EP1036610A1 - Moulage de précision et en châssis dans des aérogels organiques ou en carbone - Google Patents

Moulage de précision et en châssis dans des aérogels organiques ou en carbone Download PDF

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Publication number
EP1036610A1
EP1036610A1 EP00104214A EP00104214A EP1036610A1 EP 1036610 A1 EP1036610 A1 EP 1036610A1 EP 00104214 A EP00104214 A EP 00104214A EP 00104214 A EP00104214 A EP 00104214A EP 1036610 A1 EP1036610 A1 EP 1036610A1
Authority
EP
European Patent Office
Prior art keywords
wax
gel
sol
temperature
plastic
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
Application number
EP00104214A
Other languages
German (de)
English (en)
Other versions
EP1036610B1 (fr
Inventor
Lorenz Prof. Ratke
Jochen Prof. Dr. Fricke
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
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Deutsches Zentrum fuer Luft und Raumfahrt eV
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Application filed by Deutsches Zentrum fuer Luft und Raumfahrt eV filed Critical Deutsches Zentrum fuer Luft und Raumfahrt eV
Publication of EP1036610A1 publication Critical patent/EP1036610A1/fr
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Publication of EP1036610B1 publication Critical patent/EP1036610B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C1/00Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds
    • B22C1/16Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents
    • B22C1/165Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents in the manufacture of multilayered shell moulds
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C1/00Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds

