Classifications

• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
  • C22C47/02—Pretreatment of the fibres or filaments
  • C22C47/025—Aligning or orienting the fibres
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
• • 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
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
• • 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
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
  • Y10T29/49002—Electrical device making
  • Y10T29/49009—Dynamoelectric machine
  • Y10T29/49012—Rotor
• • 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
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
  • Y10T29/49316—Impeller making
  • Y10T29/49336—Blade making
  • Y10T29/49339—Hollow blade
  • Y10T29/49341—Hollow blade with cooling passage
  • Y10T29/49343—Passage contains tubular insert
• • 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
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
  • Y10T29/49801—Shaping fiber or fibered material
• • 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
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
  • Y10T29/49826—Assembling or joining
  • Y10T29/49947—Assembling or joining by applying separate fastener
  • Y10T29/49966—Assembling or joining by applying separate fastener with supplemental joining
  • Y10T29/49968—Metal fusion joining
• • 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
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
  • Y10T29/4998—Combined manufacture including applying or shaping of fluent material
• • 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
  • Y10T29/00—Metal working
  • Y10T29/49—Method of mechanical manufacture
  • Y10T29/49995—Shaping one-piece blank by removing material

Definitions

• the present invention relates to the manufacture of metal parts comprising internal reinforcements formed of ceramic fibers, and comprising the incorporation of a composite material insert of the type consisting of ceramic fibers in a metal matrix.
• Ceramic fibers are for example silicon carbide fibers, SiC, which have a tensile strength and compression much higher than that of a metal such as titanium.
• metal matrix ceramic son which comprise a ceramic fiber coated with metal. They are also called CMM fibers or coated wires.
• the metal provides the elasticity and flexibility to handle them.
• a known method of manufacturing such parts with reinforcement comprises producing a coil of wire coated around a mandrel.
• the coil is then incorporated into a metal container or main body in which a groove forming the housing for the insert has been previously machined.
• the depth of the groove is greater than the height of the winding.
• a lid is placed on the container and welded to its periphery.
• the cover has a post complementary shape to that of the groove, and its height is adapted to that of the coil placed in the groove so as to fill the groove.
• a hot isostatic pressing step is then carried out during which the lid is deformed and the winding is compressed by the tenon.
• the technique of hot isostatic compression consists in arranging the part in an enclosure where it is subjected to a high pressure of the order of 1000 bar and a temperature also high, of the order of 1000 0 C for a few hours.
• the metallic sheaths of the coated wires are welded together and with the walls of the groove, by diffusion, to form a dense set composed of a metal alloy in which the ceramic fibers extend annularly.
• the resulting part is then machined to the desired shape.
• the method allows the manufacture of axisymmetric aeronautical parts such as rotor discs or monobloc bladed disks as well as shafts, cylinder bodies, housings, etc.
• the applicant has developed a method of manufacturing elongated parts incorporating an insert with straight portions contributing to the transmission of unidirectional tensile forces and / or compression. This process is described in the patent application FR07 / 05453 of July 26, 2007.
• the Applicant has also developed a method of manufacturing a rectilinear insert. It consists in producing a blank of a coil-shaped insert, compacting it in a container by hot isostatic pressing and then machining the rectilinear inserts in the compacted container. Such a process is described in the patent application FR 07/05454 of July 26, 2007.
• FR 2886290 in the name of Snecma proposes to perform, alternatively, the winding directly on the main body.
• a groove there are two shoulders in it.
• the first has a bearing surface for the direct winding of a coated wire. This surface is parallel to the winding direction.
• the groove is reconstituted by placing a piece on the main body which is of complementary shape to that of a second shoulder forming a step relative to the first shoulder. Then we have the cover with the pin on the insert that has just wound and compacts the whole. This solution only partially solves the manufacturing problem because the assembly remains complex.
• metal parts comprising one or more metal matrix composite reinforcements from coiled fiber winding and a container - body and lid.
• These structures are efficient but have a high manufacturing cost.
• the machining of the main body of the container with its lid represents a significant fraction of the total cost of the parts.
• the applicant has set itself the objective of improving the process for manufacturing elongated parts in the sense of simplifying the steps of the range and reducing costs.
• this objective is achieved with a method for manufacturing a metal part reinforced with ceramic fibers, according to which: a metal housing having an upper surface is machined with a housing for an insert, and an insert formed of a bundle of metal matrix fibers in the housing, a metal cover is placed on the body so as to cover the insert, the cover is welded to the metal body, the entire metal body is treated with hot isostatic pressing cover and said treated assembly is machined to obtain said part, characterized by the fact that the insert is rectilinear, the housing forms a rectilinear groove open at each end, said groove being filled by a tongue at the time of the closing by the lid.
• the invention is based on the observation that the machining of a rectilinear groove passing through the entire body of the container is much easier to master than a non-through groove.
