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WO2018175599A1 - Circuits souples pour faisceaux électriques - Google Patents

Circuits souples pour faisceaux électriques Download PDF

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Publication number
WO2018175599A1
WO2018175599A1 PCT/US2018/023586 US2018023586W WO2018175599A1 WO 2018175599 A1 WO2018175599 A1 WO 2018175599A1 US 2018023586 W US2018023586 W US 2018023586W WO 2018175599 A1 WO2018175599 A1 WO 2018175599A1
Authority
WO
WIPO (PCT)
Prior art keywords
conductor
connecting end
insulator
harness assembly
electrical harness
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.)
Ceased
Application number
PCT/US2018/023586
Other languages
English (en)
Inventor
Kevin Michael Coakley
Malcom BROWN
Jose Juarez
Dongao YANG
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Cellink Corp
Original Assignee
Cellink Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Cellink Corp filed Critical Cellink Corp
Publication of WO2018175599A1 publication Critical patent/WO2018175599A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R16/00—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for
    • B60R16/02—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements
    • B60R16/0207—Wire harnesses
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00—Printed circuits
    • H05K1/02—Details
    • H05K1/0277—Bendability or stretchability details
    • H05K1/028—Bending or folding regions of flexible printed circuits
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K2201/00—Indexing scheme relating to printed circuits covered by H05K1/00
    • H05K2201/05—Flexible printed circuits [FPCs]
    • H05K2201/053—Tails
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K2201/00—Indexing scheme relating to printed circuits covered by H05K1/00
    • H05K2201/09—Shape and layout
    • H05K2201/09009—Substrate related
    • H05K2201/09063—Holes or slots in insulating substrate not used for electrical connections

Definitions

  • Provisional Patent Application 62/616,567 entitled: “Flexible Circuits for Electrical Harnesses” filed on 12-JAN-2018 (Docket No, CLNKPO 10P3 US), US Provisional Patent Application No. 62/485,544, entitled: "FLEXIBLE CIRCUITS FOR
  • each wire may have a round cross-sectional profile and may be individually surrounded by an insulating sleeve.
  • the cross-sectional size of each wire is selected based on the material and current transmitted by this wire.
  • resistive heating and thermal dissipation is a concern resulting in even larger cross-sectional sizes of wires in a conventional harness.
  • harnesses can be rather bulky, heavy, and expensive to manufacture.
  • automotive, aerospace and other industries strive for smaller, lighter, and less expensive components.
  • a harness assembly comprises a conductor trace, comprising a conductor lead a width to thickness ratio of at least 2, which provides for a lower thickness profile and enhances thermal conductivity with the environment.
  • a conductor trace may be formed from a thin sheet of metal.
  • the conductor trace also comprises connecting end, monolithic with the conductor lead.
  • the width to thickness ratio of the connecting end is less than that of conductor trace, allowing for direct mechanically and electrically connected to a connector of the harness assembly.
  • the connecting end may be folded, shaped, slit-rearranged, and the like to reduce its width to thickness ratio, which in some examples may be close to 1.
  • an electrical harness assembly comprises a connector and a first conductor trace.
  • the connector comprises a first contact interface and a first connecting portion.
  • the first conductor trace comprises a first conductor lead and a first connecting end.
  • the first conductor lead and the first connecting end of the first conductor trace are monolithic.
  • the first conductor lead has a width to thickness ratio of at least 2. The first connecting end of the first conductor trace electrically coupled to the first connecting portion of the connector.
  • the first connecting portion of the connector comprises a base and one or more tabs.
  • the first connecting end of the first conductor trace is crimped between the base and the one or more tabs of the first connecting portion.
  • the first connecting end of the first conductor trace may be welded to the base, in addition or instead of crimping using the tabs.
  • the first connecting portion of the connector comprises a first plate and a second plate parallel to the first plate and forming a cavity.
  • the first connecting portion further comprises a biasing element protruding into the cavity from the first plate toward the second plate. The first connecting end of the first conductor trace protrudes into the cavity and contacts the biasing element.
  • the first connecting end of the first conductor trace has a width to thickness ratio less than the width to thickness ratio of the fi rst conductor lead.
  • the first connecting end may be folded and/or reshaped.
  • the first connecting end may be slit into a plurality of strands, and wherein the plurality of strands is bundled together.
  • the electrical harness assembly further comprises a second conductor trace, comprising a second conductor lead and a second connecting end.
  • the second conductor lead and the second connecting end of the second conductor trace may be monolithic.
  • the second conductor lead may have a width to thickness ratio of at least 0,5.
  • the thickness of the second conductor lead and the thickness of the first conductor lead are identical.
  • the second conductor lead and the first conductor lead do not contact each other.
  • the second connecting end of the second conductor trace is electrically coupled to multiple connecting portions of the connector.
  • the connector may comprise one or more jumpers electrically coupling the multiple connecting portions.
  • the second conductor lead may be wider than the first conductor lead.
  • the first connecting end is a stack of multiple layers formed by folding the first conductor trace.
  • the first connecting end is a stack of two layers.
  • a car door assembly comprising a car door and an electrical harness assembly.
  • the car door comprises a surface.
  • An electrical harness assembly directly interfaces the surface of the car door.
  • the electrical harness assembly is attached to the surface of the car door.
  • the electrical harness assembly is conformal to the surface of the car door.
  • the electrical harness assembly has a widt to thickness ratio of at least about 2.
  • the electrical harness assembly may be attached to the surface of the car door along at least 90% of an interface between the electrical harness assembly and the surface [0010]
  • the electrical harness assembly comprises a first insulator, a first conductor trace, and a second insulator.
  • the first conductor trace is disposed between the first insulator and the second insulator.
  • the first insulator is disposed between the first conductor trace and the surface of the car door.
  • the first insulator is adhered to the surface of the car door using a thermally conductive mounting adhesive.
  • the thermally conductive mounting adhesive may be a thermally conductive pressure-sensitive adhesive (PSA) film.
  • the first insulator may comprise a material selected from the group consisting of polyimide (PI), polyethylene naphthalate (PEN), polyethylene terephthalate (PET), polymethyl niethacrylate (PMMA), ethyl vinyl acetate (EVA), polyethylene (PE),
  • polypropylene PP
  • polyvinyl fluoride PVF
  • polyamide PA
  • soldermask polyvinyl butyral
  • FIGS. 1 A and IB illustrate an electrical connector assembly, in accordance with some embodiments.
  • FIGS. 2A-2C illustrates an example of forming a connecting end of a conductor traces
  • FIGS, 3A-3C illustrates another example of forming a connecting end of a conductor traces.
  • FIGS. 3A-3C illustrates another example of forming a connecting end of a conductor traces.
  • FIG. 4 A illustrates an example of a partially assembled electrical harness assembly having different portions that are ready to be folded and stacked together.
  • FIG. 4B illustrates an expanded view of a portion of the electrical harness assembly shown in FIG. 4A.
