US3218199A - Process for hardening metals using explosive means - Google Patents
Process for hardening metals using explosive means Download PDFInfo
- Publication number
- US3218199A US3218199A US306650A US30665063A US3218199A US 3218199 A US3218199 A US 3218199A US 306650 A US306650 A US 306650A US 30665063 A US30665063 A US 30665063A US 3218199 A US3218199 A US 3218199A
- Authority
- US
- United States
- Prior art keywords
- explosive
- steel
- layer
- metal sheet
- inch
- 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
- 229910052751 metal Inorganic materials 0.000 title claims description 54
- 239000002184 metal Substances 0.000 title claims description 54
- 239000002360 explosive Substances 0.000 title claims description 49
- 238000000034 method Methods 0.000 title claims description 28
- 150000002739 metals Chemical class 0.000 title claims description 9
- 238000005474 detonation Methods 0.000 claims description 13
- 230000000977 initiatory effect Effects 0.000 claims description 5
- 229910000831 Steel Inorganic materials 0.000 description 20
- 239000010959 steel Substances 0.000 description 20
- 229910000617 Mangalloy Inorganic materials 0.000 description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 8
- 239000000203 mixture Substances 0.000 description 8
- 230000035939 shock Effects 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 239000003999 initiator Substances 0.000 description 4
- 238000011068 loading method Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 229910052759 nickel Inorganic materials 0.000 description 4
- 239000004264 Petrolatum Substances 0.000 description 3
- 239000011248 coating agent Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- -1 ferrous metals Chemical class 0.000 description 3
- 239000013528 metallic particle Substances 0.000 description 3
- 229940066842 petrolatum Drugs 0.000 description 3
- 235000019271 petrolatum Nutrition 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 229910000851 Alloy steel Inorganic materials 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000010951 brass Substances 0.000 description 2
- 229910052758 niobium Inorganic materials 0.000 description 2
- 239000010955 niobium Substances 0.000 description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 241000167854 Bourreria succulenta Species 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- TZRXHJWUDPFEEY-UHFFFAOYSA-N Pentaerythritol Tetranitrate Chemical compound [O-][N+](=O)OCC(CO[N+]([O-])=O)(CO[N+]([O-])=O)CO[N+]([O-])=O TZRXHJWUDPFEEY-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229920005549 butyl rubber Polymers 0.000 description 1
- 235000019693 cherries Nutrition 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 238000011221 initial treatment Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 150000003505 terpenes Chemical class 0.000 description 1
- 235000007586 terpenes Nutrition 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Images
Classifications
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49805—Shaping by direct application of fluent pressure
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49805—Shaping by direct application of fluent pressure
- Y10T29/49806—Explosively shaping
Description
Nov. 16, 1965 G. R. COWAN ETAL 3,218,199
PROCESS FOR HARDENING' METALS USING EXPLOSIVE MEANS Original Filed June 23, 1960 INVENTORS GE E R. COWAN ARNOL .HOLTZMAN United States Patent 3,218,199 PROCESS FOR HARDENING METALS USING EXPLOSIVE MEANS George R. Cowan, Woodbury, and Arnold H. Holtzman, Cherry Hill Township, N.J., assignors to E. I. du Pont de Nemours and Company, Wihnington, DeL, a corporation of Delaware Continuation of application Ser. No. 87,053, Feb. 2, 1961, which is a continuation of application Ser. No. 38,261, June 23, 1960. This application Aug. 14, 1963, Ser. 306,650
7 Claims. (Cl. 1484) This application is a continuation of our application Serial No. 87,053, filed February 2, 1961, now abandoned, which in turn, is a continuation of our application Serial No. 38,261 filed June 23, 1960, now abandoned.
The present invention relates to a process for hardening metal surfaces.
