Classifications

• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
  • C21D9/0006—Details, accessories not peculiar to any of the following furnaces
  • C21D9/0025—Supports; Baskets; Containers; Covers
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
  • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
  • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
  • B29C70/28—Shaping operations therefor
  • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
  • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F27—FURNACES; KILNS; OVENS; RETORTS
  • F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
  • F27D5/00—Supports, screens or the like for the charge within the furnace
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F27—FURNACES; KILNS; OVENS; RETORTS
  • F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
  • F27D5/00—Supports, screens or the like for the charge within the furnace
  • F27D5/0031—Treatment baskets for ceramic articles

Definitions

• the invention relates to a carrier for a heat treatment process components to be subjected, comprising at least one frame and outgoing therefrom grid of intersecting strands, wherein the frame consists of one or more preferably a polygon forming legs.
• the heat treatment processes are, for. B. sintering processes, curing, tempering or soldering processes. Typical process temperatures are between 700 0 C and 2600 0 C, with typically between 800 ° C and 1600 0 C is worked.
• corresponding grids are made of metal.
• the grids are doing by strands in the form of round rods with z. B. formed a diameter of 2 mm.
• corresponding holding devices show significant disadvantages that u. a. The following are to be seen:
• a fiber composite part in a lattice structure is known, which is used in high-temperature furnace and plant construction, in the hardening technology or sintering technology as rust.
• a fiber preform is used, which in particular according to the TFP (Tailored Fiber Placement) technology and then pyrolyzed siert d. H. carbonized or graphitized.
• a carrier for hardened material is described in DE-U-295 12 569.
• the carrier consists of carbon fiber reinforced carbon material (CFC material), which may have a protective layer of SiC, BN or TiN.
• CFC material carbon fiber reinforced carbon material
• the carrier comprises mating side legs with mutually aligned recesses, is pushed through the material to be hardened.
• the workpiece carrier may consist of a one-piece monolithic frame, are placed on the bent rods, which serve to receive workpieces.
• the support consists of a tube construction, around which the fiber bundles are wound, which run at a distance from one another.
• the present invention is based on the problem, a carrier and a method for producing a carrier of the type mentioned in such a way that even with strong thermal loads or temperature fluctuations, a delay free carrier is provided in order to subject components to the desired extent of a heat treatment can. According to a further aspect, it should be ensured that contact reactions between components to be treated and the carrier or the grid are prevented.
• the carrier or the grid itself should be produced with structurally simple measures.
• a carrier of the type mentioned above essentially in that the frame made of temperature-resistant material and the strands of carbon fibers or ceramic fibers, starting from the one or more legs of the frame forming the grid.
• the strands consisting of the fibers called fiber bundles are arranged running in chain-weft weave structure between the legs or sections of the leg of the frame. This results in a coarse weave structure, the mesh size can be designed individually to accommodate components of desired size.
• the frame consists of a leg, then this has a curved course to z.
• B. an oval or a circle réellespannen.
• the carrier may consist of a single frame or of a plurality of mutually perpendicular or parallel frame, which complement each other virtually to a one-sided open basket.
• the grid may be made by single or multi-layer fiber strands (rovings) or twisted rovings or twisted fibers or yarns in the form of z. B. cord formed. Also suitable are prefabricated mesh fabrics or a lattice structure produced using TFP (Tailored Fiber Place- ment).
• the grating When using fiber bundles, provision is made in particular for the grating to be formed by a single, virtually endless, fiber bundle extending between the legs of the frame. Detached from this, whether single or multi-ply fiber strands or twisted fibers or yarns are used as fiber bundles, which consist of carbon fibers or ceramic fibers, according to one embodiment, the legs of the frame on the longitudinal edge recesses, of sections of the fiber bundle for clamping the grid are interspersed. The recesses themselves in particular form a comb geometry in the respective longitudinal edge.
• the legs are provided with openings such as holes which are penetrated by the fiber bundle.
• openings such as holes which are penetrated by the fiber bundle.
• the mesh size of the grid can be varied.
• the fiber bundle laid in woven structure runs under pretension between the legs, which ensures that the finished grid can not sag, ie spans a plane.
• Al 2 O 3 , SiC, BN, C or B 4 C and / or combinations of these come into question as material for the rovings or fibers.
• the frame is preferably made of CFC, graphite or fiber ceramics.
