DE102016215414A1 - Screw dome for an electronic module and electronic module with a screw dome - Google Patents
Screw dome for an electronic module and electronic module with a screw dome Download PDFInfo
- Publication number
- DE102016215414A1 DE102016215414A1 DE102016215414.1A DE102016215414A DE102016215414A1 DE 102016215414 A1 DE102016215414 A1 DE 102016215414A1 DE 102016215414 A DE102016215414 A DE 102016215414A DE 102016215414 A1 DE102016215414 A1 DE 102016215414A1
- Authority
- DE
- Germany
- Prior art keywords
- carrier component
- screw
- screw dome
- dome
- electronic assembly
- 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.)
- Pending
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
- B29C65/16—Laser beams
- B29C65/1629—Laser beams characterised by the way of heating the interface
- B29C65/1635—Laser beams characterised by the way of heating the interface at least passing through one of the parts to be joined, i.e. laser transmission welding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/44—Joining a heated non plastics element to a plastics element
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
- B29C66/024—Thermal pre-treatments
- B29C66/0246—Cutting or perforating, e.g. burning away by using a laser or using hot air
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/114—Single butt joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/124—Tongue and groove joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/13—Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
- B29C66/131—Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
- B29C66/24—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight
- B29C66/242—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours
- B29C66/2422—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being circular, oval or elliptical
- B29C66/24221—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being circular, oval or elliptical being circular
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/303—Particular design of joint configurations the joint involving an anchoring effect
- B29C66/3032—Particular design of joint configurations the joint involving an anchoring effect making use of protusions or cavities belonging to at least one of the parts to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/53—Joining single elements to tubular articles, hollow articles or bars
- B29C66/532—Joining single elements to the wall of tubular articles, hollow articles or bars
- B29C66/5324—Joining single elements to the wall of tubular articles, hollow articles or bars said single elements being substantially annular, i.e. of finite length
- B29C66/53245—Joining single elements to the wall of tubular articles, hollow articles or bars said single elements being substantially annular, i.e. of finite length said articles being hollow
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/61—Joining from or joining on the inside
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
- B29C66/712—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined the composition of one of the parts to be joined being different from the composition of the other part
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7392—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7392—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
- B29C66/73921—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/74—Joining plastics material to non-plastics material
- B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/74—Joining plastics material to non-plastics material
- B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
- B29C66/7422—Aluminium or alloys of aluminium
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2791/00—Shaping characteristics in general
- B29C2791/004—Shaping under special conditions
- B29C2791/009—Using laser
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
- B29C65/561—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using screw-threads being integral at least to one of the parts to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/731—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the intensive physical properties of the material of the parts to be joined
- B29C66/7311—Thermal properties
- B29C66/73115—Melting point
- B29C66/73116—Melting point of different melting point, i.e. the melting point of one of the parts to be joined being different from the melting point of the other part
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/74—Joining plastics material to non-plastics material
- B29C66/742—Joining plastics material to non-plastics material to metals or their alloys
- B29C66/7428—Transition metals or their alloys
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- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/34—Electrical apparatus, e.g. sparking plugs or parts thereof
- B29L2031/3406—Components, e.g. resistors
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29L2031/00—Other particular articles
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- B29L2031/3443—Switches
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/34—Electrical apparatus, e.g. sparking plugs or parts thereof
- B29L2031/3481—Housings or casings incorporating or embedding electric or electronic elements
Abstract
Die Erfindung betrifft einen Schraubdom (1) für eine elektronische Baugruppe (3) sowie eine solche elektronische Baugruppe (3). Der Schraubdom (1) umfasst ein Gewindeelement (4), das ein vorgeformtes Gewinde aufweist. Des Weiteren umfasst der Schraubdom (1) einen Mantel (6) aus thermoplastischem Kunststoff, der das Gewindeelement (4) zumindest mantelseitig umgibt, und der zur Befestigung des Gewindeelements (4) an einem Trägerbauteil (2) eingerichtet ist. Die elektronische Baugruppe (3) umfasst neben dem separat gefertigten Schraubdom (1) das Trägerbauteil (2), an dem elektrische Komponenten gehaltert sind. Der Schraubdom (1) ist dabei mittels eines Laserstrahl-Fügeverfahrens an dem Trägerbauteil (2) befestigt.The invention relates to a screw dome (1) for an electronic assembly (3) and such an electronic assembly (3). The screw dome (1) comprises a threaded element (4) having a preformed thread. Furthermore, the screw dome (1) comprises a jacket (6) of thermoplastic material, which surrounds the threaded element (4) at least on the shell side, and which is adapted for fastening the threaded element (4) to a carrier component (2). The electronic assembly (3) comprises in addition to the separately manufactured screw dome (1), the support member (2) on which electrical components are mounted. The screw dome (1) is attached to the carrier component (2) by means of a laser beam joining method.
