FR2628799A1 - Insert device screwed into composite materials - threads are at variable angles according to type of composite and slot prevents too high stresses forming - Google Patents

Insert device screwed into composite materials - threads are at variable angles according to type of composite and slot prevents too high stresses forming Download PDF

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Publication number
FR2628799A1
FR2628799A1 FR8803457A FR8803457A FR2628799A1 FR 2628799 A1 FR2628799 A1 FR 2628799A1 FR 8803457 A FR8803457 A FR 8803457A FR 8803457 A FR8803457 A FR 8803457A FR 2628799 A1 FR2628799 A1 FR 2628799A1
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France
Prior art keywords
threads
composite
insert
slot
type
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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.)
Withdrawn
Application number
FR8803457A
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French (fr)
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HALLOUIN JAMES
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HALLOUIN JAMES
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Publication date
Application filed by HALLOUIN JAMES filed Critical HALLOUIN JAMES
Priority to FR8803457A priority Critical patent/FR2628799A1/en
Publication of FR2628799A1 publication Critical patent/FR2628799A1/en
Withdrawn legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B37/00Nuts or like thread-engaging members
    • F16B37/12Nuts or like thread-engaging members with thread-engaging surfaces formed by inserted coil-springs, discs, or the like; Independent pieces of wound wire used as nuts; Threaded inserts for holes
    • F16B37/122Threaded inserts, e.g. "rampa bolts"

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

The device consists of a cylindrical body (1) with two parallel threads (3, 4) ending in a bevelled edge (9), a slot (7) and a grooved guiding end (10). The angles at the top of the threads (3, 4) vary according to the type of composite material, but are always supplementary angles. The opposite end to the slot can receive a round or a hexagonal collaret (5). As the device is inserted into the composite, the bevelled edge (9) cuts through glass fibres and the material is compressed. The stresses caused by insertion of the device are reduced by the slot (7). USE/ADVANTAGE - Insert screwed into composite materials. The insert, used after moulding, offers comparable performance to existing techniques, plus improved productivity, quality and profitability.

Description

La présente invention concerne les inserts en acier ,en laiton, en zamia ou en plastique destinés a être mis en place dans des supports en matériaux composites, pour donner par exemple des taraudages, des +i 1 etages, des axes, des entretoises; elle crée,notamment un insert qui est conçu pour Etre mis en place à l'aide d'un dispositif de vissage. The present invention relates to steel, brass, zamia or plastic inserts intended to be put in place in supports made of composite materials, to give for example threads, + i 1 stages, axes, spacers; it creates, in particular an insert which is designed to be put in place using a screwing device.

La présente invention développe un insert qui , posé apres moulage sa des performances voisines de celles de l'insert surmoulé.Elle permet ainsi raugmenter la productivité ( pas d'arrêt de la presse pour mettre les inserts), la rentabilité (amortissement plus rapide) et la qualité (pose en automatique des inserts). The present invention develops an insert which, after molding, has performances close to those of the overmolded insert. It thus allows to increase the productivity (no stopping of the press to put the inserts), the profitability (faster amortization). and quality (automatic insertion of inserts).

Àu dessin annexé, l'insert comprend un corps cylindrique principal portant deux filetages parallèles se terminant en biseau et une fente. L'extrémité opposée à la fente peut recevoir une collerette ronde ou hexagonale suivant le type d'entrainement. L'autre peut comporter un bout pilote rainuré.Il peut porter en son centre soit un trou taraudé ou lisse soit un axe lisse ou fileté. In the accompanying drawing, the insert comprises a main cylindrical body carrying two parallel threads ending in a bevel and a slot. The end opposite to the slot can receive a round or hexagonal flange depending on the type of drive. The other can have a grooved pilot end, and can carry in its center either a tapped or smooth hole or a smooth or threaded pin.

L'invention est représentée,a titre d'exemple non limitati+,au dessin annexé. The invention is shown, by way of nonlimiting example +, in the accompanying drawing.

La fig.1 est une vue, partie en élévation, partie en coupe de l'insert en regard de son bossage. Fig.1 is a view, partly in elevation, partly in section of the insert opposite its boss.

Au dessin annexé, fig.1, l'insert comprend un corps généralement cylindrique désigné par (1) ayant un alésage axial fileté (5)et et sur son pourtour de filetages parallèles dont l'angle au sommet de l'un est obtu (z) et l'autre aigu (4). A une extrémité on trouve une collerette (5) et à l'autre extrémité un biseau (9) un bout pilote (11) avec une rainure (10) et une fente (8).  In the accompanying drawing, fig.1, the insert comprises a generally cylindrical body designated by (1) having a threaded axial bore (5) and and around its periphery of parallel threads whose angle at the top of one is obtu ( z) and the other acute (4). At one end there is a flange (5) and at the other end a bevel (9) a pilot end (11) with a groove (10) and a slot (8).

