• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The invention relates to a method of manufacturing hollow hollow tubular beam body stiffened in flexion, torsion and compression / buckling, as well as its ends, monobloc and multi materials obtained by metallurgical gradient and variation of the percentages of components of alloys during manufacture . It makes it possible to obtain the two ends and the body of the beam in the same operation and in a single piece, without any other contribution of material than the metal or the alloy or the composite material which composes the structure. In addition, the internal and external reinforcements of the hollow body of the beam are obtained in the same way, with variations in the dosage of the metal compounds or composites used during manufacture, so that the finished product is monoblock 3D and multi materials . Thus, compared to the usual technique of forming straight hollow beam bodies by spinning, sinking, recess or friction welding, the overall mechanical strength, rigidity and mass characteristics are greatly improved. Brought locally, the variations in the percentages of the components of the metals, alloys or composites used, increase the tenacity, the resistance. The proposed manufacturing process is specifically designed for connecting rod bodies and power shafts used in satellite systems and subsystems, aircraft structural parts, landing gear and engine holding systems. on aircraft structures, the main and secondary axes of turbojets. The proposed manufacturing method is also particularly intended for prostheses of skeletal bone of the human skeleton and prostheses of longiline bones of the equine skeleton, adapting the ends to geometrical shapes imposed by the joints of the skeletons. The proposed manufacturing method also makes it possible to obtain, in a nonlimiting manner, any curved profiles other than rectilinear, thus being able to be 3D monoblock.
    公开号:FR3035605A1
    申请号:FR1500902
    申请日:2015-04-28
    公开日:2016-11-04
    发明作者:Alain Toufine
    申请人:Alain Toufine；
    IPC主号:
    专利说明:

    [0001] The present invention relates to a process for obtaining a hollow tubular beam stiffened in flexion, torsion and compression / buckling such as the rod bodies, the junction beams, the force transmission shafts as well as the Beam core and beam ends obtained.
    [0002] The use of connecting rods in assemblies of complex kinematic functions is adapted when the forces to be transmitted are of a perfectly well-known nature, such as tensile / compressive forces, so that they are of particular interest to the aerospace industry for manufacturing systems. deployment and maintenance of aircraft landing gear, inspection hatches, flaps, aircraft engine suspension systems, as well as interfaces between subsystems and systems on satellites or launchers . Connecting rods or junction beams are mechanical members consisting of a rectilinear body (1) on which endpieces (2) are generally attached by aiming or welded or glued or riveted connection, these ends being mechanically connected. by a pivot or a patella to the members with whom they must cooperate (Figure 1). Most connecting rods and junction beams used in aeronautics and space have a tubular core of hollow cylindrical profile to gain mass with very good mechanical properties as for the landing gear, the suspension elements of the 20 engines. planes or launcher engines supports. These hollow cylindrical profiles are obtained by manufacturing methods such as spinning, sinking or recess, not allowing to place within these same profiles local reinforcements according to the need for mechanical strength, thus leading to it is possible to increase the thickness of the profile and / or concomitantly its outer radius. Techniques such as welding or rotary or linear friction welding make it possible to add local reinforcements on the outer face of the hollow cylindrical profiles in order to obtain very good mechanical strength on the link. However, the reported geometrical shapes remain simple such as in the form of "L", "T", "I", "S2" and require complex positioning tools having to conform to a cylindrical or elliptical shape when the 'machining. Some of these manufacturing methods also do not allow to obtain profiles section evolution along the axis of revolution of the connecting rod body, the connecting beam or the transmission shaft. 3035605 - 2 - For some applications, composite carbon materials are used to reduce weight and increase strength by placing carbon fibers in the directions of mechanical stress. Thus, it has been found that when mechanical loads of bending, compression and torsion combine simultaneously, the connecting rod cores, the transmission shafts are poorly adapted because by design the engineer has endeavored to separate the loadings . It has been found that this separation of loading also leads to junction architectures at the ends of the connecting rod body or of the transmission shaft, requiring several constituents each acting with respect to a given bias and therefore being able to be improved in the presence of complex loads. It has been found that when the rod body or the transmission shaft placed in a reduced environment or immersed in the flow of any fluid, the only solution to increase to iso radius and iso material the mechanical characteristics of the straight sections. , is to add uniformly distributed material inside the hollow profile, thereby increasing their mass. It has furthermore been found that the addition of internal material to the hollow profile of the main body or of the transmission shaft is not possible by the currently used machining methods. It has been found that when heat flows must pass through the ends 20 of