FR3035605B1 - Procede d'obtention de poutre tubulaire creuse raidie en flexion, torsion et compression / flambement et ame de poutre et extremites de poutre obtenues par fusion de poudres et gradients metallurgiques - Google Patents
Procede d'obtention de poutre tubulaire creuse raidie en flexion, torsion et compression / flambement et ame de poutre et extremites de poutre obtenues par fusion de poudres et gradients metallurgiques Download PDFInfo
- Publication number
- FR3035605B1 FR3035605B1 FR1500902A FR1500902A FR3035605B1 FR 3035605 B1 FR3035605 B1 FR 3035605B1 FR 1500902 A FR1500902 A FR 1500902A FR 1500902 A FR1500902 A FR 1500902A FR 3035605 B1 FR3035605 B1 FR 3035605B1
- Authority
- FR
- France
- Prior art keywords
- monobloc
- torsion
- bending
- compression
- manufacturing process
- 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.)
- Active
Links
- 230000006835 compression Effects 0.000 title abstract 2
- 238000007906 compression Methods 0.000 title abstract 2
- 238000000034 method Methods 0.000 title abstract 2
- 238000002844 melting Methods 0.000 title 1
- 230000008018 melting Effects 0.000 title 1
- 239000000843 powder Substances 0.000 title 1
- 230000008569 process Effects 0.000 title 1
- 238000004519 manufacturing process Methods 0.000 abstract 6
- 239000000956 alloy Substances 0.000 abstract 3
- 229910045601 alloy Inorganic materials 0.000 abstract 3
- 239000002131 composite material Substances 0.000 abstract 3
- 239000000463 material Substances 0.000 abstract 3
- 210000000988 bone and bone Anatomy 0.000 abstract 2
- 239000002184 metal Substances 0.000 abstract 2
- 229910052751 metal Inorganic materials 0.000 abstract 2
- 241000283073 Equus caballus Species 0.000 abstract 1
- 238000005452 bending Methods 0.000 abstract 1
- 230000005540 biological transmission Effects 0.000 abstract 1
- 150000001875 compounds Chemical class 0.000 abstract 1
- 150000002739 metals Chemical class 0.000 abstract 1
- 230000002787 reinforcement Effects 0.000 abstract 1
- 238000003466 welding Methods 0.000 abstract 1
Classifications
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/10—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of articles with cavities or holes, not otherwise provided for in the preceding subgroups
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y10/00—Processes of additive manufacturing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y80/00—Products made by additive manufacturing
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- 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
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J7/00—Piston-rods
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
- B22F10/20—Direct sintering or melting
- B22F10/28—Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2999/00—Aspects linked to processes or compositions used in powder metallurgy
-
- 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
- F16C2220/00—Shaping
- F16C2220/20—Shaping by sintering pulverised material, e.g. powder metallurgy
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- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Powder Metallurgy (AREA)
Abstract
L'invention concerne un procédé de fabrication de corps de poutre tubulaire creuse raidie en flexion, torsion et compression/flambement, ainsi que de ses extrémités, monobloc et multi matériaux obtenus par gradient métallurgique et variation des pourcentages des composants des alliages en cours de fabrication. Il permet d'obtenir les deux extrémités et le corps de la poutre dans une même opération et d'un seul tenant, sans autre apport de matière que le métal ou l'alliage ou le matériau composite qui compose la structure. De plus, les renforts internes et externes au corps creux de la poutre sont obtenus de la même manière, avec des variations dans le dosage des composés métalliques ou composites employés lors de la fabrication, en sorte que le produit fini est monobloc 3D et multi matériaux. Ainsi, par rapport à la technique usuelle de formage des corps creux rectiligne de poutre par fluotournage, enfonçage, évidement ou soudage par friction, les caractéristiques globales mécaniques de résistance, rigidité et masse sont fortement améliorées. Apportées localement, les variations dans les pourcentages des composants des métaux, des alliages ou des composites