EP1306145B1 - Thermisches Innendruck-Umformverfahren - Google Patents
Thermisches Innendruck-Umformverfahren Download PDFInfo
- Publication number
- EP1306145B1 EP1306145B1 EP02020724A EP02020724A EP1306145B1 EP 1306145 B1 EP1306145 B1 EP 1306145B1 EP 02020724 A EP02020724 A EP 02020724A EP 02020724 A EP02020724 A EP 02020724A EP 1306145 B1 EP1306145 B1 EP 1306145B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- metal plates
- forming method
- forming
- plates
- heated
- 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.)
- Expired - Lifetime
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/021—Deforming sheet bodies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/021—Deforming sheet bodies
- B21D26/031—Mould construction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/053—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure characterised by the material of the blanks
- B21D26/059—Layered blanks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D37/00—Tools as parts of machines covered by this subclass
- B21D37/16—Heating or cooling
Definitions
- the invention relates to a thermal internal pressure forming process according to the preamble of claim 1.
- the object of the invention is so the method of the type mentioned to design that also conventional, prone to recrystallization under the influence of heat Materials, such as normal aluminum or titanium, on the production side simple way without unwanted structural changes in the temperature range close to the melting point for high-quality hollow components are internally formable.
- Shortening the heating and deformation phase is a nuisance Structural transformation of materials that are sensitive in this regard is prevented and in connection with the use of conventional, non-grain size stabilized instead of superplastic materials, a much cheaper one Component manufacturing with high degrees of forming ensured without the melting point of the sheet metal near the melting point is disadvantageous affects the material properties of the finished hollow component, with the further, Effect that is particularly significant for series production Due to the shorter cycle times, correspondingly higher production rates let achieve.
- the heating and deformation phase is limited to a period of about 5 minutes according to the invention.
- the invention preferably uses conventional aluminum sheets or the like made of a non-grain size stabilized aluminum alloy at one Temperature level of about 500 ° C deformed inside.
- the sheet metal plates according to the Insert into the mold on the way via an integrated in this Heater heats up, causing loss of time during heating the blanks are created outside the mold, avoided and on the other hand - unlike when heating the sheet metal plates with the help of a heated one Pressure medium - an exact, time-separate control of heating and Deformation process is made possible.
- the internal pressure deformation is expediently carried out with the aid of a gaseous one Pressure medium, in the simplest case air, under a pressure of normally 20 to 40 bar up to pressure values of approx. 250 bar, if z. B. sharp-edged corner areas are to be formed on the hollow components.
- a gaseous one Pressure medium in the simplest case air
- these are advantageously partially precoated with a release agent.
- the structural rigidity of the hollow components can be thereby increase in a technically simple manner that between the outer sheet metal plates arranged at least one inner plate of the same material and is welded to the edge of these, which is when the Outer boards to a stiffening plate passing through the hollow body deformed.
- the hollow component 1 which is closed in cross section, is initially two sheet metal blanks 2, 3 with a wall thickness of a few mm each from conventional, non-grain size stabilized aluminum or an aluminum alloy, which on their contact surfaces - with the exception of a narrow one Edge strip - with a silicon nitride, shown in dashed lines Release agent layer 4 are occupied, with the interposition of a pressure lance 5 placed in a mold designated 6 overall.
- Mold cavity 7 provided tool upper and lower part 8, 9, which on the Are each surrounded by a heat insulation layer 10 and by a heater 11 continuously at a near the melting point the metal plates 2, 3 lying temperature level of about 500 ° C. being held.
- To monitor the temperature level are in the area the mold cavity 7 and in the edge region of the sheet metal plates 2, 3 each temperature sensors 12 arranged.
- the tool parts 8, 9 are moved together and the sheet metal plates 2, 3 under the pressure effect of the tool parts 8, 9 and the simultaneous, near melting point heating on their Release agent-free edge zones are pressure-welded to one another, while a Melt bond on the other contact surfaces due to the release agent coating 4 is prevented.
- Print medium e.g. B. compressed air
- the pressure level of the print medium is usually between 20 and 40 bar, but can vary depending on the degree of deformation and cross-sectional geometry of the hollow component 1 up to 250 bar be raised.
- the shaping tool 6 is opened and the hollow body 1 removed, whereupon the pressure lance 5 separated, the resulting Hollow body opening closed and a new production cycle started can be. It is essential that the time between heating up the metal plates 2, 3 and the removal of the hollow body 1 so short is dimensioned that a structural transformation of the sheet metal plates 2, 3 is omitted. This period of time is conventional, non-size stabilized Aluminum boards on the order of a few, namely about 5 Minutes.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Description
- Fig. 1a, b
- zwei aufeinanderfolgende Fertigungsstufen eines Hohlbauteils a.) nach dem Einlegen der Blechplatinen in das Formwerkzeug und b.) nach Beendigung des Umformprozesses; und
- Fig. 2a, b, c
- den Fertigungsablauf für ein modifiziertes, innenblechversteiftes Hohlbauteil a.) vor Beginn, b.) in einer Zwischenstufe und c.) nach Beendigung des Umformvorgangs.