Dans les conditions de service,l'insert doit faire son chemin dans des matériaux renforcés de fibres le plus souvent en verre.Pour tailler dans ces fibres de verre il faut un biseau fig. le plus tranchant possible ,que l'on obtient en coupant ces filetages (3) et (4) suivant un plan (X X') perpendiculaire à l'axe de insert < Y Y'). L'extrème minceur du biseau peut créer un crantage qui facilite l'accrochage et le vissage du premier filet de l'insert dans son support.La pression a exercer est alors plus faible et plus régulière. Under operating conditions, the insert must make its way out of fiber-reinforced materials, most often glass. To cut in these glass fibers, a bevel is required fig. as sharp as possible, which is obtained by cutting these threads (3) and (4) along a plane (X X ') perpendicular to the axis of insert <Y Y'). The extreme thinness of the bevel can create a notch which facilitates the attachment and screwing of the first thread of the insert into its support. The pressure to be exerted is then lower and more regular.

Lors de la mise en place de l'insert dans son trou, il est important que l'axe de l'un (X X') coincide avec: l'axe de l'autre (Z Z)pour obtenir ,d'une part un couple de vissage régulier indispensable pour une bonne installation et d'autre part pour eviter que ,soit des contraintes latérales trop élevées amenent une rupture du bossage (13), soit des efforts axiaux mal répartis provoquent l'arrachement de la paroi du trou (12). Le bout pilote (ii) est alors indispensable, notamment dans le cas de pose manuelle sans support de guidage et aussi dans le cas de pose automatique lorsque les variations d'entr'axe sont trop grandes.Son diamètre ne pourra excéder le diamètre du fond du trou. When placing the insert in its hole, it is important that the axis of one (X X ') coincides with: the axis of the other (ZZ) to obtain, on the one hand a regular screwing torque essential for a good installation and on the other hand to avoid that either too high lateral stresses cause the boss (13) to break, or poorly distributed axial forces cause the wall of the hole to tear off ( 12). The pilot tip (ii) is then essential, in particular in the case of manual installation without guide support and also in the case of automatic installation when the variations in the center distance are too large. Its diameter cannot exceed the diameter of the bottom the hole.

Ce bout pilote comporte une rainure (10) dans laquelle peuvent s'accumuler en partie les résidus de taraudage, prevenant ainsi les risques de bourrage et par suite la rupture du bossage. This pilot end has a groove (10) in which the tapping residues can partially accumulate, thus preventing the risks of jamming and consequently the rupture of the boss.

L'insert après avoir coupé ces fibres de verre, vient mettre en compression des matériau qui sont souvent rigides,induisant donc des contraintes de plus en plus élevées au fur et å mesure que l'insert se visse dans son bossage. Pour diminuer ces contraintes on fraise une fente ou une gouje(7) au moins sur deux filets, créant ainsi deux lèpres de taraudage, l'une (8) servant d' ébauche et l'autre (6) de finition.La fente sera suffisamment large et profonde pour permettre l'évacuation der copeaux.  The insert, after having cut these glass fibers, comes to compress materials which are often rigid, thus inducing increasingly higher stresses as the insert is screwed into its boss. To reduce these constraints, a slot or a groove (7) is milled at least on two threads, thus creating two tapping leprosy, one (8) serving as a roughing and the other (6) for finishing. wide enough and deep enough to allow chip evacuation.

Suivant les procedés de fabrication et la nature des matériau: on peut obtenir des bossages très résistants ou très fragiles .Cest la raison pour laquelle les filetages (3) et (4) sont a géométrie variable en ce sens que leur angle au sommet peut varier tout en restant supplémentaires Par exemple, lorsque le matériau support est fragile on diminuera au maximum les contraintes en utilisant un filetage très aigu (25 ) pour l'accrochage et un filetage très obtu (155 ) qui limite le faux-rond en mordant legerement dans la paroi du trou,consolidant ainsi le filetage fin sans créer de contraintes excéssives.  Depending on the manufacturing process and the nature of the material: very strong or very fragile bosses can be obtained. This is the reason why the threads (3) and (4) are of variable geometry in the sense that their apex angle can vary. while remaining additional For example, when the support material is fragile, the stresses will be reduced as much as possible by using a very sharp thread (25) for attachment and a very obtuse thread (155) which limits the runout by biting slightly in the wall of the hole, thus consolidating the fine thread without creating excessive stresses.

Inversement, lorsque le matériau est plus résistant, 1 'insert étant davantage sollicite, l'angle aigu sera plus grand (40 ) pour donner une resistance au cisaillement beaucoup plus élevée. L'angle obtu (140 ) participera davantage aux charges appliquées en pénétrant plus dans le support. Conversely, when the material is more resistant, the insert being more stressed, the acute angle will be greater (40) to give a much higher shear strength. The obtuse angle (140) will participate more in the applied loads by penetrating more into the support.

