| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 161 | Foundry cores and method for manufacturing the same | EP05425320.8 | 2005-05-13 | EP1721688A1 | 2006-11-15 | Borsato, Mario |
The present invention relates to foundry cores and a method for manufacturing the same. Particularly, the present invention relates to a hollow foundry core (1) comprising a plurality of half-cores (1a, 1b, 1c) being assembled by means of sealing elements (4a, 4b, 4c) for providing a core (1), said half-cores (1a, 1b, 1c) and said sealing elements (4a, 4b, 4c) being provided with a pressed mixture of sand and a binder.
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| 162 | CASTING PROCEDURE, PARTICULARLY FOR ENGINE CYLINDER HEAD | EP02808016.6 | 2002-12-09 | EP1545811A1 | 2005-06-29 | BASSI, Bruno |
| The present invention relates to a casting procedure for obtaining parts provided with inside cavities or holes, wherein said holes and/or cavities are obtained by laying into a mould or chill, intended to receive the molten metal, one or more cores made of sand or other material, and wherein a main core is used, realised into a special core box, along one or more secondary cores intended to be associated to said main core, comprising the following steps: coating at least one secondary core, only in the zones and by the pattern thickness with a layer of material intended to dissolve in contact with the molten metal; inserting the pre-coated secondary cores into the main core box yet to be moulded; moulding the main core box; and inserting the monolithic group obtained at the previous step, consisting of the main core, of the secondary cores and of the coating material that keeps them firmly connected, into the mould or chill intended to receive the molten metal. The cores to be coated can also be formed by hollow inserts (23) made of a heat resistant material, filled with sand polymerised resin, wherein the cavity represents the core pattern. | ||||||
| 163 | Noyau de fonderie à base de borates de potassium comportant une cavité de dissolution. | EP04300450.6 | 2004-07-19 | EP1502676A1 | 2005-02-02 | Le Nezet, André |
Noyau (10) pour la réalisation de formes creuses par fonderie, obtenu par moulage d'une coulée de sels minéraux en fusion dans un moule (16), caractérisé en ce qu'il comporte une cavité intérieure (26) destinée à permettre à un solvant d'avoir accès par capillarité au coeur du noyau afin d'en accélérer la dissolution dans la pièce (12) après usage du noyau. |
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| 164 | Verfahren zum Herstellen von Hohlräume aufweisenden Gussstücken und Giesskern-Herstellungform | EP01101463.6 | 2001-01-23 | EP1134048A1 | 2001-09-19 | Benner, Gerhard; Herrmann, Ulrich |
Die Erfindung betrifft ein Verfahren zum Herstellen von Hohlräume aufweisenden Gußstücken. Die Erfindung besteht darin, daß zunächst ein erstes Gießkemteil in der zugeordneten und an der Berührungsfläche zu einer zweiten Kerngieß-Teilform durch eine Zwischenplatte abgedeckten ersten Kemgieß-Teilform geformt, dann die Zwischenplatte von der ersten Kemgieß-Teilform entfernt und durch die zweite Kerngieß-Teilform ersetzt wird, worauf in der zweiten Kerngieß-Teilform der andere Gießkernteil unmittelbar auf den bereits geformten ersten Gießkernteil aufgeformt wird, und daß beim Formen des ersten und/oder zweiten Gießkernteils durch ein oder mehrere entsprechende Formteile in einer oder beiden Grenzflächen der Gießkernteile die Ausnehmungen, insbesondere die Entgasungskanäle vorgesehen werden. |
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| 165 | Internally grooved turbine wall | EP00302856.0 | 2000-04-05 | EP1043479A2 | 2000-10-11 | Lee, Ching-Pang |
A turbine wall (28) includes an outer surface (30) for facing combustion gases (20), and an opposite inner surface (40) for being impingement air cooled. A plurality of adjoining ridges (44) and grooves (46) are disposed in the inner surface for enhancing heat transfer by the impingement cooling air (16). |
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| 166 | Auskleidungsplatte für Formkammern | EP93120995.1 | 1993-12-28 | EP0661121B1 | 1997-12-03 | Picard, Walter |
| 167 | Method and apparatus for manufacturing one-piece water jacket cores | EP92117944.6 | 1992-10-20 | EP0578864B1 | 1997-01-08 | Kelley, Patrick M. |
| 168 | Arbeitsplatte | EP94119919.2 | 1994-12-16 | EP0665100A1 | 1995-08-02 | Picard, Walter; Winkler, Stefan; Paller, Günter, Dr. |