  • FIG. 5 illustrates an example of a connecting portion of a connector coupled to a conductor trace using a biasing element disposed in a cavity of the connecting portion.
  • FIG. 6 is a top schematic view of a conductor trace, in accordance with some embodiments.
  • FIG S. 7A and 7B are cross-sectional schematic views of different parts of the conductor trace shown in FIG. 6, in accordance with some embodiments.
  • FIGS. 8A-8C illustrate an example of folding a connecting end of a conductor trace.
  • FIGS. 9A-9C illustrate an example of shaping a connecting end of a conductor trace.
  • FIGS. lOA-lOC illustrate an example of slitting and bundling individual strands a connecting end of a conductor trace.
  • FIG. 1 1 A is a schematic top view of a conductor trace prior to folding its connecting end and attaching a terminal, in accordance with some embodiments.
  • FIG. 1 I B illustrates a schematic cross-sectional view of the attachment portion of the conductor trace shown in FIG. 1 1 A.
  • FIG. 1 IC is a schematic top view of the conductor trace shown in FIG. 11 A after folding its connecting end, in accordance with some embodiments.
  • FIG. 11D illustrates a schematic cross-sectional view of the attachment portion of the conductor trace shown in FIG. 1 IC.
  • FIG. 1 IE illustrates a schematic top view of the conductor trace shown in FIGS. 1 1A and 1 1C after attaching the terminal, in accordance with some embodiments.
  • FIGS. 12A-12C iilustrate schematic top views of different examples of a conductor trace prior to folding its connecting end, in accordance with some embodiments.
  • FIG S. 13 A - 13E illustrate schematic cross-sectional views of the attachment portion of the conductor trace after folding its connecting end, in accordance with some embodiments.
  • FIG. 14A illustrates a schematic top view of four conductor traces prior to folding and repositioning their connecting ends and attaching terminals, in accordance with some embodiments.
  • FIG. 14B illustrates a schematic top view of the four conductor traces shown in FIG. 14A after folding and repositioning their connecting ends and attaching terminals, in accordance with some embodiments.
  • FIG. 14C illustrates a schematic top view of conductor traces positioned out of plane and forming connections to terminals of the connector at different levels.
  • FIGS, 14D and 14E illustrate a schematic top view of three conductor traces before and after connecting these conductor traces to terminals.
  • FIG. 15A illustrates a schematic top view of conductor traces with partially formed connecting ends.
  • FIG. 15B illustrates a schematic top view of the conductor traces of FIG. 15A now with fully formed connecting ends.
  • FIG. 6A illustrates a schematic top view of a harness assembly comprising an insulator and multiple conductor leads adhered to and supported by the insulator.
  • FIG. 6B illustrates a schematic top view of an insulator comprising three insulator openings that divide insulator into four insulator strips.
  • FIG. 16C illustrates a schematic top view of the insulator shown in FIG. 16B with one end of the insulator turned 90° relative to the other end within a plane.
  • FIGS. 16E and 16F illustrate schematic cross-section views of the insulator strips of the insulator shown in FIG. 16C at different locations.
  • FIG. 17 is a process flowchart corresponding to a method of forming the interconnect circuit, in accordance with some embodiments.
  • FIG S. 1.8 A- 18C illustrate a schematic top view of an electrical harness assembly with a connector assembly with and without jumpers interconnecting different conductor traces of the harness assembly
  • FIG. 18D illustrates a schematic cross-section view of the connector assembly shown in FIG. 18C showing arrangement on multiple jumpers interconnecting different conductor traces of the harness assembly.
  • FIG. 19A illustrates a car door assembly comprising a car door and an electrical harness assembly mechanically supported by and thermally coupled to the car door, in accordance with some embodiments.
  • FIGS. 19B and 19C illustrate an electrical harness assembly being substantially conformal to the surface of the door
  • FIG. 19D illustrates various heat transfer aspect between a flat wire of the electrical harness assembly and the car door.
  • FIG. 20 illustrates a reference diagram of a conventional wire contacting the car door
  • FIGS. 21 A and 21B are schematic top and cross-section views showing the widths of gaps between two-conductor leads.
  • FIGS. 22A and 22B are schematic cross-section views of a conductor trace showing a base sublayer and two examples of a surface sublayer,
  • FIG. 22C is a schematic cross-section view of a conductor trace showing a base sublayer and an electrically insulating coating.
  • FIG. 23 illustrates an example of two harnesses supported on the same carrier film.
  • Electrical harnesses are used to deliver power and/or signals in various applications, such as vehicles, appliances, electronics, and the like.
  • Conventional harnesses typically utilize round wires formed from round conductive leads (e.g., solid round wires or stranded bundles of round wires) insulated by polymer shells. These round wires are often bundled together into a harness. Unfortunately, these bundles can be hard, if possible at all, to feed through narrow spaces. Furthermore, round wires have poor thermal connections to surrounding flat structures and therefore experience very little heat dissipation during their operation. As a result, larger gauge wires are often used in such harnesses to avoid excessive resistive (joule) heating.
  • joule resistive
  • harnesses formed using flat conductor traces, rather than wires with round cross-sections.
  • These conductor traces may be formed, for example, from a sheet foil.
  • all traces of the same harness may be formed from the same sheet of foil simplifying production of the harness and allowing for robust electrical connections between traces due to the monolithic nature of the sheet.
  • the formed traces may have a coplanar orientation or, more generally, the traces may be arranged as a one-dimensional array in some cross-sections of the harness.
  • a combination of the flat conductor traces and their arrangement allows forming a harness that is both thin and flexible as well as capable of thermal coupling to surrounding structures.
  • the thickness of the harness may be a combination of thicknesses of the conductor traces, one or two insulators, and one or more adhesive layers, if used.
  • a thin harness or, more specifically, a thin flexible harness can be fed through narrow spaces that may be not suitable to bundled conventional harnesses. [0055] Because of the small overall thickness and the coplanar orientation of the conductor traces, the harness can be very flexible in at least a direction
  • the flexibility may be a lot greater than that of a harness formed by the bundled wires. This flexibility may be used to conform the harness to various planar and non-planar surfaces, such as an interior surface of a car door which has many topographical variations.
  • the conformality and small thickness of the harness allows to achieve substantial cooling of individual conductor traces in the harness.
  • the conductor traces with smaller cross-sectional areas may be used in the provided harness than in conventional harnesses. This thermal coupling and small wire cross-section, in turn, leads to a smaller weight size, and cost of the harnesses.
  • One challenge with using flat conductor traces in a harness is forming electrical connections between such traces and other components, such as connectors and other traces /wires, which may have different dimensions or, more specifically, smaller width to thickness ratios.
  • connectors for wire harness may use contact interfaces that are square or round, or, more generally, have comparable widths and thicknesses, e.g., have a width to thickness ratio of about 1 or between 0. 5 and 2.
  • a conductor trace in a proposed flexible circuit may have a width to thickness ratio of at least about 2 or at least about 5 or even at least about 10.