connecting rod bodies or junction beams or transmission shafts, the bonded, riveted and screwed connection modes are not very efficient with respect to the very good thermal conductivity sought at these places. It has also been found that, in the case of carbon composite solutions, the supply, the use of these materials and their industrialization remain expensive whereas their uses are limited because they do not withstand the corrosive environments of gaseous fluids or little. and liquids, nor at high operating temperatures above 180 ° C. The present invention is based on an initial engineering phase in numerical topological optimization of structures and functional analysis, followed by the use of additive manufacturing techniques by laser sintering or electron beam of metal powders. It is an object of the present invention to provide a method of designing, manufacturing and obtaining simultaneously without any other use than the appropriate metal and / or alloy selected from the connecting rod body, the connecting beam or of the transmission shaft, of any section and variable along the axis of revolution according to the needs for recovery of mechanical forces, - internal or external reinforcing devices placed locally or on the whole of said body 5 or said shaft according to the need for recovery of mechanical forces, strong rigidities and small masses, - the envelope of revolution peripheral to said body or said shaft, of any thickness and variable along the axis of revolution according to the needs of resumption of mechanical forces, 10 - and ends of said body or said shaft according to the flow of effort to be passed through these junctions. The method of manufacturing the connecting rod body, the connecting beam or the transmission shaft, is essentially characterized in that it consists in carrying out the following steps: - manufacture in selected dimensions and in metallic material one of the two ends, called the low end, which ensures the mechanical connection with the environment, raise the internal revolution form of the connecting rod, connecting beam or transmission shaft in dimensions chosen in the same way. materials and alloys that the lower end or in metallurgical dosages or variable components by providing metal material, - simultaneously raise in the construction of the form of revolution, the local reinforcements internal and / or external to said rod body or said tree in geometric dimensions and shapes chosen from the same materials and alloys or in metallurgical dosages or variable components per app ort of metallic material, - add to said said rod body or said shaft the second end called high end in dimensions chosen from the same materials and alloys as the lower end or in metallurgical dosages or variable components by contribution of metallic material . According to an additional characteristic of the method according to the invention, in order to better withstand the compressive and buckling stresses without seriously penalizing the mass, the section may take the form of a tube (3, 3bis) of variable thickness depending on the axis of revolution, inside which are reported in any number of ribs (4) or undulations (6) (Figures 2, 3) or isogrids single wall (9) or isogrids double walls (11) (Figure 4 ). These ribs, corrugations, single wall or double wall isogrids can have variable thicknesses, heights, radii and network densities, adapted as required, and can also be placed on the outer part of the connecting rod body. . According to another additional feature of the method according to the invention, in the presence of torsional stresses applied to the hollow sections, the section may have the shape of a tube of variable thickness along the axis of revolution and inside which are arranged a variable number of interleaved elliptical ribs called helices (12, 13) of variable thickness, pitch and inclination with respect to the longitudinal axis (FIGS. 5, 6), opposing torsion-related deformations by reducing the shear angle of the cross section. According to another additional feature of the method according to the invention, an outer circumferential section 10 free of shape accident (10) (FIG. 4), able to facilitate the flow of a fluid in the gaseous or liquid state and capable of be of varying thickness or profile along the axis of revolution, can be added to the connecting rod body or to the transmission shaft. According to another additional feature of the method according to the invention, an internal section 15 free of shape accident (5, 7) (FIGS. 2, 3), able to facilitate the flow of a fluid in the gaseous state or liquid and can be of varying thickness or profile along the axis of revolution, can be added to the rod body or to the transmission shaft. According to another additional characteristic of the process according to the invention, the mechanical and thermomechanical properties can be adjusted in zones by means of metallurgical gradients obtained by varying during the manufacturing process the metallurgical percentages of the metal or the alloy or the composite used, thus making the connecting rod body or the multi-material 3D transmission shaft. According to another additional characteristic of the method according to the invention, the assemblies of the ends (2) (FIG. 1) on the connecting rod body or the transmission shaft are carried out without using targeted, welded, glued or riveted connections, only once and during the same construction operation of said rod body or said transmission shaft. The advantages and characteristics of the method according to the invention will become more clearly apparent from the description which follows and which refers to the appended drawing, which represents a non-limiting embodiment thereof.
