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FR2545556A1 - Method for manufacturing dismantleable and adjustable safety connecting rods and connecting rods obtained by this method - Google Patents

Method for manufacturing dismantleable and adjustable safety connecting rods and connecting rods obtained by this method Download PDF

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Publication number
FR2545556A1
FR2545556A1 FR8307658A FR8307658A FR2545556A1 FR 2545556 A1 FR2545556 A1 FR 2545556A1 FR 8307658 A FR8307658 A FR 8307658A FR 8307658 A FR8307658 A FR 8307658A FR 2545556 A1 FR2545556 A1 FR 2545556A1
Authority
FR
France
Prior art keywords
tubes
connecting rods
tube
threaded
mandrel
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
FR8307658A
Other languages
French (fr)
Other versions
FR2545556B1 (en
Inventor
Didier Chobert
Jean Claude Pourrat
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.)
SKF Compagnie dApplications Mecaniques SA
Original Assignee
SKF Compagnie dApplications Mecaniques SA
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 SKF Compagnie dApplications Mecaniques SA filed Critical SKF Compagnie dApplications Mecaniques SA
Priority to FR8307658A priority Critical patent/FR2545556B1/en
Publication of FR2545556A1 publication Critical patent/FR2545556A1/en
Application granted granted Critical
Publication of FR2545556B1 publication Critical patent/FR2545556B1/en
Expired legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/26Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/30Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
    • 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
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C7/00Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
    • F16C7/02Constructions of connecting-rods with constant length
    • 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
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00Articles relating to transporting
    • F16C2326/43Aeroplanes; Helicopters

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Prostheses (AREA)

Abstract

The subject of the present invention is a method for manufacturing safety connecting rods comprising a clevis at one of their ends, in which two tubes fitted into each other are used. According to the invention, the two tubes are immobilised by a mandrel or threaded tie-rod 6 and the clevis is then formed simultaneously on the two tubes 1 and 2 thus immobilised.

Description

Procédé de fabrication de bielles de sécurité démontables et ré-Method for manufacturing removable and retractable safety rods

glables et bielles obtenues par ce procédé.  glables and connecting rods obtained by this process.

Les bielles tubulaires à extrémités rétreintes ont de nom-  Tubular connecting rods with constricted ends have many

breuses applications tant en mécanique qu'en aéronautique Elles peuvent être utilisées, par exemple, comme bielles de commande de  applications in both mechanics and aeronautics They can be used, for example, as control rods for

vol, ou comme tirants de support de plancher ou d'attache d'aile.  flight, or as floor support or wing tie rods.

il est parfois nécessaire, pour des raisons de sécurité, de  it is sometimes necessary, for security reasons, to

doubler ces bielles Lorsqu'il n'y a pas de problème d'encombre-  double these rods When there is no problem of clutter-

ment, il suffit de mettre en parallèle deux chaînes complètes de bielles Mais cette disposition n'est pas applicable lorsque la  ment, it suffices to parallel two complete chains of connecting rods. But this provision is not applicable when the

place disponible est réduite.available space is reduced.

On connaît des bielles de sécurité dites "Fail Safe"l qui son  We know safety rods called "Fail Safe" l which

formées de deux tubes enfilés l'un dans l'autre Si l'un des tu-  formed of two tubes threaded one inside the other If one of the tu-

bes vient par exemple à se rompre, l'autre tube continue à assure: la transmission de l'effort Mais les bielles de ce genre jusqu'à  bes for example breaks, the other tube continues to ensure: the transmission of the force But the rods of this kind until

présent réalisées ne sont ni démontables, ni réglables.  present are neither removable nor adjustable.

La présente invention a pour objet un procédé de fabrication de bielles de sécurité, comportant une chape à une extrémité, qui  The present invention relates to a method of manufacturing safety rods, comprising a yoke at one end, which

permet au contraire d'obtenir des bielles démontables et régla-  instead allows to obtain removable and adjustable rods

bles.wheat.