  • Such conductor traces may be referred to as flat conductor traces or flat wires to distinguish them from round wires.
  • Various approaches are described herein to form electrical connections to the flat conductor traces.
  • FIGS. 1 A and IB illustrate electrical connector assembly 90, in accordance with some embodiments.
  • Electrical connector assembly 90 may be a part of harness assembly 100 further described below.
  • Electrical connector assembly 90 comprises connector 110 and first conductor trace 140a, which may be also referred to as first conductor trace 140a to distinguish from other conductor traces of the same harness, if present. For simplicity , only one conductor trace is shown in these figures.
  • Connector 1 10 comprises first contact interface 120a and first connecting portion 130a
  • First contact interface 120a may be used to make an external connection formed by connector assembly 90 and may be in the form of a pin, socket, tab, and the like.
  • First contact interface 120a and first connecting portion 130a may be made from the same materials, e.g., copper, aluminum, and the like.
  • first contact interface 120a and first connecting portion 130a are monolithic.
  • first contact interface 120a and first connecting portion 130a may be formed from the same strip of metal.
  • First conductor trace 140a comprises first conductor lead 150a and first connecting end 160a.
  • First connecting end 160a is electrically coupled to first connecting portion 130a of connector 1 0, Specifically, first connecting end 160a and first connecting portion 130a may directly contact each other and overlap within the housing of connector 1 10.
  • each connector is coupled to a different conductor trace.
  • multiple connectors may be coupled to the same conductor trace.
  • a single connector may be coupled to multiple conductor traces.
  • multiple connectors may be coupled to multiple conductor traces such that all of these connectors and traces are electrically interconnected.
  • First conductor lead 150a extends away from connector 110, e.g., to another connector 144 or forms some other electrical connection within connector assembly 90.
  • the length of first conductor lead 150a may be at least about 500 millimeters or even at least about 1000 millimeters.
  • First conductor lead 150a may be insulated on one or both sides using, for example, first insulator 142 and second insulator 144 as schematically shown in FIG. 19D and described below. In some embodiments, first insulator 142 and second insulator 144 do not extend to first connecting end 160a, allowing first connecting end 160a to directly interface first connecting portion 130a.
  • first insulator 142 and second insulator 144 may overlap with first connecting portion 130a, while still exposing another side of first connecting end 160a and allowing this side to directly interface first connecting portion 130a.
  • electrical connections to first connecting portion 130a made through openings in one of first insulator 142 and second insulator 144.
  • first insulator 142 and second insulator 144 may overlap with first connecting portion 130a.
  • external insulation to first connecting end 160a may be provided by connector 110 or by a pottant or encapsulant, which surrounds first connecting end 160a.
  • first conductor lead 150a and first connecting end 160a have the same thickness (e.g., formed from the same metal sheet).
  • First connecting end 160a may have a width to thickness ratio of at least 0.5 or, more specifically, at least about 2 or even at least about 5 or even at least about 10.
  • the width to thickness ratio of first conductor lead 150a may be the same or different.
  • first connecting portion 130a of connector 10 comprises base 132 and one or more tabs 134.
  • FIG. IB illustrates four tabs 134 extending from base 132, two from each side of base 132.
  • First connecting end 160a of first conductor trace 140a is crimped between base 32 and tabs 134.
  • the crimping provides electrical connection and mechanical coupling between first connecting portion 130a and first connecting end 160a.
  • the mechanical coupling helps to ensure that the electrical coupling is retained during operation of electrical harness assembly 100.
  • the connection between first connecting portion 130a and first connecting end 160a may be subject to mechanical stresses, creeping of the material (e.g., when one or both materials comprises aluminum), and the like.
  • the mechanical coupling helps may be used to support first connecting end 160a of first conductor trace 140a by connector 110.
  • first connecting end 160a of fi rst conductor trace 140a is also welded or otherwise additionally connected to base 132 as, for example, schematically shown at locations 133 in FIGS. 1A and IB.
  • This connection may be carried out using various means, including but not limited to ultrasonic welding, laser welding, resistance welding, brazing, or soldering.
  • This connection helps form a low-resistance, stable electrical contact between first connecting end 160a and interfacing base 132, and may be referred to as a primary electrical connection to distinguish from the electrical connection provided by a direct interface between connector 110 and first conductor trace 140a.
  • This primary electrical connection may comprise an intermix of materials of first connecting end 160a and interfacing base 132 and form a local monolithic structure at each location 133. Therefore, if surface oxidation or other changes in surface conditions of first connecting end 160a and interfacing base 132 happen later, these changes will not impact this primary electrical coupling between first connecting end 160a and interfacing base 132.
  • multiple conductor traces 140 may be stacked together and this stack is coupled to connecting portion 30 of connector 1 0. Referring to FIGS. 2A-2B, first conductor trace 140a and second conductor trace 140b are folded to form stack 151 and then connector 110 is coupled to stack 151 as shown in FIG.
  • FIGS. 3A-3C show a different folding pattern. While this example shows a stacked form by two conductor traces, one having ordinary' skill in the art would understand that any number of conductor traces may be stacked together by folding or other means.
  • FIGS. 2A- 2B and FIGS. 3A-3C illustrate first conductor trace 140a and second conductor trace 140b being joined or, more specifically, monolithic away from connector 110.
  • first conductor trace 40a and second conductor trace 140b may be completely disjoined away from connector 110 and form an electrical connection only at connector 110.
  • first conductor trace 140a and second conductor trace 140b may remain electrical insulated from each other and ma be coupled to different connectors.
  • FIG. 4A illustrates an example of electrical harness assembly 100, which is only partially assembled and does not have connectors on attached to its conductor traces.
  • Electrical harness assembly 100 comprises different portions 101 a- 10 ⁇ d , used for attachment of connectors. Prior to this attachment, various combinations of these different portions lOla-lOl d may be stacked together in a way similar to the one described above with reference to FIGS. 2A-2B and FIGS. 3A-3C.
  • portion 101a may be stacked with portion 101b such that multiple conductor traces 140a-140c of portion 101a (shown in FIG.
  • portion 101 c overlaps with corresponding conductor traces of portion 101b.
  • portion 101 c is ready to be stacked with portion lOld such that their corresponding conductor traces overlap.
  • portions 101a and 101b may be folded towards each other and inserted into a single connector that is able to accept and make connections to two or more rows of conductor traces.
  • an insulating layer may be placed in between the two portions 101a and 101b.
  • first connecting portion 130a of connector 1 10 comprises first plate 135 and second plate 137 parallel to first plate 135 and forming cavity 136.
  • First connecting portion 130a further comprises biasing element 138 protruding into cavity 136 from first plate 135 to second plate 137.
  • First connecting end 160a of first conductor trace 140a protrudes into cavity 136 and contacts biasing element 138.
  • Biasing element 138 maintains contact with first connecting end 160a even if fi rst connecting end 160a starts changing its shape (e.g., creep).