    [0003] In the accompanying drawing: - Figure (1) shows a conventional rod body geometry (1) with one of its ends reported (2) by bonded connection or welded or glued or riveted, which provide the aid a pivot or a ball joint the mechanical connection with the environment. - Figure (2) shows a sectional view of a rod body or a hollow transmission shaft (3) of any thickness within which are arranged in any number 3035605 5 - 10 - 15 - 20 - 25 - 5 - any rectilinear ribs along the axis of revolution (4), of any thickness and height. The inner profile (5) to the connecting rod body or to the transmission shaft (3) joins the tops of the ribs (4) making the system one piece. FIG. (3) is a cross-sectional view of a connecting rod body or a hollow transmission shaft (3a) of any thickness inside which are arranged in any number of rectilinear corrugations along the axis of revolution (6). of any thickness, radius and height. The inner profile (7) to the connecting rod body or the transmission shaft (3bis) joins the vertices of the corrugations (5) making the system monobloc. FIG. (4) shows a hollow cylindrical revolution profile of a connecting rod or transmission shaft body (8, 8a) on which is placed in the outer part a simple wall isogrid network (9) of height, thickness and variable density as needed. This network may be arranged similarly or not inside the profile (8). Finally, for mechanical or functional reasons when immersed in a gaseous or liquid fluid, a peripheral shell (10) of varying thickness and profile along the axis of revolution is added and joins the vertices of the isogrids (11), then forming double-walled isogrids and making the system one-piece. FIG. (5) shows a side view of the connecting rod body or of the transmission shaft in which are arranged interleaved elliptical ribs called helices (12) as wound along the axis of revolution, and of thickness, of pitch and of any height. Figure (6) shows in 3D view the disposition and the winding around the axis of revolution of the elliptical ribs called propellers (13) inside the hollow profile of the connecting rod body or the transmission shaft.
    权利要求:
    Claims (6)
    [0001]
    CLAIMS 1 °) A method for manufacturing a stiffened hollow rod body, lightened, characterized in that it consists in carrying out the following steps: - manufacture in selected dimensions and shapes and in metallic material the first of the two ends (2) which ensures the mechanical connection of the connecting rod body (1) with its environment, - raising on the first end the form of internal revolution of the connecting rod body (5, 7, 8, 8bis) in dimensions chosen from the same materials and alloys or in metallurgical assays or variable components by adding metallic material, - simultaneously raising in the construction of the form of revolution, internal or external local reinforcements (3, 3bis, 4, 6, 9, 10, 11, 13) to said body in geometric dimensions and shapes selected from the same materials and alloys or in metallurgical dosages or variable components by adding metallic material, - add to the rod body the dry wave of the two ends (2) in dimensions and shapes selected from the same materials and alloys as the first end or in metallurgical dosages or variable components by providing metal material.
    [0002]
    2) The manufacturing method according to claim 1, characterized in that the two ends (2), the casings of the body of connecting rods (3, 3a, 5, 7, 8, 8a), the internal or external local reinforcements (4). , 6, 9, 10, 11, 13) are joined and obtained almost simultaneously in a single manufacturing operation by melting metal powders or alloys or composites.