Description
Die Erfindung betrifft einen Schraubdom für eine elektronische Baugruppe. Des Weiteren betrifft die Erfindung eine elektronische Baugruppe mit einem solchen Schraubdom. The invention relates to a Schraubdom for an electronic module. Furthermore, the invention relates to an electronic assembly with such a screw dome.
Elektronische Baugruppen, die in Kraftfahrzeugen zum Einsatz kommen, wie z.B. Steuergeräte für Motoren oder/Getriebe, unterliegen aufgrund ihres Einsatzortes (im Bereich des Motors bzw. Getriebes) im Betrieb meist vergleichsweise hohen Temperaturwerten von beispielsweise 80 bis 150°C. Diesen Temperaturwerten müssen die Steuergeräte, insbesondere deren elektrische, insbesondere elektronischen Komponenten, die häufig Elemente aus Kunststoff umfassen, standhalten. Außerdem generieren die elektrischen Komponenten solcher Steuergeräte im Betrieb häufig selbst Wärme, die über eine geeignete Auslegung der Gehäuse solcher Steuergeräte abgeleitet werden muss. Als Gehäusewerkstoffe kommen deshalb häufig Metalle oder wärmeleitfähig gefüllte Kunststoffe (d.h. Kunststoffe mit einem Füllstoff mit vergleichsweise hoher Wärmeleitfähigkeit, z. B. einem Metall oder einer Keramik) zum Einsatz. Die elektrischen Komponenten der Steuergeräte sind dabei häufig über Wärmekontaktflächen mit derartigen Gehäusen verbunden, sodass die von den elektrischen Komponenten erzeugte Wärme mit hoher Effizienz abgeführt werden kann. Electronic assemblies used in motor vehicles, e.g. Due to their location (in the area of the engine or gearbox), control devices for engines or / gearboxes are usually subject to comparatively high temperature values of, for example, 80 to 150 ° C. during operation. These temperature values must withstand the control devices, in particular their electrical, in particular electronic components, which often comprise elements made of plastic. In addition, the electrical components of such control devices often generate heat themselves in operation, which must be derived via a suitable design of the housing of such control units. As housing materials, therefore, metals or thermally conductive filled plastics (i.e., plastics having a comparatively high thermal conductivity filler, eg, a metal or a ceramic) are often used. The electrical components of the control units are often connected via heat contact surfaces with such housings, so that the heat generated by the electrical components can be dissipated with high efficiency.