Definitions

  • the invention relates to a molding material for the fine and mold casting of metals or metal alloys comprising plastic and / or carbon aerogels and a process for the production of corresponding molding materials.
  • Investment casting in ceramic molded shells is a standard casting technique for precision parts to manufacture from various alloys.
  • the shapes are in usually made using the lost wax technique; d. H. a wax body
  • the part to be cast is wetted with a silica sol in several steps sanded, dried and then the shell is fired, whereby the wax is melted in an autoclave or burned.
  • Means Modern casting processes make it possible to cast in line with the shape and close to the final shape (J. Sprunk, W. Blank, W. Grossmann, E. Hauschild, H. Rieksmeier, H.G. Rosselnbruch; Investment casting for all industrial sectors, 2nd edition, headquarters for casting use, Düsseldorf 1987; K.A. Krekeler, investment casting, in: manual of manufacturing technology Vol. 1., editor G. Speer, Hanser Verlag, Kunststoff 1981).
  • Aerogels are highly porous, open-pored, oxidic solids that usually via sol-gel processes from metal alkoxides by polymerization, polycondensation to gels and subsequent supercritical drying. For some years now, it has also been possible to add plastics using sol-gel processes gel and by supercritical drying in a highly porous organic Convert solid body. Pyrolysis of such plastic aerogels under protective gas or in a vacuum at temperatures above 1000 ° C converts them into carbon aerogels around. Like the oxidic aerogels, plastic and carbon have aerogels extremely low effective thermal conductivities (order of magnitude some mW / K / m) and are considerably lighter. The physical and mechanical Properties of plastic and carbon aerogels are in the literature documented (R.W.
  • a Molding material for the fine and mold casting of metals or metal alloys comprising highly porous, open-pore plastic and / or carbon aerogels, available through sol-gel polymerization of organic plastic materials optionally followed by partial or complete pyrolysis of the obtained Plastic aerogels.
  • the molding material according to the invention is particularly suitable for use in lost wax processes and need not, as in the prior art for oxidic Gels can be applied in several steps.
  • the molds obtained in this way are filled with melt using customary techniques and the melt starts.
  • heat is dissipated over the mold shell or the molding sand.
  • pour and freeze in
  • aerogels mean, since carbon aerogels are quasi adiabatic, that the heat dissipation only via feeders and risers or specifically attached heat sink takes place, skillfully the risers and feeders can be used by yourself, but do not have to. That way is one fully controlled solidification is possible and the structure can accordingly required range of properties can be adjusted.
  • the airgel forms produced according to the invention are particularly suitable for the casting of aluminum alloys (whereby the casting mold practically does not heat up must be, since no heat dissipation takes place by itself). This increases the economy because energy costs can be reduced. Magnesium and titanium alloys also do not react with carbon, so that these carbon airgel forms also for these alloys under protective gas or Offer vacuum as film material.
  • a particular advantage of the molding materials according to the invention is that the Sol-gel formation at room temperature, that is, in particular at temperatures completed below the pour point of the wax within a few hours can be.
  • Supercritical drying as with the purely inorganic Gelling is not necessary. Nevertheless, it is possible to determine the pore size in the micrometer range adjust. When drying in the supercritical temperature range pore sizes in the nanometer range are also possible.
  • the molding materials according to the invention can also be inorganic or contain organic filler materials. These are essentially Understand solid materials that are inert under solidification conditions.
  • Inorganic Filler materials are selected, for example, from aluminum oxide, titanium dioxide and / or quartz, each in an amount of 5 to 30 vol .-%. used can be.
  • Fillers for the purposes of the present invention further comprise Fiber materials that have a fiber reinforcement with organic, inorganic or allow carbon and / or SiC fibers with approximately equal volume fractions.
  • organic fillers for example thermoplastic or thermosetting plastic particles, for example polystyrene and / or use organic (polyacrylonitrile) fibers.
  • thermoplastic or thermosetting plastic particles for example polystyrene and / or use organic (polyacrylonitrile) fibers.
  • these materials are also melted out during the pyrolysis of the plastic gels or be burned.
  • using such materials is one Control of shrinkage possible during pyrolysis.
  • Plastic aerogels based on resorcinol / formaldehyde used in suitable composition and suitable content of basic catalyst at temperatures between 20 and 50 ° C without supercritical drying in one microstructured plastic airgel can be transferred.
  • the composition of the sol-gel polymerization can be set such that, for example First, a highly viscous liquid is created, which is applied to a wax mold can be applied. This is also possible in several work steps, so that the layer thickness is adapted to the needs of the applications in the foundry can be.
  • the temperature of the conversion of the solution into a plastic airgel must be Melting point of the wax can be adjusted. After converting to a Plastic airgel can melt the wax and at the same time the conversion to a carbon airgel takes place in the absence of air.
  • Dependent the composition of the starting solution, the gelation temperature, the density of the resulting porous body can be made into molds, as both plastic and carbon airgel, on a micrometer scale are smooth on the surface and reproduce sharp contours.
  • the production of molds up to the plastic airgel usually takes 1 to 3 days, often only up to 24 hours.
  • the pyrolysis time is determined by the thickness the mold shell; with a wall thickness of 1 cm, for example, the time is less than 24 hours, usually 10 hours.
  • a glass container in which a wax model (weighted down with steel plates) of the Shaped body was filled with the solution until the model was complete was covered.
  • the container was closed. Gelled within two hours the solution in an air circulator (Heraeus) at 40 ° 0. It became a color change the clear solution observed after ocher yellow / light brown. The drying of the gel was obtained in the air circulator over 24 hours. Subsequently the wax was melted out at a temperature of 60 ° C.
  • the plastic airgel was placed in a cold muffle furnace brought in.
  • the oven was slowly (3 hours) heated to 1050 ° 0, where continuous nitrogen (argon or another protective gas is possible analogously) was blown through to avoid oxidation.
  • the temperature of 1050 ° C was maintained for 24 hours.
  • the mixture was then cooled with a constant gas flow and the carbon dioxide airgel form taken.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Mold Materials And Core Materials (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Catalysts (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Carbon And Carbon Compounds (AREA)
EP00104214A 1999-03-17 2000-03-01 Moulage de précision et en châssis dans des aérogels organiques ou en carbone Expired - Lifetime EP1036610B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19911847A DE19911847A1 (de) 1999-03-17 1999-03-17 Fein- und Formguß in Kunststoff/Kohlenstoff-Aerogelen
DE19911847 1999-03-17

Publications (2)

Publication Number Publication Date
EP1036610A1 true EP1036610A1 (fr) 2000-09-20
EP1036610B1 EP1036610B1 (fr) 2005-08-31

Family

ID=7901270

Family Applications (1)

Application Number Title Priority Date Filing Date
EP00104214A Expired - Lifetime EP1036610B1 (fr) 1999-03-17 2000-03-01 Moulage de précision et en châssis dans des aérogels organiques ou en carbone

Country Status (4)

