WO2013017767A1 - Bielle mécanique tubulaire - Google Patents
Bielle mécanique tubulaire Download PDFInfo
- Publication number
- WO2013017767A1 WO2013017767A1 PCT/FR2012/051670 FR2012051670W WO2013017767A1 WO 2013017767 A1 WO2013017767 A1 WO 2013017767A1 FR 2012051670 W FR2012051670 W FR 2012051670W WO 2013017767 A1 WO2013017767 A1 WO 2013017767A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- connecting rod
- hollow body
- tubular
- tubular connecting
- opening
- Prior art date
Links
- 238000005520 cutting process Methods 0.000 claims description 2
- 230000000903 blocking effect Effects 0.000 description 8
- 238000003466 welding Methods 0.000 description 7
- 239000000725 suspension Substances 0.000 description 6
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 239000011324 bead Substances 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910001092 metal group alloy Inorganic materials 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 238000009987 spinning Methods 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 239000007844 bleaching agent Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C7/00—Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
- F16C7/02—Constructions of connecting-rods with constant length
-
- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B7/00—Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections
- F16B7/18—Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections using screw-thread elements
- F16B7/182—Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections using screw-thread elements for coaxial connections of two rods or tubes
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/21—Elements
- Y10T74/2142—Pitmans and connecting rods
Definitions
- the present invention relates to a tubular mechanical link.
- Tubular mechanical rods are used, that is to say hollow bodies, especially in areas where the search for mass gain is a constant concern.
- the tubular mechanical rods are for example used on the landing gear (brake bar), in the maintenance systems in the open position of the maintenance covers (bonnet , ...), in engine suspension systems (interface transmitting the thrust between the engine and the mast of the wing), etc.
- a tubular mechanical connecting rod is conventionally composed of a hollow body, having at each of its ends a rod head.
- Each end of the rod is typically shaped as a male or female clevis, so as to allow the fixing of the connecting rod by pin or other means to the bodies with which it must cooperate.
- tubular mechanical connecting rod by means of welding operation (s) proves delicate and generally requires, because of the disadvantages inherent to the weld detailed above, additional machining steps to obtain a connecting rod. geometry and mass in accordance with the specifications in force in the field of aeronautics.
- a connecting rod must be able to take considerable thrust forces generated by the turbojet, while having the lowest mass possible. Therefore, it is important on the one hand that the metal alloy forming the rod is adapted as much as possible to the operating conditions, so as to have the most interesting specific properties possible (mechanical properties divided by the density), and on the other hand that the connecting rod is tubular.
- the object of the present invention is to provide a tubular mechanical connecting rod which has been manufactured by eliminating welding operations and which consequently is free of any defects inherent to the welding.
- tubular connecting rod comprises: a hollow body comprising at least one end provided with an opening,
- a small-bore head arranged to be fitted through the opening, said connecting rod head having at least one blocking means arranged to position the connecting rod head relative to the opening of the hollow body in a determined locking position,
- tubular connecting rod being characterized in that the end of the hollow body is provided with at least one slot.
- the term "grip" means that the connecting rod head is secured to the end of the hollow body by a secure fit.
- the locked fit is obtained because of the complementarity of the shapes that present the end of the connecting rod and the end of the hollow body and which allows the engagement of the big end in the end of the hollow body in a determined locking position .
- the end of the hollow body is provided with a plurality of uniformly distributed slots which open on the opening of the hollow body. This gives elasticity to the hollow body and thus facilitates the catching of the dimensional tolerances between the first part or the second part of the big end and the hollow body.
- the end of the non-opening side slot is provided with a radius to limit the stress concentrations, this radius may even be greater than half the width of the slot.
- the connecting rod head is monobloc.
- the connecting rod head is formed:
- a first part which comprises at least a first blocking means arranged to position said first part relative to the opening of the hollow body in a first determined locking position
- a second portion which comprises at least a second blocking means arranged to position said second portion relative to the hollow body in a second determined locking position.
- the first part and the second part of the big end can have been obtained by cutting a whole big end. If the end of the connecting rod is formed of two distinct parts as described above, this has the advantage of not being confronted with strict dimensional tolerance requirements which must be met when a substantially cylindrical piece of a hollow cylinder.
- the connecting rod head is monobloc, the dimensional tolerances compensation will be performed only with the slots of the hollow body.
- the locking means is a shoulder.
- the connecting rod head comprises at least a second fixing means intended to cooperate with the first fastening means so as to fix the end of the hollow body on the connecting rod head.
- the second fixing means is a bore.