Um im Bedarfsfall eine Wartung und/oder Nachrüstung der Steuergeräte zu ermöglichen, werden die Gehäuse der Steuergeräte meist (reversibel) mittels Schraubverbindungen verschlossen. Gleichermaßen werden häufig auch Anbauteile oder die die elektrischen Komponenten tragenden Platinen (Leiterplatten) mittels Schrauben an den Gehäusen befestigt. Um eine möglichst stabile Verschraubung an den häufig mittels Gießverfahren (z.B. Kunststoff-Spritzgießen oder Metall-Druckguss) hergestellten, vergleichsweise dünnwandigen Gehäusewänden zu ermöglichen, werden üblicherweise sogenannte Schraubdome eingesetzt. Dabei handelt es sich um zylindrische oder kegelförmige Fortsätze des Gehäuses, in die eine (Gewinde-)Bohrung zur Aufnahme der Schrauben eingebracht ist. Insbesondere beim Kunststoff-Spritzgießen ist aufgrund der Wanddickensprünge am Übergang zu den Schraubdomen häufig mit Verzug zu rechnen, sodass eine exakte Ausrichtung der Schraubdome und damit eine präzise Positionierung der anzuschraubenden Teile nur mit vergleichsweise hohem Aufwand, insbesondere bei der Herstellung der korrespondierenden Spritzgießform (auch als Werkzeug bezeichnet) verbunden ist. Beim Metall-Druckguss tritt häufig das Problem auf, dass die zur Ausformung der Schraubdome, insbesondere deren Gewindebohrungen, eingesetzten Formkerne durch wiederholtes Überströmen durch das Metall ausgewaschen werden und/oder brechen können, sodass eine aufwändige und teure Instandhaltung des entsprechenden Werkzeugs erforderlich ist. In order to enable maintenance and / or retrofitting of the control units if necessary, the housing of the control units are usually (reversibly) closed by means of screw. Similarly, often attachments or the electrical components bearing circuit boards (circuit boards) are attached by screws to the housings. In order to enable the most stable possible screw connection to the comparatively thin-walled housing walls which are frequently produced by means of casting methods (for example plastic injection molding or metal die casting), so-called screw domes are usually used. These are cylindrical or conical extensions of the housing, in which a (threaded) bore is introduced for receiving the screws. In particular, in plastic injection molding is due to the Wanddickensprünge at the transition to the screw domes often expected to delay, so that an exact alignment of the screw and thus precise positioning of the parts to be screwed only with relatively high effort, especially in the production of the corresponding injection mold (also known as Tool referred) is connected. In the case of metal diecasting, the problem often arises that the mandrels used for forming the screw domes, in particular their threaded bores, can be washed out and / or broken by repeated overflowing through the metal, so that expensive and expensive maintenance of the corresponding tool is required.
Der Erfindung liegt die Aufgabe zugrunde, bei einer elektronischen Baugruppe auf einfache Weise eine Verschraubung mit hoher Positioniergenauigkeit zu ermöglichen. The invention has for its object to allow for an electronic assembly in a simple way a screw with high positioning accuracy.
Diese Aufgabe wird erfindungsgemäß gelöst durch einen Schraubdom mit den Merkmalen des Anspruchs 1. Des Weiteren wird diese Aufgabe erfindungsgemäß gelöst durch eine elektronische Baugruppe mit den Merkmalen des Anspruchs 6. Vorteilhafte und teils für sich erfinderische Ausführungen und Weiterbildungen der Erfindung sind in den Unteransprüchen und der nachfolgenden Beschreibung dargelegt. This object is achieved by a Schraubdom with the features of
Der erfindungsgemäße Schraubdom dient zum Einsatz an einer elektronischen Baugruppe. Der Schraubdom ist dabei vorzugsweise zur (vorzugsweise „nachträglichen“ und) freien Positionierung an einem Trägerbauteil einer solchen elektronischen Baugruppe eingerichtet und vorgesehen. Im bestimmungsgemäßen Montagezustand dient der Schraubdom insbesondere zur Halterung einer (Befestigungs-)Schraube und damit mittelbar zur Halterung eines Bauelements der elektronischen Baugruppe an dem Trägerbauteil. Der Schraubdom umfasst dabei ein Gewindeelement, das ein vorgeformtes Gewinde, insbesondere ein Innengewinde, aufweist. Des Weiteren umfasst der Schraubdom einen Mantel aus thermoplastischem Kunststoff, der das Gewindeelement zumindest mantelseitig umgibt. Der Mantel ist dabei zur Befestigung des Gewindeelements an dem Trägerbauteil der elektronischen Baugruppe eingerichtet. Mithin handelt es sich bei dem Schraubdom um ein separat von dem Trägerbauteil gefertigtes Bauelement. The Schraubdom invention is intended for use on an electronic module. The screw dome is preferably designed and provided for (preferably "subsequent" and) free positioning on a carrier component of such an electronic assembly. In the intended mounting state of the screw dome is used in particular for holding a (fastening) screw and thus indirectly for holding a component of the electronic module to the support member. The screw dome in this case comprises a threaded element which has a preformed thread, in particular an internal thread. Furthermore, the screw dome comprises a jacket of thermoplastic material which surrounds the threaded element at least on the shell side. The jacket is set up for fastening the threaded element to the carrier component of the electronic assembly. Consequently, the screw dome is a component manufactured separately from the carrier component.
