the members of the energy storage device shown inFIG. 1 . -
FIG. 3 is a schematic plan view of a second face of one of the members of the energy storage device shown inFIG. 1 . -
FIG. 4 is a schematic side view of a portion of one of the members of the energy storage device taken along cut line 4-4 shown inFIG. 2 , with some hidden line detail removed for clarity. -
FIG. 5 is an enlarged schematic plan view of a portion of one of the members of the energy storage device shown inFIG. 2 showing a plurality of locating protrusions. -
FIG. 6 is an enlarged schematic plan view of a portion of one of the members of the energy storage device shown inFIG. 3 showing a plurality of compression features. -
FIG. 7 is a schematic plan view of a first alternative shape of one of the locating protrusions. -
FIG. 8 is a schematic plan view of a second alternative shape of one of the locating protrusions. -
FIG. 9 is a schematic plan view of a third alternative shape of one of the locating protrusions. -
FIG. 10 is a schematic plan view of a fourth alternative shape of one of the locating protrusions. -
FIG. 11 is an enlarged schematic side view of one of the plurality of the locating protrusions manufactured from an active material, and shown in an initial and/or final shape. - Referring to the Figures, wherein like numerals indicate like parts throughout the several views, an assembly for a vehicle is shown generally at 20. As shown herein, the
assembly 20 includes anenergy storage device 22, such as but not limited to a battery pack or a fuel cell pack. However, theassembly 20 may include some othervehicular assembly 20 not shown or described herein, including but not limited to adashboard assembly 20 or abody panel assembly 20. Although the invention disclosed herein is described incorporated into theenergy storage device 22, it should be appreciated that the invention may be incorporated into othervehicular assemblies 20, and that theenergy storage device 22 is simply described as an exemplary embodiment of avehicular assembly 20 including the invention. - Referring to
FIGS. 1 through 3 , theenergy storage device 22 includes a plurality of generallyplanar members 24. Each of the members includes afirst face 26, shown inFIG. 2 , and asecond face 28, shown inFIG. 3 . Thefirst face 26 and thesecond face 28 of the plurality ofplanar members 24 are defined by opposing, i.e., opposite, surfaces of each of theplanar members 24. The plurality ofplanar members 24 are arranged face-to-face adjacent each other along alongitudinal axis 30 to define acontinuous stack 32 ofplanar members 24. Accordingly, eachfirst face 26 of one of theplanar members 24 is disposed adjacent asecond face 28 of another of theplanar members 24. Thestack 32 ofplanar members 24 may include any number ofplanar members 24. For example, theenergy storage device 22 may include several hundred of theplanar members 24. It should be appreciated that the exposed face of the end members of thestack 32 are not disposed adjacent otherplanar members 24. - For the purpose of describing the invention, the plurality of
planar members 24 is described herein in terms of afirst member 34, shown inFIG. 2 , and asecond member 36, shown inFIG. 3 . However, it should be appreciated that thestack 32 ofplanar members 24 may include, but is not required to include, more than thefirst member 34 and thesecond member 36, and that the description of thefirst member 34 and thesecond member 36 is applicable to all of the plurality ofplanar members 24. - Referring also to
FIGS. 4 through 6 , each of thefirst member 34 and thesecond member 36 may include a plurality of elastically deformable locating protrusions 38 (depicted in groups 38.1, 38.2 and 38.3, for example, inFIG. 2 ) extending outward from an outer surface of thefirst face 26. The locatingprotrusions 38 on thefirst member 34 and thesecond member 36 extend outward from thefirst face 26 of each member along acentral axis 40 of each of the locatingprotrusions 38 respectively. Each of the locatingprotrusions 38 includes a cross sectional shape perpendicular to their respectivecentral axis 40. The cross sectional shape of the locatingprotrusions 38 may define, but is not limited to, one of a circular shape shown inFIG. 4 , a heptagon shape shown inFIG. 7 , an octagon shape shown inFIG. 8 , a decagon shape shown inFIG. 9 , or a dodecagon shape shown inFIG. 10 . The various locatingprotrusions 38 may also be of different sizes or varying scales within thesame assembly 20 and ormembers 24, incorporating both a coarse and fine locating sequence. - Each of the