- the tubular connecting rod comprises:
- said two crank heads having at least one blocking means arranged to position the crankshaft relative to the opening of the hollow body in a determined locking position.
- FIG. 1 represents a perspective view of a support structure of a turbojet engine with an aircraft mast incorporating two tubular connecting rods according to the invention
- FIG. 2 is a perspective view of a portion of one of the two tubular rods shown in FIG. 1;
- FIG. 3 is a front view of a portion of one of the two tubular rods shown in FIG. 1;
- FIG. 4 is a sectional view along the plane IV of Figure 2 of the tubular connecting rod portion of Figure 2.
- the suspension device shown in FIG. 1 comprises two tubular connecting rods 1, 23 whose first ends 3 each comprise a female yoke intended to cooperate with a front part of the turbojet engine, and whose second ends 26 each comprise a male yoke (no visible in Figure 1) which cooperate with a suspension beam 17.
- the suspension beam 17 is intended to cooperate with a suspension mast the turbojet engine (not shown), and with the ferrule of the intermediate casing, via appropriate connecting rods 24, 25.
- the shoulder 19 constitutes a first means of blocking the first part 5 of the connecting rod 21 relative to the opening 4 of the hollow body 2.
- the shoulder 20 constitutes a second means of blocking the second portion 6 of the connecting rod 21 relative to the opening 4 of the hollow body 2.
- the end 3 is provided with a plurality of counterbores 12 into which unrepresented fastening screws may be introduced.
- the first portion 5 and the second portion 6 of the connecting rod 21 are provided with a plurality of bores 22 arranged so that when said first and second portions 5 , 6 are positioned respectively in their first determined blocking position and second determined blocking position, the bores 22 are in the extension of countersinks 12 and fixing screws may be introduced.
- the bores of the hollow body 2 and the first parts 5 and / or second parts 6 of the head of the rod 21 may be made in a single operation, once the first parts 5 and / or second parts 6 of the head of the connecting rod 21 positioned relative to the hollow body 2.
- the end 3 of the hollow body 2 is provided with a plurality of slots 18 which open on the opening 4 which give it a certain elasticity and thus facilitate the fitting of the connecting rod head 21 in the hollow body 2.
- the connecting rod head 21 comprises an axis 13, a nut 9 and rings 10 and 11.
- This crank head 21 may also comprise a not shown ball joint.
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BR112014000544A BR112014000544A2 (pt) | 2011-08-01 | 2012-07-13 | haste de conexão tubular |
EP12743516.2A EP2739866A1 (fr) | 2011-08-01 | 2012-07-13 | Bielle mécanique tubulaire |
CA2842574A CA2842574A1 (fr) | 2011-08-01 | 2012-07-13 | Bielle mecanique tubulaire |
RU2014106786/11A RU2014106786A (ru) | 2011-08-01 | 2012-07-13 | Трубчатая механическая соединительная штанга |
CN201280038206.2A CN103717921A (zh) | 2011-08-01 | 2012-07-13 | 管状机械连接杆 |
US14/171,024 US20140174251A1 (en) | 2011-08-01 | 2014-02-03 | Tubular mechanical connecting rod |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1157035A FR2978689B1 (fr) | 2011-08-01 | 2011-08-01 | Bielle mecanique tubulaire |
FR11/57035 | 2011-08-01 |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US14/171,024 Continuation US20140174251A1 (en) | 2011-08-01 | 2014-02-03 | Tubular mechanical connecting rod |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2013017767A1 true WO2013017767A1 (fr) | 2013-02-07 |
Family
ID=46614548
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR2012/051670 WO2013017767A1 (fr) | 2011-08-01 | 2012-07-13 | Bielle mécanique tubulaire |
Country Status (8)
Country | Link |
---|---|
US (1) | US20140174251A1 (fr) |
EP (1) | EP2739866A1 (fr) |
CN (1) | CN103717921A (fr) |
BR (1) | BR112014000544A2 (fr) |
CA (1) | CA2842574A1 (fr) |
FR (1) | FR2978689B1 (fr) |
RU (1) | RU2014106786A (fr) |
