EP1954998A1 - Induction furnace - Google Patents
Induction furnaceInfo
- Publication number
- EP1954998A1 EP1954998A1 EP05849749A EP05849749A EP1954998A1 EP 1954998 A1 EP1954998 A1 EP 1954998A1 EP 05849749 A EP05849749 A EP 05849749A EP 05849749 A EP05849749 A EP 05849749A EP 1954998 A1 EP1954998 A1 EP 1954998A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- infiltration
- induction furnace
- crucible
- carbon
- coil
- 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.)
- Granted
Links
- 230000006698 induction Effects 0.000 title claims abstract description 20
- 230000008595 infiltration Effects 0.000 claims abstract description 41
- 238000001764 infiltration Methods 0.000 claims abstract description 41
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 21
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 20
- 239000000463 material Substances 0.000 claims abstract description 19
- 238000002844 melting Methods 0.000 claims abstract description 3
- 230000008018 melting Effects 0.000 claims abstract description 3
- 230000001939 inductive effect Effects 0.000 claims abstract 2
- 238000004804 winding Methods 0.000 claims description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 239000000110 cooling liquid Substances 0.000 claims description 2
- 239000000835 fiber Substances 0.000 claims description 2
- 239000004744 fabric Substances 0.000 claims 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 10
- 229910052710 silicon Inorganic materials 0.000 description 10
- 239000010703 silicon Substances 0.000 description 10
- 238000010438 heat treatment Methods 0.000 description 6
- 239000011265 semifinished product Substances 0.000 description 6
- 229910010293 ceramic material Inorganic materials 0.000 description 5
- 238000010304 firing Methods 0.000 description 4
- 238000011068 loading method Methods 0.000 description 4
- 238000003763 carbonization Methods 0.000 description 3
- 239000002131 composite material Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000000197 pyrolysis Methods 0.000 description 3
- 239000011347 resin Substances 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 239000000654 additive Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000002791 soaking Methods 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000005672 electromagnetic field Effects 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 238000009421 internal insulation Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 244000045947 parasite Species 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B6/00—Heating by electric, magnetic or electromagnetic fields
- H05B6/02—Induction heating
- H05B6/22—Furnaces without an endless core
- H05B6/24—Crucible furnaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27B—FURNACES, KILNS, OVENS, OR RETORTS IN GENERAL; OPEN SINTERING OR LIKE APPARATUS
- F27B14/00—Crucible or pot furnaces
- F27B14/06—Crucible or pot furnaces heated electrically, e.g. induction crucible furnaces with or without any other source of heat
- F27B14/061—Induction furnaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27B—FURNACES, KILNS, OVENS, OR RETORTS IN GENERAL; OPEN SINTERING OR LIKE APPARATUS
- F27B14/00—Crucible or pot furnaces
- F27B14/08—Details peculiar to crucible or pot furnaces
- F27B14/10—Crucibles
Definitions
- the present invention relates to an induction furnace and in particular to an induction furnace as defined in the preamble of the attached first claim.
- composite ceramic materials are known for braking applications obtained through infiltrations of silicon into a mixture comprising a plurality of carbon filaments and additives. Said infiltration normally takes place at a temperature in which the silicon is in a molten state.
- preparation of said composite materials can be carried out by: - mixing the plurality of filaments with binding resin, pitch and other additives; placing the resulting mixture in a mold to obtain a shaped semi-finished product by means of heating and applying pressure; - firing the semi-finished product in a furnace with a temperature such as to cause carbonization or pyrolysis of the resin.
- the semi-finished product acquires a certain porosity due to the loss of volatile material at the carbonization or resin pyrolysis temperatures .
- the semi-finished product is then subjected to an infiltration process which comprises further firing with materials to be infiltrated, in this case silicon. Said firing takes place at a temperature such as to cause melting of the silicon and its infiltration into the pores of the semi-finished product.
- the above-described infiltration step (which in this case is also called silication) is very time consuming and costly.
- Said step comprises heating of the silicon to between 1400 0 C and 1700 0 C to reach a molten state "and a decrease in pressure from 900mbar to 300mbar to facilitate the infiltration process.
- specific furnaces are used which can supply the desired temperatures and can be placed under vacuum.