In US. Patent 2,703,297 to N. A. MacLeod a process is described for hardening the surface of manganese steel. This process comprises placing a layer of explosive material contiguous to the surface to be hardened and detonating the explosive. This process is capable of providing a hardness of about 400 on the Vickers scale on the surface of manganese steel, this hardness gradually decreasing to a value of 200 Vickers at a depth below the surface of one inch. This process is quite satisfactory for many applications. However in other instances a greater increase in hardness, both in magnitude and in depth, than can be attained by this process is desirable.
We have found that we are able to harden metallic surfaces to a substantially greater degree and depth than has been heretofore possible when we position a metal sheet parallel to the surface to be hardened and separated therefrom by an air space, place a layer of explosiveon the outside surface of the said metal sheet, and initiate the explosive. Moreover, we have determined that through the use of the above-described process we are able to harden not only manganese steel, as described in the aforesaid MacLeod patent, but other steel alloys, such as stainless steel, vanadium steel and the like, and also non-ferrous metals and alloys thereof, such as nickel, niobium, cobalt, and their alloys.
A more completed understanding of the process of the present invention may be had by reference to the accompanying figure which is a schematic representation of an assembly for carrying out the hardening process. In the figure, 1 represents a supporting means of a shock-transmitting material, for example, alloy steel. The metallic specimen, the upper surface of which is to be hardened, is indicated by 2. 3 is a flexible metal sheet, for example, a brass or steel shim, that is supported above the surface of specimen 2 at a uniform spacing therefrom by small projections 7 in the surface of the sheet. The air space separating sheet 3 from the surface of the specimen is indicated at 8. 4 is a layer of explosive on the outer surface of sheet 3 and which preferably extends somewhat beyond the steel in at least one direction to provide a convenient portion for attachment of an electric initiator as at 5. Energy is carried to initiator 5 by lead wires 6.
The following examples further describe the process of our invention. They are illustrative only, however, and are not to be considered as limiting the invention in any manner. In all cases, unless otherwise specified, the explosive composition used was prepared by blending 85 parts of PETN, 7.5 parts of butyl rubber, and 7.5 parts of a thermoplastic terpene resin (mixture of polymers of fi-pinene having the formula (C H commercially available as Piccolyte S10 manufactured by the Penn- 3,Zl8,l99 Patented Nov. 16, 1965 sylvania Industrial Corporation), and rolling the blend into sheet, the thickness of the sheet determining the weight per unit area. The composition has a velocity of detonation of about 7200 meters per second, and the sheets are strong, flexible, and nonresilient. Compositions of this type and their preparation are described in detail in US. Patent 2,999,743 which is incorporated herein by reference.
EXAMPLE 1 A rectangular block of Hadfields manganese steel was placed on a supporting plate of stainless steel. A thin (0.002 in.) sheet of shim steel having dimension corresponding to those of the manganese steel block was cemented to a 0.165 inch-thick sheet of the abovedescribed explosive having a weight per unit area of 4 grams per square inch. Convex protrusions of 0.01 inch were located in the surface of the shim steel as a convenient means of providing the required air space. This composite layer was placed, shim-side down, on the steel block, and an electric initiator was taped to the explosive layer, and subsequently actuated. Before detonation of the explosive, the manganese steel had a uniform hardness of 200 Vickers; after detonation of the explosive the hardness at 0.005 inch below the surface was 550 Vickers an increase of 350 in the hardness value. The hardened surface was smooth and free of contamination by the shim layer. The hardness at 0.025 inch below the surface was 430 and at 0.035 inch 375. After a second treatment, following the same steps, the hardness of the Hadfields steel sample near the surface was not noticeably increased, the surface hardness obtained with the first shot being approximately the maximum hardness known for Hadfields steel. However, at a depth of 0.25 inch below the surface the hardness had been increased from a value of 280, obtained by the initial treatment, to a value of 380.