Le procédé selon l'invention, dans lequel on utilise deux tu-  The method according to the invention, in which two tu-

bes enfilés l'un dans l'autre, est caractérisé en ce qu'on immo-  bes strung one inside the other, is characterized in that one immo-

bilise les deux tubes par un mandrin ou tirant fileté et en ce  bilise the two tubes by a mandrel or threaded tie and in this

qu'on forme ensuite la chape simultanément sur les deux tubes ain-  then form the yoke simultaneously on the two tubes thus

si immobilisés -if immobilized -

Dans ces conditions, après formation de la bielle, on peut  Under these conditions, after forming the connecting rod, one can

visser ou dévisser le tirant, donc régler la longueur de la biel-  screw or unscrew the tie rod, so adjust the length of the connecting rod

le Si on démonte la bielle, les taraudages des deux tubes restent en concordance, de sorte qu'on peut remettre en place le tirant  If you disassemble the connecting rod, the threads of the two tubes remain in concordance, so that you can replace the tie rod

sans difficulté.without difficulty.

Dans un mode de réalisation avantageux de l'invention, on ré-  In an advantageous embodiment of the invention,

treint l'une des extrémités du tube intérieur sur un mandrin file-  one end of the inner tube on a file mandrel

té, on emmanche le tube intérieur dans un tube extérieur de lon-  tee, the inner tube is plugged into a long outer tube

gueur plus grande de façon que ce tube extérieur fasse saillie pax rapport à l'extrémité taraudée du tube intérieur, on rétreint la  geur larger so that this outer tube protrudes pax relative to the threaded end of the inner tube, we shrink the

partie en saillie du tube extérieur sur un mandrin fileté identi-  projecting part of the outer tube on a threaded mandrel identi-

que au premier, on fait pivoter les deux tubes de façon à mettre en concordance le filetage des deux extrémités des deux tubes et  that at the first, the two tubes are pivoted so as to bring the threads of the two ends of the two tubes into agreement and

on visse un tirant de réglage dans ces extrémités.  we screw an adjustment tie in these ends.

-2 - L'invention a également pour objet les bielles de sécurité  -2 - The invention also relates to safety connecting rods

obtenues par ce procédé.obtained by this process.

On a décrit ci-après, à titre d'exemple non limitatif, un  We have described below, by way of nonlimiting example, a

mode de mise en oeuvre du procédé selon l'invention, avec référen-  mode of implementing the method according to the invention, with reference

ce au dessin annexé dans lequel:this in the appended drawing in which:

Les Figures la à lc sont des vues en coupe longitudinale mon-  Figures 1a to 1c are views in longitudinal section shown

trant le formage du tube intérieur; Les Figures 2 a et 2 b sont des vues en coupe longitudinale montrant le formage du tube extérieur;  trant the forming of the inner tube; Figures 2 a and 2 b are views in longitudinal section showing the forming of the outer tube;

La Figure 3 montre en coupe longitudinale les deux tubes en-  Figure 3 shows in longitudinal section the two tubes in

filés l'un dans l'autre; La Figure 4 montre la formation du rétreint de l'extrémité en saillie du tube extérieur; La Figure 5 montre les deux tubes assemblés; La Figure 6 montre en coupe longitudinale la bielle terminée;  spun into each other; Figure 4 shows the formation of the constriction of the projecting end of the outer tube; Figure 5 shows the two tubes assembled; Figure 6 shows in longitudinal section the completed connecting rod;

La Figure 7 est une vue en bout de la bielle.  Figure 7 is an end view of the connecting rod.

La bielle fabriquée selon l'invention comporte un corps inté-  The connecting rod manufactured according to the invention comprises an integrated body

rieur 1 et un corps extérieur 2.laughing 1 and an external body 2.

