WO2014079651A1 - Casting mould with chamfered end faces on inner walls - Google Patents
Casting mould with chamfered end faces on inner walls Download PDFInfo
- Publication number
- WO2014079651A1 WO2014079651A1 PCT/EP2013/072382 EP2013072382W WO2014079651A1 WO 2014079651 A1 WO2014079651 A1 WO 2014079651A1 EP 2013072382 W EP2013072382 W EP 2013072382W WO 2014079651 A1 WO2014079651 A1 WO 2014079651A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- end faces
- wall elements
- mold
- mold according
- chamfered
- 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.)
- Ceased
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/22—Moulds for peculiarly-shaped castings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D17/00—Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
- B22D17/20—Accessories: Details
- B22D17/22—Dies; Die plates; Die supports; Cooling equipment for dies; Accessories for loosening and ejecting castings from dies
Definitions
- the invention relates to a mold having inside walls with end faces which are chamfered.
- Molds for making hollow components with internal structures such as turbine blades, often have multiple channels in which liquid material propagates.
- an oxide layer often forms in this region, because in this intermediate region two liquid fronts collide, which then form an oxide film layer in this thin region.
- the object is achieved by a casting mold according to claim 1.
- Figure 2, 3 a casting molds according to the invention.
- Figure 1 shows a mold 1 'according to the prior art.
- a propagation direction of a liquid metal, which is introduced into the mold 1 'or the longitudinal direction of outer 4', 4 '' and inner 7 ', 7' 'wall elements of the mold 1' is designated by the reference numeral 19.
- the propagation direction 19 is nearly parallel to the walls 4 ', 4' ', 7', 7 '' ( Figures 1, 2); 103 ', 103 ", 106', 106" (FIG. 3).
- the mold 1 ' accordinging to the prior art, in the direction of propagation 19 of the molten metal to be infiltrated seen opposite the inner wall elements 7', 7 '', wherein between the outer wall elements 4 ', 4' 'of
- Mold 1 'in the mold 1' solidified metal walls 2 ', 2' 'of a cast component results.
- the inner wall elements 7 ', 7'' have an opening 13' for two incoming liquid fronts 22 ', 22'', in the 13' penetrates the liquid metal and thus forms an inner structure 25 ', that is, a connection between the walls. 2 ', 2''of the later cast component.
- An end face 10 'of the inner wall element 7' and an end face 10 '' of the opposite inner wall element 7 '' are formed perpendicular to the direction of propagation 19.
- FIG. 2 shows a casting mold 1 according to the invention, in which, in comparison to FIG. 1, an end face 40 of an inner wall element 31 (analogous to 7 ') is designed differently.
- the end face 40 is chamfered and extends at an angle other than 90 ° to the propagation direction 19 or to the outer surface 50 of the inner wall element 31.
- the end face 40 of the inner wall elements 7 '', 31 is beveled, which is washed by the liquid front 22 ', 22' 'first.
- the liquid front 34, 37 of the liquid material is influenced and an inventive opening 43, in which the two liquid fronts 34, 37 meet, moves with its contact line 60, away from the bevelled end face 40 and away from a breakthrough 43 between the end faces 10 '', 40 of the inner wall elements 7 '', 31 in a mechanically less critical area, so that a casting with walls 54 ', 54' 'is formed, which has a higher strength.
- end faces 112 ', 112' 'of adjacent, in particular parallel inner wall elements 103', 106 '; 103 '', 106 '', beveled (Fig. 3), which then have an angle different from 90 ° to the side surface 51 ', 51' '.
- An inner wall 55 is formed between the inner wall elements 103 ', 106', 103 ", 106" when the metal solidifies.
- End faces 109 ', 109''of the wall elements 103', 103 '', which lie opposite the beveled end faces 112 ', 112'', are preferably not beveled but extend perpendicularly to the propagation direction 19 or to the side surfaces 51 ', 51''.
- all end faces 112 ', 112' ' are chamfered to the same side.
- the angle of the chamfered end faces 40, 112 ', 112' 'to the propagation direction 19 may preferably be between 45 ° and 60 °.
- the entire end face 40, 112 ', 112' ' is chamfered.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Continuous Casting (AREA)
- Mold Materials And Core Materials (AREA)
Abstract
Description
Gussform mit angeschrägten Stirnseiten bei inneren Wänden Mold with beveled ends on inner walls
Die Erfindung betrifft eine Gussform, die im Inneren Wände mit Stirnseiten aufweist, die angeschrägt sind. The invention relates to a mold having inside walls with end faces which are chamfered.