EXAMPLE 2 In experiments done for comparative purposes, the conditions of Example 1 were reproduced, i.e., the explosive and manganese steel sample were identical, however no thin layer of steel was employed, the explosive being placed directly on the surface to be hardened, as described in the aforementioned US. Patent 2,703,297 to MacLeod. After detonation of the explosive, the steel at a depth of 0.005 inch had a hardness value of 370 Vickers. At a depth of 0.025 inch the hardness was 320 and at 0.035 inch 310. Similarly, in other experiments, the surface hardness of a nickel specimen was observed to be only 200 when the explosive was detonated directly on the surface, whereas a surface hardness value of 310 Vickers was obtained when the technique of Example 1 was ap plied to a second nickel specimen.
EXAMPLE 3 The procedure of Example 1 was repeated except that the air space between the surface to be hardened and the thin flexible steel sheet was increased from 0.010 inch to 0.040 inch. The hardening eflect obtained was somewhat less than that obtained in Example 1. At a depth of 0.005 inch the hardness of the Hadfields steel was 460, and at 0.025 inch 380. When a gap of 0.020 inch was employed, hardening results intermediate between those from the gaps of 0.010 inch and 0.040 inch were obtained.
EXAMPLE 4 Table I, which follows, shows the results obtained with a series of shots carried out on Hadfields steel with various explosive loadings. The steel shim was 0.005 inch thick, and the air space was 0.020 inch.
3 Table I Viclrers hardness of Hadfields steel sample at depth of in. in. in. in
Explosive loading (g./sq. in.) O. 005 0. 075 0.150 0. 250 2 540 320 275 240 550 340 300 285 550 355 320 305 Thus it is apparent that, as the amount of explosive was increased, the degree, of the hardening effect also increased.
EXAMPLE 5 Table Ilf'which follows, shows the effect on the metal hardening of variations in thickness of the flexible steel shim. The explosive was that of Example 1, the metal sample wasl-ladfields steel, and the air space provided was 0.020 inch.
As indicated by the above example, the depth of the hardening effect is increased by an increase in the thickness of the flexible metal sheet. Consequently, by varying the thickness of this sheet and the mass of the explosive employed it is possible to exercise great control over the hardness profile of the metal or alloy.
As we have demonstrated in the foregoing examples, our process is applicable to both ferrous and non-ferrous metals and alloys, and the hardening effect which is achieved is surprisingly and materially increased over that which results when the evplosive is placed directly on the surface to be hardened according to prior known techniques. Moreover, we have shown that increasing hardcning at a substantial depth below the surface of the metal is achieved by successive shots in accordance with the novel process.
Naturally, the physical conditions requisite for optimum results will depend somewhat on the nature of the metallic surface to be hardened. Generally speaking, the greatest increase in hardness for any metallic surface will result when the air space provided is between 0.010 and 0.025 inch. As an alternative to the exemplified projections in the metal sheet, the air space may be provided by small metallic particles or other supporting means. Such alternatives are within the purview of the invention.
It is preferably that the metal sheet be flexible for reasons of facile contouring to surfaces of irregular configuration. Hence, its thickness will preferably not exceed a value of a few mils. Sometimes it is beneficial to lubricate the surface to be hardened slightly, e.g., by applying a thin coating of petrolatum, to insure against adherence of the thin metal sheet, although this is not usually necessary.
The thickness of the explosive layer will, of course, depend upon the depth of the hardening effect that is desired to be attained. The only maximum parameter imposed on the amount of explosive used, is that it must not be so great as to cause disintegration of the thin metal sheet or extensive deformation or fracture of the specimen. Obviously, the explosive layer must be of at least sufficient thickness to propagate a detonation. Usually, explosive loadings of about from 1 to grams per square 4 inch, corresponding to thicknesses of about from 40 to 420 mils, are employed.