    [0003]
    3) Method of manufacture according to any one of claims 1 to 2, characterized in that the two ends (2), the casings of the body of connecting rods (3, 3a, 5, 7, 8, 8a), the reinforcements Internal or external premises (4, 6, 9, 10, 11, 13) are obtained by varying the metallurgical percentages of the alloy or metal or composite used during manufacture.
    [0004]
    4) Method of manufacture according to any one of claims 1 to 3, characterized in that the rod body thus manufactured is of any variable section along the axis of revolution, mufti materials and 3D monobloc.
    [0005]
    5. Manufacturing process according to any one of claims 1 to 4, characterized in that the geometric shapes and the mechanical properties thus obtained are transposable to the connecting rods of the aircraft landing gear holding systems.
    [0006]
    6 °) manufacturing method according to any one of claims 1 to 4, characterized in that the geometric shapes and mechanical properties thus obtained are transposable to the connecting rods of aircraft engines holding systems and launchers. 3035605 - 7 - 7 °) Manufacturing process according to any one of claims 1 to 4, characterized in that the geometric shapes and mechanical properties thus obtained are transposable to the holding rods subsystems and satellite systems. 8. Manufacturing process according to any one of claims 1 to 4, characterized in that the geometric shapes and the mechanical properties thus obtained are transposable to the transmission shafts of turbo machines. 9 °) manufacturing method according to any one of claims 1 to 4, characterized in that the geometric shapes and the mechanical properties thus obtained are transposable to the junction beams.
    类似技术:
    公开号 | 公开日 | 专利标题
    FR3035605A1|2016-11-04|PROCESS FOR OBTAINING HOLLOW TUBULAR BEAM, FLEXIBLE RAIDIE, TORSION AND COMPRESSION / FLAMING, AND BEAM END, AND BEAM EXTREMITS OBTAINED BY FUSION OF POWDERS AND METALLURGIC GRADIENTS
    Fernandez2017|Advanced deployable shell-based composite booms for small satellite structural applications including solar sails
    Kabir2000|Finite element analysis of composite pressure vessels with a load sharing metallic liner
    US20090212155A1|2009-08-27|Engine pylon made from composite material
    FR2579954A1|1986-10-10|
    JP2012507645A5|2012-12-27|
    US20110215193A1|2011-09-08|Hybrid torque box for a thrust reverser
    FR3029833A1|2016-06-17|PROCESS FOR OBTAINING HIGHLY ANISOTROPIC SANDWICH STRUCTURES INTEGRATING MECHANICAL, THERMAL, AND SOUL FUNCTIONS AND SKINS OF STRUCTURES OBTAINED BY METALLURGIC GRADIENT OR COMPOSITE
    JPH08502928A|1996-04-02|Frame using hollow member, and method of manufacturing and using the same
    Rajesh et al.2017|A review on material selection and fabrication of composite solid rocket motor | casing
    Doorbar et al.2018|4.19 Development of Continuously-Reinforced Metal Matrix Composites for Aerospace Applications
    EP2097255A2|2009-09-09|Hybrid composite-metal aircraft landing gear and engine support beams
    GB2371007A|2002-07-17|Friction welding
    EP3118119B1|2021-12-29|Beam with hybrid cross-sectional structure
    Mirtsch et al.2006|Vault structures enabling sustainable products
    Arani et al.2007|Investigating elastic stability of cylindrical shell with an elastic core under axial compression by energy method
    FR3071290B1|2019-09-13|AUXETICAL SHOCK
    Barynin et al.1999|Aerospace composite lattice structures