Country Link
US (2) US6599953B1 (fr)
EP (1) EP1036610B1 (fr)
AT (1) ATE303214T1 (fr)
DE (2) DE19911847A1 (fr)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1077097A1 (fr) * 1999-08-18 2001-02-21 DLR Deutsches Zentrum für Luft- und Raumfahrt e.V. Utilisation d'aérogels en plastique et/ou en carbone comme matériau de noyeau
DE10216403A1 (de) * 2002-04-12 2003-11-13 Deutsch Zentr Luft & Raumfahrt Aerogelgebundene Formstoffe mit hoher Wärmeleitfähigkeit
WO2005046909A1 (fr) * 2003-11-11 2005-05-26 Deutsches Zentrum für Luft- und Raumfahrt e.V. Aerogels contenant une matiere de charge
DE102004027382A1 (de) * 2004-06-04 2006-01-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Thermisch zersetzbare Kohlenstoff-Aerogelsande
EP2204246A3 (fr) * 2008-11-12 2012-01-04 Deutsches Zentrum für Luft- und Raumfahrt e.V. Noyaux de fonderie dotés de propriétés de dénoyautage I améliorées
CN102343285A (zh) * 2011-07-18 2012-02-08 南京工业大学 一种块状硅-炭复合气凝胶的制备方法
CN102351506A (zh) * 2011-07-18 2012-02-15 南京工业大学 一种块状耐高温硅-炭复合气凝胶材料的制备方法
WO2017102231A1 (fr) * 2015-12-15 2017-06-22 Robert Bosch Gmbh Distributeur en particulier pour pièces de fonte constituées de fonte
CN109675620A (zh) * 2017-10-18 2019-04-26 中国石油化工股份有限公司 含钴催化剂及其制备方法和应用

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19911847A1 (de) * 1999-03-17 2000-09-28 Deutsch Zentr Luft & Raumfahrt Fein- und Formguß in Kunststoff/Kohlenstoff-Aerogelen
US6806299B2 (en) * 2001-05-18 2004-10-19 The Regents Of The University Of California Preparation of hydrophobic organic aeorgels
WO2006010449A2 (fr) * 2004-07-23 2006-02-02 Ceramtec Ag Innovative Ceramic Engineering Noyaux de fonderie en ceramique
US20070089849A1 (en) * 2005-10-24 2007-04-26 Mcnulty Thomas Ceramic molds for manufacturing metal casting and methods of manufacturing thereof
US8851442B2 (en) * 2008-01-22 2014-10-07 Honeywell International Inc. Aerogel-bases mold for MEMS fabrication and formation thereof
US8293657B2 (en) 2010-11-05 2012-10-23 Honeywell International Inc. Sacrificial layers made from aerogel for microelectromechanical systems (MEMS) device fabrication processes
JP5997831B2 (ja) 2012-04-23 2016-09-28 ゼネラル・エレクトリック・カンパニイ 局所的な壁厚さ制御を伴うタービン翼
DE102016223619A1 (de) * 2015-12-15 2017-06-22 Robert Bosch Gmbh Schlichte zum Auftragen auf die poröse Oberfläche von Formen und/oder Kernen für den Metallguss
WO2018078512A1 (fr) * 2016-10-24 2018-05-03 Blueshift International Materials, Inc. Aérogel polymère organique renforcé par des fibres
CA3051470A1 (fr) 2017-01-26 2018-08-02 Blueshift International Materials, Inc. Aerogels polymeres organiques comprenant des microstructures
BG67252B1 (bg) * 2017-06-27 2021-02-15 Е.Миролио ЕАД Метод за получаване на вискозна изкуствена коприна с променяща се дебелина, продукт, получен по този метод и инсталация за реализиране на метода
CN107498003A (zh) * 2017-08-10 2017-12-22 合肥市田源精铸有限公司 一种轻质耐磨钢铸件的加工方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4873218A (en) * 1988-05-26 1989-10-10 The United States Department Of Energy Low density, resorcinol-formaldehyde aerogels
DE19721600A1 (de) * 1997-05-23 1998-11-26 Hoechst Ag Nanoporöse interpenetrierende organisch-anorganische Netzwerke
DE19738466C1 (de) * 1997-09-03 1998-12-24 Deutsch Zentr Luft & Raumfahrt Stranggußvorrichtung

Family Cites Families (5)

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Publication number Priority date Publication date Assignee Title
US5242647A (en) * 1990-08-23 1993-09-07 Regents Of The University Of California Method of casting aerogels
DE19523382C2 (de) * 1995-06-30 2003-04-30 Jochen Fricke Kohlenstoffaerogele und Verfahren zu deren Herstellung
WO1997017308A1 (fr) * 1995-11-09 1997-05-15 Aspen Systems, Inc. Materiau souple super-isolant a base d'aerogel et procede de fabrication
WO1997043116A1 (fr) * 1996-05-15 1997-11-20 Hyperion Catalysis International, Inc. Structures de carbone poreuses et rigides, leurs procedes de fabrication et d'utilisation et produits les contenant
DE19911847A1 (de) * 1999-03-17 2000-09-28 Deutsch Zentr Luft & Raumfahrt Fein- und Formguß in Kunststoff/Kohlenstoff-Aerogelen