We have determined that the detonation velocity of the explosive composition must exceed by at least 25% the sonic velocity of both the metal specimen to be hardened and the metal sheet adjacent the explosive for satisfactory hardening results, and this represents a critical feature of the invention. At lower detonation velocities, the hardening is substantially diminished, and the metal sheet invariably tends to adhere to the substrate despite efforts to discourage this, as for example, by the use of a lubricant described above. Those skilled in the art will recognize that the term sonic velocity of the metal referred to in this paragraph has somewhat different meanings in differing circumstances. For example, this term will have a different significance to the physicist when dealing with plastic shock wave phenomena in solids as contrasted with elastic shock wave phenomena. It is the former with which we are concerned for purposes or" the present invention. The term sonic velocity as used throughout this application in connection with metals and metallic compositions refers to the velocity of the plastic shock wave which forms when a stress which is applied just exceeds the elastic limit for unidimensional compression of the particular metal or metallic system involved. The value of this sonic velocity may be obtained by means of the relation.
V:\/K/d where V is the sonic velocity in cm./sec.; K is the adiabatic bulk modulus in dynes/cm. and d is the density in g./crn. Values of K may be obtained from values of Youngs modulus, E and Poissons ratio, 1/ by means of the relation Values of d and K or E and 1/ are readily available in the literature (see for example American Institute of Physics Handbook, McGraw-Hill, New York, 1957).
Alternatively, the sonic velocity may be ascertained from published values of the velocity of the plastic shock wave as a function of the particle velocity imparted to the metal by the shock wave in the manner described by R. G. McQueen and S. P. Marsh, Journal of Applied Physics 31 (7), 1253 (1960).
In those cases where literature data are unavailable, values of V may be obtained by carrying out shock wave measurements as described by R. G. McQueen and S. P. Marsh (loc. cit.) in the references cited by them. Alternatively, V may be ascertained from the relation where C is the velocity of elastic compressional waves and C is the velocity of elastic shear waves in the metal. The required velocities of the elastic waves may be measured by well-known methods. For illustration purposes, sonic velocity values as used herein for representative metals are set forth in the following table:
Metal: Sonic velocity, m./scc.
Zinc 3000 Copper 4000 Magnesium 4500 Niobium -Q 4500 Austenitic stainless steel 4500 Nickel 4700 Titanium 4800 Iron 4800 Molybdenum 5200 Aluminum 5500 The explosive layer may be initiated by any conventional means, and the positioning of the initiating means on the explosive layer is not critical. Thus, the layer of explosive may be initiated at a corner, in the center, or at any point along an edge. If desired, a line-wave initiator may be used to initiate simultaneously an entire edge of the explosive layer. In the Examples the explosive used was in the form of a coherent, flexible, self-supporting sheet, and this represents a preferred form of explosive for purposes of the present invention inasmuch as uniformity of loading and ease of application are greatly facilitated therewith. However, if desired, the explosive could be applied in a paste or gelled form, or could be in a packaged form suitable for this particular use. The explosive layer may be bonded to the metal sheet prior to the positioning of the metal sheet over the surface to he hardened or simply may be rested on the metal sheet after the metal sheet has been positioned.
No limitations are imposed on the dimensions or nature of the metallic specimen that may be hardened by the described process. Those metals whose ductility is so slight that they fracture after only a 5% or less elongation in tension are, in general, so brittle that they do not lend themselves readily to hardening. Thus, it is with those metals which may be elongated in tension to an extent greater than 5% without fracture that this inventiOn wil find its greatest utility.
Although We have illustrated the use of a steel block as a shock-transmitting support for the specimen, it is to be noted that such is not critical to the invention. Further, although We have exemplified, and for economic reasons generally prefer, steel as the material of the thin metal sheet, other materials, e.g., lead or brass, may be employed. The nature of the composition of the thin metal sheet is not critical; because it functions solely as an impact means its metallurgical properties are of little significance.
Having described our invention fully, we intend to be limited only by the following claims.
