EP2643114A1 - Method for producing high-temperature resistant jet engine component - Google Patents
Method for producing high-temperature resistant jet engine componentInfo
- Publication number
- EP2643114A1 EP2643114A1 EP11793368.9A EP11793368A EP2643114A1 EP 2643114 A1 EP2643114 A1 EP 2643114A1 EP 11793368 A EP11793368 A EP 11793368A EP 2643114 A1 EP2643114 A1 EP 2643114A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- phase
- metal powder
- molten state
- low
- jet engine
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/12—Both compacting and sintering
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/22—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip
- B22F3/225—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces for producing castings from a slip by injection molding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/24—After-treatment of workpieces or articles
- B22F3/26—Impregnating
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/047—Making non-ferrous alloys by powder metallurgy comprising intermetallic compounds
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/0475—Impregnated alloys
Definitions
- the invention relates to a method for near-net-shape production of geometrically complex designed, consisting of an intermetallic phase engine components.
- the invention has for its object to develop a method for cost-effective, near net shape production of existing from an intermetallic phase, high temperature resistant engine components with geometrically complex structure.
- the basic idea of the invention lies in the use of metal powder spraying for the production of engine components made of an intermetallic phase, but where the binder is a low-melting metallic phase in molten or near-molten state and the metal powder is made from a higher-melting metallic phase and the molded part which is present in the result of an injection molding process and essentially corresponds to the final contour is not debinded, but is subjected to a heat treatment to produce an intermetallic phase.
- the binder is a low-melting metallic phase in molten or near-molten state
- the metal powder is made from a higher-melting metallic phase and the molded part which is present in the result of an injection molding process and essentially corresponds to the final contour is not debinded, but is subjected to a heat treatment to produce an intermetallic phase.
- the mixing of the molten or near-molten state low-melting phase with the high-melting-phase metal powder is carried out under the action of kneading and shearing forces generated by an extruder screw in an extruder.
- good mixing and temperature increase and a reduction in viscosity of the metal powder-melt mixture for carrying out the injection molding process are ensured.
- the metal powder-melt mixture can be additionally heated in the extruder by means of heating means.
- the engine component which has been demolded after solidification can be subjected to a machining finish before the heat treatment.
- a first low-melting phase For example, aluminum, in the molten state
- a second refractory metallic phase for example, iron
- the first low-melting point metallic phase may also be present in a not completely molten state - in the case of the aluminum used here in a below the melting point temperature range between 400 ° C and 600 ° C -.
- the metal powder produced from a metallic phase in this case iron
- the two metallic phases are intensively mixed with one another. Due to the shearing and kneading forces exerted by the extruder screw 4 on the mixture, the viscosity of the mixture continues to decrease. Due to the mechanical force and optionally an extruder heating, the mixture is also heated.
- step IV The previously brought into a low-viscosity, injection-moldable state mixture of a powdery high-melting metallic phase and a low-melting molten metallic phase (Fe, Al) is now introduced in step IV by injection molding in a mold 5.
- the casting process for the injection molding required binder is not made of thermoplasti ⁇ rule plastics and waxes, but is formed by the binder acting as a molten, low Schmel ⁇ collapsing metallic phase.
- the metal powder Binder mixture can either be injected directly from the extruder 4 in the mold 5 or, as the drawing shows, are first introduced into a cylinder 6 and then pressed by means of a pressure piston 7 in the cavity 8 of the mold 5.
- a molded part corresponding to the final shape or substantially the final shape of the engine component is removed from the mold after cooling and solidification, which can be machined in a further step VI with little machining effort.
