US2065170A - Magnesium alloy - Google Patents
Magnesium alloy Download PDFInfo
- Publication number
- US2065170A US2065170A US80015A US8001536A US2065170A US 2065170 A US2065170 A US 2065170A US 80015 A US80015 A US 80015A US 8001536 A US8001536 A US 8001536A US 2065170 A US2065170 A US 2065170A
- Authority
- US
- United States
- Prior art keywords
- magnesium
- alloy
- magnesium alloy
- per cent
- crucible
- 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
- 229910000861 Mg alloy Inorganic materials 0.000 title description 5
- 229910045601 alloy Inorganic materials 0.000 description 9
- 239000000956 alloy Substances 0.000 description 9
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 7
- 239000011777 magnesium Substances 0.000 description 7
- 229910052749 magnesium Inorganic materials 0.000 description 7
- 238000005266 casting Methods 0.000 description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 4
- 239000003795 chemical substances by application Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 239000004576 sand Substances 0.000 description 3
- DDFHBQSCUXNBSA-UHFFFAOYSA-N 5-(5-carboxythiophen-2-yl)thiophene-2-carboxylic acid Chemical compound S1C(C(=O)O)=CC=C1C1=CC=C(C(O)=O)S1 DDFHBQSCUXNBSA-UHFFFAOYSA-N 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- TWRXJAOTZQYOKJ-UHFFFAOYSA-L Magnesium chloride Chemical compound [Mg+2].[Cl-].[Cl-] TWRXJAOTZQYOKJ-UHFFFAOYSA-L 0.000 description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 2
- WCUXLLCKKVVCTQ-UHFFFAOYSA-M Potassium chloride Chemical compound [Cl-].[K+] WCUXLLCKKVVCTQ-UHFFFAOYSA-M 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- 239000005864 Sulphur Substances 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 239000004411 aluminium Substances 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- 229910052787 antimony Inorganic materials 0.000 description 2
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 239000011733 molybdenum Substances 0.000 description 2
- 229910052759 nickel Inorganic materials 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- UHOVQNZJYSORNB-UHFFFAOYSA-N Benzene Chemical compound C1=CC=CC=C1 UHOVQNZJYSORNB-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- GANNOFFDYMSBSZ-UHFFFAOYSA-N [AlH3].[Mg] Chemical compound [AlH3].[Mg] GANNOFFDYMSBSZ-UHFFFAOYSA-N 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 235000021388 linseed oil Nutrition 0.000 description 1
- 239000000944 linseed oil Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910001629 magnesium chloride Inorganic materials 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 235000019198 oils Nutrition 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000001103 potassium chloride Substances 0.000 description 1
- 235000011164 potassium chloride Nutrition 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000007528 sand casting Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
- C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
Definitions
- Patented Dec. 22, 1936 ATENT OFFICE No Drawing. Application May 15,. 1936, Serial No. 80,015. In Switzerland May 15, 1935 ICIaim.
- This invention relates to a magnesium alloy which is to be used more particularly in the construction of internal combustion engines.
- the magnesium alloys hitherto known are not adequately resistant to corrosion and are not sufficiently hard, especially at the operating temperatures of the engine amounting to 200-300", and this results in excessive wear and inutility, for example of pistons.
- the magnesium alloy according to the present invention has the composition given below:-
- steel material may be added in addition to such an alloy.
- the alloy can be used either for pistons for internal combustion engines or for engine blocks, aircraft construction and so forth, particularly in consequence of its resistivity to corrosion and its specific gravity of about 1.8.
- Example 1 In a steel crucible a flux is melted which serves at the same time both as a cleansing and a covering agent and which consists of a mixture of one part of potassium chloride and one part of magnesium chloride; the whole is thoroughly mixedand is cast into slabs.
- Previously preliminary alloys are made in a suitable manner from the remaining alloy constituents, which alloys are then melted together to the so-called main preliminary alloy. This latter, preheated to -100", is added to the magnesium melt, in which it slowly dissolves. The fluxing agent rises to the surface during the fusion operation and covers the melt.
- the whole is thoroughly stirred and heated to 800-850.
- the crucible is then removed from the furnace and allowed to cool for some minutes down to casting temperature (700-750").
- casting temperature 700-750"
- the salts and impurities are preferably taken off with the casting ladle. Casting is eifected directly from the crucible with great care with the ladle as well.
- the stream being poured or cast is dusted with sulphur powder in order to prevent oxidation.
- the casting mould is preferably provided with a filter of core sand.