• the solution of the invention is of particular interest with the introduction of two inserts, of elongate shape, arranged in two parallel rectilinear branches or not.
• an annular insert with two rectilinear branches interconnected by two parts arcuate.
• the housing is machined according to the precise shape of the insert. Adjusting the shape of the housing to that of the insert has proved to be a very delicate and expensive operation.
• the machining and setting up more simple without sacrificing the strength of the piece in the end since the fibers work essentially in their longitudinal direction in the central section of the piece.
• the lid comprises a plate and one or more tabs secured to the plate. More particularly, the plate and the tongue or tabs are obtained by machining the same thick plate. According to one variant, the tongue or tabs and the plate form separate pieces.
• a chamfer is machined on the upper edge of the groove forming the housing of the insert. This chamfer allows the gradual settlement of the tongue on the insert and to obtain a gradual deformation, that is to say without discontinuity.
• the invention is particularly advantageous when the insert is of polygonal cross section, in particular rectangular. It can be oval or circular.
• the insert is either formed of bundled metal-coated fibers or formed of ceramic fibers in a single metal matrix.
• FIG. 1 shows the various steps 1a, 1b, 1c, 1 Id of manufacture of a piece of elongate shape according to the known prior art of the present applicant;
• FIG. 2 shows an example of a part obtained after machining a container incorporating inserts
• Figure 3 shows in perspective a metal body machined according to the invention
• Figure 4 shows in perspective tabs associated with a plate to form the lid closing the metal body of Figure 3;
• Figure 5 shows in exploded perspective the various components before assembly.
• a container 1 with a main body 4 of elongate shape, for forming a connecting rod of a landing gear for example.
• a groove 41 has been machined on each of the two faces of the body 4. This groove makes it possible to hold an insert 3 which comprises two rectilinear portions parallel or not between them joined at the ends by a portion of an arc of a circle.
• the inserts are of the ceramic fiber type coated with metal such as titanium.
• the grooves and the inserts are of complementary shapes so that the insert is fit without play in the groove.
• Two covers 5 are provided with a projecting portion forming a pin 51 and cover the faces of the body 4.
• the pin bears on the insert housed in the groove and closes the latter.
• the cover 5 is welded, for example by electron beam, to the body 4, providing a vacuum inside the container.
• the container is visible in Figure Ib; it is partly torn off to show the inserts.
• the container is then placed in an enclosure to undergo hot isostatic compression treatment.
• 1c shows that the edges 42 of the groove 41 are chamfered so as to provide clearance with the part of the cover 5 adjacent to the post 51.
• Figure Id shows the part blank obtained with two inserts visible in transparency.
• the blank is then machined so as to obtain the part 8 shown in FIG. 2.
• This part 8 has recesses 81 between the branches 82.
• the ceramic fibers are incorporated in the branches 82 which ensure the transmission of the forces in traction and compression .
• the inserts used are annular but as described in the patent application FR 07/05454 they can be formed of straight elements bars. In the latter case the rectilinear elements are incorporated in the container after being compacted before. The solution of the invention makes it possible to obtain such parts more economically.
• a metal body 10 of elongate shape with respect to the figure an upper face 10A and a lower face 10B.
• Two rectilinear grooves 10Al, 10A2 and 10B1, 10B2 were machined on each of the two faces.
• the grooves pass through the body 10 in the direction of the length and open into both end faces 1OC and 1OD.
• the length of the grooves is equal to that L of the body 10. They serve as a housing for rectilinear inserts 11, formed of bundles of coated ceramic fibers and of length 1 less than L.
• the upper edge 10Al ', 10A2', 1 OBl ' and 10B2 'of the groove portion of the insert housing is chamfered.
• a tongue 14 covers each insert 11 disposed in its housing.
• the tongue 14 of the same length L that the body 10 comprises a cutting height so as to form two end portions 14a and 14b and a central portion 14c of length 1.
• the plate 12 covers the upper face 10A respectively lower 10B of the body 10.
• the height of the tongue is equal to the depth of the groove which must be sufficient to contain the insert 11.
• a metal body, of titanium alloy for example, is prepared with an upper planar face and a lower planar face;
• Two straight rectilinear grooves 10Al, 10A2 and 10Bl10B2 are machined on each of the two upper and lower faces.
• the grooves open on the end faces of the body.
• This operation is relatively simple because one only has to consider the depth and the width of the groove.
• Two chamfered central zones 10Al ', 10A2' and 10B 1 ', 10B2' are machined on the free faces of the grooves, of length corresponding to that of the inserts.
• the inserts 11 are placed in the grooves at the chamfered areas.
• the inserts are formed of an assembled bundle of coated rectilinear fibers.
• the inserts are prefabricated according to the method described in patent application FR 07/05454.
• the inserts in this case form bars with fibers ceramics in a metal matrix. They are rectilinear elements already compacted by hot isostatic compression.
• the tabs 14 are placed on the inserts 11 with the central portion 14c along the insert and the end portions 14a and 14b at the end of the insert 11.
• the plates are placed and vacuum-welded on the faces of the body 10.
• the containers thus prepared are introduced into a hot isostatic compression chamber. It is heated and put into compression for compaction of the container.
• the blank obtained is ready to be machined.
• the method of the invention thus makes it possible to produce any elongate piece incorporating one or more rectilinear inserts.