Arbeitsplatte (1), bestehend aus einer metallischen Grundplatte (2) und einer auf dieser ein- oder beidseitig angeordneten dünneren Verschleißschutzplatte (4), wobei die Verschleißschutzplatte (4) mit der Grundplatte (2) mittels einer Klebstoffolie (3) vollflächig verbunden ist, die aus einem strukturellen Trägermaterial und einem auf diesem beidseitig aufgebrachten polymeren Klebstoff gebildet ist. |
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| 169 | Method and apparatus for manufacturing one-piece water jacket cores | EP92117944.6 | 1992-10-20 | EP0578864A1 | 1994-01-19 | Kelley, Patrick M. |
A one-piece water jacket core for an internal combustion engine is formed by providing a first core box portion (10) and a second core box portion (20) adapted for assembly and formation of the one-piece water jacket core. The first core box portion includes a first cavity (11) adapted to form a lower portion of the one-piece water jacket core and the second core box portion includes a second cavity (21) adapted to form an upper portion of the one-piece water jacket core. A plurality of movable members (12) are pivotally carried adjacent to, and preferably by, one of the core box portions. Each of the pivotal movable members includes a portion adapted to form a water jacket port (12a) and to be pivoted, after assembly of the first and second core box portions, to a position forming one of the water jacket ports in the one-piece water jacket core. The invention is particularly adapted for the formation of one-piece water jacket cores with a cold-cure process. |
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| 170 | Heteroporöses Formwerkzeug zur Herstellung von Gussformen aus Formsand und Verfahren zu dessen Herstellung | EP88202375.7 | 1988-10-20 | EP0316978B1 | 1992-01-22 | Knöss, Walter Dipl.-Ing. |
| 171 | Gas heating apparatus of core box for a moulding machine | EP86420216.3 | 1986-08-25 | EP0257166A1 | 1988-03-02 | Kawai, Sumikazu; Katashima, Seiji |
A gas heating apparatus of core box (10,10a) for a moulding machine comprising boring a number of heating gas passages (11) in the rear surface of cavity for blowing of a core box (10,10a) and disposing gas burners (12) facing respectively opposite to the openings (11a) of one side of said heating gas passages (11). |
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| 172 | Core box for foundry cores | EP85109563 | 1985-07-30 | EP0173096A3 | 1987-01-07 | Tauber, Otto; Döring, Alfons; Heckers, Hermann |
| Die Erfindung bezieht sich auf eine Kernbüchse (6, 7) für die pneumatische Herstellung von Gießkernen aus Sand, mit innerhalb der Kernbüchse (6, 7) angeordneten und an deren Wandung anliegenden, nach erfolgter Füllung der Kernbüchse (6, 7) zu entfernenden Losteilen (8). Das bei den bekannten Kernbüchsen dieser Art vorhan dene Problem des Übertritts von Kernsand an Schlitzen, die sich zwischen der Wandung der Kernbüchse (6, 7) und den Losteilen (8) ergeben, und die hierdurch verursachten Feh ler am Kern vermeidet die Erfindung durch eine oder meh rere aus einem elastischen Material bestehende Dichtun gen (9) für die zwischen der Wandung der Kernbüchse (6, 7) und den Anlageflächen der Losteile (8) bestehenden Nahtstellen. | ||||||
| 173 | Core molding method and core molding device | US15100798 | 2014-11-25 | US10016807B2 | 2018-07-10 | Kazuyuki Tsutsumi; Yusaku Takagawa |
| When a core die is being removed from a core while being rotated around its axis, the hardening time of self-hardening sand, the frictional forces generated between the core and the core die during die removal, and the strength of the core during die removal are optimized. | ||||||
| 174 | RAILCAR COUPLER CORE WITH VERTICAL PARTING LINE AND METHOD OF MANUFACTURE | US15244886 | 2016-08-23 | US20170036683A1 | 2017-02-09 | F. Andrew Nibouar; Jerry R. Smerecky; Kelly S. Day; Vaughn Makary; Nick Salamasick |
| A method of casting a core includes the steps of preparing a first half of a corebox, preparing a second half of a corebox such that the parting line of a core formed from the first and second coreboxes runs along the vertical axis of the core. | ||||||
| 175 | Method for the production of a hollow metal part by means of casting | US14394715 | 2013-04-11 | US09452469B2 | 2016-09-27 | Yves Longa; Jean De Ruffray |
| A method for producing a hollow metal part by casting, wherein a destructible core (20) is provided including a body (22) made of aggregate, and a shell (40) which surrounds the body and adheres thereto; the core (20) is positioned inside a mold (50); metal is melted and the liquid metal is injected, generally under pressure, into the mold (50), surrounding the core (20) embodying an interior space of the part; after solidification of the part, the body is disaggregated and it is removed through removal openings provided in the shell and the part; and the shell is destroyed and removed through removal openings provided in the part. | ||||||