  • Biasing element 138 may be a spring or, more specifically, a set of springs, such as leaf springs.
  • first connecting end 160a of first conductor trace 140a may have a width to thickness ratio different than the width to thickness ratio of first conductor lead 150a,
  • first conductor lead 150a may be a foil strip, while first connecting end 160a may be patterned or formed into some other shape (e.g., from the same foil strip).
  • Different width to thickness ratios allow first connecting end 160a to form robust electrical and mechanical connection to a connector and, at the same time, allow first conductor lead 150a to maintain low thickness profile away from the connector.
  • first connecting end 160a and first conductor lead 150a may be achieved in various ways.
  • first connecting end 160a may be folded, as for example, schematically shown in FIGS. 8A-8C.
  • first connecting end 160b may be reshaped, as for example, schematically shown in FIGS. 9A-9C.
  • first connecting end 160a may be slit into a plurality of strands, which are bundled together, as for example, schematically shown in FIGS. 1.
  • OA- I OC may be slit into a plurality of strands, which are bundled together.
  • FIG. 11 A is a schematic top view of conductor trace 140, comprising conductor lead 150 and connecting end 160, prior to folding connecting end 160 and attaching terminal 1 11 to connecting end 160.
  • Terminal 1 1 1 may be a part of a connector described above or the entire connector.
  • connecting end 160 comprises attachment portion 162, fold portion 164, and transition portion 166, such that transition portion 166 is between conductor lead 150 and fold portion 164, while fold portion 164 is positioned between attachment portion 162 and transition portion 166.
  • Fold portion 164 and transition portion 166 are optional.
  • conductor lead 150 interfaces directly with attachment portion 162.
  • one of fold portion 164 and transition portion 166 is positioned between conductor lead 150 and attachment portion 162.
  • At least attachment portion 162 comprises multiple strands 161, which may be formed by slitting a metal sheet.
  • FIG. 1 IB illustrates a schematic cross-sectional view of attachment portion 162 prior to its folding. Strands 161 may be coplanar at this stage.
  • conductor lead 150 and connecting end 160 may be monolithic, e.g., formed from the same sheet of metal. All components of connecting end 160, which may be attachment portion 162, fold portion 164, and transition portion 166 (in this example) are also monolithic. Various processing techniques may be used to form each of these portions, such as slitting, die cutting, and/or laser cutting.
  • connection portion 162 changes during folding of connecting end 160 as, for example, schematically shown in FIGS. 1 1 C and 1 ID.
  • attachment portion 162 is reshaped into a bundle that has a smaller width-to-thickness ratio than attachment portion 162 prior to folding. More specifically, strands 161 are rearranged from their original coplanar shape to a new arrangement.
  • conductor lead 150 remains substantially the same.
  • terminal 111 may be attached (e.g., crimped) to attachment portion 162 as, for example, schematically shown in FIG. 1 IE.
  • Various other attachment techniques e.g., welding, soldering
  • Attachment portion 162 directly interfaces and overlaps with terminal 1 1 1 as, for example, schematically shown in FIG, 1 IE.
  • attachment portion 162 Prior to folding, attachment portion 162 comprises multiple strands 161, separated by slits and/or gaps as, for example, shown in FIGS, 1 1 A and 1 IB.
  • a slit is defined as a separation between two adjacent strands that has zero or minimal width but allows these strands to move out of plane with respect to each other. Gaps have a measurable width and usually formed by removal of material while forming strands 161.
  • FIGS. 11A and 11B illustrate six strands 161 forming attachment portion 162.
  • any number of strands 161 is within the scope (two, three, four, etc.).
  • all strands 161 have the same width (Ws) and gaps between any pair of adjacent strands 161 have the same width (W T ) and separated by the same gap.
  • strands 161 may have different widths and/or gaps. Various combinations of widths and/or gaps may be used to ensure tighter packing in the bundle.
  • the total width (W T ) of attachment portion 162 is a combination of all widths of stands and all widths of gaps, if such gaps are present.
  • fold portion 164 When fold portion 164 is present, it extends to terminal 1 1 1 but does not overlap with terminal 1 1 1. Fold portion 164 may also comprise strands 161 or parts thereof. However, when conductor trace 140 is folded, portions of strands 161 have different arrangements in fold portion 164 and in attachment portion 162.
  • the portion of strands 161 in fold portion 164 may be twisted and/or folded to provide transition to the arrangement of strands in attachment portion 162,
  • the portion of strands 161 in attachment portion 162 may be substantially parallel to each other, e.g., aligned along the center axis extending in the X direction. This parallel arrangement in attachment portion 162 allows applying large crimping forces to attachment portion 162 without braking strands 161, which in turn
  • Transition portion 166 may not have individual strands, gaps, or slits.
  • Transition portion 166 may be positioned between conductor lead 150 and fold portion 164 and use to transition from a smaller width of conductor lead 1 50 (W L ) to a much larger width (W T ) of fold portion 164. Transition portion 166 effectively allows protecting rooted ends of strands 161 from stresses. Transition portion 166 may be also partially folded. However, the degree of folding may be less than that of fold portion 164.
  • FIGS. 12A and 12B illustrate two examples of conductor traces 140 with strands 161 having different lengths. As described above, strands 161 are folded from their initial coplanar arrangement (e.g., shown in FIGS. 12A and 12B as well as FIGS.
  • FIGS. 1 1C and 1 ID This folding is used to accommodate terminal 11 that typically has a smaller width-to-thickness ratio than strands 161 in their initial unfolded state.
  • the folding process involves bringing strands 161 closed to center axis 141 of conductor trace 140. However, some strands 161 are further away from center axis 141 and need to be folded more than strands 161 that are closer to center axis 141. To accommodate this difference in folding distances, strands 161 that are further away from center axis 141 may be longer than strands 161 that are closer to center axis 141.
  • This length difference may be provided by different curvatures of strands 161 as, for example shown in FIG. 12 A.
  • the projection of strands 161 onto center axis 141 may be substantially the same.
  • the free ends of strands 161 may be substantially coplanar.
  • substantially coplanar is defined as deviation from a common plane of less than 5 millimeters or even less than 2 millimeters. It should be noted that the free ends of strands 161 may remain substantially coplanar during and after folding.
  • FIG. 12B illustrates another example in which all strands are straight and/or substantially parallel to center axis 141 in their initial flat shape / before folding.
  • substantially parallel is defined as angular difference of less than 10° or even less than 5°.
  • the free ends of strands 161 are not coplanar before folding. However, after folding, the free ends of strands 161 may be substantially coplanar.
  • the free ends of strands 161 are not
  • substantially coplanar after folding these free ends may be trimmed to ensure that newly formed ends (i.e., trimmed ends) are substantially coplanar.
  • various features of conductor traces 140 described above may be used to yield substantially coplanar free ends of strands 161 after folding of conductor traces 140 without a need for trimming.
  • trimming operation may be used in conjunction with one or both features described above with reference to FIGS. 12A and 12B.
