Method for producing a cast component with an insert
09670870 ยท 2017-06-06
Assignee
Inventors
Cpc classification
F02F1/004
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02F3/0084
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02F2200/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B22D21/007
PERFORMING OPERATIONS; TRANSPORTING
B22D15/02
PERFORMING OPERATIONS; TRANSPORTING
B22C9/22
PERFORMING OPERATIONS; TRANSPORTING
B22D19/0081
PERFORMING OPERATIONS; TRANSPORTING
B22C3/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
B22C3/00
PERFORMING OPERATIONS; TRANSPORTING
B22C9/22
PERFORMING OPERATIONS; TRANSPORTING
F02F3/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B22D21/00
PERFORMING OPERATIONS; TRANSPORTING
C22C21/06
CHEMISTRY; METALLURGY
B22D15/02
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for producing a cast component may include providing an insert part including an insert body having a circumferential face; coating the circumferential face with an adapter layer made of silicon oxide; arranging the insert part in a casting mold; and positively locking a casting encapsulation of the insert part and the adapter layer with an aluminum alloy to produce the cast component, wherein the aluminum alloy has a magnesium proportion of at least 0.3% by weight.
Claims
1. A method for producing a cast component, comprising: a) providing an insert part including an insert body having a circumferential face; b) coating the circumferential face with an adapter layer made of silicon oxide, wherein coating the circumferential face with the adapter layer includes: dipping the insert body into a solution comprising a water glass; and curing the water glass to form a silicon oxide via heating the insert body; c) arranging the insert part in a casting mold; and d) positively locking a casting encapsulation of the insert part and the adapter layer with an aluminum alloy to produce the cast component, wherein the aluminum alloy has a magnesium proportion of at least 0.3% by weight.
2. The method as claimed in claim 1, wherein: the insert part is a cylinder liner and the cast component is a cylinder block for an internal combustion engine.
3. The method as claimed in claim 1, wherein the water glass comprises Na.sub.2O.sub.3Si.
4. The method as claimed in claim 1, wherein curing the water glass to form the silicon oxide further includes heating the insert body to a temperature of 400 C. or higher.
5. The method as claimed in claim 4, wherein the water glass comprises Na.sub.2O.sub.3Si.
6. The method as claimed in claim 1, wherein the magnesium proportion of the aluminum alloy is at least 0.5% by weight.
7. The method as claimed in claim 1, wherein the insert part is a piston ring carrier and the cast component is a piston for an internal combustion engine.
8. A method for producing a cast component, comprising: providing an insert part including an insert body having a circumferential face; coating the circumferential face with an adapter layer made of silicon oxide, wherein coating the circumferential face includes: applying a silicone resin to the circumferential face; and curing the silicone resin to form a silicon oxide via heating the insert body; arranging the insert part in a casting mold; and positively locking a casting encapsulation of the insert part and the adapter layer with an aluminum alloy to produce the cast component, wherein the aluminum alloy has a magnesium proportion of at least 0.3% by weight.
9. The method as claimed in claim 8, wherein the magnesium proportion of the aluminum alloy is at least 0.5% by weight.
10. The method as claimed in claim 9, further comprising diluting the silicone resin with a solvent before applying the silicone resin to the circumferential face.
11. The method as claimed in claim 8, wherein the silicone resin has a layer thickness of 5 m to 10 m before curing the silicone resin.
12. The method as claimed in claim 8, wherein coating the circumferential face further includes diluting the silicone resin with a solvent before applying the silicone resin to the circumferential face.
13. The method as claimed in claim 8, further comprising diluting the silicone resin with a solvent before applying the silicone resin to the circumferential face.
14. The method as claimed in claim 8, wherein curing the silicone resin to form a silicon oxide via heating the insert body includes heating the insert body to a temperature of 400 C. or higher.
15. The method as claimed in claim 8, wherein the insert part is a cylinder liner and the cast component is a cylinder block for an internal combustion engine.
16. The method as claimed in claim 8, wherein the insert part is a piston ring carrier and the cast component is a piston for an internal combustion engine.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In the drawings, in each case diagrammatically:
(2)
(3)
(4)
DETAILED DESCRIPTION
(5) In each case in a roughly diagrammatic longitudinal section,
(6) According to a first variant, the application of an adapter layer 4 of this type takes place in two method steps: in a first step, a silicone resin is applied to the regions of the circumferential face 3 which are to be encapsulated by casting. In a second step, the silicone resin is cured to form silicon oxide by way of heating of the liner body 2. In order to transform the organic silicone resin into silicon oxide, the liner body 2 can be heated to a temperature of 400 C. or more, for example with the aid of a suitable furnace. It is true here in general that a low layer thickness aids a rapid curing process, which has an advantageous effect on the industrial manufacture of the cylinder liner in large numbers. Particularly satisfactory results during the oxidation of the silicone resin are achieved if the silicone resin which is applied to the circumferential face 3 has a layer thickness of from 5 to 10 m before the curing to form silicon oxide. To this end, the silicone resin can be diluted by means of a solvent before the application to the circumferential face 3.
(7) According to a second variant which is an alternative to the first variant, the application of the adapter layer 4 takes place by way of dipping of the cylinder liner into a solution of water glass. Here, all water-soluble sodium, potassium and silicon silicates which have solidified from a melt are covered by the term water glass, in particular also Na.sub.2O.sub.3Si. Said silicates have glass-like, that is to say amorphous material properties. After dipping of the cylinder liner into a water glass solution of this type, the cylinder liner is dehydrated, that is to say cured, in an analogous manner to the first variant which is described in the preceding text, by way of heating of the cylinder liner, preferably to a temperature of 400 C. or more in order that predominantly silicon oxide remains.
(8) The cylinder liner which is coated with silicon oxide in accordance with the two above-described variants can then be inserted into a casting mold 5 which is shown diagrammatically in
(9) As a further, second exemplary application for the method according to the invention,
(10)
(11) The above explanations with respect to the exemplary scenario of
(12) The piston ring carrier which is coated with silicon oxide in accordance with the two described variants is subsequently inserted into a suitable casting mold and is encapsulated in a positively locking manner by casting with an aluminum alloy 7 in said casting mold, which aluminum alloy 7 then completes the piston ring carrier 1 with respect to the piston, said aluminum alloy 7 having a magnesium proportion of at least 0.3% by weight, preferably of at least 0.5% by weight. The adapter layer 4 of silicon oxide which is applied on the circumferential face 3 of the ring carrier body 2 causes, in an analogous way to the example of