DE2433131A1 - Self-adhesive elastic mounting device - which is used for elastic supports and couplings, contains magnets to hold parts together - Google Patents

Self-adhesive elastic mounting device - which is used for elastic supports and couplings, contains magnets to hold parts together

Info

Publication number
DE2433131A1
DE2433131A1 DE2433131A DE2433131A DE2433131A1 DE 2433131 A1 DE2433131 A1 DE 2433131A1 DE 2433131 A DE2433131 A DE 2433131A DE 2433131 A DE2433131 A DE 2433131A DE 2433131 A1 DE2433131 A1 DE 2433131A1
Authority
DE
Germany
Prior art keywords
self
elastic
adhesive
parts
couplings
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.)
Granted
Application number
DE2433131A
Other languages
German (de)
Other versions
DE2433131C3 (en
DE2433131B2 (en
Inventor
Juergen Schletter
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.)
SGF Sueddeutsche Gelenkscheibenfabrik GmbH and Co KG
Original Assignee
SGF Sueddeutsche Gelenkscheibenfabrik GmbH and Co KG
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 SGF Sueddeutsche Gelenkscheibenfabrik GmbH and Co KG filed Critical SGF Sueddeutsche Gelenkscheibenfabrik GmbH and Co KG
Priority to DE19742433131 priority Critical patent/DE2433131C3/en
Publication of DE2433131A1 publication Critical patent/DE2433131A1/en
Publication of DE2433131B2 publication Critical patent/DE2433131B2/en
Application granted granted Critical
Publication of DE2433131C3 publication Critical patent/DE2433131C3/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/373—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by having a particular shape
    • F16F1/3732—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by having a particular shape having an annular or the like shape, e.g. grommet-type resilient mountings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
    • F16D3/50—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive with the coupling parts connected by one or more intermediate members
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/3605—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers characterised by their material

Abstract

The mounting is self adhesive and elastic, and homogenous, alternatively it may consist of several layers of a suitable elastomer material. The outer layers contain embedded or connected magnets, or magnetic powder. The magnetic adhesion replaces the conventional mechanical connections between mounting and parts. The mounting can be manufactured independently of the shape or form of the sections to be connected. The top (1) and bottom (3) parts of the device may be flat or they may be of complementary shapes, and they are separated by a sandwich layer of the elastomer material. The top and bottom parts are made of ferromagnetic material.

Description

Selbsthaftendes elastisches Element Die Erfindung betrifft ein selbsthaftendes elastisches Element unbestimmter, dem jeweiligen Einsatzzweck angepaßter äußerer Form, das zwischen Eisenteilen mit entsprechender Antiform angeordnet wird. Solche selbsthaftenden elastischen Elemente Ubertragen alle Arten von Kräften zwischen den elastisch zu verbindenden Metallteilen. Die Eigenschaften des Elastomers erlauben eine elastische, schwingungs- und stoßdämpfende Ubertragung aller Kräfte, eine Unterbrechung von Geräuschen, Vibrations- oder Stromflüssen. Die Selbsthaftung ergibt bei Uberlastung einen Rutscheffekt und das selbsthaftende elastische Element wirkt als Sicherheitsteil.Self-Adhesive Elastic Element The invention relates to a self-adhesive one elastic element of indeterminate, the respective application adapted outer Shape that is arranged between iron parts with a corresponding anti-shape. Such self-adhesive elastic elements transfer all kinds of forces between the metal parts to be elastically connected. Allow the properties of the elastomer an elastic, vibration and shock-absorbing transmission of all forces, an interruption of noises, vibrations or electricity flows. The self-liability results in case of overload a slip effect and the self-adhesive elastic element acts as a safety part.

Bisher werden die Kräfte von Metallteilen in die elastischen Elemente Uber Schrauben, Steckbolzen oder sinnreich angeordnete Erhebungen und Vertiefungen formschlüssig oder durch Klemmen oder Anvulkanisieren der elastischen Elemente an die Metallteile kraftschlüssig Ubertragen.So far, the forces of metal parts in the elastic elements Via screws, socket pins or ingeniously arranged elevations and depressions form-fitting or by clamping or vulcanizing the elastic elements the metal parts transfer positively.

Bei Formschlußübertragung bedürfen alle diese elastischen und metallischen Teile eines hohen Grades von formgebender Bearbeitung und die elastischen Teile mUssen oft eng tolerierte Formen, Bohrungen und Teilkreise besitzen.In the case of positive locking transmission, all of these require elastic and metallic ones Parts of a high degree of shaping and the elastic parts Often have to have closely toleranced shapes, bores and pitch circles.

Bei kraftschlussigen Verbindungen sind aufwendige Klemmvorrichtungen bei oft großen Abmessungen erforderlich bzw. das Anvulkanisieren der elastischen Elemente an die Metallteile erfordert eine Bearbeitung der Oberfläche, den Einsatz von Haftvermittlern und das Aufheizen der Metallteile zusammen mit den elastischen Teilen in den dadurch besonders umfangreichen und schwierigen Vulkanisierwerkzeugen.In the case of frictional connections, complex clamping devices are required Often required for large dimensions or vulcanization of the elastic ones Elements to the metal parts requires a processing of the surface, the use of adhesion promoters and the heating of the metal parts together with the elastic ones Parts in the vulcanizing tools that are particularly extensive and difficult as a result.