- the furnaces generally used are substantially of two types: the so-called discontinuous or batch furnaces and tunnel furnaces .
- the batch type furnaces carry out a step to load a quantity of material equal to their capacity, a heating step, a soaking step at a given temperature together with a vacuum for silication and a cooling step.
- the loading capacity of these furnaces is generally 250 kg of material.
- the duration of the heating, soaking and cooling cycle varies between 24 and 48 hours in order to allow infiltration which lasts about 10 minutes.
- the tunnel type furnaces foresee loading of the material to be treated in a special loading station, transit in the heating area and unloading from a loading station. Even though they permit a continuous flow of finished material, said furnaces have the disadvantage of a structural complexity even greater than the batch type furnaces: it is sufficient to consider that the material has to transit in an area where a vacuum is present.
- the object of the present invention is to satisfy that need by providing an infiltration furnace which is economical, structurally simple, with low cycle times and versatile in use.
- the furnace 1 includes a supporting structure 2 provided with a chamber 3 inside which, by means of an vacuum pump 4 placed outside the chamber 3, a partial vacuum can be formed.
- a hole 5, made in one of the walls of the supporting structure 2, enables communication between the chamber 3 and the vacuum pump 4.
- the vacuum pump 4 is such as to bring the working pressure in the chamber 3 from between 800 mbar and 900 mbar to between 0.01 mbar and 500 mbar, and more preferably equal to approximately 2 mbar.
- the internal walls of the chamber 3 are provided with a thermally insulating lining.
- said lining comprises graphite felt panels 6 coupled to the internal walls of the chamber 3.
- the furnace 1 which is particularly an induction furnace, includes an infiltration crucible 7 and a coil 8 placed inside the chamber 3.
- the inside of the chamber 3 is also provided with supporting elements 9 for the crucible 7 such as to keep the crucible 7 at a distance from the internal walls of the chamber 3 and in particular from the panels 6 of the internal insulation lining of the chamber 3.
- the coil 8 comprises inductor windings wound around the infiltration crucible 7.
- the windings of the coil 8 are in contact with some of the walls of the infiltration crucible 7.
- the windings of the coil 8 could be wound around the infiltration crucible 7 but be placed at a distance from it, for example, they could be adjacent to the panels forming the internal lining 6 of the chamber 3.
- the coil 8 is formed of a copper pipe wound spirally around the infiltration crucible 7 and filled with a cooling liquid, such as running water, flowing inside it.
- the coil 8 is fed by an alternating current generator connected to the coil 8 and not shown in the figure.
- the infiltration crucible 7 of the induction furnace 1 is made of Carbon/Carbon, and is formed of walls 10, 11, 12 which define an infiltration chamber 13 inside the crucible 7 and such as to house a workpiece 14 in ceramic material to be subjected to infiltration and the material 15 intended to be infiltrated inside the workpiece 14.
- said walls 10, 11, 12 include an upper plate 10, a lower plate 11 and a lateral annular wall 12 placed between the upper plate 10 and the lower plate 11.
- the lateral annular wall 12 is a substantially circular wall and the two upper 10 and lower 11 plates are two disk- shaped plates .
- the type of Carbon/Carbon of which the infiltration crucible is made is preferably long fiber Carbon/Carbon fabric, with a 0/45° orientation in the upper 10 and lower 11 plates and unidirectional in the circumference of the lateral annular wall 12.
- the density of the Carbon/Carbon used to make the infiltration crucible 7 is in the range of 1 g/cm 3 and 1.9 g/cm 3 , more preferably equal to approximately 1.7 g/cm 3 .
- the workpiece 14 to be subjected to infiltration is a semi-finished workpiece, ring or disk shaped, and previously subjected to a carbonization step (or pyrolysis) such as to determine the formation of porosity in the workpiece 14.
- the chamber 13 inside the crucible has a volume approximately twice that of the semifinished workpiece 14 to be subjected to infiltration, so that the space between the workpiece 14 and the internal walls of the chamber 13 can be filled with the material 15 intended to be infiltrated into the porosity of the workpiece 14.
- said material 15 is silicon, for example pure silicon, or an alloy of silicon and aluminum or copper, in grains or powder.