  • FIG. 12C illustrates an example of conductor trace 140 in which gaps 163 between strands 161 terminate with stress relief features 165.
  • Stress relief features 165 may be free from sharp comers, e.g., corners with a curvature radius of less than 1 millimeter.
  • stress relief features 165 may have a circular profile and may have a minimum radius of at least 2 millimeters or even at least 5 millimeters. Elimination of the sharp corners allows reducing stress concentration points while folding and after folding of conductor trace 140.
  • strands 161 may be bent, twisted, and/or folded around center axis 141 while conductor lead 150 remains flat.
  • FIGS. 13A-13D illustrate different examples of bundles formed by strands 161 in attachment portion 162.
  • Strands 161 are specifically formed and folded to fill cross-sectional profile 167, which a circular profile in this example. It should be noted that, in some examples, strands 161 are formed from the same sheet of metal and, as such, have the same thickness. The width of strands 161 and, as a result, the width-thickness ratios may be the same or different. Controlling the number of strands 161, the width of each strand 161, and the folded orientation of each strand 161 may be used to achieve different filling ratios, which are generally much higher than, for example, is possible with round wires 161 ' shown in FIG. 13E, as reference.
  • the filling ratio is defined as a sum of all cross-sectional areas of strands 161 divided by the area of cross-sectional profile 167. In some embodiments, this filling ratio is at least about 80% or even at least about 90%.
  • FIG. 13 A illustrates an example of a bundle formed by strands 161, which all have the same rectangular cross-sectional profile. Furthermore, the orientations of these rectangular cross-sectional profiles are the same, e.g., all long side are parallel to each other.
  • FIG. 13B illustrates an example of a bundle formed by strands 161 all having the same square cross-sectional profile.
  • FIG. 13C illustrates an example of a bundle formed by strands 161 having both rectangular and square cross-sectional profiles.
  • FIG. 13D illustrates another example of a bundle formed by strands 161 all having the same rectangular cross- sectional profile.
  • the orientations of these rectangular cross-sectional profiles differ.
  • some strands 161 are turned 90° relative to other strands. Any degree of turn is within the scope,
  • FIGS. 14A and 14B illustrate four conductor traces 140 before and after connecting these conductor traces 140 to terminals 111 , Folding of connecting ends 160 and crimping of terminals 111 to these connecting ends 160 are described above with reference to FIGS. 1 lA-1 IE.
  • the orientation of terminals 1 11 may be different from the orientation of center axes 141 of individual connecting ends 160. Referring to FIGS. 14A and 14B, center axes 141 of individual connecting ends 160 are spaced apart more than terminals 111 , This larger spacing may be due to connecting ends 160 being formed from the same metal sheet, while terminals 1 11 may have to be positioned in the same compact connector. To accommodate this difference, conductor leads 150 may be folded to align their connecting ends 160 with terminals 111.
  • folding of conductor leads 150 may cause one or more conductors lead to overlap.
  • conductor traces 140 remain electrically insulated when their conductor leads 150 overlap.
  • conductor leads 150 may be insulated at the overlap location, e.g., one or more insulator layers may be positioned between two overlapping conductor leads 150.
  • conductor traces 140 may be positioned out of plane and form connections to different terminals of the connector at different levels.
  • FIGS. 14D and 14E illustrate three conductor traces 140a-140c before and after connecting these conductor traces 140a-140c to terminals 1 lOa-l 10c
  • conductor traces 140a- 140c Prior to connecting these conductor traces 140a-140c to terminals 110a- 110c, conductor traces 140a- 140c may extend within a bendable plane, e.g., define by first insulator 142 or a temporary liner.
  • spacing between connecting ends 160a and 160c may not be sufficient to accommodate connecting end 160b, As a result, connecting end 160b is formed in a pre-folded state and positioned between conductor leads 150a and 150c as shown in FIG. 14D.
  • connecting ends 160a and 160c are connecting and connected to their respective terminals 110a and 1 10c, more space is available in between these connecting ends 160a and 160c and can now accommodate connecting end 160b, at least in the folded state, as shown in FIG. 14E.
  • FIG. 15A illustrates conductor traces 140 with partially formed connecting ends 160.
  • strands 161 do not have free ends. This feature simplifies handling of connecting ends 160, especially, transferring conductor traces 140 from one supporting substrate to another, folding connecting ends 160, and/or performing other operations.
  • strands 161 supported by bridging part 169. Bridging part 169 may be removed before or after folding connecting ends 160.
  • FIG. 15B illustrates an example of hybrid conductor traces 140, which include one conductor lead 150 and two connecting ends 160a and 160b.
  • one connecting end 160a may be used for power transmission (and rated for a higher current) while another connecting end 160b may be used for signal (and rated for a smaller current).
  • the size of each connecting end is selected for these current ratings and to accommodate corresponding connector terminals.
  • FIG. 16A illustrates harness assembly 100 comprising first insulator 142 and multiple conductor leads 150a-150c adhered to and supported by first insulator 142
  • First insulator 142 comprises different insulator openings 143a-143c that allow various manipulation of first insulator 142 and corresponding conductor leads 150a- 150c,
  • insulator opening 143c extends to one edge of first insulator 142 and defines two harness portions 103a and 103b that can be manipulated independently from each other. Insulator openings 143a and 143b do not extend to the edge but are used to provide additional flexibility to harness portion 103a as will now be explained with reference to FIGS. 16B-16F.
  • first insulator 142 comprising three insulator openings 143a-143c that divide insulator into four insulator strips 145a- 145d. Each strip may support a separate conductor trace (not shown) when insulator 143 is a part of a harness. It should be noted that first insulator 142 is a part of the harness when manipulations shown in FIGS. 16C are performed with first insulator 142.
  • FIG. 16C illustrates one end of first insulator 142 turned 90° relative to the other end within the X-Y plane.
  • Insulator openings 143a- 143c allow first insulator 142 to turn and bend without significant out of plane distortions of individual insulator strips 145a-145d.
  • One having ordinary skills in the art would understand that such bending would be difficult without insulator openings because of the flat profile of first insulator 142 (small thickness in the Z direction) and relatively low flexibility of material s forming first insulator 142.
  • Adding insulator openings 143 a- 143c allows different routing of each of four insulator strips 145a-145d thereby increasing flexibility and decreasing the out of plane distortion.
  • FIGS. 16E and 16F represent cross- sections of insulator strips 145a-145d at different locations of first insulator 142. As shown in these figures, insulator strips 145a ⁇ 145d may be brought closer together and turned 90° around each of the respective center axis at some point (B-B) in the bend. To achieve this type of orientation, the length of each insulator may be different as, for example, shown in FIG. 16B.
  • FIG. 17 is a process fl owchart corresponding to method 1700 of forming an electrical harness or portions thereof, in accordance with some embodiments.
  • Method 1700 may commence with laminating a conductor to a supporting substrate during step 1710.
