US2194982A - Stable phosphide alloys of at least quaternary constituency - Google Patents
Stable phosphide alloys of at least quaternary constituency Download PDFInfo
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- US2194982A US2194982A US140580A US14058037A US2194982A US 2194982 A US2194982 A US 2194982A US 140580 A US140580 A US 140580A US 14058037 A US14058037 A US 14058037A US 2194982 A US2194982 A US 2194982A
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- phosphorus
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- quaternary
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- 229910045601 alloy Inorganic materials 0.000 title description 58
- 239000000956 alloy Substances 0.000 title description 58
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 41
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 38
- 229910052751 metal Inorganic materials 0.000 description 38
- 239000002184 metal Substances 0.000 description 38
- 235000014786 phosphorus Nutrition 0.000 description 27
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 26
- 229910052698 phosphorus Inorganic materials 0.000 description 26
- 239000011574 phosphorus Substances 0.000 description 26
- 229910052742 iron Inorganic materials 0.000 description 20
- 229910052759 nickel Inorganic materials 0.000 description 19
- 150000002739 metals Chemical class 0.000 description 17
- 239000000243 solution Substances 0.000 description 17
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 16
- 229910052802 copper Inorganic materials 0.000 description 16
- 239000010949 copper Substances 0.000 description 16
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 11
- 229910052799 carbon Inorganic materials 0.000 description 11
- 239000000126 substance Substances 0.000 description 11
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 10
- 229910052748 manganese Inorganic materials 0.000 description 10
- 239000011572 manganese Substances 0.000 description 10
- 229910052804 chromium Inorganic materials 0.000 description 7
- 239000011651 chromium Substances 0.000 description 7
- 239000000470 constituent Substances 0.000 description 7
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 6
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 6
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 6
- 150000001875 compounds Chemical class 0.000 description 6
- 230000007797 corrosion Effects 0.000 description 6
- 238000005260 corrosion Methods 0.000 description 6
- 238000003754 machining Methods 0.000 description 6
- 229910052710 silicon Inorganic materials 0.000 description 6
- 239000010703 silicon Substances 0.000 description 6
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 5
- 235000011167 hydrochloric acid Nutrition 0.000 description 5
- 229910052750 molybdenum Inorganic materials 0.000 description 5
- 239000011733 molybdenum Substances 0.000 description 5
- 235000011149 sulphuric acid Nutrition 0.000 description 5
- 239000004615 ingredient Substances 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 239000006104 solid solution Substances 0.000 description 4
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 4
- 229910052721 tungsten Inorganic materials 0.000 description 4
- 239000010937 tungsten Substances 0.000 description 4
- 229910001096 P alloy Inorganic materials 0.000 description 3
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 3
- 230000035515 penetration Effects 0.000 description 3
- DPTATFGPDCLUTF-UHFFFAOYSA-N phosphanylidyneiron Chemical compound [Fe]#P DPTATFGPDCLUTF-UHFFFAOYSA-N 0.000 description 3
- 229920006395 saturated elastomer Polymers 0.000 description 3
- 229910002058 ternary alloy Inorganic materials 0.000 description 3
- 229910000640 Fe alloy Inorganic materials 0.000 description 2
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 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
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 238000005275 alloying Methods 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
- 229910052796 boron Inorganic materials 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- VAKIVKMUBMZANL-UHFFFAOYSA-N iron phosphide Chemical compound P.[Fe].[Fe].[Fe] VAKIVKMUBMZANL-UHFFFAOYSA-N 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229910017604 nitric acid Inorganic materials 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- 239000011135 tin Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052720 vanadium Inorganic materials 0.000 description 2
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 230000003750 conditioning effect Effects 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 238000005555 metalworking Methods 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000012466 permeate Substances 0.000 description 1
- 125000002743 phosphorus functional group Chemical group 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 239000001117 sulphuric acid 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
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/02—Alloys containing less than 50% by weight of each constituent containing copper
Definitions
- This invention relates to high phosphorus iron alloys distinguished by the quality of inherent resistance to both physical and chemical deteriorating influences encountered in the use of articles made therefrom; and particularly alalloy resistant to chemical deterioration and con-- sisting of a foundation metal, typified by iron, with a high proportion of phosphorus that converts at least a substantial portion of-thefoundationmetal into its phosphide, and a disembrittling or strengthening element, comprising a metal capable of combining with phosphorus to form its own phosphide also in solution in the alloy, and physically conditioning the alloy in were considered, and copper and chromium were.