    US20160311195A1|2016-10-27|Composite preforms with supplemental load bearing plies
    Fadavian et al.2015|A comparative review study on the manufacturing processes of composite grid structures
    Rusin et al.2019|Stages of plastic flow of silumin-matrix-based composites during compression
    Gandra et al.2021|Development of linear friction welding to add external features to spacecraft and launchers systems
    Asraff et al.2006|New concepts in structural analysis and design of double walled LPRE thrust chambers
    Lee et al.2001|Development of Metal Matrix Composites for NASA's Advanced Propulsion Systems
    Texler2020|Advanced Additive Composites Manufacturing and What it Means for High Powered Sub-Orbital Rocketry
    同族专利:
    公开号 | 公开日
    FR3035605B1|2021-08-27|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    JP4317135B2|2002-10-24|2009-08-19|ツェットエフレムフェルダーメタルヴァーレンアクチエンゲゼルシャフト|Method for manufacturing a tie rod casing|
    US20090100963A1|2005-03-31|2009-04-23|Airbus France|Hollow structural rod and production method thereof|
    US20120251235A1|2009-12-15|2012-10-04|Airbus Operations Gmbh|Force transmission fitting for lightweight components|
    DE202010012407U1|2010-08-31|2010-11-25|Leibniz-Institut Für Festkörper- Und Werkstoffforschung Dresden E.V.|crank|
    EP2620594A1|2012-01-27|2013-07-31|Honeywell International Inc.|Multi-material turbine components|
    DE102013219250A1|2012-09-26|2014-03-27|Bayerische Motoren Werke Aktiengesellschaft|Component part, useful in chassis of motor vehicle e.g. passenger car, comprises lightweight material and high-strength material applied on higher loaded location by laser melting and applied in the form of ribs or mesh|
    EP2792436A2|2013-04-19|2014-10-22|Sikorsky Aircraft Corporation|Integrally formed stiffener|
    WO2014195657A1|2013-06-06|2014-12-11|Aircelle|Profiled two-part connecting rod designed to be positioned in an aircraft engine flow|
    EP2886448A1|2013-12-20|2015-06-24|Airbus Operations GmbH|A load bearing element and a method for manufacturing a load bearing element|EP3604127A1|2018-08-02|2020-02-05|Safran Landing Systems UK Limited|Aircraft landing gear assembly|
    EP3623287A1|2018-09-17|2020-03-18|Safran Landing Systems UK Limited|Aircraft landing gear component|
    FR3087235A1|2018-10-15|2020-04-17|Renault S.A.S.|BALANCED ROTARY SHAFT, ESPECIALLY A CRANKSHAFT, PARTIALLY CARRIED OUT BY AN ADDITIVE MANUFACTURING TECHNIQUE, MANUFACTURING METHOD AND MOTOR EQUIPPED WITH SUCH A SHAFT|
    法律状态:
    2016-04-11| PLFP| Fee payment|Year of fee payment: 2 |
    2016-11-04| PLSC| Search report ready|Effective date: 20161104 |
    2017-04-04| PLFP| Fee payment|Year of fee payment: 3 |
    2017-11-17| TP| Transmission of property|Owner name: OPT'ALM, FR Effective date: 20171017 |
    2019-03-18| PLFP| Fee payment|Year of fee payment: 5 |
    2020-04-29| PLFP| Fee payment|Year of fee payment: 6 |
    2021-04-19| PLFP| Fee payment|Year of fee payment: 7 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1500902A|FR3035605B1|2015-04-28|2015-04-28|PROCESS FOR OBTAINING A HOLLOW TUBULAR BEAM STRONG IN BENDING, TORSION AND COMPRESSION / BURNING AND BEAM CORE AND BEAM ENDS OBTAINED BY MELTING POWDERS AND METALLURGIC GRADIENTS|FR1500902A| FR3035605B1|2015-04-28|2015-04-28|PROCESS FOR OBTAINING A HOLLOW TUBULAR BEAM STRONG IN BENDING, TORSION AND COMPRESSION / BURNING AND BEAM CORE AND BEAM ENDS OBTAINED BY MELTING POWDERS AND METALLURGIC GRADIENTS|
    [返回顶部]