Vorzugsweise ist das Gewindeelement zur Ausbildung des Mantels mit dessen Kunststoff in einem Spritzgießprozess umspritzt. D. h. es handelt sich bei dem Gewindeelement um ein Einlegeteil. Preferably, the threaded element for forming the shell with the plastic encapsulated in an injection molding process. Ie. it is in the threaded element to an insert.
Dadurch, dass der Schraubdom separat von dem Trägerbauteil ausgeführt ist, kann dieser vorteilhafterweise je nach Bedarf (insbesondere beliebig) an dem Trägerbauteil positioniert werden. Insbesondere aus diesem Grund können bei einer nachträglichen Befestigung des Schraubdoms oder ggf. mehrerer Schraubdome an dem Trägerbauteil vorteilhafterweise auch vergleichsweise kleine Positionstoleranzen (und somit eine hohe Passgenauigkeit) erreicht werden, ohne dass dabei ein hoher Aufwand bei der Herstellung des gesamten Trägerbauteils betrieben werden müsste. Durch die Umhüllung des Gewindeelements mit thermoplastischem Kunststoff kann des Weiteren auf einfache Weise eine gegebenenfalls zum Befestigung des Gewindeelements erforderliche Geometrie ausgebildet werden, während als Gewindeelement vorzugsweise auf ein Standartbauteil zurückgegriffen werden kann. Dadurch können wiederum Kosten für Lagerhaltung vieler unterschiedlicher Gewindeelemente eingespart werden. Because the screwing dome is designed separately from the carrier component, it can advantageously be positioned on the carrier component as required (in particular as desired). For this reason in particular, comparatively small positional tolerances (and thus a high accuracy of fit) can advantageously be achieved with a subsequent attachment of the screw dome or, if appropriate, a plurality of screw domes on the support component, without requiring a high outlay in the production of the entire support component. By wrapping the threaded element with thermoplastic material can further easily a If necessary, geometry required for fastening the threaded element can be formed, while a standard component can preferably be used as the threaded element. As a result, in turn costs for storage of many different threaded elements can be saved.
In einer bevorzugten Ausführung handelt es sich bei dem Kunststoff des Mantels um einen laserstrahlschweißbaren thermoplastischen Kunststoff. Der Schraubdom ist in diesem Fall insbesondere dazu eingerichtet, mittels eines Laserstrahl-Fügeverfahrens an dem Trägerbauteil befestigt zu werden. Vorzugsweise handelt es sich bei dem Kunststoff des Mantels des Schraubdoms um einen laserstrahltransparenten Kunststoff. Dies ist beispielsweise für den Fall zweckmäßig, dass das Trägerbauteil aus einem laserstrahlschweißbaren, laserstrahlabsorbierenden thermoplastischen Kunststoff gebildet ist. Entsprechend umgekehrt ist der Mantel des Schraubdoms aus einem laserstrahlabsorbierenden (laserstrahlschweißbaren) Kunststoff ausgeführt, wenn das Trägerbauteil aus einem laserstrahltransparenten (laserstrahlschweißbaren) Kunststoff gebildet ist. In a preferred embodiment, the plastic of the shell is a laser-weldable thermoplastic material. The screw dome is in this case in particular adapted to be fixed by means of a laser beam joining method to the support member. Preferably, the plastic of the jacket of the screw dome is a laser-transparent plastic. This is expedient, for example, in the case where the carrier component is formed from a laser-beam-weldable, laser-beam-absorbing thermoplastic material. Correspondingly, conversely, the jacket of the screw dome is made of a laser-beam-absorbing (laser-beam-weldable) plastic, when the carrier component is formed from a laser-beam-transparent (laser-beam-weldable) plastic.