• the frame may have legs made in TFP (Tailored Fiber Placement) technique, which may be assembled by connectors. But it is also possible, from a carbon fiber reinforced carbon plate a frame z. B. cut out by means of a water jet. Also, portions of a corresponding plate can be assembled into a frame.
• TFP Trimed Fiber Placement
• each leg should span a plane which is perpendicular to the grid formed by the grid. formed plane runs. Consequently, if the legs of the frame consist of flat elements, their flat sides should extend perpendicular to the grid.
• the support consists of bottom and side frames, which are each holder for a grid.
• each side frame is a flat element and / or the lower leg is an angle element and / or a side element extending perpendicularly to the latter is in each case a round element.
• the flat element designed as a leg should furthermore span with its flat side a plane in which or in which approximately the grid held by the frame runs.
• Adjacent flat legs which abut one another at right angles or approximately at right angles, can be connected via a plug connection, which in turn extend within a round element. It is provided that the respective flat leg of the frame merges flush with the outer longitudinal edge side in each end face of a round leg.
• Al 2 O 3 and / or SiC and / or BN and / or C or combinations of one or more of these are suitable as the fiber material.
• a matrix for the weave structure may be provided, which may consist of the following materials and / or combinations thereof: carbon, B 4 C, Al 2 O 3 , SiC, Si 3 N 4 or mullite.
• the matrix can be deposited from the gas phase by means of CVD and / or CVI or can be produced by pyrolysis of a precursor material such as phenolic resin, furan resin or silicon precursors. A combination of corresponding process steps is also possible.
• a surface coating may additionally be applied to the fiber-ceramic holding structure.
• the surface coating may consist of oxides, nitrides and / or carbides of the 3rd and 4th main group and / or 3rd to 6th subgroup of the Periodic Table and / or carbon.
• the webs of the finished grid typically have a diameter between 1 mm and 10 mm, preferably between 2 mm and 4 mm.
• the frame is preferably square or rectangular with a leg length of up to 2000 mm and a height of between 10 mm and 300 mm. Typical dimensions can be:
• the frame z. B. from a correspondingly bent leg or z. B. consist of two complementary to a corresponding geometry legs.
• a fiber-ceramic holding structure consisting of frame and grid is made available with which metallic and / or ceramic components or components thereof can be positioned or fixed in a heat treatment process.
• metallic and / or ceramic components or components thereof can be positioned or fixed in a heat treatment process.
• the mesh size of the grid must be interpreted accordingly.
• the grid extends at a distance to the respective longitudinal edge of each frame leg.
• the carrier according to the invention exhibits thermal shock resistance, low density and lower heat capacity. A creeping is also not given. Further are to be mentioned as special advantages that embrittlement does not take place. Also, a long life is guaranteed. Compared to metallic fixtures, a significant reduction in rejects is noted.
• Another advantage of the invention is the good flow through the grid structure. This results in great advantages when used in the curing technology, z. B. in the 01 or gas quenching.
• the invention also relates to a method for producing a grid of intersecting strands of carbon fibers or ceramic fibers using a frame, from which the strands of desired lattice structure are stretched accordingly, then introduced into the fibers matrix and then the grid of the Frame is removed.
• the grid of sections extending from the frame can be cut off as if they were separated.
• the grid can also be removed as a unit from the frame, as long as the strands emanate from edge-side recesses.
• the matrix can be deposited from the gas phase and / or formed by pyrolysis of a precursor material. Further, surface removal may be done before removing the grid from the frame.
• oxides, nitrides and / or carbides of the 3rd and 4th main group and / or 3rd to 6th order groups of the Periodic Table and / or carbon or combinations thereof may be used.
• Al 2 O 3 , SiC, BN, C or combinations or sub-combinations of these come into consideration as fiber material.
• material for the matrix carbon, B 4 C, Al 2 O 3 , SiC, Si 3 N 4 or mullite or combinations or sub-combinations of these can be used.
• FIG. 1 shows a first embodiment of a carrier
• Fig. 3 is a first view of a third embodiment of a carrier
• FIG. 4 shows a second view of the carrier according to FIG. 3.
• FIGS. 1 and 2 show embodiments of a quasi-two-dimensional carrier according to the invention
• FIGS. 3 and 4 show a three-dimensional carrier in the form of an open basket, which has a cuboid geometry.
• a carrier 10 is shown purely in principle, as a fiber-ceramic support structure in particular for positioning or fixing of z.
• the heat treatment processes are, for. As sintering operations, curing, tempering or soldering processes, which are carried out at temperatures between 700 ° C and 2600 ° C, typically between 800 0 C and 1600 ° C.
• the carrier 10 In order for the carrier 10 to be warp-free, regardless of occurring thermal cycles, it consists of carbon fiber-reinforced carbon or a fiber ceramic and comprises a frame 11 with legs 12, 14, 16, 18 and a grid 20 extending therefrom is in the embodiment of FIG. 1 via a comb-like structure of upper longitudinal edges 22, 24, 26, 28 of the legs 12, 14, 16, 18 forming projections 30, 32, 34, 36 stretched and preferably consists of a continuous carbon fiber strand. Also, a ceramic fiber strand in question.