Gussformen zur Herstellung hohler Bauteile mit inneren Strukturen, wie bei Turbinenschaufeln, weisen oft mehrere Kanäle auf, in denen sich flüssiges Material ausbreitet. Molds for making hollow components with internal structures, such as turbine blades, often have multiple channels in which liquid material propagates.
Dabei bestehen zwischen einzelnen Kanalwänden der Gussform Lücken, die im späteren Gussteil Verbindungselemente darstellen . There are gaps between individual channel walls of the casting mold, which represent connecting elements in the later casting.
Dabei bildet sich oft in diesem Bereich eine Oxidschicht aus, weil in diesem Zwischenbereich zwei Flüssigkeitsfronten aufeinander stoßen, die dann in diesem dünnen Bereich eine Oxidfilmschicht ausbilden. In this case, an oxide layer often forms in this region, because in this intermediate region two liquid fronts collide, which then form an oxide film layer in this thin region.
Es ist daher Aufgabe der Erfindung oben genanntes Problem zu lösen. It is therefore an object of the invention to solve the above-mentioned problem.
Die Aufgabe wird gelöst durch eine Gussform gemäß Anspruch 1. The object is achieved by a casting mold according to claim 1.
In den Unteransprüchen sind weitere vorteilhafte Maßnahmen aufgelistet, die beliebig miteinander kombiniert werden können, um weitere Vorteile zu erzielen. In the dependent claims further advantageous measures are listed, which can be combined with each other in order to achieve further advantages.
Es zeigen: Figur 1 eine Gussform nach dem Stand der Technik,1 shows a mold according to the prior art,
Figur 2, 3 eine erfindungsgemäße Gussformen. Figure 2, 3 a casting molds according to the invention.
Die Beschreibung und die Figuren stellen nur Ausführungsbeispiele der Erfindung dar. Figur 1 zeigt eine Gussform 1' nach dem Stand der Technik. The description and the figures represent only embodiments of the invention. Figure 1 shows a mold 1 'according to the prior art.
Eine Ausbreitungsrichtung eines flüssigen Metalls, das in die Gussform 1' eingebracht wird oder die Längsrichtung äußerer 4', 4'' und innerer 7', 7'' Wandelemente der Gussform 1' ist mit dem Bezugszeichen 19 gekennzeichnet. A propagation direction of a liquid metal, which is introduced into the mold 1 'or the longitudinal direction of outer 4', 4 '' and inner 7 ', 7' 'wall elements of the mold 1' is designated by the reference numeral 19.
Die Ausbreitungsrichtung 19 verläuft nahezu parallel zu den Wänden 4', 4'', 7', 7'' (Fig. 1, 2); 103', 103'', 106', 106'' (Fig. 3) . The propagation direction 19 is nearly parallel to the walls 4 ', 4' ', 7', 7 '' (Figures 1, 2); 103 ', 103 ", 106', 106" (FIG. 3).
Die Gussform 1' nach dem Stand der Technik weist in der Ausbreitungsrichtung 19 des einzugießenden flüssigen Metalls gesehen gegenüberliegende die inneren Wandelemente 7', 7'' auf, wobei das zwischen den äußeren Wandelementen 4', 4'' derThe mold 1 'according to the prior art, in the direction of propagation 19 of the molten metal to be infiltrated seen opposite the inner wall elements 7', 7 '', wherein between the outer wall elements 4 ', 4' 'of
Gussform 1' in der Gussform 1' erstarrte Metall Wände 2', 2'' eines Gussbauteil ergibt. Mold 1 'in the mold 1' solidified metal walls 2 ', 2' 'of a cast component results.