In einer zweckmäßigen Ausführung weist der Mantel des Schraubdoms an einem als „Befestigungsende“ bezeichneten Ende eine flanschartige Auskragung auf. Für den bevorzugten Fall, dass der Schraubdom eine näherungsweise zylindrische Grundform aufweist, ist diese Auskragung insbesondere als radialer Vorsprung ausgebildet (im Folgenden kurz als „Flansch“ bezeichnet). An diesem Flansch ist eine – vorzugsweise quer zu einer Schraubrichtung des Gewindeelements ausgerichtete – Auflagefläche ausgebildet, an der im bestimmungsgemäßen Montagezustand eine stoffschlüssige und/oder formschlüssige Verbindung mit dem Trägerbauteil ausgebildet ist. Die Auflagefläche ist in zweckmäßiger Weise durch eine quer zur Schraubrichtung verlaufende Oberfläche des Flansches selbst gebildet. Bevorzugt weist der Flansch allerdings einen entlang der Schraubrichtung vorstehenden Steg auf, der insbesondere ringförmig geschlossen ausgebildet ist, und an dessen Freiende die Auflagefläche ausgeformt ist. Für den Fall, dass der Schraubdom mittels des Laserstrahl-Fügeverfahrens an dem Trägerbauteil befestigt, wird durch den Steg vorteilhafterweise ausreichend thermoplastischer Kunststoff vorgehalten, so dass für eine Fügeverbindung mit ausreichender Festigkeit einen entsprechend langer „Schweißweg“ (auch: Einsinkweg) möglich ist. In an expedient embodiment, the jacket of the screw dome has a flange-like projection on an end designated as "fastening end". For the preferred case that the screw dome has an approximately cylindrical basic shape, this projection is in particular formed as a radial projection (hereinafter referred to briefly as "flange"). On this flange a - preferably aligned transversely to a screwing of the threaded element - bearing surface is formed on which in the intended mounting state is formed a cohesive and / or positive connection with the support member. The bearing surface is suitably formed by a transversely extending to the screw surface of the flange itself. However, the flange preferably has a web projecting along the screwing direction, which web is designed to be closed in an annular manner in particular, and at the free end of which the bearing surface is formed. In the event that the screw dome attached by means of the laser beam joining method to the support member, advantageously sufficient thermoplastic material is held by the web, so that for a joint connection with sufficient strength a correspondingly long "sweat path" (also: Einsinkweg) is possible.
In einer zweckmäßigen Ausführung handelt es sich bei dem Gewindeelement um eine insbesondere metallische Gewindebuchse. Dadurch wird bei der Montage der elektronischen Baugruppe vorteilhafterweise ein automatisches Einschrauben der in dem Schraubdom aufzunehmenden Schraube vereinfacht. In an expedient embodiment, the threaded element is a particular metallic threaded bushing. As a result, an automatic screwing in the screwed dome to be screw is advantageously simplified during assembly of the electronic module.
In einer weiteren zweckmäßigen Ausführung ist das Gewindeelement, insbesondere die Gewindebuchse, form- und stoffschlüssig in dem Mantel verankert. Das heißt, dass das Gewindeelement auf seiner Außenseite Vorsprünge und/oder Einschnitte aufweist, in denen sich der thermoplastische Kunststoff des Mantels „verkrallen“ kann, sodass auch bei hohen Einschraubmomenten und/oder Axialkräften ein Verdrehen des Gewindeelements in bzw. ein Ausziehen des Gewindeelements aus dem Mantel effektiv verhindert wird. Die stoffschlüssige Verankerung wird durch eine Haftung des thermoplastischen Kunststoffs an dem metallischen Gewindeelement gebildet. In a further expedient embodiment, the threaded element, in particular the threaded bush, is anchored positively and materially in the shell. This means that the threaded element has on its outer side projections and / or cuts, in which the thermoplastic material of the shell "claw" can, so even at high screw-in and / or axial forces twisting of the threaded member in or a withdrawal of the threaded element the coat is effectively prevented. The cohesive anchoring is formed by an adhesion of the thermoplastic material to the metallic threaded element.
Die erfindungsgemäße elektronische Baugruppe umfasst ein Trägerbauteil, an dem elektrische Komponenten, wie z.B. wenigstens eine Leiterplatte, Schaltungsbauteile und dergleichen gehaltert sind. Des Weiteren umfasst die elektronische Baugruppe wenigstens einen Schraubdom der vorstehend beschriebenen Art, der separat von dem Trägerbauteil gefertigt ist. Der Schraubdom ist dabei mittels eines Laserstrahl-Fügeverfahrens an dem Trägerbauteil befestigt. The electronic assembly according to the invention comprises a carrier component to which electrical components, such as e.g. at least one printed circuit board, circuit components and the like are held. Furthermore, the electronic assembly comprises at least one screw dome of the type described above, which is manufactured separately from the carrier component. The screw dome is fastened to the carrier component by means of a laser beam joining method.