  • the conductor may be a metal sheet, e.g., metal foil .
  • the supporting substrate may be a temporary liner or an insulator of the electrical harness. If the temporar' liner is used, this liner may be later removed and, in some examples, replaced within an insulator.
  • Method 1700 may proceed with patterning the conductor during step 1720.
  • One or more conductor traces are formed during this step.
  • a conductor trace may include a conductor lead and a first connecting end.
  • Patterning the conductor may involve techniques including, but not limited to, punching, flat bed die cutting, match-metal die cutting, male/female die cutting, rotary die cutting, laser cutting, laser ablation, waterjet cutting, machining, or etching.
  • Method 1700 may proceed with shaping the attachment portion of conductor during optional step 1730, For example, individual strands may be folded or otherwise rearranged into a shape that has a smaller width-to-thickness ratio than before this step as described above with reference to FIGS. 8A-10C.
  • the width-to-thickness ratio of the attachment portion matches to that ratio of the terminal.
  • step 1730 may involve stacking of different conductor traces as described above with reference to FIGS. 2A-4B.
  • Method 1700 may proceed with attaching a connector terminal to the attachment portion during step 1740.
  • the connector terminal may be crimped and/or welded to the terminal as described above with reference to FIGS. 1A-1B.
  • a mechanical biasing attachment may be formed between the connector terminal and the attachment portion as described above with reference to FIG. 5.
  • step 1740 also comprises optional step 1745 of attaching one or more terminals to the housing of a connector.
  • the terminals may be inserted into the plastic housing. An example of the assembly formed during step 1745 is shown in FIG, 14C.
  • Method 1700 may proceed with attaching an insulator to the patterned conductor during step 1750.
  • step 1750 is performed after step 1740.
  • step 1750 is performed before step 1740.
  • the insulator attached during the step 1750 is a permanent component of the electrical harness.
  • insulator materials are insulator comprises a material selected from the group consisting of polyimide (PI), polyethylene naphthalate (PEN), polyethylene terephthalate (PET), polymethyl methacrylate (PMMA), ethyl vinyl acetate (EVA), polyethylene (PE), polypropylene (PP), polyvinyl fluoride (PVF), polyamide (PA), soldermask, and polyvinyl butyral (PVB).
  • Method 1 700 may proceed with unfolding the conductor traces during optional step 1760. Various aspects of this step are described above with reference to FIGS. 14A-14B and 14D-14E. Unfolding of the conductor traces may be performed before or after adding the terminals.
  • Method 1700 may proceed with attaching the harness to a carrier (e.g., heat sink) during optional step 1770.
  • a carrier e.g., heat sink
  • the carrier may be a car door as will be described below with reference to FIGS. 19A-19C.
  • electrical harness assembly 100 further comprises second conductor trace 140b, which in turn comprises second conductor lead 150b and second connecting end 160b.
  • second conductor trace 140b which in turn comprises second conductor lead 150b and second connecting end 160b.
  • the thickness of second conductor trace 140b and the thickness of first conductor trace 140a may be identical.
  • first conductor trace 140a and second conductor trace 140b may be formed from the same foil sheet.
  • first conductor lead 150a and second conductor lead 150b are formed from the same material.
  • Second conductor trace 140b and first conductor trace 140a may not contact each other.
  • second conductor trace 140b and first conductor trace 140a may be separated by a gap.
  • second connecting end 160b of second conductor trace 140b is electrically coupled to multiple connecting portions of connector 110.
  • FIGS. 18B illustrate second connecting end 160b being electrically coupled to five connecting portions 130b-130f of connector 110. As such, making an electrical connection to any one of corresponding contact interface 120b-120f will result in an electrical connection to second connecting end 160b.
  • the multiple connecting portions may be
  • jumpers 170 interconnected by one or more jumpers 170 as, for example, schematically shown in FIGS. 18B-18D.
  • Jumpers 170 allow current balancing to be achieved within connector 1 10 such that a relatively constant current density can be maintained across the cross-section of second connecting end 160b, thereby allowing the use of thinner materials for second connecting end 160b and second conductor trace 140b.
  • Second conductor trace 140b may have a larger current carrying capability than first conductor trace 140a. More specifically, second conductor trace 140b may be wider than first conductor trace 140a as, for example, shown in FIG. 18B. To accommodate this variation in trace width, connecting portions 130a- 13 Of may comprise a top-down crimp connector such as a zero-insertion force (ZIF) connector, for example. Similarly, connector 110 may be designed to accommodate wires 180a, 180b of varying diameter, as shown in FIG. 18B-18C. Thus, connector 110 can interconnect conductor traces 140a, 140b of varying width to wires 180a, 180b of varying diameter with minimal current crowding and/or joule heating effects in either element.
  • ZIF zero-insertion force
  • FIG. 19A illustrates car door assembly 200 comprising car door 210 and electrical harness assembly 100, in accordance with some embodiments.
  • Electrical harness assembly 100 may be attached to and mechanically supported by car door 210 and may have a fiat cross-sectional profile.
  • electrical assembly 100 may be adhered to car door 210.
  • electrical harness assembly 100 which is fiat, may be in thermal communication with car door 210.
  • each of conductor leads 1 50 of electrical harness assembly 100 may be in thermal communication with car door 210.
  • This thermal communication is used for thermal control of conductor leads 150 while passing electrical currents through conductor leads 150. More specifically, this thermal communication allows using conductor leads 50 with smaller (e.g., 30-90% smaller) cross- sectional areas than those in conventional harnesses, which utilize round wires with minimal thermal communication to car doors.
  • Car door 210 provides a large thermal mass for heat dissipation from conductor leads 150 when conductor leads 50 heats up while passing electrical currents.
  • Reducing the cross-sectional area of conductor leads 150 corresponds to a reduction in weight of conductor leads 150, For example, many modern cars utilize 1,000-4,000 meters of electrical cables with a total weight of up to 50 kilograms and even up to 100 kilograms. Any reduction in weight helps with fuel economy, car handling, and cost savings.
  • a combination of the smaller cross-sectional area and of the flat profile of electrical harness assembly 100 allows substantially reducing the thickness of electrical harness assembly 100. Specifically, the contribution by electrical harness assembly 100 to the thickness of car door assembly 200 is reduced. As such, car door assembly 200 may be made thinner with electrical harness assembly 100 described herein than with a conventional round-wire bundled harness.
  • electrical harness assembly 100 may be attached to surface 212 of car door 210. Furthermore, electrical harness assembly 100 may follow the profile of surface 212. In other words, electrical harness assembly 100 may be substantially conformal surface 212 as, for example, schematically shown in FIGS. 19A and 19B. This conformality ensures that all parts of electrical harness assembly 100 are in thermal communication with car door 210. [00108] In some embodiments, surface 212 of car door 210 may have indent
  • indent 214 to accommodate electrical harness assembly 100 as, for example, schematically shown in FIG. 19C.
