US1051380A - Manufacture of armor-plates. - Google Patents
Manufacture of armor-plates. Download PDFInfo
- Publication number
- US1051380A US1051380A US61378711A US1911613787A US1051380A US 1051380 A US1051380 A US 1051380A US 61378711 A US61378711 A US 61378711A US 1911613787 A US1911613787 A US 1911613787A US 1051380 A US1051380 A US 1051380A
- Authority
- US
- United States
- Prior art keywords
- plate
- manufacture
- plates
- armor
- final
- 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
- 238000004519 manufacturing process Methods 0.000 title description 10
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- 229910000831 Steel Inorganic materials 0.000 description 4
- 238000001816 cooling Methods 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- 238000010009 beating Methods 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 239000011651 chromium Substances 0.000 description 2
- 235000019628 coolness Nutrition 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229910000669 Chrome steel Inorganic materials 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 239000004568 cement Substances 0.000 description 1
- 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 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- -1 venadium Chemical compound 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/02—Pretreatment of the material to be coated
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D7/00—Modifying the physical properties of iron or steel by deformation
- C21D7/02—Modifying the physical properties of iron or steel by deformation by cold working
- C21D7/04—Modifying the physical properties of iron or steel by deformation by cold working of the surface
- C21D7/06—Modifying the physical properties of iron or steel by deformation by cold working of the surface by shot-peening or the like
Definitions
- This invention relates to the manufacture of armor plates that are composed of nickel steel alloyed with one or more of the metals chromium, venadium, tantalum, molybdenum, etc., and that are subjected during their manufacture to heat treatment, such as for example-that disclosed in the specification of the prior British Patent No. 4,328 of the year 1893.
- the chief objectot' the invention is to improve the structure of the back portion of the plate so that its resisting power in attack will be strengthened, thus rendering the plate particularly suitable for resisting penetration bycappecl projectiles.
- the plate. after having been rolled and annealed in the usual manner, is subjected to cementa tion on both sides; then after treatment by known methods adopted in the manufacture of armor plates such for example as that hereinafter set forth, and after machining,
- the said plate is finally'hardened on each side in succession, the final hardenings being effected at the appropriate final face hardening temperature; the side that is last hardened constituting the face proper of the plate when in its finished condition.
- An intermediate low heat (1100 F. to 1250" F.) may be given to plates of high carbon percentage, between the two final hardenings.
- the effect of heating for the second final hardening is to reduce the extreme hardness of the back portion of the plate produced by the first final hardening and to leave it considerably improved as regards tensile strength without materially affecting the tensile strength of the middle portion ofthe plate. 1
- the steel referred to contains to .a per cent. of carbon, .3 to .& per cent. of manganese, 3.7 to 3.9 per cent. of nickel, and 1.7 to 2 percent. of chromium.
- a plate of this steel after being rolled and annealed is subjected to cementation in the ordinaryinanner, ex cept that it is cement ed on the face and the back simultaneously, instead of on the face only as is usual.
- ce nentation for the requisite time which varies with the thickness of the plate, amounting to from about fifteen days for a six inch plate to about eighteen days for a twelve inch plate, the cemented plate is heated to from 1450 F. to 1550 F. and bent to shape while hot.
- the plate is placed on asand bed with the back upward and is differentially hardened to a depth "of about two thirds the thickness of the plate. After bein sprinkled in the regular way it will be found that the face proper is concave. The plate is then again bedded on sand with the face proper upward this time, and is finally differentially hardened in the known manner, thereby llllparting to the face proper a hardened layer of about 1%- inches to 1%;- inches thickness for a six inch plate and about 2 to 3 inches for thicker plates.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
Description
"Jill'ALIl, a subject of the King Britain residing at Highfield Hall, Ches tel-field, in the county'of Derby, England,
ill
ATENT OFFICE.
JOHN LAWRENCE BENTHALL, OF CHESTERFIELD, ENGLAND, ASSIGNOR T0 VICKERS,
LIMITED, OF WESTMINSTER, ENGLAND.
MANUFACTURE OF ARMOR-PLATES.
aosnaso. I v
NoDrawing.
Specification of Letters Patent.
Patented Jan. 28. 1
To all whom 1' it may concern Belt known that 1, JOHN Lswnnn on BEN- of' Great have invented certain new and useful Improvements in the Manufacture of Armor- Plates, of which the following is a specification. v
This invention relates to the manufacture of armor plates that are composed of nickel steel alloyed with one or more of the metals chromium, venadium, tantalum, molybdenum, etc., and that are subjected during their manufacture to heat treatment, such as for example-that disclosed in the specification of the prior British Patent No. 4,328 of the year 1893.