first member 34 and thesecond member 36 may define acavity 42 extending inward into thesecond face 28 of thefirst member 34 and thesecond member 36 respectively. Preferably, thecavity 42 extends inward adepth 44 that is equal to or greater than alength 46 of the locatingprotrusions 38. Each of thefirst member 34 and thesecond member 36 may further include a plurality ofcompression features FIG. 3 ) disposed within thecavity 42 of thefirst member 34 and thesecond member 36 respectively. The plurality of compression features 48, 50, 52 may include but are not limited to a combination of at least onecompression protrusion 48, at least onecompression rib 50, and at least onecompression ridge 52. Eachcompression protrusion 48 is a generally cylindrical shaft that extends along an axis that is parallel with thecentral axis 40 of each of the locatingprotrusions 38 respectively. Eachcompression rib 50 is an intermediate or interior wall that extends between opposing side walls of thefirst member 34 and thesecond member 36 respectively, and that extends along plane that is parallel with thecentral axis 40 of each of the locatingprotrusions 38 respectively. Eachcompression ridge 52 is a ridge of material disposed peripherally about the side walls of thefirst member 34 and thesecond member 36 respectively, and that extend along a line parallel with thecentral axis 40 of each of the locatingprotrusions 38 respectively inward toward a center of thecavity 42. The compression protrusions 48, thecompression ribs 50 and thecompression ridges 52 are all spaced from each other to define at least one region therebetween that is substantially equal to yet slightly smaller than one of the locatingprotrusions 38. Accordingly, insertion of the locatingprotrusions 38 into the region between the various compression features 48, 50, 52 forces the locatingprotrusion 38 and/or at least one of the compression features 48, 50, 52 to compress. - Accordingly, each of the
first member 34 and thesecond member 36 are preferably identical, with each of thefirst member 34 and thesecond member 36 including a plurality of elasticallydeformable locating protrusions 38, and each of thefirst member 34 and thesecond member 36 defining acavity 42 and including a plurality of elastically deformable compression features 48, 50, 52 disposed within their respective cavities. - The locating
protrusions 38 and the compression features 48, 50, 52 include and are manufactured from an elastically deformable material. For example, the locatingprotrusions 38 and the compression features 48, 50, 52 may include and be manufactured from a polymer material, including but not limited to a plastic. Additionally, the locatingprotrusions 38 may include, but are not required to include, an active material capable of changing between a first shape and a second shape in response to a signal, such as but not limited to an electrical signal or a thermal signal. As described in greater detail below, upon applying the signal, the active material forming the locatingprotrusions 38 changes from a non-energized shape into a temporary, energized shape, i.e., the first shape. Upon removal of the signal, the active material changes back to the non-energized shape, e.g., the second shape. - Each adjacent pair of members, i.e., the
first member 34 and thesecond member 36, includes the locatingprotrusions 38 of thefirst member 34 disposed within thecavity 42 of thesecond member 36. The locatingprotrusions 38 of thefirst member 34 are disposed within thecavity 42 of thesecond member 36 in press fit engagement with the compression features 48, 50, 52 of thesecond member 36. Insertion of the locatingprotrusions 38 into thecavity 42 elastically deforms one of the locatingprotrusions 38 and/or at least one of the compression features 48, 50, 52. The elastic deformation between each of the locatingprotrusions 38 and at least one of the compression features 48, 50, 52 secures thefirst member 34 and thesecond member 36 together, relative to each other. The average of the elastic deformation between all of the locatingprotrusions 38 of thefirst member 34 and all of the compression features 48, 50, 52 of thesecond member 36 precisely and consistently aligns thefirst member 34 relative to thesecond member 36 along thelongitudinal axis 30 of thestack 32. - While the invention has so far been described to include multiple