Ziel der Erfindung ist ein selbsthaftendes elastisches Element, das in einfachen Werkzeugen in Abwesenheit der zu verbindenden Metallteile hergestellt werden kann, mit simplen und daher billigen metallischen Anschlußteilen verbunden und auf einfache Weise montiert werden kann.The aim of the invention is a self-adhesive elastic element that made in simple tools in the absence of the metal parts to be joined can be connected with simple and therefore cheap metallic connecting parts and can be easily assembled.

Gemäß der Erfindung besteht ein selbsthaftendes elastisches Element aus einem homogenen oder aus mehreren Schichten aufgebauten Teil aus geeigneten Elastomeren, das oder dessen äußere Schichten durch Einlagern bzw. Anlagern von Magneten selbst an Metallteilen haftet Diese selbsthaftenden Kräfte ersetzen oder ergänzen die bisher üblichen Verbindungen zwischen Elastomer und Metallteil.According to the invention there is a self-adhesive elastic element from a homogeneous or composed of several layers of suitable parts Elastomers, the or its outer layers by incorporation or attachment of Magnet itself adheres to metal parts These self-adhesive forces replace or complete the previously common connections between elastomer and metal part.

Anhand der Zeichnungen Blatt I und Blatt II werden einige Gestaltungsmöglichkeiten der Erfindung erläutert.Using the drawings on sheet I and sheet II, some design options are shown the invention explained.

Es bedeuten: Figur 1 = das selbsthaftende elastische Element gemäß der Erfindung als einfache Lagerung im Schnitt Figur 2 = die Draufsicht von Figur 1 Figur 3 = das selbsthaftende elastische Element gemäß der Erfindung als konische Lagerung im Schnitt Figur 4 = die Draufsicht von Figur 3 Figur 5 = das selbsthaftende elastische Element gemäß der Erfindung als Teil einer konischen elastischen Kupplung Figur 6 = die Seitenansicht von Figur 5 Figur 7 = das selbsthaftende elastische Element gemäß der Erfindung als Teil einer elastischen Ringkupplung Figur 8 = die Seitenansicht von Figur 7 Das selbsthaftende elastische Element 2 gemäß der Erfindung, angeordnet als Lagerung, haftet zwischen dem Oberteil 1 und dem Unterteil 3. Das Oberteil 1 ist mit dem Aggregat und das Unterteil 3 ist mit dem Rahmen oder Fundament verbunden. Oberteil 1 und Unterteil 3 bestehen wie bisher üblich aus ferromagnetischem Material.It denotes: FIG. 1 = the self-adhesive elastic element according to FIG of the invention as a simple storage in section Figure 2 = the top view of Figure 1 Figure 3 = the self-adhesive elastic element according to the invention as a conical Storage in section Figure 4 = the top view of Figure 3 Figure 5 = the self-adhesive elastic element according to the invention as part of a conical elastic coupling Figure 6 = the side view of Figure 5 Figure 7 = the self-adhesive elastic Element according to the invention as part of an elastic ring coupling Figure 8 = the Side view of Figure 7 The self-adhesive elastic element 2 according to the invention, arranged as a storage, adheres between the upper part 1 and the lower part 3. The upper part 1 is with the unit and the lower part 3 is with connected to the frame or foundation. Upper part 1 and lower part 3 exist as before usually made of ferromagnetic material.

Als konische Lagerung ausgebildet, befindet sich das selbsthaftende Element 2 zwischen dem konischen Oberteil 4 und dem konischen Unterteil 5, wobei wiederum das konische Oberteil 4 mit dem Aggregat und das konische Unterteil 5 mit dem Rahmen oder Fundament verbunden ist.The self-adhesive one is designed as a conical bearing Element 2 between the conical upper part 4 and the conical lower part 5, wherein again the conical upper part 4 with the unit and the conical lower part 5 with is connected to the frame or foundation.

In Figur 5 und 6 ist das selbsthaftende elastische Element 2 gemäß der Erfindung als Teil einer konischen elastischen Kupplung ausgebildet und haftet zwischen dem treibenden Flansch 6 und getriebenem Flansch 7.In Figures 5 and 6, the self-adhesive elastic element 2 is according to of the invention designed as part of a conical elastic coupling and adheres between the driving flange 6 and driven flange 7.

Als Teil bzw. als Zwischenring ist das selbsthaftende elastische Element 2 in einer elastischen Ringkupplung ausgebildet und haftet zwischen dem Innenring 9 und dem Außenring 8.The self-adhesive elastic element is used as part or as an intermediate ring 2 formed in an elastic ring coupling and adheres between the inner ring 9 and the outer ring 8.