Ce double filetage en forme de " W ' permet d'absorber les variations dimensionnelles propres a tous les assemblages , sans provoquer la rupture du bossage.En effet, le filet obtu en cas de variation dimensionnelle du trou penetre progressivement dans la paroi du trou, alors qn fond plat ou une nervure arrondie crée des tensions élevées amenant la rupture du support.  This double thread in the shape of "W 'makes it possible to absorb the dimensional variations specific to all the assemblies, without causing the rupture of the boss. so that a flat bottom or a rounded rib creates high tensions leading to the rupture of the support.

Claims (7)

REVENDICATIONS 1) Insert caractérisé en ce qil comprend un corps cylindrique(1) ! recevant un double filetage(3 et 4) se terminant en biseau(9),une fente(7) et un bout pilote(11) rainuré(10). 1) Insert characterized in that it comprises a cylindrical body (1)! receiving a double thread (3 and 4) ending in bevel (9), a slot (7) and a pilot end (11) grooved (10). 2) Dispositif selon la revendication i caractérisé en ce que les angles au sommet des filetages(3 et 4) sont supplémentaires. 2) Device according to claim i characterized in that the angles at the top of the threads (3 and 4) are additional. 3) Dispositif selon les revendications i et 2 caractérisé en ce que les angles au sommmet des filetages (3 et 4) varient suivant la nature du matériau support tout en restant supplémentaires. 3) Device according to claims i and 2 characterized in that the angles at the top of the threads (3 and 4) vary according to the nature of the support material while remaining additional. 4) Dispositif suivant les revendications 1,2 et caractérisé en ce que lpinterval entre deux filetages aigus(4) a la forme d'un "w". 4) Device according to claims 1,2 and characterized in that lpinterval between two acute threads (4) has the shape of a "w". 5) Dispositif selon la revendication 1 caractérisé en ce que le double filetage(3 et 4) se termine par un biseau, obtenu par un plan de coupe perpendiculaire à l lae de l'insert.  5) Device according to claim 1 characterized in that the double thread (3 and 4) ends with a bevel, obtained by a cutting plane perpendicular to the lae of the insert. 6) Dispositif selon la revendication i caractérisé en ce que la fente(7) dégage au moins deux livres de taraudage par filetage ,l'une pour l'ébauche(B) ,l'autre pour la finition(6) 6) Device according to claim i characterized in that the slot (7) releases at least two pounds of thread tapping, one for the blank (B), the other for the finish (6) 7) Dispositif selon la revendication i caractérisé en ce que le bout pilote(11) centre et guide l'insert dans son trou. 7) Device according to claim i characterized in that the pilot tip (11) centers and guides the insert in its hole. e > Dispositif selon la revendication i caractérisé en ce que le bout pilote(11) comporte une rainure de dégagement(10) des résidus de taraudage.  e> Device according to claim i characterized in that the pilot tip (11) has a relief groove (10) of the tapping residues.
FR8803457A 1988-03-17 1988-03-17 Insert device screwed into composite materials - threads are at variable angles according to type of composite and slot prevents too high stresses forming Withdrawn FR2628799A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8803457A FR2628799A1 (en) 1988-03-17 1988-03-17 Insert device screwed into composite materials - threads are at variable angles according to type of composite and slot prevents too high stresses forming

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8803457A FR2628799A1 (en) 1988-03-17 1988-03-17 Insert device screwed into composite materials - threads are at variable angles according to type of composite and slot prevents too high stresses forming

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FR2628799A1 true FR2628799A1 (en) 1989-09-22

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19732615A1 (en) * 1997-07-29 1999-02-04 Ejot Verbindungstech Gmbh & Co Cold-rolled self-tapping screw for use with thermoplastics
EP1447205A2 (en) 2003-02-07 2004-08-18 Bayerische Motoren Werke Aktiengesellschaft Anchoring element for a structural element

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3246179C1 (en) * 1982-12-14 1984-02-09 Kerb-Konus-Vertriebs-Gmbh, 8454 Schnaittenbach Method for producing self-tapping thread inserts
DE3301088C1 (en) * 1983-01-14 1984-02-16 Kerb-Konus-Vertriebs-Gmbh, 8454 Schnaittenbach Self-tapping threaded insert
DE3242059A1 (en) * 1981-10-05 1984-05-17 I.T.W. De France, Beauchamp, Val D'oise FASTENERS

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3242059A1 (en) * 1981-10-05 1984-05-17 I.T.W. De France, Beauchamp, Val D'oise FASTENERS
DE3246179C1 (en) * 1982-12-14 1984-02-09 Kerb-Konus-Vertriebs-Gmbh, 8454 Schnaittenbach Method for producing self-tapping thread inserts
DE3301088C1 (en) * 1983-01-14 1984-02-16 Kerb-Konus-Vertriebs-Gmbh, 8454 Schnaittenbach Self-tapping threaded insert

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19732615A1 (en) * 1997-07-29 1999-02-04 Ejot Verbindungstech Gmbh & Co Cold-rolled self-tapping screw for use with thermoplastics
EP1447205A2 (en) 2003-02-07 2004-08-18 Bayerische Motoren Werke Aktiengesellschaft Anchoring element for a structural element

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