identical members 24, each defining both the locatingprotrusions 38 and the compression features 48, 50, 52, it should be appreciated that the members need not be identical. For example, as shown inFIG. 1 , theassembly 20 may include each of the generallyplanar members 24 defining one of the locating features 38 and the compression features 48, 50, 52, with anelongated member 56 defining the other of the locating features 38 and the compression features 48, 50, 52. As shown, the generallyplanar members 24 define the compression features 48, 50, 52, with theelongated member 56 defining the locatingprotrusions 38. Theelongated member 56 spans alength 54 of thestack 32 ofplanar members 24, thereby securing the generallyplanar members 24 together and positioning the generallyplanar members 24 relative to each other. - A method of manufacturing the
assembly 20 is provided. While the method is described relative to the exemplaryenergy storage device 22 shown in the drawings, it should be appreciated that the scope of the method is not limited to the manufacture of theenergy storage device 22, but is also applicable to the manufacture ofother assemblies 20. - The method includes forming the
first member 34 to include the plurality of elasticallydeformable locating protrusions 38. Thefirst member 34 is formed such that the locatingprotrusions 38 extend outward from the exterior surface, i.e., thefirst face 26, of thefirst member 34. The locatingprotrusions 38 may be formed in any desirable area of thefirst face 26. Preferably, the locatingprotrusions 38 are formed in areas having a critical alignment requirement, including but not limited to cooling channels, side profiles, tie rod holes, battery cells, seal areas, etc. - Forming the
first member 34 may include forming the plurality of locatingprotrusions 38 integrally with thefirst member 34 from a common material. For example, thefirst member 34 and the locatingprotrusions 38 may be formed through a plastic injection molding process or the like from a polymer, i.e., plastic material. Alternatively, thefirst member 34 and the locatingprotrusions 38 may be machined into thefirst member 34 through conventional machining processes. - Alternatively, forming the
first member 34 to include the plurality of locatingprotrusions 38 may include forming the locatingprotrusions 38 separately from thefirst member 34. The separate and distinct locatingprotrusions 38 may be formed from the same material used for thefirst member 34, or alternatively, may be formed from a different material than used to form thefirst member 34, such as but not limited to an active material. If the locatingprotrusions 38 are formed separately from thefirst member 34, then forming thefirst member 34 to include the plurality of locatingprotrusions 38 includes mounting the locatingprotrusions 38 to the pre-formedfirst member 34. The locatingprotrusions 38 may be mounted in any suitable manner, such as but not limited to fasteners, chemical bonding, welding, or over molding. For example, if the locatingprotrusions 38 are formed separately from thefirst member 34, then, forming the locatingprotrusions 38 separately from thefirst member 34 may include over molding the plurality of locatingprotrusions 38 onto the pre-formedfirst member 34. - The method further includes forming the
second member 36 to define acavity 42, and to include the plurality of elastically deformable compression features 48, 50, 52 disposed within thecavity 42. As described above, each member may include both the locatingprotrusions 38 on thefirst face 26 and thecavity 42 with the compression features 48, 50, 52 therein on thesecond face 28, or may alternatively include separate members, such as theelongated member 56 described above. Thecavity 42 with the compression features 48, 50, 52 are formed in positions along the second member that generally correspond to and align with the locatingprojections 38 of thefirst member 34. - Forming the
second member 36 may include forming the plurality of compression features 48, 50, 52 integrally with thesecond member 36 from a common material. For example, thesecond member 36 and the compression features 48, 50, 52 may be formed through a plastic injection molding process or the like from a polymer, i.e., plastic material. Alternatively, thesecond member 36 and the compression features 48, 50, 52 may be machined into thesecond member 36 through conventional machining processes. - The method further includes inserting the locating