- the cores are made from red core sand, if desired mixed with 2 to 3' per cent. sulphur powder, and with the lowest possible linseed oil content. Before drying the cores have a 20 per cent. ammonium fluoride solution blown on them. Whenever possible all pieces are to be cast with rising.
- the material can also be used in chill moulds and in the die-cast process.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
Description
Patented Dec. 22, 1936 ATENT OFFICE No Drawing. Application May 15,. 1936, Serial No. 80,015. In Switzerland May 15, 1935 ICIaim.
This invention relates to a magnesium alloy which is to be used more particularly in the construction of internal combustion engines.
The magnesium alloys hitherto known are not suficiently resistant to corrosion and are not sufficiently hard, especially at the operating temperatures of the engine amounting to 200-300", and this results in excessive wear and inutility, for example of pistons.
Such drawbacks and other disadvantages are avoided according to the present invention, according to which one starts out from a magnesium-aluminium alloy with small silicon content with hardness raising addition of antimony, nickel, chromium and molybdenum, and the brittleness brought about by the addition is removed by choosing the aluminium content comparatively high and admixing copper and titanium with the alloy.
The magnesium alloy according to the present invention has the composition given below:-
Per cent Aluminium 14 18 Silir-nn 0.1 1
Antimony 3 8 Nickel 2 5 Chromium 0.05- 0.5 Manganese 0.1 l Molybdenum 0.05- 0.5 Copper- 6 8 Titanium 0.1 2
the rest being magnesium.
If desired up to 5 per cent. of steel material may be added in addition to such an alloy.
According as to whether the magnesium content is lower or higher within the said limits the alloy can be used either for pistons for internal combustion engines or for engine blocks, aircraft construction and so forth, particularly in consequence of its resistivity to corrosion and its specific gravity of about 1.8.
Whereas the alloys hitherto proposed in the best cases attained at ordinary temperature Brinell hardness of about 50, which sank to about 5 at 200-3002 experiments have shown that an alloy according to the invention shows at ordinary temperature a Brinell hardness exceeding 100, e. g. 120-130, and at 300 C. the still satisfactory hardness of 30.
' scored or corroded, and that the engine almost immediately started up again. Pistons subsequently removed were of mirror-like smoothness and the cylinder walls also were not scored or corroded in the'slightest. The benzine consumption fell very largely and the oil consumption was equal to zero.
Example In a steel crucible a flux is melted which serves at the same time both as a cleansing and a covering agent and which consists of a mixture of one part of potassium chloride and one part of magnesium chloride; the whole is thoroughly mixedand is cast into slabs.
In the heated crucible fiuxing agent to the extent of 3 to 8 per cent. of the charge is fused and thereupon magnesium is added. until the crucible is filled up to 5 cm. below the edge. According as the magnesium melts down the rest of the same is added.
Previously preliminary alloys are made in a suitable manner from the remaining alloy constituents, which alloys are then melted together to the so-called main preliminary alloy. This latter, preheated to -100", is added to the magnesium melt, in which it slowly dissolves. The fluxing agent rises to the surface during the fusion operation and covers the melt.
When everything is, liquid the whole is thoroughly stirred and heated to 800-850. The crucible is then removed from the furnace and allowed to cool for some minutes down to casting temperature (700-750"). Before casting the salts and impurities are preferably taken off with the casting ladle. Casting is eifected directly from the crucible with great care with the ladle as well. Preferably the stream being poured or cast is dusted with sulphur powder in order to prevent oxidation.
In order to make sand castings a special sand for magnesium is used which is moistened with a 20 per cent. aqueous ammonium fluoride solution.
The casting mould is preferably provided with a filter of core sand. The cores are made from red core sand, if desired mixed with 2 to 3' per cent. sulphur powder, and with the lowest possible linseed oil content. Before drying the cores have a 20 per cent. ammonium fluoride solution blown on them. Whenever possible all pieces are to be cast with rising.
The material can also be used in chill moulds and in the die-cast process.
I claim;
A magnesium alloy of the following composition:
v the rest magnesium.
FRITZ CHRISTEN.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH2065170X | 1935-05-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2065170A true US2065170A (en) | 1936-12-22 |
Family
ID=4567362
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US80015A Expired - Lifetime US2065170A (en) | 1935-05-15 | 1936-05-15 | Magnesium alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2065170A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2823996A (en) * | 1953-08-03 | 1958-02-18 | Gardner Daniel | Magnesium alloy |
-
1936
- 1936-05-15 US US80015A patent/US2065170A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2823996A (en) * | 1953-08-03 | 1958-02-18 | Gardner Daniel | Magnesium alloy |
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