Der Vorteil des selbsthaftenden elastischen Elementes 2 gemäß der Erfindung liegt in der einfachen Herstellung, der einfachen Montage, der vielseitigen Anwendbarkeit und darin, daß bei Uberschreiten der vorgesehenen Kräfte die Verbindung gelöst wird, was größere Schäden oder Bruch an Maschinen vermeidet. Dies ist besonders bei elastischen Kupplungen wichtig.The advantage of the self-adhesive elastic element 2 according to FIG Invention lies in the simple manufacture, the simple assembly, the versatile Applicability and the fact that if the intended forces are exceeded, the connection solved, which avoids major damage or breakage to machines. This is special important for flexible couplings.

Die Erfindung beschränkt sich nicht auf elastische Lagerungen und elastische Kupplungen, sondern kann überall dort angewendet werden, wo ein Elastomer an magnetischen Metallteilen haften soll.The invention is not limited to elastic bearings and elastic couplings, but can be used wherever an elastomer should adhere to magnetic metal parts.

Claims (1)

Patentanspruch (Schutzanspruch)Patent claim (protection claim) 1. Selbsthaftendes elastisches Element dadurch gekennzeichnet, daß es aus Elastomer besteht, in das Magnete oder Magnetpulver eingebettet oder angelagert sind.1. Self-adhesive elastic element characterized in that it consists of elastomer in which magnets or magnetic powder are embedded or deposited are. L e e r s e i t eL e r s e i t e
DE19742433131 1974-07-10 1974-07-10 Elastic connection between two components made of ferromagnetic material Expired DE2433131C3 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19742433131 DE2433131C3 (en) 1974-07-10 1974-07-10 Elastic connection between two components made of ferromagnetic material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19742433131 DE2433131C3 (en) 1974-07-10 1974-07-10 Elastic connection between two components made of ferromagnetic material

Publications (3)

Publication Number Publication Date
DE2433131A1 true DE2433131A1 (en) 1976-01-22
DE2433131B2 DE2433131B2 (en) 1977-10-20
DE2433131C3 DE2433131C3 (en) 1978-06-08

Family

ID=5920181

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19742433131 Expired DE2433131C3 (en) 1974-07-10 1974-07-10 Elastic connection between two components made of ferromagnetic material

Country Status (1)

Country Link
DE (1) DE2433131C3 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2357773A1 (en) * 1976-07-05 1978-02-03 Hurth Masch Zahnrad Carl TILTING PIVOT FOR ARTICULATED JOINTS, ESPECIALLY FOR CARDAN JOINTS OR SIMILAR JOINTS
EP0031775A1 (en) * 1980-01-03 1981-07-08 Containeering Corporation Cistern comprising a vessel contained within a parallelepiped framework
ITRM20130481A1 (en) * 2013-08-23 2015-02-24 Andrea Dipanati ANTIVIBRATION MAGNETIC SUPPORT FOR OUTDOOR UNITS OF AIR-CONDITIONERS.
CN104712692A (en) * 2013-12-12 2015-06-17 波音公司 Motion-damping systems and methods including the same
US9670981B2 (en) 2013-12-12 2017-06-06 The Boeing Company Motion-damping systems and methods including the same
EP4357238A1 (en) * 2022-10-19 2024-04-24 B/E Aerospace (UK) Limited Retainers

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2357773A1 (en) * 1976-07-05 1978-02-03 Hurth Masch Zahnrad Carl TILTING PIVOT FOR ARTICULATED JOINTS, ESPECIALLY FOR CARDAN JOINTS OR SIMILAR JOINTS
EP0031775A1 (en) * 1980-01-03 1981-07-08 Containeering Corporation Cistern comprising a vessel contained within a parallelepiped framework
FR2473018A1 (en) * 1980-01-03 1981-07-10 Containeering Corp CONTAINER-TANK COMPRISING A TANK RETAINED WITHIN A PARALLELEPIPEDIC FRAMEWORK
ITRM20130481A1 (en) * 2013-08-23 2015-02-24 Andrea Dipanati ANTIVIBRATION MAGNETIC SUPPORT FOR OUTDOOR UNITS OF AIR-CONDITIONERS.
CN104712692A (en) * 2013-12-12 2015-06-17 波音公司 Motion-damping systems and methods including the same
EP2896562A1 (en) * 2013-12-12 2015-07-22 The Boeing Company Motion-damping systems and methods including the same
US9509204B2 (en) 2013-12-12 2016-11-29 The Boeing Company Motion-damping systems between base structure and an attached component and methods including the same
US9670981B2 (en) 2013-12-12 2017-06-06 The Boeing Company Motion-damping systems and methods including the same
AU2014240296B2 (en) * 2013-12-12 2017-08-24 The Boeing Company Motion-damping systems and methods including the same
US10487906B2 (en) 2013-12-12 2019-11-26 The Boeing Company Motion-damping systems and methods including the same
EP4357238A1 (en) * 2022-10-19 2024-04-24 B/E Aerospace (UK) Limited Retainers

Also Published As

Publication number Publication date
DE2433131C3 (en) 1978-06-08
DE2433131B2 (en) 1977-10-20

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C3 Grant after two publication steps (3rd publication)