protrusions 38 of thefirst member 34 into thecavity 42 of thesecond member 36 in press fit engagement with the plurality of compression features 48, 50, 52. Inserting the plurality of locatingprotrusions 38 into thecavity 42 in press fit engagement includes elastically deforming the locatingprotrusions 38 and/or at least one of the compression features 48, 50, 52. In so doing, the elastic deformation of the locatingprotrusion 38 and/or at least one of the compression features 48, 50, 52 secures thefirst member 34 and thesecond member 36 relative to each other. Additionally, the average of the elastic deformation between all of the plurality of locatingprotrusions 38 and all of the plurality of compression features 48, 50, 52 precisely and repeatably aligns thefirst member 34 relative to thesecond member 36. - If the material used to form the plurality of locating
protrusions 38 includes an active material, in which the activematerial locating protrusions 38 include a first shape when in the energized state, and a second shape when in the de-energized shape, then the method further includes energizing the locatingprotrusions 38 to cause each of the plurality of locatingprotrusions 38 to change into the first shape prior to inserting the plurality of locatingprotrusions 38 into thecavity 42. The method further includes de-energizing the locatingprotrusions 38 to cause each of the locatingprotrusions 38 to change into the second shape after the plurality of locatingprotrusions 38 are inserted into thecavity 42. If the second shape is an initial and/or final shape, and the first shape is a temporary installation shape, then energizing the locatingprotrusions 38 causes the shape of the locatingprotrusions 38 to change from the initial shape, i.e., the second shape, into the temporary installation shape, i.e., the first shape. Upon the locatingprotrusions 38 being inserted into thecavity 42 and into engagement with the compression features 48, 50, 52, the locatingprotrusions 38 may be de-energized to cause the locatingprotrusions 38 to thereby change back into the initial and/or final shape. - For example, the first shape, e.g. the temporary installation shape, may include but is not limited to a cylindrical shape, and the second shape, e.g., the initial and/or final shape, may include but is not limited to an inverted taper, shown generally at 58 in
FIG. 11 , extending along thecentral axis 40 of each respective locatingprotrusion 38. Accordingly, the inverted taper of the locatingprotrusions 38 may wedge into or otherwise more firmly grasp the compression features 48, 50, 52 to better secure the locatingprotrusions 38 within thecavity 42. - Once the locating
protrusions 38 are inserted into the cavities into press fit engagement with the compression features 48, 50, 52, then the method may further include fixing thefirst member 34 and thesecond member 36 together. Fixing thefirst member 34 and thesecond member 36 may include permanently attaching thefirst member 34 and thesecond member 36 together. Thefirst member 34 and thesecond member 36 may be permanently attached in any suitable manner specific to the type ofassembly 20 being manufactured. For example, fixing thefirst member 34 and thesecond member 36 together may include but is not limited to fastening thefirst member 34 and thesecond member 36 together with a fastener, welding thefirst member 34 and thesecond member 36 together, or bonding thefirst member 34 and thesecond member 36 together with a chemical adhesive. In so doing, the press-fit engagement between the locatingprotrusions 38 of thefirst member 34 and the compression features 48, 50, 52 of thesecond member 36 are only intended to be a temporary alignment and attachment, with the final and permanent attachment being achieved through other fixing processes. - While exemplary modes for carrying out the invention have been described in detail, those familiar with the art to which this invention relates will recognize various alternative designs and embodiments for practicing the invention within the scope of the appended claims.
Claims (20)
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US14/086,018 US20140080036A1 (en) | 2010-11-09 | 2013-11-21 | Vehicle Component and Component Assembly Comprising Elastic Averaging Features |
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2011
- 2011-09-12 US US13/229,926 patent/US9812684B2/en active Active
- 2011-11-03 DE DE102011117562A patent/DE102011117562A1/en not_active Withdrawn
- 2011-11-08 CN CN2011103490278A patent/CN102463882A/en active Pending
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2013
- 2013-11-21 US US14/086,018 patent/US20140080036A1/en not_active Abandoned
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Also Published As
Publication number | Publication date |
---|---|
DE102011117562A1 (en) | 2012-05-10 |
CN102463882A (en) | 2012-05-23 |
US9812684B2 (en) | 2017-11-07 |
US20120115010A1 (en) | 2012-05-10 |
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