Die inneren Wandelemente 7', 7'' weisen einen Durchbruch 13' für zwei ankommende Flüssigkeitsfronten 22', 22'' auf, in den 13' das flüssige Metall eindringt und so eine innere Struktur 25' bildet, also eine Verbindung zwischen den Wänden 2', 2'' des späteren Gussbauteils. Im Bereich des Durchbruchs 13' sind verbreiterte Flüssigkeitsfronten 22v, 22VI vorhanden. Gestrichelt angedeutet ist die Kontaktlinie 20' der Flüssigkeitsfronten 22v, 22VI, die sich gegebenenfalls aufgrund von Oxidfilmen auf den Flüssigkeitsfronten 22v, 22VI schmelzmetallurgisch nicht optimal im Durchbruch 13' verbinden. Danach verlaufen die Flüssigkeitsfronten 22''', 22IV wieder wie vorher (= 22', 22''). The inner wall elements 7 ', 7''have an opening 13' for two incoming liquid fronts 22 ', 22'', in the 13' penetrates the liquid metal and thus forms an inner structure 25 ', that is, a connection between the walls. 2 ', 2''of the later cast component. In the area of the breakthrough 13 'widened liquid fronts 22 v , 22 VI are present. Dashed lines indicate the contact line 20 'of the liquid fronts 22 v , 22 VI , which may not optimally melt due to oxide films on the liquid fronts 22 v , 22 VI metallurgically in breakthrough 13' connect. Thereafter, the liquid fronts 22 ''', 22 IV again as before (= 22', 22 '').
Eine Stirnseite 10' des inneren Wandelements 7' und eine Stirnseite 10'' des gegenüberliegenden inneren Wandelements 7'' sind senkrecht zur Ausbreitungsrichtung 19 ausgebildet. An end face 10 'of the inner wall element 7' and an end face 10 '' of the opposite inner wall element 7 '' are formed perpendicular to the direction of propagation 19.
Innerhalb des Durchbruchs 13' kommt es manchmal zu Rissen, wenn das Metall in der inneren Struktur 25' des ausgefüllten Durchbruchs 13' entlang der gestrichelt angedeuteten Linie erstarrt . Within the breakthrough 13 ', cracks sometimes occur when the metal in the inner structure 25' of the filled Breakthrough 13 'solidified along the dashed line indicated.
Figur 2 zeigt eine erfindungsgemäße Gussform 1, bei der im Vergleich zu Figur 1 eine Stirnseite 40 eines inneren Wandelements 31 (analog zu 7') anders ausgebildet ist. FIG. 2 shows a casting mold 1 according to the invention, in which, in comparison to FIG. 1, an end face 40 of an inner wall element 31 (analogous to 7 ') is designed differently.
Die Stirnseite 40 ist angeschrägt und verläuft unter einem von 90° verschiedenen Winkel zur Ausbreitungsrichtung 19 oder zur Außenfläche 50 des inneren Wandelements 31. The end face 40 is chamfered and extends at an angle other than 90 ° to the propagation direction 19 or to the outer surface 50 of the inner wall element 31.
Vorzugsweise ist die Stirnseite 40 der inneren Wandelemente 7'', 31 angeschrägt, die von der Flüssigkeitsfront 22', 22'' zuerst umgespült wird. Durch diese asymmetrische Ausgestaltung der Stirnseite 40 des Wandelements 31 wird die Flüssigkeitsfront 34, 37 des flüssigen Materials beeinflusst und ein erfindungsgemäßer Durchbruch 43, in dem die zwei Flüssigkeitsfronten 34, 37 aufeinandertreffen, verlagert sich mit seiner Kontaktlinie 60, weg von der abgeschrägten Stirnseite 40 und weg von einem Durchbruch 43 zwischen den Stirnseiten 10'', 40 der inneren Wandelemente 7'', 31 in einen mechanisch weniger kritischen Bereich, so dass ein Gussteil mit Wänden 54', 54'' entsteht, das eine höhere Festigkeit aufweist. Preferably, the end face 40 of the inner wall elements 7 '', 31 is beveled, which is washed by the liquid front 22 ', 22' 'first. As a result of this asymmetrical configuration of the end face 40 of the wall element 31, the liquid front 34, 37 of the liquid material is influenced and an inventive opening 43, in which the two liquid fronts 34, 37 meet, moves with its contact line 60, away from the bevelled end face 40 and away from a breakthrough 43 between the end faces 10 '', 40 of the inner wall elements 7 '', 31 in a mechanically less critical area, so that a casting with walls 54 ', 54' 'is formed, which has a higher strength.
Ebenso können die Stirnseiten 112', 112'' von nebeneinander verlaufenden, insbesondere parallelen inneren Wandelementen 103', 106'; 103'', 106'', abgeschrägt werden (Fig. 3), die dann einen von 90° verschiedenen Winkel zur Seitenfläche 51', 51'' aufweisen. Likewise, the end faces 112 ', 112' 'of adjacent, in particular parallel inner wall elements 103', 106 '; 103 '', 106 '', beveled (Fig. 3), which then have an angle different from 90 ° to the side surface 51 ', 51' '.