- the presentapplication deals with alloys that are quaternary or more .complexthan quaternary. It has been found that while the ternary alloys are very resistant to attacks of corrosive influences, they are nevertheless, on long exposure 40 to concentrated strong acids, subject to intergranular corrosion which deteriorates them with respect to the special purposes for which they are made. Hence, under the present invention, I add to the iron, phosphided to the desired degree, a plurality of corrective metals, themselves noble or forming noble phosphides, which in their immune condition, dissolve in the crystals of the iron and one another and prevent, substantially or entirely, not only deterioration of the iron, but
- the invention proceeds upon the principle of forming alloys of quaternary or more complex constituency, in which two of the constituent elements are iron and phosphorus and. the 'additional two or more constituent elements are sev lected from the groupof elements, nickel, copper, u
- the foundation metal is made to also contain, in solution therewith, a third metal, a portion or all of which remains compounded with phosphorus when in solution and thus renders the alloy quaternary in constituency, or a fourth or even fifth additional metal, portions or all of which are compounded with phosphorus when in solution in the foundation metal, thus making alloys 7 more complex than quaternary, not only do these additional third, fourth or fifth metals leave the phosphided foundation metal properly conditioned physically, but ,the compounded or phosphided portions thereof are largely responsible for giving 'to the alloy exceptional resistance to severe chemical attack, as well as physical integrity
- alloys also leave the alloy with an initial chemical resistance proportional to the portions of the added metals that .become compounded with phosphorus. They also provide alloys in which, under prolonged severe chemical attack, the metallic portions of the exposed surface slowly yield toreaction until there is left a surface made up so largely of the compounded or phosphided constituents of the alloy as to cause a tapering oil of the rate of solution of even those alloys which are lower in percentages of the compounds or phosphides, until the continued rate of yield to chemical attack upon the newly exposed surface of the compounded ingredient in an alloy having a lower percentage of composition ingredients, drops 01! to approximately that of quaternary or more complex alloys having higher percentages of phosphide compounds.
- the objects of the invention may be realized in articlesor materials produced by casting, rolling, extruding, drawing or forging of the quaternary or more complex phosphide alloys having high resistance to a wide range of corrosive influences.
- the quaternary or more complex alloys of this 'invention'm-ay be made with any phosphorus content between 1.70% phosphorus,which forms a saturated solid solution of iron phosphide in iron (10.91% FeaP in iron), and a content of about 25% phosphorus which, in the instance of iron,
- Alloys containing from 5% to 50% of the quaternary or more complex phosphide compounds are capable of being processed by rolling or other metal working methods, while those alloys compounded with more than 50% of metal phosphides are best shaped by casting and finishing by machining or grinding.
- This alloy has a solution rate in all concentrations of sulphuric acid and hydrochloric acid, at all temperatures of .003 inch penetration per year.
- Another alloy of this group having only fair machining properties I identify as D-36003-C.” i: llgas a Rockwell hardness of 45 on the C scale.
- This alloy has a solution rate of .002 inch per year in all concentrations of sulphuric and hydrochloric acids, at all temperatures.
- the carbon, manganese and silicon are non-essentials.
- Rockwell hardness of this sample is 48 on the C scale and the solution rate in sulphuric and hy-.
- Solution rate of this alloy is .0018 inch per year in sulphuric and hydrochloric acids and a Rockwell hardness of 52 on the C scale.