WO (1) | WO2013017767A1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6606110B2 (ja) * | 2017-01-13 | 2019-11-13 | フタバ産業株式会社 | パイプの接合方法 |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB948567A (en) * | 1961-10-13 | 1964-02-05 | Servomecanismos S A | Improvements in or relating to adjustable rigid coupling arrangements for connecting two parts of a mechanism in end to end relationship |
GB1233628A (fr) * | 1968-03-26 | 1971-05-26 | ||
EP0839593A1 (fr) | 1996-10-29 | 1998-05-06 | AEROSPATIALE Société Nationale Industrielle | Procédé de fabrication d'une pièce creuse de révolution, par fluotournage, et pièce obtenue par ce procédé |
US6145548A (en) * | 1998-03-19 | 2000-11-14 | Staubli Faverges | Connector for loom connecting rod and drawing mechanism |
US20010050469A1 (en) * | 2000-06-09 | 2001-12-13 | Trw Fahrwerksysteme Gmbh & Co. Kg | Joint rod for a motor vehicle |
US20020071719A1 (en) * | 2000-12-09 | 2002-06-13 | Moore Daniel Lee | Swivel insert for a control rod |
US20030086756A1 (en) * | 2001-11-07 | 2003-05-08 | Trotter Jason K | Modular linkage system |
US20050002592A1 (en) * | 2002-11-29 | 2005-01-06 | James Rogers | Rod end device for a motor vehicle |
EP1870196A1 (fr) | 2006-06-20 | 2007-12-26 | Protac | Procédé de fabrication d' un arbre de bielle mécanique |
FR2940378A1 (fr) * | 2008-12-24 | 2010-06-25 | Messier Dowty Sa | Procede de fabrication d'une bielle en metal, renforcee par des fibres longues. |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2766079A (en) * | 1952-05-09 | 1956-10-09 | William H Browne | Rod end bearing |
US3646512A (en) * | 1970-09-01 | 1972-02-29 | George J Borgstede | Vehicle trailer bed overload indicating system |
FR2396201A1 (fr) * | 1977-06-28 | 1979-01-26 | Aerospatiale | Accouplement entre un embout et une barre, notamment pour une bielle de longueur ajustable |
DE3738432A1 (de) * | 1987-11-12 | 1989-06-01 | Trw Ehrenreich Gmbh | Verbindung eines kugelgelenkschaftes mit einem rohr |
DE102010043778A1 (de) * | 2010-11-11 | 2012-05-16 | Zf Friedrichshafen Ag | Lenkerelement mit Überlastsicherung |
-
2011
- 2011-08-01 FR FR1157035A patent/FR2978689B1/fr active Active
-
2012
- 2012-07-13 WO PCT/FR2012/051670 patent/WO2013017767A1/fr active Application Filing
- 2012-07-13 RU RU2014106786/11A patent/RU2014106786A/ru not_active Application Discontinuation
- 2012-07-13 CA CA2842574A patent/CA2842574A1/fr not_active Abandoned
- 2012-07-13 CN CN201280038206.2A patent/CN103717921A/zh active Pending
- 2012-07-13 EP EP12743516.2A patent/EP2739866A1/fr not_active Withdrawn
- 2012-07-13 BR BR112014000544A patent/BR112014000544A2/pt not_active IP Right Cessation
-
2014
- 2014-02-03 US US14/171,024 patent/US20140174251A1/en not_active Abandoned
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB948567A (en) * | 1961-10-13 | 1964-02-05 | Servomecanismos S A | Improvements in or relating to adjustable rigid coupling arrangements for connecting two parts of a mechanism in end to end relationship |
GB1233628A (fr) * | 1968-03-26 | 1971-05-26 | ||
EP0839593A1 (fr) | 1996-10-29 | 1998-05-06 | AEROSPATIALE Société Nationale Industrielle | Procédé de fabrication d'une pièce creuse de révolution, par fluotournage, et pièce obtenue par ce procédé |
US6145548A (en) * | 1998-03-19 | 2000-11-14 | Staubli Faverges | Connector for loom connecting rod and drawing mechanism |
US20010050469A1 (en) * | 2000-06-09 | 2001-12-13 | Trw Fahrwerksysteme Gmbh & Co. Kg | Joint rod for a motor vehicle |
US20020071719A1 (en) * | 2000-12-09 | 2002-06-13 | Moore Daniel Lee | Swivel insert for a control rod |
US20030086756A1 (en) * | 2001-11-07 | 2003-05-08 | Trotter Jason K | Modular linkage system |
US20050002592A1 (en) * | 2002-11-29 | 2005-01-06 | James Rogers | Rod end device for a motor vehicle |
EP1870196A1 (fr) | 2006-06-20 | 2007-12-26 | Protac | Procédé de fabrication d' un arbre de bielle mécanique |
FR2940378A1 (fr) * | 2008-12-24 | 2010-06-25 | Messier Dowty Sa | Procede de fabrication d'une bielle en metal, renforcee par des fibres longues. |
Also Published As
Publication number | Publication date |
---|---|
BR112014000544A2 (pt) | 2017-02-14 |
FR2978689A1 (fr) | 2013-02-08 |
US20140174251A1 (en) | 2014-06-26 |
FR2978689B1 (fr) | 2014-05-02 |
RU2014106786A (ru) | 2015-09-10 |
CA2842574A1 (fr) | 2013-02-07 |
EP2739866A1 (fr) | 2014-06-11 |