We claim:
1. A process for hardening metallic surfaces which comprises positioning a thin, flexible metal sheet parallel to the metal surface to be hardened and adjacent thereto but separated therefrom to provide an air space between said surface and said sheet, placing a layer of a detonating explosive on the exterior surface of said metal sheet, said layer of explosive having a velocity of detonation greater than about of the sonic velocity of the said metals, and initiating said explosive layer, the amount of said explosive being sufiicient to propagate a detonation but insufficient to disintegrate said metal sheet.
2. A process according to claim 1 wherein the said metallic surface is of a metal which can be elongated in tension to an extent greater than 5% without fracture.
3. A process according to claim 1 wherein the said metallic surface is austenitic manganese steel.
4. A process according to claim 3 wherein said metal sheet is a flexible sheet of steel.
5. The process of claim 1 wherein said air space is between about 0.010 and 0.025 inch in thickness.
6. The process of claim 1 wherein said air space is maintained prior to initiation of said explosive layer by scattering small metallic particles on said surface to be hardened prior to positioning said metal sheet and explosive layer thereover.
7. The process for hardening metallic surfaces which comprises applying a thin coating of petrolatum to the metal surface to be hardened, applying a plurality of small metal particles to said surface having said petrolatum coating, positioning a sheet of resilient metal parallel to said surface and spaced therefrom by said metallic particles a distance of about from 0.010 to 0.025 inch, placing a layer of detonating explosive on the exterior surface of said metal sheet, said layer of explosive having a velocity of detonation greater than about 125% of the sonic velocity of said metal sheet and said metal to be hardened, and initiating said explosive layer, the amount of said explosive being sutficient to propagate a detonation but insufiicient to disintegrate said metal sheet.
References Cited by the Examiner UNITED STATES PATENTS 1,440,601 1/1923 Holran 102-24 2,412,967 12/1946 Church et al. 891.02 2,628,559 2/1953 Jasse 10224 2,667,836 2/1954 Church et a1. 89-1.02 XR 2,703,297 3/1955 MacLcod 184-4 HYLAND BIZOT, Primary Examiner.
Claims (1)
1. A PROCESS FOR HARDENING METALLIC SURFACES WHICH COMPRISES POSITIONED A THIN, FLEXIBLE METAL SHEET PARALLEL TO THE METAL SURFACE TO BE HARDENED AND ADJACENT THERETO BUT SEPARATED THEREFROM TO PROVIDE AN AIR SPACE BETWEEN SAID SURFACE AND SAID SHEET, PLACING A LAYER OF A DETONATING EXPLOSIVE ON THE EXTERIOR SURFACE OF SAID METAL SHEET, SAID LAYER OF EXPLOSIVE HAVING A VELOCITY OF DETONATION GREATER THAN ABOUT 125% OF THE SONIC VELOCITY OF THE SAID METALS, AND INITIATING SAID EXPLOSIVE LAYER, THE AMOUNT OF SAID EXPLOSIVE BEING SUFFICIENT TO PROPAGATE A DETONATION BUT SUFFICIENT TO DISINTEGRATE SAID METAL SHEET.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US306650A US3218199A (en) | 1963-08-14 | 1963-08-14 | Process for hardening metals using explosive means |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US306650A US3218199A (en) | 1963-08-14 | 1963-08-14 | Process for hardening metals using explosive means |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3218199A true US3218199A (en) | 1965-11-16 |
Family
ID=23186237
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US306650A Expired - Lifetime US3218199A (en) | 1963-08-14 | 1963-08-14 | Process for hardening metals using explosive means |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3218199A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3624237A (en) * | 1968-09-23 | 1971-11-30 | Nitro Nobel Ab | Apparatus for bonding together metal sheets by explosive welding |