employés, accroissent la ténacité, la résistance. Le procédé de fabrication proposé est particulièrement destiné aux corps de bielle et aux arbres de transmission d'efforts employés dans les systèmes et sous-systèmes de satellites, aux pièces structurales d'aéronefs, aux systèmes de maintien des trains d'atterrissage et des moteurs sur les structures avion, aux axes principaux et secondaires des turbo réacteurs. Le procédé de fabrication proposé est aussi particulièrement destiné aux prothèses d'os longilignes du squelette humain et aux prothèses d'os longilignes du squelette d'équidé, en adaptant les extrémités aux formes géométriques imposées par les articulations des squelettes. Le procédé de fabrication proposé permet également d'obtenir de façon non limitative des profils courbés quelconques autres que rectilignes, pouvant ainsi être monobloc 3D.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1500902A FR3035605B1 (fr) | 2015-04-28 | 2015-04-28 | Procede d'obtention de poutre tubulaire creuse raidie en flexion, torsion et compression / flambement et ame de poutre et extremites de poutre obtenues par fusion de poudres et gradients metallurgiques |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1500902A FR3035605B1 (fr) | 2015-04-28 | 2015-04-28 | Procede d'obtention de poutre tubulaire creuse raidie en flexion, torsion et compression / flambement et ame de poutre et extremites de poutre obtenues par fusion de poudres et gradients metallurgiques |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3035605A1 FR3035605A1 (fr) | 2016-11-04 |
FR3035605B1 true FR3035605B1 (fr) | 2021-08-27 |
Family
ID=54291326
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1500902A Active FR3035605B1 (fr) | 2015-04-28 | 2015-04-28 | Procede d'obtention de poutre tubulaire creuse raidie en flexion, torsion et compression / flambement et ame de poutre et extremites de poutre obtenues par fusion de poudres et gradients metallurgiques |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3035605B1 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3604127B1 (fr) * | 2018-08-02 | 2021-04-28 | Safran Landing Systems UK Ltd | Ensemble de train d'atterrissage d'avion |
EP3623287B1 (fr) * | 2018-09-17 | 2021-03-24 | Safran Landing Systems UK Limited | Composant de train d'atterrissage d'aéronef |
FR3087235B1 (fr) * | 2018-10-15 | 2020-12-11 | Renault Sas | Arbre rotatif equilibre, notamment vilebrequin de moteur, realise en partie par une technique de fabrication additive, procede de fabrication et moteur equipe d'un tel arbre |
FR3114365B1 (fr) * | 2020-09-23 | 2022-09-09 | Safran Aircraft Engines | Bielle creuse |
FR3121390B1 (fr) * | 2021-03-31 | 2023-11-03 | Renault Sas | Biellette de suspension obtenue par une technique de fabrication additive |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10249768B3 (de) * | 2002-10-24 | 2004-07-29 | ZF Lemförder Metallwaren AG | Verfahren zur Herstellung eines Spurstangengehäuses |
FR2883940B1 (fr) * | 2005-03-31 | 2008-10-10 | Airbus France Sas | Bielle structurale creuse et procede de fabrication d'une telle bielle |
DE102009058359A1 (de) * | 2009-12-15 | 2011-06-16 | Airbus Operations Gmbh | Krafteinleitungsbeschlag für Leichtbaukomponenten |
DE202010012407U1 (de) * | 2010-08-31 | 2010-11-25 | Leibniz-Institut Für Festkörper- Und Werkstoffforschung Dresden E.V. | Kurbelarm |
US9266170B2 (en) * | 2012-01-27 | 2016-02-23 | Honeywell International Inc. | Multi-material turbine components |
DE102013219250A1 (de) * | 2012-09-26 | 2014-03-27 | Bayerische Motoren Werke Aktiengesellschaft | Bauelement im Fahrwerk eines Kraftfahrzeugs mit durch Laserschmelzen aufgebauter Verstärkung |
US20140315040A1 (en) * | 2013-04-19 | 2014-10-23 | Sikorsky Aircraft Corporation | Integrally formed stiffener |
FR3006727B1 (fr) * | 2013-06-06 | 2015-11-13 | Aircelle Sa | Bielle de liaison profilee en deux pieces, prevue pour etre disposee dans un flux d'un moteur d'aeronef |
EP2886448B1 (fr) * | 2013-12-20 | 2017-03-08 | Airbus Operations GmbH | Élément porteur de charge et procédé de fabrication dudit élément |
-
2015
- 2015-04-28 FR FR1500902A patent/FR3035605B1/fr active Active
Also Published As
Publication number | Publication date |
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FR3035605A1 (fr) | 2016-11-04 |
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