[go: up one dir, main page]

US1713766A - Alloy - Google Patents

Alloy Download PDF

Info

Publication number
US1713766A
US1713766A US621663A US62166323A US1713766A US 1713766 A US1713766 A US 1713766A US 621663 A US621663 A US 621663A US 62166323 A US62166323 A US 62166323A US 1713766 A US1713766 A US 1713766A
Authority
US
United States
Prior art keywords
alloy
beryllium
chromium
iron
alloy containing
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
Application number
US621663A
Inventor
George G Marshall
Harold S Booth
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US621663A priority Critical patent/US1713766A/en
Application granted granted Critical
Publication of US1713766A publication Critical patent/US1713766A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium

Definitions

  • the present invention relates to an alloy containing chromiun'r and beryllium and iron, which possesses many properties which make it of great utility in the arts.
  • Chromium alloys as a rule are quite heavy, that is to say, they are of high specific gravity, and by the alloying of beryllium with chromium the specific gravity of the resultant alloy is materially decreased so that structures fabricated from the alloy possess all the desirable qualities inherent in the chromium, but are much lighter than where .the alloy is made of the usual chromium alloys.
  • the beryllium content may be increased to the maximum with corresponding reduction of iron and chromium content.
  • the presence of the beryllium produces an alloy of lower specific gravity than would be the case if the beryllium were not present, and in addition the beryllium and chromium performs certain other useful functions in the alloy, which makes its presence desirable, as for instance, the beryllium and chromium forms a skin oxide or compound chromate upon the out side of the alloy which is very adherent and protects the underlying metal against deterioration, due to a further oxidation, which is important, particularly where the article which is fabricated out of the alloy is subj ect to repeated heating and cooling, and the temperature to which it is heated is comparatively high, which would tend to induce oxidizing effects.
  • the chromium, beryllium, iron-alloy exhibits the property of nonwarping even when repeatedl heated and cooled. This is an important eature, and makes the alloy particularly useful in all those places where a structure is required to withstand repeated beatings and coolings, and is also sub ect to high temperature.
  • a very important property of this alloy is its resistance to corrosion, due to acids as well as alkalies. As is Well known, the hot dilute forms of the various acids are exceedingly corroding in their actions upon most metals.
  • the alloy containing beryllium and chromium and iron, is exceedingly resistant to acids and alkalies. This fact, coupled with Application filed February 27, 1923. Serial No. 621,663.
  • the ferro-chrome where ferro-chrome is used as the basis of the alloy is heated in the electric furnace to fusion and beryllium is added, the beryllium usually being added shortly before the batch of alloy is poured from the furnace, at which time it is desirable to add a small quantity of silicon in order to produce greater fluidity and secure an easy pouring of the batch.
  • the amount of silicon used is very small, and should not appear in the final alloy in greater quantities than 1 per cent, as the silicon tends to make the alloy grainy, and decreases its tensile strength.
  • chromium and beryllium While the above proportions are considered to produce the best results, for certain purposes higher percentages of chromium and beryllium may be used. For example, an increase in the chromium content up to 20% raises the melting point and resistance to oxidation. The upper limits of the chromium and beryllium content have been found to be chromium substantially 42%, iron 46% and beryllium 12%. This alloy, however, is extremely brittle and hard to work but has great resistance to oxidation and is useful for its nonwarping qualities and may be advantageously used in carbonizing boxes and other articles which are required to withstand high temperatures.
  • An alloy having proportions of chromium, iron and beryllium within the limits above specified has a very high melting point, in the neighborhod of 2500 F and from this springs its ability to withstand high temperatures.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Soft Magnetic Materials (AREA)