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4873218A (en) * 1988-05-26 1989-10-10 The United States Department Of Energy Low density, resorcinol-formaldehyde aerogels
DE19721600A1 (de) * 1997-05-23 1998-11-26 Hoechst Ag Nanoporöse interpenetrierende organisch-anorganische Netzwerke
DE19738466C1 (de) * 1997-09-03 1998-12-24 Deutsch Zentr Luft & Raumfahrt Stranggußvorrichtung

Non-Patent Citations (4)

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ALLKEMPER J ET AL: "Chill casting into aerogels", SCRIPTA METALLURGICA ET MATERIALIA, vol. 29, 1993, pages 1495 - 1500, XP000925332 *
FRICKE J ET AL: "Aerogels: production, characterization, and applications", THIN SOLID FILMS,CH,ELSEVIER-SEQUOIA S.A. LAUSANNE, vol. 297, no. 1-2, 1 April 1997 (1997-04-01), pages 212 - 223, XP004125997, ISSN: 0040-6090 *
HRUBESH L W: "Aerogel applications", JOURNAL OF NON-CRYSTALLINE SOLIDS,NL,NORTH-HOLLAND PUBLISHING COMPANY, AMSTERDAM, vol. 225, no. 1-3, 15 April 1998 (1998-04-15), pages 335 - 342, XP004178562, ISSN: 0022-3093 *
TSCHEUSCHNER D ET AL: "Investment casting in silica aerogels", MATERIAL SCIENCE FORUM, vol. 329-330, 2000, pages 479 - 486, XP000925267 *

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1077097A1 (fr) * 1999-08-18 2001-02-21 DLR Deutsches Zentrum für Luft- und Raumfahrt e.V. Utilisation d'aérogels en plastique et/ou en carbone comme matériau de noyeau
DE10216403A1 (de) * 2002-04-12 2003-11-13 Deutsch Zentr Luft & Raumfahrt Aerogelgebundene Formstoffe mit hoher Wärmeleitfähigkeit
DE10216403B4 (de) * 2002-04-12 2004-03-18 Deutsches Zentrum für Luft- und Raumfahrt e.V. Aerogelgebundene Formstoffe mit hoher Wärmeleitfähigkeit
WO2005046909A1 (fr) * 2003-11-11 2005-05-26 Deutsches Zentrum für Luft- und Raumfahrt e.V. Aerogels contenant une matiere de charge
DE102004027382A1 (de) * 2004-06-04 2006-01-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. Thermisch zersetzbare Kohlenstoff-Aerogelsande
DE102004027382B4 (de) * 2004-06-04 2006-03-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Thermisch zersetzbare Kohlenstoff-Aerogelsande
EP2204246A3 (fr) * 2008-11-12 2012-01-04 Deutsches Zentrum für Luft- und Raumfahrt e.V. Noyaux de fonderie dotés de propriétés de dénoyautage I améliorées
CN102343285A (zh) * 2011-07-18 2012-02-08 南京工业大学 一种块状硅-炭复合气凝胶的制备方法
CN102351506A (zh) * 2011-07-18 2012-02-15 南京工业大学 一种块状耐高温硅-炭复合气凝胶材料的制备方法
CN102343285B (zh) * 2011-07-18 2013-04-10 南京工业大学 一种块状硅-炭复合气凝胶的制备方法
WO2017102231A1 (fr) * 2015-12-15 2017-06-22 Robert Bosch Gmbh Distributeur en particulier pour pièces de fonte constituées de fonte
CN109675620A (zh) * 2017-10-18 2019-04-26 中国石油化工股份有限公司 含钴催化剂及其制备方法和应用
CN109675620B (zh) * 2017-10-18 2021-07-09 中国石油化工股份有限公司 含钴催化剂及其制备方法和应用

Also Published As

Publication number Publication date
US6599953B1 (en) 2003-07-29
US20030212152A1 (en) 2003-11-13
EP1036610B1 (fr) 2005-08-31
DE50011046D1 (de) 2005-10-06
US6887915B2 (en) 2005-05-03
DE19911847A1 (de) 2000-09-28
ATE303214T1 (de) 2005-09-15

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