Le corps intérieur 1 est formé par un tube 3 (Figure la) dont on rétreint d'abord l'une des extrémités 3 a sur un mandrin fileté (Figure lb) On rétreint-ensuite la partie centrale 3 b du tube de  The inner body 1 is formed by a tube 3 (Figure la), one of the ends of which is first shrunk 3 a on a threaded mandrel (Figure lb). The central part 3 b of the tube is then shrunk.

manière à lui donner le diamètre extérieur de l'extrémité 3 a (Fi-  so as to give it the outside diameter of the end 3 a (Fi-

gure lc).gure lc).

Le corps extérieur 2 est formé à partir d'un tube cylindri-  The outer body 2 is formed from a cylindrical tube.

que 4 (Figure 2 a) dont le diamètre intérieur est égal au diamètre extérieur du tube 3 et qui est plus long que ce tube 3 On rétreint l'une des extrémités et la partie centrale du tube 4 de façon à  than 4 (Figure 2 a) whose inside diameter is equal to the outside diameter of the tube 3 and which is longer than this tube 3 One of the ends and the central part of the tube 4 is constricted so as to

donner à la partie rétreinte 4 a un diamètre intérieur égal au dia-  give the constricted part 4 has an internal diameter equal to the diameter

mètre extérieur de la partie rétreinte 3 a-3 b du corps intérieur 1.  outer meter of the constricted part 3 a-3 b of the inner body 1.

On emmanche le corps intérieur 1 dans le corps extérieur 2  The inner body 1 is inserted into the outer body 2

qui fait alors saillie par rapport au corps 1 (Figure 3).  which then protrudes from the body 1 (Figure 3).

On rétreint ensuite la partie en saillie du corps 2 sur un mandrin fileté 5 dont le diamètre èt le pas correspondent à ceux du  The projecting part of the body 2 is then constricted on a threaded mandrel 5 whose diameter and pitch correspond to those of the

taraudage formé dans l'extrémité 3 a du corps 1 (Figure 4).  thread formed in the end 3a of the body 1 (Figure 4).

Puis on fait pivoter le corps 1 par rapport au corps 2 de fa-  Then the body 1 is pivoted relative to the body 2 so that

çon à mettre en concordance le filetage de l'extrémité 3 a et celui du mandrin 5, et on remplace le mandrin 5 par un tirant de réglage  lesson in matching the thread of the end 3 a and that of the mandrel 5, and the mandrel 5 is replaced by an adjustment rod

6 qu'on visse dans cette extrémité 3 a (Figure 5).  6 that is screwed into this end 3 a (Figure 5).

Enfin on rétreint simultanément les deux corps de bielle 1 et 2 maintenus solidaires par le tirant 6, à leur extrémité opposée -3- à ce tirant (Figures 6 et 7), de façon à former la chape Les perçages 7 sont effectués alors que les deux corps 1 et 2 sont  Finally, the two rod bodies 1 and 2 are simultaneously constricted, held together by the tie rod 6, at their opposite end -3- to this tie rod (Figures 6 and 7), so as to form the yoke The holes 7 are made while the two bodies 1 and 2 are

assemblés l'un à l'autre.assembled together.

Les diverses opérations de rétreint peuvent être faites par exemple par martelage ou à la presse. Il va de soi que la présente invention ne doit pas être con  The various shrinking operations can be done for example by hammering or with the press. It goes without saying that the present invention should not be con

sidérée comme limitée au mode de réalisation décrit et représen-  considered to be limited to the embodiment described and represented

té, mais en couvre, au contraire, toutes les variantes.  té, but covers, on the contrary, all the variants.