| 176 | RAILCAR COUPLER CORE WITH VERTICAL PARTING LINE AND METHOD OF MANUFACTURE | US14921622 | 2015-10-23 | US20160107659A1 | 2016-04-21 | F. Andrew Nibouar; Jerry R. Smerecky; Kelly S. Day; Vaughn Makary; Nick Salamasick |
| A method of casting a core includes the steps of preparing a first half of a corebox, preparing a second half of a corebox such that the parting line of a core formed from the first and second coreboxes runs along the vertical axis of the core. | ||||||
| 177 | Method for molding sand mold and sand mold | US14360577 | 2012-11-27 | US09314837B2 | 2016-04-19 | Masaomi Mitsutake; Hirotsune Watanabe; Tomokazu Suda; Yusuke Kato; Toshihiko Zenpo |
| By mixing, stirring and kneading, with water glass (11) as a binder, sand (7), a surfactant (9), and water (10), foamed sand (S) is generated. The foamed sand (S) is packed in a cavity of a metallic mold and solidified to form a sand mold. By using the sand mold, aluminum is cast. By using water glass that is an inorganic binder, during casting, harmful gas and odor are not generated. Further, when a molar ratio n of water glass (Na2O nSiO2 mH2O) is adjusted in the range of 0.65 to 1.30, a quantity of water (H2O) generated by heating water glass with a high temperature melt during casting can be suppressed. Thereby, hydrogen gas (H2) according to a reaction between water (H2O) and aluminum (Al) can be suppressed from being generated and casting quality can be improved. | ||||||
| 178 | Ceramic casting core having an integral vane internal core and shroud backside shell for vane segment casting | US13998541 | 2013-11-07 | US20150122450A1 | 2015-05-07 | Ching-Pang Lee; Gerald L. Hillier; Jae Y. UM; Gm Salam Azad |
| A cast ceramic core (110), including: an airfoil portion (116) shaped to define an inner surface (56) of an airfoil (52) of a vane segment (50); and a shell portion (122) having a backside-shaping surface (120) shaped to define a backside surface (68) of a shroud (62) of the vane segment. The backside-shaping surface has a higher elevation (132) and a lower elevation (134). The higher elevation is set apart from a nearest point (138) on the airfoil portion by the lower elevation. The airfoil portion and the shell portion are cast as a monolithic body during a single casting pour. | ||||||
| 179 | INVESTMENT CASTING METHOD FOR GAS TURBINE ENGINE VANE SEGMENT | US14073922 | 2013-11-07 | US20150122446A1 | 2015-05-07 | Ching-Pang Lee; Gerald L. Hillier; Jae Y. Um; Gm Salam Azad |
| An investment casting method for a cast ceramic core (110), including an airfoil portion (116) shaped to define an inner surface (56) of an airfoil (52) of a vane segment (50) and an integral shell portion (122) having a backside-shaping surface (120) shaped to define a backside surface (68) of a shroud (62) of the vane segment. The backside-shaping surface has a higher elevation (132) and a lower elevation (134). The higher elevation is set apart from a nearest point (138) on the airfoil portion by the lower elevation. The airfoil portion and the shell portion are cast as a monolithic body during a single casting pour. | ||||||
| 180 | Ceramic core with composite insert for casting airfoils | US14121824 | 2014-10-21 | US20150053365A1 | 2015-02-26 | Boyd A. Mueller; Darren K. Rogers; Timothy J. Molamphy |
| A multi-wall ceramic core for casting an airfoil with one or more internal cooling passages is made by preforming at least one fugitive core insert to have a joint-forming surface with a male and/or female joint feature and then forming at least one fugitive core insert in-situ adjacent and integrally connected and fused to the at least one preformed core insert at the joint-forming surface to form an interlocked, fused joint to form a composite core insert that includes features to form internal passage surfaces in the core when the composite core insert is removed. Another aspect involves preforming first and second fugitive core inserts to have respective joint-forming surfaces with respective snap-fittable joint features and assembling the first and second fugitive core inserts to form a composite core insert by snap fitting the snap-fittable joint features together to form an interlocked joint. The composite core insert is placed in a core molding die cavity, and a fluid ceramic material is introduced into the die cavity to form the ceramic core body incorporating the fugitive composite core insert therein. | ||||||