- the carbon and manganese are non-essentials.
- Solution rate'of this alloy is .0032 inch penetra-- tion per year in nitric acid and its Rockwell hardness is 62 on the 0 scale.
- the carbon is merely an incident of essential elements. causes it to contribute refinement oi grain.
- Examples of alloys in the lower phosphorus group which have excellent machining and mechanical properties and are capable of being rolled or forged are those which are'designated F5"fand F-11,as follows: c
- Solution rate of this alloy in sulphuric and hydrochloric acids is .0038 inch per year and its Rockwell hardness is 20 on the C scale.
- Solution rate of this alloy is .006 inch penetration per year in nitric acid and its Rockwell hardness is 18 on the 0 scale.
- the alloys herein described maybe prepared by melting together the constituents of the alloy,
- the foundation metal in the non- .fused state is subjected to the reaction of high phosphorus alloys in the fused state and under conditions which will cause the high phosphorus fused alloys to enter into solution with the foundation metal and convert the latter into an alloy of all of the ingredients to a depth depending upon duration of submergence, heat of the bath and other conditions-which promote the reaction.
- a physically and chemically resistant iron phosphorus alloy comprising iron in a proportion of from about 35% to about 71%; phosphorus from about 1.70% to about 25%: nickel from about 6% to about 37% and in addition to said nickel, from about 5% to about 25% of one or more other nonferruginous corrective metals having the capacity of combining with phosphorus to form their own phosphides and the The manganese is in a proportion that phosphide, said other nonferruginous metals being taken from. the'list copper, chromium,
- molybdenum molybdenum, tungsten, manganese, titanium, tin,
- Alow. carbon, high phosphorus alloy having substantial resistance to both physical and chemical influences, said alloy being of at least quaternary constituency and comprising essentially,
- nickel about 24.27% and copper about 24.25%; each of said metals existing largely in the form of its phosphide and the nickel and copper phosno? nsmman woman.
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- Engineering & Computer Science (AREA)
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- Organic Chemistry (AREA)
- Electroplating And Plating Baths Therefor (AREA)
Description
Patented Mar. 26, 1940 UNITED STATE-S PATENT oFFIcE STABLE PHOSPHIDE ALLOYS OF AT LEAST QUATEBNARY CONSTITUENCY Boy Barnard McCaulcy, Chicago Heights, Ill.
No Drawing. Application May 3, 1937,
- Serial No. 140,580
12 Claims. ('01. 75-123) This invention relates to high phosphorus iron alloys distinguished by the quality of inherent resistance to both physical and chemical deteriorating influences encountered in the use of articles made therefrom; and particularly alalloy resistant to chemical deterioration and con-- sisting of a foundation metal, typified by iron, with a high proportion of phosphorus that converts at least a substantial portion of-thefoundationmetal into its phosphide, and a disembrittling or strengthening element, comprising a metal capable of combining with phosphorus to form its own phosphide also in solution in the alloy, and physically conditioning the alloy in were considered, and copper and chromium were.
given as elements typical of the many metals having the capacity to physically condition high phosphide alloys.
35 The presentapplication deals with alloys that are quaternary or more .complexthan quaternary. It has been found that while the ternary alloys are very resistant to attacks of corrosive influences, they are nevertheless, on long exposure 40 to concentrated strong acids, subject to intergranular corrosion which deteriorates them with respect to the special purposes for which they are made. Hence, under the present invention, I add to the iron, phosphided to the desired degree, a plurality of corrective metals, themselves noble or forming noble phosphides, which in their immune condition, dissolve in the crystals of the iron and one another and prevent, substantially or entirely, not only deterioration of the iron, but
50 the inter-granular corrosion to which ternary alloys are susceptible; the improvement resulta ing from this addition being due to the formation of finer grained alloys resulting in better intrametal solution, better grain envelopment and 55 more even distribution of the constituents of the chemical compound; also to the fact that a chemical compound of quaternary or more complex constituency produces a more complex and therefore more stable oxide space lattice? and to the fact that an alloy of inter-metallic compounds 5 and solid solutions gives the most stable form of alloy and one having a lower aflinity for oxygen than would follow from the rule of mere mixtures as distinguished from chemical compositions.