The chief objectot' the invention is to improve the structure of the back portion of the plate so that its resisting power in attack will be strengthened, thus rendering the plate particularly suitable for resisting penetration bycappecl projectiles.
According to this invention, the plate. after having been rolled and annealed in the usual manner, is subjected to cementa tion on both sides; then after treatment by known methods adopted in the manufacture of armor plates such for example as that hereinafter set forth, and after machining,
the said plate is finally'hardened on each side in succession, the final hardenings being effected at the appropriate final face hardening temperature; the side that is last hardened constituting the face proper of the plate when in its finished condition. An intermediate low heat (1100 F. to 1250" F.) may be given to plates of high carbon percentage, between the two final hardenings. The effect of heating for the second final hardening is to reduce the extreme hardness of the back portion of the plate produced by the first final hardening and to leave it considerably improved as regards tensile strength without materially affecting the tensile strength of the middle portion ofthe plate. 1
In order that the invention may be clearly understood and readily carried into effect, 1 will describe the same more fully with reference to a specific method of manufacturing an armor plate from nickel chrome steel being understood that the invention isnot restricted to steel of this particular composition or to thedetail's of the method of manufacture set forth. v A
The steel referred to contains to .a per cent. of carbon, .3 to .& per cent. of manganese, 3.7 to 3.9 per cent. of nickel, and 1.7 to 2 percent. of chromium. A plate of this steel after being rolled and annealed is subjected to cementation in the ordinaryinanner, ex cept that it is cement ed on the face and the back simultaneously, instead of on the face only as is usual. After being subjected to ce nentation for the requisite time which varies with the thickness of the plate, amounting to from about fifteen days for a six inch plate to about eighteen days for a twelve inch plate, the cemented plate is heated to from 1450 F. to 1550 F. and bent to shape while hot. ,'It is then heated to from 1560 F. to 1620" F. andoil hardened in the ordinary way. The plate is then heated to from 1200 F. to 1350 F. and cooled in air on supports. It is then heated to from 1100 F. to 1250 F. according to the amount of carbon in its composition and is then sprinkled with water and cooled down to the atmospheric temperature. The plate is then machined and drilled where necessary prior to the final hardenings.
To perform the final hardenings the plate is placed on asand bed with the back upward and is differentially hardened to a depth "of about two thirds the thickness of the plate. After bein sprinkled in the regular way it will be found that the face proper is concave. The plate is then again bedded on sand with the face proper upward this time, and is finally differentially hardened in the known manner, thereby llllparting to the face proper a hardened layer of about 1%- inches to 1%;- inches thickness for a six inch plate and about 2 to 3 inches for thicker plates. It will also be found that this second final hardening, namely that applied to the face proper, has resulted in the hardness of the back, which has been hardened to a depth of about two thirds the thickness of the plate, as abovementioned, being drawn out by the second difierential hardening, but the structure of the back will with a tensile strength very much greater than before. The two final hardenings,
namely those upon the back and face respectively, are of course efi'ected by raising- What I claim and desire to secure by Let-- -ters Patent of the United States is 1. In the-manufacture of armor plates, subjecting both sides ofthe plate to cementation, then subjecting the cemented plate to successive beatings and coolings, and subsequently subjecting the plate to final hardenin on each side in succession.
plate, subjecting tofinal hardening on each side 11131100851011.
3. In the manufacture of armor plates,
rollingand annealing the plate, sub ecting it to cementat-ion on both sides, heati it to. a temperature suitable for voil hardening,
cooling 1t with oil, heating it to a temperature suitable for air hardening,'cooling it in air, heating it to a. temperature suitable In testimony whereof I afiix In y sigma-- the manufacture of armor plates, l ture in presence of two witnesses.
subjecting both sides of'the plate to cementation simultaneously, then subjecting the cemented plate to successive beatings and coolings and then, after machining said JOHN LAWRENCE BENTHALL.
lVit-nesses:
HENRY KING, ALFRED Pmxs.
' 0071.! of thin potent may be obtained for five cents each, by addressing the f Commissioner of Patents,
Washington, D. 0.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US61378711A US1051380A (en) | 1911-03-11 | 1911-03-11 | Manufacture of armor-plates. |
| US682734A US1051799A (en) | 1911-03-11 | 1912-03-09 | Manufacture of armor-plates. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US61378711A US1051380A (en) | 1911-03-11 | 1911-03-11 | Manufacture of armor-plates. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1051380A true US1051380A (en) | 1913-01-28 |
Family
ID=3119643
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US61378711A Expired - Lifetime US1051380A (en) | 1911-03-11 | 1911-03-11 | Manufacture of armor-plates. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1051380A (en) |
-
1911
- 1911-03-11 US US61378711A patent/US1051380A/en not_active Expired - Lifetime
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