Description

Patented May Zll, W2
GEORGE G. MARSHALL AND HAROLD S. BOOTH, OF CLEVELAND, OHIO.
ALLOY.
No Drawing.
The present invention relates to an alloy containing chromiun'r and beryllium and iron, which possesses many properties which make it of great utility in the arts.
Chromium alloys as a rule are quite heavy, that is to say, they are of high specific gravity, and by the alloying of beryllium with chromium the specific gravity of the resultant alloy is materially decreased so that structures fabricated from the alloy possess all the desirable qualities inherent in the chromium, but are much lighter than where .the alloy is made of the usual chromium alloys. v
It is obvious where the lightness of the resistant alloy is of special advantage, that the beryllium content may be increased to the maximum with corresponding reduction of iron and chromium content.
In all of the instances which have just been mentioned, the presence of the beryllium produces an alloy of lower specific gravity than would be the case if the beryllium were not present, and in addition the beryllium and chromium performs certain other useful functions in the alloy, which makes its presence desirable, as for instance, the beryllium and chromium forms a skin oxide or compound chromate upon the out side of the alloy which is very adherent and protects the underlying metal against deterioration, due to a further oxidation, which is important, particularly where the article which is fabricated out of the alloy is subj ect to repeated heating and cooling, and the temperature to which it is heated is comparatively high, which would tend to induce oxidizing effects.
The chromium, beryllium, iron-alloy exhibits the property of nonwarping even when repeatedl heated and cooled. This is an important eature, and makes the alloy particularly useful in all those places where a structure is required to withstand repeated beatings and coolings, and is also sub ect to high temperature.
A very important property of this alloy is its resistance to corrosion, due to acids as well as alkalies. As is Well known, the hot dilute forms of the various acids are exceedingly corroding in their actions upon most metals. The alloy containing beryllium and chromium and iron, is exceedingly resistant to acids and alkalies. This fact, coupled with Application filed February 27, 1923. Serial No. 621,663.
the fact that the alloy containing beryllium produces a lighter alloy than the irorr or chromium alloy alone, marks an important property, inasmuch as the usual forms of acid containers or conductors wherein iron and chromium are used as the basis of the alloy, are exceedingly heavy, and where, as in the present instant, the resultant alloy contaming beryllium is much lighter, the importance of this property will be appreciated.
In making the alloy, the ferro-chrome where ferro-chrome is used as the basis of the alloy, is heated in the electric furnace to fusion and beryllium is added, the beryllium usually being added shortly before the batch of alloy is poured from the furnace, at which time it is desirable to add a small quantity of silicon in order to produce greater fluidity and secure an easy pouring of the batch. The amount of silicon used is very small, and should not appear in the final alloy in greater quantities than 1 per cent, as the silicon tends to make the alloy grainy, and decreases its tensile strength.
The desired properties of the alloy are best exhibited in an alloy containing chromium 4% to 6% beryllium 2% to 10% and iron approximately As a specific example of an alloy produced and having the desired qualities, we would give the followmg:
Chromium 6%, iron 90%, beryllium 4%.
While the above proportions are considered to produce the best results, for certain purposes higher percentages of chromium and beryllium may be used. For example, an increase in the chromium content up to 20% raises the melting point and resistance to oxidation. The upper limits of the chromium and beryllium content have been found to be chromium substantially 42%, iron 46% and beryllium 12%. This alloy, however, is extremely brittle and hard to work but has great resistance to oxidation and is useful for its nonwarping qualities and may be advantageously used in carbonizing boxes and other articles which are required to withstand high temperatures.
An alloy having proportions of chromium, iron and beryllium within the limits above specified has a very high melting point, in the neighborhod of 2500 F and from this springs its ability to withstand high temperatures.
This application is in part a continuation of our co-pending application Serial No. 278,822, filed February 24, 1919.
Having described our invention, we claim:
5 1. An alloy containing beryllium, iron and chro ium in substantially the following proportions ;-beryllium 2% to 12%, iron 46% to 90%,chromium 4% to 42%.
2. An alloy containing beryllium, iron and 10 chromium in substantially the following proportions beryllium 2% to 10%, iron 90%, chromium 4% to 6%.
3. An alloy containing beryllium, iron and chromium in substantially the following proportions beryllium 4%, iron 90%, chr0- mium 4%.
In testimony whereof, we our signatures.
HAROLD S. BOOTH. GEORGE G. MARSHALL.
hereunto aflix
US621663A 1923-02-27 1923-02-27 Alloy Expired - Lifetime US1713766A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US621663A US1713766A (en) 1923-02-27 1923-02-27 Alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US621663A US1713766A (en) 1923-02-27 1923-02-27 Alloy

Publications (1)

Publication Number Publication Date
US1713766A true US1713766A (en) 1929-05-21

Family

ID=24491097

Family Applications (1)

Application Number Title Priority Date Filing Date
US621663A Expired - Lifetime US1713766A (en) 1923-02-27 1923-02-27 Alloy

Country Status (1)

Country Link
US (1) US1713766A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3188732A (en) * 1960-01-14 1965-06-15 Westinghouse Electric Corp Diffusion-bonding of metal members

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3188732A (en) * 1960-01-14 1965-06-15 Westinghouse Electric Corp Diffusion-bonding of metal members

Similar Documents

Publication Publication Date Title
US2137281A (en) Copper alloys
US1713766A (en) Alloy
US1641752A (en) Oxidation-resisting material
US1892316A (en) Noncorrosive steel alloy
US1942261A (en) Alloy
US2169188A (en) Copper base alloy
US1538337A (en) Alloy
US1759477A (en) Alloy of high surface stability comprising nickel and silicon
US1538360A (en) Malleable noncorrodible alloy
US935863A (en) Alloy and process for its production.
US2007430A (en) Copper alloy
US2210673A (en) Copper base alloy
US1932838A (en) Aluminum alloys
US1932843A (en) Aluminum alloys
US1389133A (en) Heat-resisting alloy
US1273762A (en) Alloy.
US2169189A (en) Copper base alloy
US3350197A (en) Ferrosilicon alloys
US1508032A (en) Corrosion-resisting ferrous alloy
US2169187A (en) Copper base alloy
US1839089A (en) Stable surface alloy steel
US2210672A (en) Copper base alloy
US1431725A (en) Titanium alloy
US1932840A (en) Aluminum alloys
US1850416A (en) Art of metallurgy