Zwischen den inneren Wandelementen 103', 106', 103'', 106'' bildet sich bei Erstarrung des Metalls noch eine innere Wand 55. An inner wall 55 is formed between the inner wall elements 103 ', 106', 103 ", 106" when the metal solidifies.
Stirnseiten 109', 109'' der Wandelemente 103', 103'', die den abgeschrägten Stirnseiten 112', 112'' gegenüberliegen, sind vorzugsweise nicht abgeschrägt, sondern verlaufen senkrecht zur Ausbreitungsrichtung 19 oder zu deren Seitenflächen 51', 51' ' . End faces 109 ', 109''of the wall elements 103', 103 '', which lie opposite the beveled end faces 112 ', 112'', are preferably not beveled but extend perpendicularly to the propagation direction 19 or to the side surfaces 51 ', 51''.
Zwischen dem inneren Wandelementes 103', 106' bzw. 103'', 106'' gibt es Durchbrüche 53' bzw. 53''. Between the inner wall element 103 ', 106' and 103 '', 106 '' there are openings 53 'and 53' '.
Vorzugsweise sind alle Stirnseiten 112', 112'' zur selben Seite abgeschrägt. Der Winkel der abgeschrägten Stirnseiten 40, 112', 112'' zur Ausbreitungsrichtung 19 kann vorzugsweise zwischen 45° und 60° betragen. Preferably, all end faces 112 ', 112' 'are chamfered to the same side. The angle of the chamfered end faces 40, 112 ', 112' 'to the propagation direction 19 may preferably be between 45 ° and 60 °.
Zu welcher Seite die abgeschrägten Stirnseiten 40, 112', 112'' zeigen, spielt keine Rolle. To which side the beveled end faces 40, 112 ', 112' 'show, does not matter.
Vorzugsweise ist die gesamte Stirnseite 40, 112', 112'' abgeschrägt . Preferably, the entire end face 40, 112 ', 112' 'is chamfered.
Claims
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP13786645.5A EP2890508A1 (en) | 2012-11-22 | 2013-10-25 | Casting mould with chamfered end faces on inner walls |
| RU2015124077A RU2015124077A (en) | 2012-11-22 | 2013-10-25 | CASTING FORM WITH SLOPED ENDS ON INTERNAL WALLS |
| IN3290DEN2015 IN2015DN03290A (en) | 2012-11-22 | 2013-10-25 | |
| CN201380061123.XA CN104812510A (en) | 2012-11-22 | 2013-10-25 | Casting mould with chamfered end faces on inner walls |
| US14/443,105 US20150283604A1 (en) | 2012-11-22 | 2013-10-25 | Casting mold having beveled end faces on inner walls |
| JP2015543364A JP2015535487A (en) | 2012-11-22 | 2013-10-25 | Mold with end faces chamfered on the inner wall |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP12193768.4A EP2735387A1 (en) | 2012-11-22 | 2012-11-22 | Mould with bevelled end faces in inner walls |
| EP12193768.4 | 2012-11-22 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2014079651A1 true WO2014079651A1 (en) | 2014-05-30 |
Family
ID=47227649
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/EP2013/072382 Ceased WO2014079651A1 (en) | 2012-11-22 | 2013-10-25 | Casting mould with chamfered end faces on inner walls |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20150283604A1 (en) |
| EP (2) | EP2735387A1 (en) |
| JP (1) | JP2015535487A (en) |
| CN (1) | CN104812510A (en) |
| IN (1) | IN2015DN03290A (en) |
| RU (1) | RU2015124077A (en) |
| WO (1) | WO2014079651A1 (en) |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011153182A1 (en) * | 2010-06-01 | 2011-12-08 | Siemens Energy, Inc. | Method of casting a component having interior passageways |
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| US2312796A (en) * | 1941-10-27 | 1943-03-02 | Donald J Campbell | Casting metals |
| US3494709A (en) * | 1965-05-27 | 1970-02-10 | United Aircraft Corp | Single crystal metallic part |
| US3897817A (en) * | 1973-08-27 | 1975-08-05 | Caterpillar Tractor Co | Sand casting mold |
| US4062399A (en) * | 1975-12-22 | 1977-12-13 | Howmet Turbine Components Corporation | Apparatus for producing directionally solidified castings |
| US4549599A (en) * | 1978-10-19 | 1985-10-29 | United Technologies Corporation | Preventing mold and casting cracking in high rate directional solidification processes |