CN103717921A (zh) | 2014-04-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR3059631B1 (fr) | Dispositif de liaison entre un longeron en aluminium de vehicule et un bras de suspension | |
FR2647166A1 (fr) | Organe de rivetage aveugle, procede d'assemblage et assemblages obtenus | |
FR3065441A1 (fr) | Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage fixee a un caisson de voilure a l'aide d'une liaison boulonnee | |
FR2964364A1 (fr) | Mat d'accrochage de turboreacteur pour aeronef comprenant des attaches voilure avant alignees | |
EP2140151A2 (fr) | Rivet aveugle hautes performances notamment pour fixation de structure | |
EP2643600B1 (fr) | Procédé de fabrication d'une bielle mécanique tubulaire, et bielle obtenue par un tel procédé | |
FR2935953A1 (fr) | Partie arriere d'aeronef comprenant deux semi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef. | |
EP2334556B1 (fr) | Partie arriere d'aeronef comprenant une structure de support de moteurs traversant le fuselage et reliee a celui-ci par au moins une bielle | |
WO2006103372A1 (fr) | Bielle structurale creuse et procede de fabrication d'une telle bielle | |
FR2946712A1 (fr) | Bielle pour la construction aeronautique et procede de fabrication d'une telle bielle | |
WO2013017767A1 (fr) | Bielle mécanique tubulaire | |
EP3699092B1 (fr) | Ensemble de pièces assemblées par un arbre traversant pouvant être monté en cas d'alignement approximatif entre les pièces | |
FR3061149A1 (fr) | Structure primaire d'un mat pour groupe propulseur d'aeronef comportant une partie pyramidale a montants convergents | |
FR2956706A1 (fr) | Bague d'assemblage de pieces, de preference pour attache de mat d'accrochage de turbomachine d'aeronef | |
EP3396196B1 (fr) | Mécanisme de filtrage des vibrations destiné à être agencé entre un équipement et un fuselage d'aeronef, siège equipé d'un tel mécanisme | |
EP2006555A1 (fr) | Arbre de transmission de mouvements et/ou d'efforts en rotation | |
CA2011512C (fr) | Aiguille destinee a l'execution d'operations avec des fils, meches ou cordons souples et dispositif pour l'utilisation d'une telle aiguille | |
WO2017085379A1 (fr) | Systeme d'assemblage de deux pieces avec organe de guidage et element de verrouillage integres | |
FR2857888A1 (fr) | Procede de fabrication d'un element de couplage, en particulier d'une fourche pour joints de cardan, et element de couplage ainsi obtenu | |
EP3056393A1 (fr) | Dispositif structurel d'armature de banquette de véhicule à entretoise d'ancrage d'éléments de ceintures de sécurité | |
EP2009204B1 (fr) | Ensemble pour grille barreaudée et outil d'assemblage correspondant. | |
FR3094963A1 (fr) | Outillage de maintien des panneaux latéraux d’une structure primaire d’un mât d’aéronef lors de son assemblage et procédé d’assemblage d’une structure primaire d’un mât d’aéronef utilisant ledit outillage de maintien | |
FR3026151A1 (fr) | Dispositif d'assemblage a ecrou-barillet, ensemble structurel d'aeronef comprenant un tel dispositif, et procede d'assemblage correspondant | |
FR2918097A1 (fr) | Ensemble pour grille barreaudee et outil d'assemblage correspondant. | |
FR3105165A1 (fr) | Élément de cadre pour fuselage d’aéronef pourvu d’ouvertures adaptées à un montage par enfilage de raidisseur. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 12743516 Country of ref document: EP Kind code of ref document: A1 |
|
ENP | Entry into the national phase |
Ref document number: 2842574 Country of ref document: CA |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
REEP | Request for entry into the european phase |
Ref document number: 2012743516 Country of ref document: EP |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2012743516 Country of ref document: EP |
|
ENP | Entry into the national phase |
Ref document number: 2014106786 Country of ref document: RU Kind code of ref document: A |
|
REG | Reference to national code |
Ref country code: BR Ref legal event code: B01A Ref document number: 112014000544 Country of ref document: BR |
|
ENP | Entry into the national phase |
Ref document number: 112014000544 Country of ref document: BR Kind code of ref document: A2 Effective date: 20140109 |