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• Chemical & Material Sciences (AREA)
• Engineering & Computer Science (AREA)
• Materials Engineering (AREA)
• Mechanical Engineering (AREA)
• Metallurgy (AREA)
• Organic Chemistry (AREA)
• Manufacture Of Alloys Or Alloy Compounds (AREA)

Applications Claiming Priority (2)

Publications (2)

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Family Cites Families (52)

• 2007
  • 2007-12-28 FR FR0709172A patent/FR2925896B1/fr not_active Expired - Fee Related
• 2008
  • 2008-12-24 EP EP08867577A patent/EP2245205B1/de active Active
  • 2008-12-24 AT AT08867577T patent/ATE516381T1/de not_active IP Right Cessation
  • 2008-12-24 CA CA2710547A patent/CA2710547C/fr not_active Expired - Fee Related
  • 2008-12-24 US US12/810,949 patent/US8458886B2/en active Active
  • 2008-12-24 WO PCT/EP2008/068294 patent/WO2009083573A1/fr not_active Ceased
  • 2008-12-24 CN CN200880123122.2A patent/CN101952473B/zh active Active
  • 2008-12-24 BR BRPI0821441A patent/BRPI0821441A8/pt not_active IP Right Cessation
  • 2008-12-24 ES ES08867577T patent/ES2373388T3/es active Active
  • 2008-12-24 RU RU2010131656/02A patent/RU2477762C2/ru not_active IP Right Cessation
  • 2008-12-24 JP JP2010540143A patent/JP5539222B2/ja not_active Expired - Fee Related
• 2010
  • 2010-06-24 IL IL206628A patent/IL206628A0/en unknown

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