Vorzugsweise umfasst die elektronische Baugruppe auch weitere Bauelemente, wie z.B. einen oder mehrere Gehäusedeckel zum vorzugsweise mediendichten Einhausen der elektrischen Komponenten, einen Kühlkörper, Steckkontakte zum elektrischen Verbinden der elektrischen Komponenten mit einer Energiequelle und/oder anderen elektronischen Baugruppen. Vorzugsweise ist wenigstens eines der Bauelemente und/oder der elektrischen Komponenten dabei mittels einer Schraube an dem Schraubdom oder einem der ggf. mehreren Schraubdome befestigt. Preferably, the electronic assembly also includes other components, such as e.g. one or more housing cover for preferably media-tight housing of the electrical components, a heat sink, plug contacts for electrically connecting the electrical components to a power source and / or other electronic components. Preferably, at least one of the components and / or the electrical components is fastened by means of a screw to the screw dome or one of the possibly more screw domes.
Vorzugsweise handelt es sich bei dem Trägerbauteil um ein Gehäuseelement eines Gehäuses der elektronischen Baugruppe. Beispielsweise bildet das Trägerbauteil eine „Gehäusewanne“ aus, in der die elektrischen Komponenten angeordnet und gehaltert sowie mittels des vorstehend beschriebenen Gehäusedeckels mediendicht eingehaust sind. The carrier component is preferably a housing element of a housing of the electronic module. By way of example, the carrier component forms a "housing pan" in which the electrical components are arranged and held and, by means of the housing cover described above, are enclosed in a media-tight manner.
In einer zweckmäßigen Ausführung ist das Trägerbauteil aus dem laserstrahlschweißbaren, insbesondere dem laserstrahlabsorbierenden thermoplastischen Kunststoff ausgebildet. Dadurch wird auf besonders einfache Weise eine Fügeverbindung mit dem Schraubdom, dessen Mantel in diesem Fall vorzugsweise aus dem laserstrahltransparenten thermoplastischen Kunststoff gebildet ist, ermöglicht. Zur Ausbildung der Fügeverbindung wird dabei vorzugsweise der laserstrahl-transparente Mantel, insbesondere dessen Flansch, auf das Trägerbauteil aufgesetzt und mittels eines Laserstrahls durchstrahlt. Dabei erwärmt sich der laserstrahlabsorbierende Kunststoff des Trägerbauteils bis zu seiner Schmelztemperatur (d. h. bis zu dem Temperaturwert, an dem der Kunststoff aufschmilzt). Insbesondere wird dabei durch den laserstrahlabsorbierenden Kunststoff auch der laserstrahltransparente Kunststoff des Schraubdoms bis zu seiner Schmelztemperatur erwärmt, sodass eine Kunststoff-Laserschweißnaht zwischen den beiden Bauelementen ausgebildet wird. In an expedient embodiment, the carrier component is formed from the laser-beam-weldable, in particular the laser-beam-absorbing thermoplastic material. This makes it possible in a particularly simple manner a joint connection with the screw dome, the jacket is preferably formed in this case from the laser-transparent thermoplastic. To form the joint connection is preferably the laser-transparent shell, in particular its flange, placed on the support member and irradiated by means of a laser beam. In this case, the laser-beam-absorbing plastic of the carrier component heats up to its melting temperature (ie, up to the temperature value at which the plastic melts). In particular, the laser-beam-transparent plastic of the screw-type dome is heated up to its melting temperature by the laser-beam-absorbing plastic, so that a plastic laser weld seam is formed between the two components.