4 -4 -

Claims (3)

REVENDICATIONS 1 Procédé de fabrication de bielles de sécurité comportant une chape à l'une de leurs extrémités, dans lequel on utilise deux  1 Method for manufacturing safety connecting rods comprising a yoke at one of their ends, in which two tubes enfilés l'un dans l'autre, caractérisé en ce qu'on immobili-  tubes threaded one inside the other, characterized in that one immobilizes se les deux tubes par un mandrin ou tirant fileté 6 et en ce qu'on forme ensuite la chape simultanément sur les deux tubes ainsi im- mobilisés.  se the two tubes by a mandrel or threaded tie rod 6 and in that the yoke is then formed simultaneously on the two tubes thus immobilized. 2 Procédé selon la revendication 1, caractérisé en ce qu'on rétreint l'une des extrémités du tube intérieur 1 sur un mandrin fileté, qu'on emmanche le tube intérieur 1 dans un tube extérieur 2 de longueur plus grande de façon que ce tube extérieur fasse saillie par rapport à l'extrémité taraudée du tube intérieur, qu'on2 Method according to claim 1, characterized in that one of the ends of the inner tube 1 is constricted on a threaded mandrel, that the inner tube 1 is fitted into an outer tube 2 of greater length so that this tube outside protrude from the threaded end of the inner tube, which rétreint la partie en saillie du tube extérieur sur un mandrin fi-  shrinks the protruding part of the outer tube on a solid mandrel leté 5 identique au premier, qu'on fait pivoter les deux tubes 1  smoothness 5 identical to the first, that we rotate the two tubes 1 et 2 de façon à mettre en concordance le filetage des deux extré-  and 2 so as to match the threads of the two ends mités des deux tubes et qu'on visse un tirant de réglage 6 dans.  mites of the two tubes and that a tie rod 6 in. ces extrémités.these ends. 3 Bielle obtenue par le procédé défini à la revendication 1 ou 2.  3 connecting rod obtained by the process defined in claim 1 or 2.
FR8307658A 1983-05-03 1983-05-03 METHOD FOR MANUFACTURING DISMANTLABLE AND ADJUSTABLE SECURITY CONNECTING RODS AND CONNECTING RODS OBTAINED BY THIS PROCESS Expired FR2545556B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8307658A FR2545556B1 (en) 1983-05-03 1983-05-03 METHOD FOR MANUFACTURING DISMANTLABLE AND ADJUSTABLE SECURITY CONNECTING RODS AND CONNECTING RODS OBTAINED BY THIS PROCESS

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8307658A FR2545556B1 (en) 1983-05-03 1983-05-03 METHOD FOR MANUFACTURING DISMANTLABLE AND ADJUSTABLE SECURITY CONNECTING RODS AND CONNECTING RODS OBTAINED BY THIS PROCESS

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FR2545556A1 true FR2545556A1 (en) 1984-11-09
FR2545556B1 FR2545556B1 (en) 1985-08-09

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2599793A1 (en) * 1986-06-09 1987-12-11 Aerospatiale Connecting rod system intended to resist a longitudinal forces threshold
FR2883939A1 (en) * 2005-03-29 2006-10-06 Airbus France Sas ROD AND METHOD FOR MANUFACTURING SUCH ROD
EP2607229A3 (en) * 2011-12-22 2014-03-26 Airbus Operations, S.L. Composite rod, manufacturing method and tool

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1189383A (en) * 1957-12-31 1959-10-02 Sud Aviation Improvements made to connecting rods and their manufacturing process
FR2077485A1 (en) * 1970-01-22 1971-10-29 Creuzet Robert

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1189383A (en) * 1957-12-31 1959-10-02 Sud Aviation Improvements made to connecting rods and their manufacturing process
FR2077485A1 (en) * 1970-01-22 1971-10-29 Creuzet Robert

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2599793A1 (en) * 1986-06-09 1987-12-11 Aerospatiale Connecting rod system intended to resist a longitudinal forces threshold
FR2883939A1 (en) * 2005-03-29 2006-10-06 Airbus France Sas ROD AND METHOD FOR MANUFACTURING SUCH ROD
EP2607229A3 (en) * 2011-12-22 2014-03-26 Airbus Operations, S.L. Composite rod, manufacturing method and tool
US9091387B2 (en) 2011-12-22 2015-07-28 Airbus Operations, S.L. Composite rod, manufacturing method and tool

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Publication number Publication date
FR2545556B1 (en) 1985-08-09

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