  • the depth of indent 214 may be substantially the same as the thickness of electrical harness assembly 100 such that top surface 104 of electrical harness assembly 100 and a portion of surface 212 surrounding indent 214 are substantially coplanar.
  • the indent may be shallower and a portion of electrical harness assembly 100 may protrude above the portion of surface 212 surrounding indent 214.
  • Electrical harness assembly 100 may comprise first insulator 142 and second insulator 144 such that conductor lead 150 is positioned between first insulator 142 and second insulator 144.
  • FIG. 19D is a schematic illustration of first insulator 142, conductor lead 150, and second insulator 144 disposed on car door 210.
  • First insulator 142 may be an adhesive layer that adheres electrical harness assembly 100 to car door 2 0, [00110]
  • first insulator 142 is or comprises a thermally conductive mounting adhesive. This adhesive may have a thermal conductivity of least about 0.2 W/raK (e.g., about 0.7 W/mK) or even at least about 1.0 W/mK. This level of thermal conductivity may be obtained in an inorganic particle-filled dielectric film or in a thermally conductive pressure-sensitive adhesive (PSA) film, for example.
  • PSA thermally conductive pressure-sensitive adhesive
  • first insulator 142 examples include but are not limited to polyimide (PI), polyethylene naphthalate (PEN), polyethylene terephthalate (PET), polymethyl methacrylate (PMMA), ethyl vinyl acetate (EVA), polyethylene (PE), polypropylene (PP), polyvinyl fluoride (PVF), polyamide (PA), soldermask, or polyvinyl butyrai (PVB).
  • the composition and thickness of first insulator 142 may ⁇ be chosen to maximize heat dissipation through first insulator 142, prevent dielectric breakdown to the surrounding environment, act as a sufficient mechanical barrier to air and moisture, and minimize distortion of features of conductor leads 120.
  • first insulator 142 may be between 1 micrometer and 500 micrometers or, more specifically, between 10 micrometers and 125 micrometers.
  • first insulator 142 includes an adhesive layer on the side facing, car door 210.
  • the adhesive layer include, but are not limited to polyolefin adhesives, polyester adhesives, polyimide adhesives, acrylics, epoxies, cross-linking adhesives, PSAs, and/or thermoplastic adhesives.
  • the adhesive layer may be filled with thermally conductive, electrically insulating particles (e.g., alumina) to facilitate heat transfer through the adhesive material .
  • the material composition of second insulator 144 may be the same or different as the material composition of first insulator 142.
  • first insulator 142 may be made from a material which is more heat conductive that the material of second insulator 144.
  • second insulator 144 may be made from a material that has better mechanical properties than first insulator 142 to externally protect conductor lead 150 from damage once the harness is applied to car door 210 and/or to support conductor lead 150 and other components of electrical harness 100 before harness is applied to door 200.
  • the thickness of second insulator 144 may be the same or different as the thickness of first insulator 142.
  • one of the insulators e.g., second insulator 1414
  • first insulator 142 may be thinner to ensure heat transfer between conductor lead 150 and car door 210.
  • First insulator 142 and second insulator 144 may be continuous sheets without any openings. First insulator 142 and second insulator 144 may extend entire length of conductor lead 150 while allowing connecting end 160 to extend beyond first insulator 142 and second insulator 144. Alternatively, in some embodiments, second insulator 144 may extend underneath and provide support to connecting end 160 while first insulator 142 may leave connecting end 160 exposed, thus allowing access to a first surface of connecting end 160. In some embodiments, first insulator 142 and second insulator 144 may be sealed again an insulating enclosure of connector 110.
  • the term "insulator” refers to a stmcture having an electrical conductivity of less than 10 S/cm.
  • the term “conductor” refers to a stmcture having an electrical conductivity of at least about 10,000 S/cm.
  • the term “thermal conductor” refers to a structure having a thermal conductivity of at least about0.2 W/mK. Structures with a thermal conductivity of less than 0.1 W/mK may be referred to as "thermal insulators.” It should be noted that a thermal conductor may be also an electrical conductor but it does not have to be.
  • a class of electrically insulating materials such as diamond and aluminum nitride, are good thermal conductors. The materials may be used, for example, as a surface coating.
  • Electrical conductors are typically thermally conductive.
  • electro-thermal conductor refers to a stmcture having an electrical conductivity of greater than 10,000 S/cm and a thermal conductivity of greater than 10 W/mK.
  • electrically isolated may refer to a lack of a physical connection between two electrical conductors, either directly or through one or more other electrical conductors.
  • the width of gap 152 between two- conductor leads 50a and 150b may be between about 100 micrometers and 3 millimeters or, more specifically, between about 250 micrometers and 1 millimeter.
  • the aspect ratio of gap 152, as defined by the width of gap 52 divided by the conductor thickness (which is effective the depth of gap 152) may less than about 10 or, more specifically, less than about 5 or even less than about 2, Gap 152 may be empty or filled with an adhesive.
  • First insulator 142 and second insulator 144 maintain the orientation of conductor leads 150a and 150b and prevent conductor leads 150a and 150b from shorting.
  • Electrical harness assembly 100 may comprise one or more connectors (e.g., connectors 1 10a- 1 0c shown in FIG. 19 A) for connecting to electrical devices 220 of car door assembly 200 and outside of car door assembly 200.
  • electrical devices 220 include but are not limited to speakers, lights, door lock, window regulators, power mirrors, and the like.
  • electrical harness assembly 100 may be used for other applications as well, e.g., in which thermal sinks are available and can be thermally coupled to electrical harness assembly 100.
  • electrical harness assembly 100 may be used for various appliances (e.g., refrigerators, washer / driers, HVAC).
  • conductor trace 140 comprises base sublayer 002 and surface sublayer 006 as, is shown in FIG. 22 A, for example.
  • Surface sublayer 1006 may have a different composition than base sublayer 1002.
  • First insulator 142 or second insulator 144 may be laminated over surface sublayer 1006. More specifically, at least a portion of surface sublayer 1006 may directly interface first insulator 142 or second insulator 144 (or an adhesive used for attaching first insulator 142 or second insulator 144 to conductor trace 140).
  • surface sublayer 1006 is disposed between base sublayer 1002 and first insulator 142 or second insulator 144.
  • Surface sublayer 1006 may be specifically selected to improve adhesion of first insulator 142 or second insulator 144 to conductor trace 140, and/or other purposes as described below.
  • Base sublayer 1002 may comprise a metal selected from the group consisting of aluminum, titanium, nickel, copper, steel, and alloys comprising these metals.
  • the material of base sublayer 002 may be selected to achieve desired electrical and thermal conductivities of overall conductor trace 140 while maintaining minimal cost.
  • Surface sublayer 1006 may comprise a metal selected from the group consisting of tin, lead, zinc, nickel, silver, palladium, platinum, gold, indium, tungsten, molybdenum, chrome, copper, alloys thereof, organic solderability preservative (OSP), or other electrically conductive materials.