The invention proceeds upon the principle of forming alloys of quaternary or more complex constituency, in which two of the constituent elements are iron and phosphorus and. the 'additional two or more constituent elements are sev lected from the groupof elements, nickel, copper, u
chromium, molybdenum, tungsten, manganese, titanium, tin, antimony, cobalt, lead, vanadium, zirconium and boron; these'additional elements being themselves noble or combined with 'phos: phorus to form noble phosphides and having the capacity of alloying with the foundation metal, iron and the phosphorus to form the complete phosphides; and the selection of these additional elements being governed by the suitability with respect to the physical or chemical properties be- 25 stowed by their phosphides upon the resultant alloys, considering the uses to which the alloys are to be put.
Numerous experiments prove that the improved chemical resistance bestowed upon metal prod- 3n ucts by the present invention is largely contributed by those proportions of the added metals that remain compounded with phosphorus in the alloy. Hence, if instead of a ternary alloy, consisting merely of iron, phosphorus 'and a metal which physically conditions iron 'phosphide, the foundation metal is made to also contain, in solution therewith, a third metal, a portion or all of which remains compounded with phosphorus when in solution and thus renders the alloy quaternary in constituency, or a fourth or even fifth additional metal, portions or all of which are compounded with phosphorus when in solution in the foundation metal, thus making alloys 7 more complex than quaternary, not only do these additional third, fourth or fifth metals leave the phosphided foundation metal properly conditioned physically, but ,the compounded or phosphided portions thereof are largely responsible for giving 'to the alloy exceptional resistance to severe chemical attack, as well as physical integrity. They also leave the alloy with an initial chemical resistance proportional to the portions of the added metals that .become compounded with phosphorus. They also provide alloys in which, under prolonged severe chemical attack, the metallic portions of the exposed surface slowly yield toreaction until there is left a surface made up so largely of the compounded or phosphided constituents of the alloy as to cause a tapering oil of the rate of solution of even those alloys which are lower in percentages of the compounds or phosphides, until the continued rate of yield to chemical attack upon the newly exposed surface of the compounded ingredient in an alloy having a lower percentage of composition ingredients, drops 01! to approximately that of quaternary or more complex alloys having higher percentages of phosphide compounds. As a result of this, where exact sizes on machined surfaces are not a factor, alloys of lower percentages of composition ingredients (phosphided metals) can be made to build up excellent resistance to the "most severe corrosive influences. The importance of these points will be appreciated when it is recognized that in a coarsegrain ternary phosphide alloy, inter-granular corrosion would to a large extent lower chemical resistance by loosening and removing compounded surface constituents and establishing progressive corrosion of the metallic constituents, whereas in the present invention initial corrosion merely exposes a new compounded surface substantially immune to corrosion.
The objects of the invention may be realized in articlesor materials produced by casting, rolling, extruding, drawing or forging of the quaternary or more complex phosphide alloys having high resistance to a wide range of corrosive influences.
The quaternary or more complex alloys of this 'invention'm-ay be made with any phosphorus content between 1.70% phosphorus,which formsa saturated solid solution of iron phosphide in iron (10.91% FeaP in iron), and a content of about 25% phosphorus which, in the instance of iron,
would form the compound FezP. Similarly, 7.09% of copper phosphide (CuaP) in which the phosphorus is 1.00%, will dissolve in and form a saturated solid solution with copper. And so with other metals.
Alloys containing from 5% to 50% of the quaternary or more complex phosphide compounds are capable of being processed by rolling or other metal working methods, while those alloys compounded with more than 50% of metal phosphides are best shaped by casting and finishing by machining or grinding.