• the fiber strand forming the grid 20 has, in particular, Al 2 O 3 , SiC, BN, C or combinations of these as fiber material.
• the legs 12, 14, 16, 18, which according to the exemplary embodiment of FIG. 2 can be plugged together or connected in any other way, also consist of CFC or ceramic material. It would also be possible, the legs continuously, so form the frame integrally, by z. B. cutting from a carbon fiber reinforced carbon plate by means of z. B. water jet.
• the grid 20 has a matrix, this can be deposited from the gas phase (eg CVD / CVI) or by pyrolysis of a precursor material such as. As phenolic resin, furan resin or Si precursors are formed.
• Suitable materials for the matrix are carbon, B 4 C, Al 2 O 3 , SiC, Si 3 N 4 or multiline or combinations or subcombinations thereof.
• a surface coating may be provided, which may consist of oxides, nitrides and / or carbides of the 3rd and 4th main group and / or 3rd to 6th subgroup of the Periodic Table and / or carbon or combinations or sub-combinations thereof to a contact reaction between the support structure and the components to be thermally treated.
• the holding structure is understood to be the frame 11 and / or the grid 20.
• a carrier 38 to be removed from FIG. 2 likewise comprises a frame 40 with legs 42, 44, 46, 48, which are plugged together and between which a grid 50 is stretched.
• the legs 42, 44, 46, 48 bores 52, 54, of a single or multi-ply fiber strands or twisted yarn are interspersed, which consists or consist of the above explanations of carbon fibers or ceramic fibers.
• the carbon fibers consisting in particular of single or multi-layer fiber strands (rovings) or twisted fiber strands (cord) for forming the lattices 20, 50 are woven into a woven structure, depending on the thighs 12, 14, 16, 18 and 42, respectively , 44, 46, 48 outgoing and used projections 32, 34, 36, 30 and bores 52, 54, the distance between the strands can be set to the desired extent. Also, the strands 20, 50 forming strands, ie in particular the fiber strands or yarns are laid in a woven structure (warp and weft).
• FIGS. 3 and 4 show a carrier 100 in basket form, which in turn consists of side frames 102, 104, 106, 108 and bottom frame 110 and grids 112, 114, 116, 118 and 120 mounted thereon.
• a corresponding carrier 100 is intended, for example, for receiving metallic or ceramic components or components which are to be subjected to a heat treatment process.
• the side frames 102, 104, 106, 108 consist of upper flat elements 121, 122, 124 and 125 and base elements extending angle elements 126, 128, 130, 132, which in turn form the bottom frame 110.
• Round elements 134, 136, 138, 140 form the side legs of the side frames 102, 104, 106, 108.
• FIGS. 3 and 4 show that the longitudinal legs 121, 122, 124, 125, 126, 128, 130, 132 are connected to one another via plug connections which extend within the round elements 134, 136, 138, 140 and flush with each other on the outside, as the illustrations illustrate.
• the grids 112, 114, 116, 118 are formed by single or multi-layer fiber strands, as illustrated by FIGS. 1 and 2.
• the strands forming the grids pass through unspecified holes in the side legs 121, 122, 124, 126 and the leg sections 142, 144, 146, 148 of the angle elements 126, 128, 130 and 132 extending in their planes extending portions of the angle members 126, 128, 130, 132 extend along the outer surface of the grid 120 and thus serve as a support for the basket 100th
• the grids 112, 114, 116, 118, 120 or their fiber strands have as fiber material in particular Al 2 O 3 , SiC, BN, C or combinations or sub-combinations thereof. If the respective grid 112, 114, 116, 118, 120 has a matrix, this can be deposited from the gas phase (for example CVD / CVI) or can be formed by pyrolysis of a precursor material such as, for example, phenolic resin, resin or silicon precursors.
• a precursor material such as, for example, phenolic resin, resin or silicon precursors.
• Suitable materials for the matrix are carbon, B 4 C, Al 2 O 3 , SiC, Si 3 N 4 or multiline or combinations or subcombinations thereof.
• a surface coating may be provided, which may consist of oxides, nitrides and / or carbides of the third and fourth main group and / or 3rd to 6th subgroup of the Periodic Table and / or carbon or combinations or sub-combinations thereof to a contact reaction between the Garmped and the components to be thermally treated to prevent.
• the support structure is understood to be the respective frame 112, 114, 116, 118, 120 and / or the grid 102, 104, 106, 108, 110 mounted thereon.
• the legs 121, 122, 124, 125, 126, 128, 130, 132, 134, 136, 138, 140 may be made of CFC or ceramic material.
• the carrier 10, 38 or the basket 100 can be used for positioning or fixing components to be subjected to a heat treatment process, then there is also the possibility to use the respective grid 20, 50 per se. For this purpose, this can be solved by the frame 11, 40. Thus, it is in the,sbei game of FIG. 1, it is only necessary that the grid 20 of the projections 30, 32, 34, 36 removed so is removed. To use the grid 50 of FIG. 2, the bores 52, 54 passing through sections are separated.
• the carbon fiber-reinforced carbon body - be it the grid, be it the frame - by means of siliconizing z.