  • the material of surface sublayer 1006 may be selected to protect base sublayer 1002 from oxidation, improve surface conductivity when forming electrical and/or thermal contact to device, improve adhesion to conductor trace 140, and/or other purposes.
  • the addition of a coating of OSP on top of surface sublayer 1006 may help prevent surface sublayer 1006 itself from oxidizing over time.
  • aluminum may be used for base sublayer 1002. While aluminum has a good thermal and electrical conductivity, it forms a surface oxide when exposed to air. Aluminum oxide has poor electrical conductivity and may not be desirable at the interface between conductor trace 140 and, for example, connection portion 130 of connector 1 10. In addition, in the absence of a suitable surface sublayer, achieving good, uniform adhesion between the surface oxide of aluminum and many adhesive layers may be challenging.
  • Surface sublayer 1006 may have a thickness of between about 0,01 micrometers and 10 micrometers or, more specifically, between about 0.1 micrometers and 1 micrometer.
  • thickness of base sublayer 1002 may be between about 10 micrometers and 1000 micrometers or, more specifically, between about 100 micrometers and 500 micrometers.
  • base sublayer 1002 may represent at least about 90% or, more specifically, at least about 95% or even at least about 99% of conductor trace 140 by volume.
  • conductor trace 140 further comprises one or more intermediate sublayers 1004 disposed between base sublayer 1002 and surface sublayer 1006.
  • Intermediate sublayer 1004 has a different composition than base sublayer 1002 and surface sublayer 1006.
  • the one or more intermediate sublayers 1004 may help prevent intermetallic formation between base sublayer 1002 and surface sublayer 1006.
  • intermediate sublayer 1004 may comprise a metal selected from group consisting of chromium, titanium, nickel, vanadium, zinc, and copper.
  • conductor trace 140 may comprise roiled metal foil.
  • the horizontally-elongated grain structure of roiled metal foil may help increase the resistance to crack propagation in conductor trace 140 under cyclical loading conditions. This may help increase the fatigue life of harness assembly 100.
  • conductor trace 140 comprises electrically insulating coating 1008 forming surface 1009 of conductor trace 140 opposite of device-side surface 1007 as, for example, shown in FIG. 22C. At least a portion of this surface 1009 may remain exposed in harness assembly 100 and may be used for heat removal from harness assembly 100. In some embodiments, surface 1009 remains exposed in harness assembly 100 in its entirety.
  • Insulating coating 1008 may be selected for relatively high thermal conductivity and relatively high electrical resistivity and may comprise a material selected from group consisting of silicon dioxide, silicon nitride, anodized alumina, aluminum oxide, boron nitride, aluminum nitride, diamond, and silicon carbide. Alternatively, insulating coating may compri se a composite material such as a polymer matrix loaded with thermally conductive, electrically insulating inorganic particles.
  • conductor trace 140 is solderabie.
  • the aluminum may be positioned as the base sublayer, while the surface sublayer may be made from a material having a melting temperature that is above the melting temperature of the solder. Otherwise, if the surface sublayer melts during circuit bonding, oxygen may penetrate through the surface sublayer and oxidize aluminum within the base sublayer. This in turn may reduce the conductivity at the interface of the two sublayers and potentially cause a loss of mechanical adhesion.
  • a surface sublayer may be formed from zinc, silver, palladium, platinum, copper, nickel, chrome, tungsten, molybdenum, or gold.
  • FIG. 23 illustrates an example of first electrical harness 100a and second electrical harness 100b, both supported on the same carrier film 2300.
  • This example simplifies handling of electrical harness 100a and electrical harness 100b during their production, storage, and initial application.
  • electrical connections can be formed to conductor leads 150a-1.50d prior to separating electrical harness 100a and electrical harness 100b from carrier film 2300.
  • adhesive layer 2310a may be use for attaching electrical harness 100a to other support structures, e.g., heat sinks.
  • First insulator portion 142a and second insulator portion 142b insulate conductor leads 150a-150d of first electrical harness 100a and second electrical harness 100b.
  • Cut opening 2320 may be positioned between electrical harness 100a and electrical harness 100b to allow independent removal of each harness from carrier film 2300.
  • first insulator portion 142a and adhesive layer 2310a may optionally be combined into a single layer or be separate layers.
  • second insulator portion 142b and adhesive layer 2310b may optionally be combined into a single layer or be separate layers.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • General Engineering & Computer Science (AREA)
  • Connections Effected By Soldering, Adhesion, Or Permanent Deformation (AREA)

Abstract

La présente invention concerne des ensembles de faisceaux électriques et des procédés de formation de tels ensembles de faisceaux. Un ensemble de faisceaux comprend une piste conductrice comprenant un fil conducteur ayant un rapport largeur/épaisseur d'au moins 2, ce qui permet d'obtenir un profil d'épaisseur plus bas et améliore la conductivité thermique avec l'environnement. Selon certains exemples, une piste conductrice peut être constituée d'une feuille de métal mince. La piste conductrice comprend également une extrémité de connexion, d'un bloc avec le fil conducteur. Le rapport largeur/épaisseur de l'extrémité de connexion est inférieur à celui de la piste conductrice, permettant d'obtenir une connexion mécanique et électrique directe à un connecteur de l'ensemble de faisceaux. L'extrémité de connexion peut être pliée, façonnée, fendue et analogue afin de réduire son rapport largeur/épaisseur, lequel, selon certains exemples, peut être proche de 1.
PCT/US2018/023586 2017-03-21 2018-03-21 Circuits souples pour faisceaux électriques Ceased WO2018175599A1 (fr)

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US62/474,448 2017-03-21
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US10446956B2 (en) 2017-04-14 2019-10-15 Cellink Corporation Flexible circuits for electrical harnesses

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US5993247A (en) * 1997-12-01 1999-11-30 General Motors Corporation Electrical connection for flex circuit device
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JP2004127741A (ja) * 2002-10-03 2004-04-22 Furukawa Electric Co Ltd:The コネクタ付きフラットケーブルの固定方法及びコネクタ付きフラットケーブルの固定構造
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US5460530A (en) * 1991-09-26 1995-10-24 Sumitomo Wiring Systems, Ltd. Arranging method of a wire harness for a door
US6152763A (en) * 1996-09-10 2000-11-28 The Whitaker Corporation Electrical contact for termination to flat conductive member
US5993247A (en) * 1997-12-01 1999-11-30 General Motors Corporation Electrical connection for flex circuit device
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JP2003203699A (ja) * 2002-01-08 2003-07-18 Auto Network Gijutsu Kenkyusho:Kk フレキシブル・フラット・ケーブルのコネクタ接続構造
JP2004127741A (ja) * 2002-10-03 2004-04-22 Furukawa Electric Co Ltd:The コネクタ付きフラットケーブルの固定方法及びコネクタ付きフラットケーブルの固定構造
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US10446956B2 (en) 2017-04-14 2019-10-15 Cellink Corporation Flexible circuits for electrical harnesses

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