| US4289191A (en) * | 1980-04-02 | 1981-09-15 | United Technologies Corporation | Injection molding thermoplastic patterns having ceramic cores |
| US4538671A (en) * | 1981-04-29 | 1985-09-03 | American Dental Association Health Foundation | Arc furnace for the production of small investment castings of reactive or refractory metals such as titanium |
| CN1003844B (en) * | 1985-05-21 | 1989-04-12 | 西屋电气公司 | Method for manufacturing gas turbine blades with mixed crystal structure |
| US4641703A (en) * | 1985-11-27 | 1987-02-10 | General Motors Corporation | Countergravity casting mold and core assembly |
| US4982777A (en) * | 1988-08-22 | 1991-01-08 | Metal Casting Technology Inc. | Countergravity casting method and apparatus |
| GB9121364D0 (en) * | 1991-10-09 | 1991-11-20 | Rolls Royce Plc | A mould for casting components |
| US5295530A (en) * | 1992-02-18 | 1994-03-22 | General Motors Corporation | Single-cast, high-temperature, thin wall structures and methods of making the same |
| US5950705A (en) * | 1996-12-03 | 1999-09-14 | General Electric Company | Method for casting and controlling wall thickness |
| US5791395A (en) * | 1996-12-16 | 1998-08-11 | Sarksiyan; Gevork | One shot multi-color metal casting method |
| JP2001018048A (en) * | 1999-06-30 | 2001-01-23 | Sony Corp | Injection molding method of low melting point metal material, injection molding apparatus and housing |
| US6467531B1 (en) * | 1999-10-18 | 2002-10-22 | Clyde D. Doney | Method and apparatus for producing investment castings in a vacuum |
| US6860315B2 (en) * | 2001-07-26 | 2005-03-01 | Copeland Corporation | Green sand casting method and apparatus |
| US7296615B2 (en) * | 2004-05-06 | 2007-11-20 | General Electric Company | Method and apparatus for determining the location of core-generated features in an investment casting |
| US20070201980A1 (en) * | 2005-10-11 | 2007-08-30 | Honeywell International, Inc. | Method to augment heat transfer using chamfered cylindrical depressions in cast internal cooling passages |
| US8413709B2 (en) * | 2006-12-06 | 2013-04-09 | General Electric Company | Composite core die, methods of manufacture thereof and articles manufactured therefrom |
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| JP4553271B1 (en) * | 2009-12-24 | 2010-09-29 | 株式会社古久根 | Casting method and reticulated disappearance model |
| CN102078919B (en) * | 2010-12-17 | 2012-07-25 | 西安西工大超晶科技发展有限责任公司 | Precision casting method of double-layer thin-wall bent pipe casting |
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| US20140110077A1 (en) * | 2012-10-23 | 2014-04-24 | United Technologies Corporation | Casting Process and Apparatus |
| US9835035B2 (en) * | 2013-03-12 | 2017-12-05 | Howmet Corporation | Cast-in cooling features especially for turbine airfoils |
-
2012
- 2012-11-22 EP EP12193768.4A patent/EP2735387A1/en not_active Withdrawn
-
2013
- 2013-10-25 WO PCT/EP2013/072382 patent/WO2014079651A1/en not_active Ceased
- 2013-10-25 JP JP2015543364A patent/JP2015535487A/en active Pending
- 2013-10-25 US US14/443,105 patent/US20150283604A1/en not_active Abandoned
- 2013-10-25 RU RU2015124077A patent/RU2015124077A/en not_active Application Discontinuation
- 2013-10-25 EP EP13786645.5A patent/EP2890508A1/en not_active Withdrawn
- 2013-10-25 CN CN201380061123.XA patent/CN104812510A/en active Pending
- 2013-10-25 IN IN3290DEN2015 patent/IN2015DN03290A/en unknown
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2011153182A1 (en) * | 2010-06-01 | 2011-12-08 | Siemens Energy, Inc. | Method of casting a component having interior passageways |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2890508A1 (en) | 2015-07-08 |
| US20150283604A1 (en) | 2015-10-08 |
| JP2015535487A (en) | 2015-12-14 |
| CN104812510A (en) | 2015-07-29 |
| IN2015DN03290A (en) | 2015-10-09 |
| EP2735387A1 (en) | 2014-05-28 |
| RU2015124077A (en) | 2017-01-10 |
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