An alloy of the higher phosphorus type, which I identify as D36001--A" and which has very 'good mechanical and machining properties and a Rockwell hardness of 26 on the C scale, analyzed, including the desirable but not indispensable manganese and the carbon and silicon nonessentials or impurities, is-
Per cent Carbon .08 Manganese 13 .Si1icon .08 Phosphorus 6. 38 Nickel- 24.27 Copper 24 .25 Iron-..- 44. 78
This alloy has a solution rate in all concentrations of sulphuric acid and hydrochloric acid, at all temperatures of .003 inch penetration per year.
Another alloy of an allied group of metals which I distinguish by the arbitrary mark "B-l and which has good machining properties and a Rockwell hardness of 36 on the C scale, is-
Per cent Carbon .29 Manganese .14 Sulphur .03 Silicon .12 Phosphorus 23.88 Nickel 8.79 Copper 5.85 Iron 82.78
The solution rateof this alloy is .0045 inch per year in sulphuric and hydrochloric acids. The
carbon, manganese, sulphur and silicon existing in fractions of 1% are believed not to materially lend to or aifect properties bestowed by themvention. I
Another alloy of this group having only fair machining properties I identify as D-36003-C." i: llgas a Rockwell hardness of 45 on the C scale.
Per cent Carbon .14 Manganese .48 Silicon .15 Phosphorus 10.01 Nickel 38.54 Copper 11.72 Iron 40.98
This alloy has a solution rate of .002 inch per year in all concentrations of sulphuric and hydrochloric acids, at all temperatures. The carbon, manganese and silicon are non-essentials.
Alloys embodying the essentials of the foregoing formulas together with additional elements but which are not capable of machining and must be shaped by grinding, are illustrated by the three following typical examples. designated, respectively, as "M-2, 5-F-1" and I -360187, to-wit:
ill-2 Per cent Carbon .15 Manganese .12 Phosphorus 14.81 Nickel 35.49 Copper 9.34
. Tungsten 2.18 Iron 38.03
Rockwell hardness of this sample is 48 on the C scale and the solution rate in sulphuric and hy-.
Solution rate of this alloy is .0018 inch per year in sulphuric and hydrochloric acids and a Rockwell hardness of 52 on the C scale. The carbon and manganese are non-essentials.
Solution rate'of this alloy is .0032 inch penetra-- tion per year in nitric acid and its Rockwell hardness is 62 on the 0 scale. In this formula the carbon is merely an incident of essential elements. causes it to contribute refinement oi grain.
Examples of alloys in the lower phosphorus group which have excellent machining and mechanical properties and are capable of being rolled or forged are those which are'designated F5"fand F-11,as follows: c
Per cent Carbon .09 Manganese 37 Silicon .12 Phosphorus 2.96 Nickel 23.15 Copper 20.07 Iron 53.34
Solution rate of this alloy in sulphuric and hydrochloric acids is .0038 inch per year and its Rockwell hardness is 20 on the C scale.
Solution rate of this alloy is .006 inch penetration per year in nitric acid and its Rockwell hardness is 18 on the 0 scale.
The alloys herein described maybe prepared by melting together the constituents of the alloy,
in which case a homogeneous alloy will result. Or they may be prepared by the process of my Letters Patent No. 2,007,978, issued July 16, 1935,.
in which case the foundation metal in the non- .fused state is subjected to the reaction of high phosphorus alloys in the fused state and under conditions which will cause the high phosphorus fused alloys to enter into solution with the foundation metal and convert the latter into an alloy of all of the ingredients to a depth depending upon duration of submergence, heat of the bath and other conditions-which promote the reaction.