In einer alternativen Ausführung ist das Trägerbauteil aus Metall, beispielsweise Aluminium oder Stahl, gebildet. Auch in diesem Fall ist der Schraubdom mittels Laserstrahlfügen an dem Trägerbauteil fixiert. Dazu wird zunächst – insbesondere unmittelbar vor dem Aufsetzen des Schraubdoms – die Fügefläche des Trägerbauteils (mikro-)strukturiert. Diese Strukturierung erfolgt insbesondere mittels eines Laserstrahls. Dabei wird eine wellen- oder sägezahnartige Oberflächenstruktur vorzugsweise mit Hinterschneidungen ausgebildet, wobei die Größe der Struktur im Bereich von weniger als 1 mm, vorzugsweise im Bereich von weniger als 0,3 mm liegt. Anschließend wird der Flansch des Schraubdoms auf die strukturierte Fläche des Trägerbauteils aufgesetzt und mittels eines Laserstrahls durchstrahlt, sodass sich das Metall des Trägerbauteils lokal erwärmt. Dadurch wird indirekt der laserstrahltransparente Kunststoff des Schraubdoms bis zu seiner Schmelztemperatur erwärmt. Der schmelzflüssige Kunststoff fließt dann – unter Wirkung eines vorzugsweise zwischen dem Schraubdom und dem Trägerbauteil aufgebrachten Fügedrucks – in die Oberflächenstruktur des Trägerbauteils ein und bildet dabei eine insbesondere stoff- und formschlüssige Verbindung aus. Durch die Ausführung des Trägerbauteils aus Metall wird insbesondere auch bei den im Motor- oder Getrieberaum eines Kraftfahrzeugs üblicherweise hohen Einsatztemperaturen eine vergleichsweise stabile Ausführung der elektronischen Baugruppe ermöglicht. Des Weiteren ist auch eine Wärmeabfuhr von den elektrischen Komponenten der elektronischen Baugruppe durch das Metall des Trägerbauteils hindurch ermöglicht. Die in dieser Ausführung gebildete Fügeverbindung wird hier und im Folgenden auch als Metall-Kunststoff-Laserfügeverbindung bezeichnet. In an alternative embodiment, the carrier component is made of metal, for example aluminum or steel. Also in this case, the screw dome is fixed to the support member by means of laser beam joining. For this purpose, the joining surface of the carrier component is first (micro) structured, in particular immediately prior to placement of the screw dome. This structuring takes place in particular by means of a laser beam. In this case, a wavy or sawtooth-like surface structure is preferably formed with undercuts, wherein the size of the structure in the range of less than 1 mm, preferably in the range of less than 0.3 mm. Subsequently, the flange of the screw dome is placed on the structured surface of the carrier component and irradiated by means of a laser beam, so that the metal of the carrier component heats up locally. As a result, the laser-transparent plastic of the screw dome is indirectly heated to its melting temperature. The molten plastic then flows into the surface structure of the carrier component, under the action of a joining pressure which is preferably applied between the screw dome and the carrier component, thereby forming a connection, in particular a material and positive connection. Due to the design of the carrier component made of metal, a comparatively stable design of the electronic assembly is made possible, in particular even in the case of the usually high operating temperatures in the engine or gear compartment of a motor vehicle. Furthermore, a heat dissipation from the electrical components of the electronic assembly through the metal of the support member is made possible. The joining connection formed in this embodiment is referred to here and below as a metal-plastic laser joining connection.
In einer zweckmäßigen Ausführung liegt der Schraubdom, insbesondere dessen Flansch, von einer Einschraubseite des Gewindeelements her auf dem Trägerbauteil auf. In an expedient embodiment, the screw dome, in particular its flange, rests on the carrier component from a screw-in side of the threaded element.
In einer besonders bevorzugten Ausführung durchgreift der Schraubdom das Trägerbauteil. Dadurch ist zumindest ein Teil der Länge des Schraubdoms in dem Trägerbauteil angeordnet, sodass eine vergleichsweise flache Bauform der Einheit aus Trägerbauteil und Schraubdom ermöglicht ist. In a particularly preferred embodiment, the screw dome engages through the carrier component. As a result, at least part of the length of the screw dome is arranged in the carrier component, so that a comparatively flat design of the unit consisting of carrier component and screw dome is made possible.
In einer bevorzugten Weiterbildung der vorstehend beschriebenen Ausführung liegt der Flansch des Mantels des Schraubdoms auf einer in Einschraubrichtung rückwärtigen Seite (im Folgenden auch als „Rückseite“ bezeichnet) des Trägerbauteils auf diesem auf. Mit anderen Worten hintergreift der Schraubdom mit seinem Flansch das Trägerbauteil und bildet somit einen (insbesondere zusätzlichen) Formschluss mit dem Trägerbauteil, sodass insbesondere eine Aufnahme von axialen Zugkräften, die durch die Schraube eingeleitet werden, verbessert ist. In a preferred embodiment of the embodiment described above, the flange of the jacket of the screw is located on a rear side in the screwing direction (hereinafter also referred to as "back") of the support member on this. In other words, the screw dome with its flange engages behind the carrier component and thus forms a (in particular additional) positive connection with the carrier component, so that in particular a recording of axial tensile forces which are introduced by the screw is improved.