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• Engineering & Computer Science (AREA)
• Chemical & Material Sciences (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Crystallography & Structural Chemistry (AREA)
• Thermal Sciences (AREA)
• Materials Engineering (AREA)
• Metallurgy (AREA)
• Organic Chemistry (AREA)
• Physics & Mathematics (AREA)
• Ceramic Engineering (AREA)
• Composite Materials (AREA)
• Ceramic Products (AREA)
• Furnace Charging Or Discharging (AREA)
• Inorganic Fibers (AREA)
• Separation Using Semi-Permeable Membranes (AREA)
• Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
• Laminated Bodies (AREA)
• Chemical Vapour Deposition (AREA)
• Powder Metallurgy (AREA)
• Heat Treatments In General, Especially Conveying And Cooling (AREA)
• Woven Fabrics (AREA)

Priority Applications (7)

Applications Claiming Priority (4)

Publications (3)

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Family Applications (1)

Country Status (11)

Cited By (11)

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Family Cites Families (15)

• 2004
  • 2004-06-14 KR KR1020057023961A patent/KR20060020675A/ko not_active Ceased
  • 2004-06-14 CA CA002529325A patent/CA2529325A1/en not_active Abandoned
  • 2004-06-14 AT AT04739863T patent/ATE371044T1/de not_active IP Right Cessation
  • 2004-06-14 MX MXPA05013446A patent/MXPA05013446A/es active IP Right Grant
  • 2004-06-14 EP EP04739863A patent/EP1636391B1/de not_active Expired - Lifetime
  • 2004-06-14 US US10/560,287 patent/US7740474B2/en not_active Expired - Fee Related
  • 2004-06-14 JP JP2006515923A patent/JP2006527351A/ja not_active Abandoned
  • 2004-06-14 ES ES04739863T patent/ES2291888T3/es not_active Expired - Lifetime
  • 2004-06-14 WO PCT/EP2004/006381 patent/WO2004111562A2/de not_active Ceased
  • 2004-06-14 PL PL04739863T patent/PL1636391T3/pl unknown
  • 2004-06-14 DE DE502004004737T patent/DE502004004737D1/de not_active Expired - Lifetime

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