- the lateral annular wall 12 of the infiltration crucible 7 is provided with an insulating lining 16 to prevent or reduce loss of heat accumulated in the infiltration chamber 13 through the lateral wall 12.
- said insulating lining 16 is an annular layer of lining placed outside the lateral wall 12 and held between the upper plate 10 and the lower plate 11.
- the semi-finished workpiece 14 in ceramic material is placed inside the infiltration crucible 7 together with the material 15, for example silicon, to be infiltrated into the porosity of the workpiece 14.
- the vacuum pump 4 is activated to bring the pressure inside the chamber 3 of the furnace 1 from a value of approximately in the range of 800 - 900 mbar to a value of approximately in the range of 0.01 - 250 mbar.
- the coil 8 is fed by an alternating current signal with a frequency and a strength such as to heat the walls of the crucible 7 and, in particular, the two plates 10 and 11. Said heating takes place as a result of parasite currents induced inside the two plates 10 and 11 by the electromagnetic field produced by the passage of the alternating current in the coil 8.
- the two plates 10 and 11 transmit heat to the inside of the infiltration chamber 13 until a temperature is reached at which the material to be infiltrated 15 turns into a molten state.
- the two plates 10 and 11 are heated until a temperature of approximately between 1400 0 C and 1700 0 C is reached inside the infiltration chamber 13. In this temperature range, the silicon melts and infiltrates into the porosity of the semi-finished workpiece 14.
- an induction furnace according to the invention makes it possible to complete infiltration of a semi-finished product in much shorter times than those of the above-described furnaces known in the art.
- an furnace according to the present invention is able to take the material contained inside it to the infiltration temperature of 1500 0 C in approximately 10-15 minutes.
- a furnace according to the invention makes it possible to carry out the infiltration process economically even on single workpieces of small dimensions .
- the presence of a crucible made in Carbon/Carbon also makes it possible to guarantee excellent resistance of the furnace to high temperatures.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Crucibles And Fluidized-Bed Furnaces (AREA)
- Furnace Details (AREA)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SI200532014T SI1954998T1 (en) | 2005-12-02 | 2005-12-02 | Induction furnace |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/IT2005/000708 WO2007063562A1 (en) | 2005-12-02 | 2005-12-02 | Induction furnace |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1954998A1 true EP1954998A1 (en) | 2008-08-13 |
EP1954998B1 EP1954998B1 (en) | 2015-07-15 |
Family
ID=36691736
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05849749.6A Active EP1954998B1 (en) | 2005-12-02 | 2005-12-02 | Induction furnace |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1954998B1 (en) |
SI (1) | SI1954998T1 (en) |
WO (1) | WO2007063562A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021001163A1 (en) * | 2019-07-04 | 2021-01-07 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Container device for molten metal, and vehicle |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1394098B1 (en) * | 2009-03-24 | 2012-05-25 | Brembo Ceramic Brake Systems Spa | INDUCTION OVEN AND INFILTRATION PROCESS |
ITMI20110401A1 (en) * | 2011-03-14 | 2012-09-15 | Petroceramics S P A | METHOD FOR INFILTRATION OF A POROUS MATERIAL WITH A SECOND MATERIAL AND ITS PLANT |
DE102012208170A1 (en) | 2012-05-16 | 2013-11-21 | Fct Anlagenbau Gmbh | Device for heat treatment of a workpiece |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5858486A (en) * | 1995-02-27 | 1999-01-12 | Sgl Carbon Composites, Inc. | High purity carbon/carbon composite useful as a crucible susceptor |
-
2005
- 2005-12-02 SI SI200532014T patent/SI1954998T1/en unknown
- 2005-12-02 EP EP05849749.6A patent/EP1954998B1/en active Active
- 2005-12-02 WO PCT/IT2005/000708 patent/WO2007063562A1/en active Application Filing
Non-Patent Citations (1)
Title |
---|
See references of WO2007063562A1 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021001163A1 (en) * | 2019-07-04 | 2021-01-07 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Container device for molten metal, and vehicle |
Also Published As
Publication number | Publication date |
---|---|
SI1954998T1 (en) | 2015-12-31 |
WO2007063562A1 (en) | 2007-06-07 |
EP1954998B1 (en) | 2015-07-15 |
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