Nachfolgend werden Ausführungsbeispiels der Erfindung in einer Zeichnung näher erläutert. Darin zeigen: Hereinafter, embodiment of the invention will be explained in more detail in a drawing. Show:
Einander entsprechende Teile sind in allen Figuren stets mit gleichen Bezugszeichen versehen. Corresponding parts are always provided with the same reference numerals in all figures.
In
In
Die Laserstrahl-Fügeverbindung
In einem alternativen, ebenfalls anhand von
In einem weiteren, ebenfalls anhand von
In
In einem weiteren Ausführungsbeispiel gemäß
Um zusätzlich zu der Laserstrahl-Fügeverbindung
In einem weiteren Ausführungsbeispiel der elektronischen Baugruppe
In den Ausführungsbeispielen gemäß
Bei dem Trägerbauteil
Der Gegenstand der Erfindung ist nicht auf die vorstehend beschriebenen Ausführungsbeispiele beschränkt. Vielmehr können weitere Ausführungsformen der Erfindung von dem Fachmann aus der vorstehenden Beschreibung abgeleitet werden. Insbesondere können die anhand der verschiedenen Ausführungsbeispiele beschriebenen Einzelmerkmale der Erfindung und deren Ausgestaltungsvarianten auch in anderer Weise miteinander kombiniert werden. The object of the invention is not limited to the embodiments described above. Rather, other embodiments of the invention may be derived by those skilled in the art from the foregoing description. In particular, the individual features of the invention described with reference to the various exemplary embodiments and their design variants can also be combined with one another in a different manner.
BezugszeichenlisteLIST OF REFERENCE NUMBERS
- 1 1
- Schraubdom screw boss
- 2 2
- Trägerbauteil support component
- 3 3
- elektronische Baugruppe electronic assembly
- 4 4
- Gewindebuchse threaded bushing
- 6 6
- Mantel coat
- 8 8th
- Flansch flange
- 10 10
- Befestigungsende attachment end
- 12 12
- Auflagefläche bearing surface
- 14 14
- Ringsteg ring land
- 16 16
- Schraubrichtung screwing
- 17 17
- Laserstrahl-Fügeverbindung Laser beam joint connection
- 20 20
- Oberfläche surface
- 21 21
- Ringsteg ring land
- 22 22
- Bohrung drilling
- 24 24
- Oberfläche surface
- 26 26
- Ringnut ring groove
- 28 28
- Durchgangsbohrung Through Hole
Claims (10)
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102019219841A1 (en) * | 2019-12-17 | 2021-06-17 | Robert Bosch Gmbh | Electronic device |
US11078948B2 (en) | 2019-02-18 | 2021-08-03 | Ford Global Technologies, Llc | Fastener boss and motor vehicle component incorporating that fastener boss |
CN113263297A (en) * | 2021-05-29 | 2021-08-17 | 唐山津丰泓泵业股份有限公司 | Novel screw pump screw sleeve processing technology |
US11325289B2 (en) | 2019-10-16 | 2022-05-10 | Ford Global Technologies, Llc | Method of forming a screw boss in an injection molded polymer part |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11078948B2 (en) | 2019-02-18 | 2021-08-03 | Ford Global Technologies, Llc | Fastener boss and motor vehicle component incorporating that fastener boss |
US11325289B2 (en) | 2019-10-16 | 2022-05-10 | Ford Global Technologies, Llc | Method of forming a screw boss in an injection molded polymer part |
DE102019219841A1 (en) * | 2019-12-17 | 2021-06-17 | Robert Bosch Gmbh | Electronic device |
CN113263297A (en) * | 2021-05-29 | 2021-08-17 | 唐山津丰泓泵业股份有限公司 | Novel screw pump screw sleeve processing technology |
CN113263297B (en) * | 2021-05-29 | 2022-03-08 | 唐山津丰泓泵业股份有限公司 | Novel screw pump screw sleeve processing technology |
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