Claims (6)
- Thermisches Innendruck-Umformverfahren, bei dem randseitig miteinander verschweißte Metallplatinen in einem Formwerkzeug, bis nahe der Schmelztemperatur der Metallplatinen erwärmt und im erwärmten Zustand durch Einleiten eines Druckmediums zwischen die Platinen bis zur Anlage an der Formkavität des Formwerkzeuges zu einem Hohlkörper aufgeweitet und anschließend aus dem Formwerkzeug entnommen werden,
dadurch gekennzeichnet, dass die Metallplatinen aus einem nicht korngrößenstabilisierten Werkstoff bestehen und für die Erwärmungs- und Innenhochdruckverformungsphase der Metallplatinen eine kurze, unterhalb der Gefügeumwandlungszeit des nicht korngrößenstabilisierten Werkstoffs bei Erwärmungstemperatur liegende Zeitspanne von etwa 5 Minuten eingehalten wird. - Umformverfahren nach Anspruch 1, dadurch gekennzeichnet, dass die nicht-korngrößenstabilisierten Metallplatinen aus Aluminium oder einer Aluminiumlegierung bestehen und auf eine Temperatur von etwa 500 °C erwärmt werden.
- Umformverfahren nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass
die Metallplatinen nach dem Einlegen in das Formwerkzeug auf dem Wege über eine in dieses integrierte Heizeinrichtung erwärmt werden. - Umformverfahren nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass
die Metallplatinen mit einem Innendruck von maximal 250 bar druckgasverformt werden. - Umformverfahren nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass
die Metallplatinen an ihren an die Schweißnaht angrenzenden Kontaktflächen mit einem Trennmittel beschichtet werden. - Umformverfahren nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass
zwischen die äußeren Metallplatinen zumindest eine weitere, randseitig mit den Außenplatinen verschweißte und nach dem Aufweiten der Außenplatinen ein den Hohlkörper durchsetzendes Innenblech bildende Metallplatine eingesetzt wird.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10153139A DE10153139A1 (de) | 2001-10-27 | 2001-10-27 | Thermisches Innendruck-Umformverfahren |
DE10153139 | 2001-10-27 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1306145A1 EP1306145A1 (de) | 2003-05-02 |
EP1306145B1 true EP1306145B1 (de) | 2004-09-01 |
Family
ID=7703966
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP02020724A Expired - Lifetime EP1306145B1 (de) | 2001-10-27 | 2002-09-14 | Thermisches Innendruck-Umformverfahren |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1306145B1 (de) |
DE (2) | DE10153139A1 (de) |
ES (1) | ES2225707T3 (de) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006058988A1 (de) * | 2006-12-14 | 2008-06-26 | Elringklinger Ag | Abschirmbauteil, insbesondere Hitzeschild |
DE102006058989A1 (de) * | 2006-12-14 | 2008-06-19 | Elringklinger Ag | Abschirmbauteil, insbesondere Hitzeschild |
DE102008045441B3 (de) * | 2008-09-02 | 2010-02-18 | Otto Fuchs Kg | Verfahren zum Herstellen eines Strangpressprofilabschnittes aus einer aushärtbaren Aluminiumlegierung |
CN102284587A (zh) * | 2011-04-21 | 2011-12-21 | 上海板换机械设备有限公司 | 热辐射板板对的鼓胀成型加工工艺 |
CN102873166B (zh) * | 2012-10-19 | 2014-12-24 | 上海桦厦实业有限公司 | 飞行器球壳等温成形方法及其装置 |
CN103567271A (zh) * | 2013-10-11 | 2014-02-12 | 中航飞机股份有限公司西安飞机分公司 | 一种钛合金板材充气热胀成形方法 |
CZ2016574A3 (cs) | 2016-09-19 | 2018-03-28 | Západočeská Univerzita V Plzni | Způsob výroby dutých těles a zařízení k provádění tohoto způsobu |
FR3125974A1 (fr) | 2021-08-05 | 2023-02-10 | Airbus Operations | Procédé et dispositif de fabrication de pièce à partir d’une plaque en matériau déformable, en particulier pour un bord d’un élément d’un aéronef. |
FR3125975A1 (fr) * | 2021-08-05 | 2023-02-10 | Airbus Operations | Procédé et dispositif de fabrication de pièce à partir d’un coussin en matériau déformable, en particulier pour un bord d’un élément d’un aéronef. |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2361215A1 (de) * | 1973-12-08 | 1975-06-12 | Volkswagenwerk Ag | Verfahren zur herstellung von hohlkoerpern |
DE19531035C2 (de) * | 1995-08-23 | 1998-10-15 | Alcan Gmbh | Verfahren zur Herstellung von Hohlkörpern aus Aluminium oder Aluminiumlegierungen |
DE19946290B4 (de) * | 1999-09-27 | 2006-07-06 | Vaw Aluminium Ag | Verfahren zur Herstellung eines Kraftstoffbehälters für Kraftfahrzeuge |
-
2001
- 2001-10-27 DE DE10153139A patent/DE10153139A1/de not_active Withdrawn
-
2002
- 2002-09-14 EP EP02020724A patent/EP1306145B1/de not_active Expired - Lifetime
- 2002-09-14 DE DE50200917T patent/DE50200917D1/de not_active Expired - Lifetime
- 2002-09-14 ES ES02020724T patent/ES2225707T3/es not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE50200917D1 (de) | 2004-10-07 |
ES2225707T3 (es) | 2005-03-16 |
DE10153139A1 (de) | 2003-05-08 |
EP1306145A1 (de) | 2003-05-02 |
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