- the molded part is subjected to a specific heat treatment tailored to the two metallic phases, in this case iron and aluminum, to produce a high-temperature-resistant intermetallic phase. Since, in contrast to the known metal powder injection molding using a thermoplastic binder, a compact (non-porous) molded part is already present after the demolding, shrinkage of the component during the heat treatment provided for producing the intermetallic compound is not difficult to control.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102010061959A DE102010061959A1 (en) | 2010-11-25 | 2010-11-25 | Method of making high temperature engine components |
PCT/EP2011/070438 WO2012069373A1 (en) | 2010-11-25 | 2011-11-18 | Method for producing high-temperature resistant jet engine component |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2643114A1 true EP2643114A1 (en) | 2013-10-02 |
EP2643114B1 EP2643114B1 (en) | 2014-10-01 |
Family
ID=45217512
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11793368.9A Not-in-force EP2643114B1 (en) | 2010-11-25 | 2011-11-18 | Method for producing high-temperature resistant jet engine component |
Country Status (4)
Country | Link |
---|---|
US (1) | US20130266470A1 (en) |
EP (1) | EP2643114B1 (en) |
DE (1) | DE102010061959A1 (en) |
WO (1) | WO2012069373A1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10597761B2 (en) | 2014-06-12 | 2020-03-24 | University Of Florida Research Foundation, Inc. | Self-repairing metal alloy matrix composites, methods of manufacture and use thereof and articles comprising the same |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1458074A1 (en) * | 1963-05-07 | 1970-01-08 | Int Standard Electric Corp | Process for injection molding and heat treatment of aluminum alloys as well as aluminum alloys and products made from them |
GB8622458D0 (en) * | 1986-09-18 | 1986-10-22 | Alcan Int Ltd | Alloying aluminium |
DE3935955C1 (en) * | 1989-10-27 | 1991-01-24 | Mtu Muenchen Gmbh | |
US5330701A (en) * | 1992-02-28 | 1994-07-19 | Xform, Inc. | Process for making finely divided intermetallic |
US5765623A (en) * | 1994-12-19 | 1998-06-16 | Inco Limited | Alloys containing insoluble phases and method of manufacture thereof |
US6024806A (en) * | 1995-07-19 | 2000-02-15 | Kubota Corporation | A1-base alloy having excellent high-temperature strength |
SG80596A1 (en) * | 1998-08-04 | 2001-05-22 | Nat Iniversity Of Singapore | Metastable aluminium-titanium materials |
DE19907118C1 (en) * | 1999-02-19 | 2000-05-25 | Krauss Maffei Kunststofftech | Injection molding apparatus for producing molded metal parts with dendritic properties comprises an extruder with screw system |
DE10120172C1 (en) * | 2001-04-24 | 2002-11-14 | Forschungszentrum Juelich Gmbh | Manufacture of components by metal injection molding (MIM) |
US6860314B1 (en) * | 2002-08-22 | 2005-03-01 | Nissei Plastic Industrial Co. Ltd. | Method for producing a composite metal product |
US6955532B2 (en) * | 2002-09-25 | 2005-10-18 | University Of Rochester | Method and apparatus for the manufacture of high temperature materials by combustion synthesis and semi-solid forming |
US20040261970A1 (en) * | 2003-06-27 | 2004-12-30 | Cyco Systems Corporation Pty Ltd. | Method and apparatus for producing components from metal and/or metal matrix composite materials |
DE10343781B4 (en) * | 2003-09-22 | 2009-02-12 | Mtu Aero Engines Gmbh | Process for the production of components |
DE102004029789A1 (en) * | 2004-06-19 | 2006-01-05 | Mtu Aero Engines Gmbh | Production of a component of a gas turbine, especially of an aircraft engine, comprises forming a component using a metal injection molding method and processing the component formed on its surface |
US7387763B2 (en) * | 2004-07-27 | 2008-06-17 | General Electric Company | Preparation of sheet by injection molding of powder, consolidation, and heat treating |
DE602006012188D1 (en) * | 2005-03-29 | 2010-03-25 | Kobe Steel Ltd | AL-BASE ALLOY WITH EXCEPTIONAL HEAT RESISTANCE, EDIBILITY AND STIFFNESS |
US7691214B2 (en) * | 2005-05-26 | 2010-04-06 | Honeywell International, Inc. | High strength aluminum alloys for aircraft wheel and brake components |
US20080169077A1 (en) * | 2007-01-11 | 2008-07-17 | Yahya Hodjat | Method of reinforcing low melting temperature cast metal parts |
US8118556B2 (en) * | 2007-01-31 | 2012-02-21 | Caterpillar Inc. | Compressor wheel for a turbocharger system |
MX2012010807A (en) * | 2010-03-24 | 2013-01-22 | Rheinfelden Alloys Gmbh & Co Kg | Method for producing die-cast parts. |
-
2010
- 2010-11-25 DE DE102010061959A patent/DE102010061959A1/en not_active Withdrawn
-
2011
- 2011-11-18 EP EP11793368.9A patent/EP2643114B1/en not_active Not-in-force
- 2011-11-18 US US13/989,278 patent/US20130266470A1/en not_active Abandoned
- 2011-11-18 WO PCT/EP2011/070438 patent/WO2012069373A1/en active Application Filing
Non-Patent Citations (1)
Title |
---|
See references of WO2012069373A1 * |
Also Published As
Publication number | Publication date |
---|---|
EP2643114B1 (en) | 2014-10-01 |
DE102010061959A1 (en) | 2012-05-31 |
WO2012069373A1 (en) | 2012-05-31 |
US20130266470A1 (en) | 2013-10-10 |
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