What is claimed is:
1. A physically and chemically resistant iron phosphorus alloy comprising iron in a proportion of from about 35% to about 71%; phosphorus from about 1.70% to about 25%: nickel from about 6% to about 37% and in addition to said nickel, from about 5% to about 25% of one or more other nonferruginous corrective metals having the capacity of combining with phosphorus to form their own phosphides and the The manganese is in a proportion that phosphide, said other nonferruginous metals being taken from. the'list copper, chromium,
molybdenum, tungsten, manganese, titanium, tin,
antimony, cobalt, lead, vanadium, zirconium and 6- boron; a substantial proportion of each metal of-the alloy being in solution therein in the form of its own phosphide.
2. The alloy described in claim 1 when the proportion of phosphorus combinedwith each metal of the alloy produces the eutectic phosphide of said metal'and the solution of the said phosphide in the metal itself is a saturated solu-' tion.
. 3. A high phosphorus iron alloy as describedin claim 1 in which the proportions of the phosphides of" the corrective metals exceed those which the iron'phosphide will contain in solid solution and such phcsphides largely permeate the. grain-boundaries of the iron phosphide.
4..A'lhigh phosphoru's'alloy as described in claim 1 in which the nonferrugin'ous corrective metals other than nickel comprised in the alloy are copper and one of the metals molybdenum or tungsten. c 5. An allo'y as described in claim 1 in which" the nonferruginous corrective metals other than nickel comprise copper and molybdenum of which the molybdenum is in. aproportion of about 1.42%;of the alloy.
6. An alloy as described in claim 1 in which the nonferruginous corrective metal other than nickel comprises-chromium.
7. An alloy as described in claim 1 in which the nonferruginous corrective metal other than nickel comprises chromium from about 17% to about 19%.
8. An alloy as described in claim 1 in which the nonferruginous corrective metal other than nickel comprises chromium in a proportion of a about 17% and manganese in a proportion of about 2%. f Y
9. An alloy as described in claim l-in which the iron is about 70.54%; the phosphorus'is about 2.43%; the nickel is about 8.31% and the nonferruginous corrective metal other than nickel comprises chromium about 18.26%.
10 An alloy as described in claim 1, in which the, non-ferruginous corrective metals comprise nickel in a proportion of from about 6% to about u 37%; and copper in a proportion of fromabout, '5%toabout25%.' I v v 1 11. An alloy as described in claim 1, in which the iron is" from about 44% to 54%; the phosphorus is from about 3% to about 1%: and the nonferruginous corrective metals comprise nickel in a proportion "of from about 24 to about 25% and copper in a proportion of from about 20% to about25%.. Y r
12. Alow. carbon, high phosphorus alloy having substantial resistance to both physical and chemical influences, said alloy being of at least quaternary constituency and comprising essentially,
iron about 44.76%;phosphorus about 6.88%:
nickel about 24.27% and copper about 24.25%; each of said metals existing largely in the form of its phosphide and the nickel and copper phosno? nsmman woman.
3 capacity of alloying with the nickel and with m
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US140580A US2194982A (en) | 1937-05-03 | 1937-05-03 | Stable phosphide alloys of at least quaternary constituency |
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US140580A US2194982A (en) | 1937-05-03 | 1937-05-03 | Stable phosphide alloys of at least quaternary constituency |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2427517A (en) * | 1943-09-18 | 1947-09-16 | Lincoln Electric Co | Method of making an electrical contact member containing commingled copper and steel |
US2462056A (en) * | 1945-04-19 | 1949-02-15 | Roy B Mccauley | Hard alloys |
US2864693A (en) * | 1956-04-24 | 1958-12-16 | Coast Metals Inc | Brazing alloys |
-
1937
- 1937-05-03 US US140580A patent/US2194982A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2427517A (en) * | 1943-09-18 | 1947-09-16 | Lincoln Electric Co | Method of making an electrical contact member containing commingled copper and steel |
US2462056A (en) * | 1945-04-19 | 1949-02-15 | Roy B Mccauley | Hard alloys |
US2864693A (en) * | 1956-04-24 | 1958-12-16 | Coast Metals Inc | Brazing alloys |
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