| US3726460A (en) * | 1971-07-29 | 1973-04-10 | Creative Metals Inc | Explosive bonding device |
| US3850698A (en) * | 1972-06-23 | 1974-11-26 | Ind Materials Ltd | Altering material properties |
| US3987529A (en) * | 1971-11-01 | 1976-10-26 | Asahi Kasei Kogyo Kabushiki Kaisha | Valve and method for manufacturing the same |
| US4401477A (en) * | 1982-05-17 | 1983-08-30 | Battelle Development Corporation | Laser shock processing |
| US6071357A (en) * | 1997-09-26 | 2000-06-06 | Guruswamy; Sivaraman | Magnetostrictive composites and process for manufacture by dynamic compaction |
| WO2016037231A1 (en) * | 2014-09-08 | 2016-03-17 | Bradken Resources Pty Limited | Explosive hardening of track shoes |
| US9719158B2 (en) | 2014-12-29 | 2017-08-01 | Progress Rail Services Corporation | Explosively depth hardened crawler shoes |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1440601A (en) * | 1921-01-06 | 1923-01-02 | John R Holran | Explosive charge |
| US2412967A (en) * | 1941-04-23 | 1946-12-24 | Joseph H Church | Petard missile |
| US2628559A (en) * | 1945-02-06 | 1953-02-17 | Ct D Etudes M B A Soc | Explosive drill |
| US2667836A (en) * | 1950-03-28 | 1954-02-02 | Joseph H Church | Apparatus for the use of shaped explosive charges |
| US2703297A (en) * | 1951-03-26 | 1955-03-01 | Kelly L Taulbee | Method of hardening manganese steel |
-
1963
- 1963-08-14 US US306650A patent/US3218199A/en not_active Expired - Lifetime
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1440601A (en) * | 1921-01-06 | 1923-01-02 | John R Holran | Explosive charge |
| US2412967A (en) * | 1941-04-23 | 1946-12-24 | Joseph H Church | Petard missile |
| US2628559A (en) * | 1945-02-06 | 1953-02-17 | Ct D Etudes M B A Soc | Explosive drill |
| US2667836A (en) * | 1950-03-28 | 1954-02-02 | Joseph H Church | Apparatus for the use of shaped explosive charges |
| US2703297A (en) * | 1951-03-26 | 1955-03-01 | Kelly L Taulbee | Method of hardening manganese steel |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3624237A (en) * | 1968-09-23 | 1971-11-30 | Nitro Nobel Ab | Apparatus for bonding together metal sheets by explosive welding |
| US3726460A (en) * | 1971-07-29 | 1973-04-10 | Creative Metals Inc | Explosive bonding device |
| US3987529A (en) * | 1971-11-01 | 1976-10-26 | Asahi Kasei Kogyo Kabushiki Kaisha | Valve and method for manufacturing the same |
| US3850698A (en) * | 1972-06-23 | 1974-11-26 | Ind Materials Ltd | Altering material properties |
| US4401477A (en) * | 1982-05-17 | 1983-08-30 | Battelle Development Corporation | Laser shock processing |
| US6071357A (en) * | 1997-09-26 | 2000-06-06 | Guruswamy; Sivaraman | Magnetostrictive composites and process for manufacture by dynamic compaction |
| WO2016037231A1 (en) * | 2014-09-08 | 2016-03-17 | Bradken Resources Pty Limited | Explosive hardening of track shoes |
| US9719158B2 (en) | 2014-12-29 | 2017-08-01 | Progress Rail Services Corporation | Explosively depth hardened crawler shoes |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3137937A (en) | Explosive bonding | |
| US3218199A (en) | Process for hardening metals using explosive means | |
| US3834881A (en) | Foamed metal article | |
| EP0324231B1 (en) | Improved method of making explosively bonded multi-laminar composite metal plate | |
| US2383511A (en) | Method of making same | |
| US5067649A (en) | Bonding metal components | |
| JPH01157785A (en) | Method of explosive-welding alloy aluminum | |
| US4120439A (en) | Method for welding by explosion of powder material on a firm surface | |
| US2818360A (en) | Method for the aluminum cladding of ferrous base metal and product thereof | |
| Meyers | Shock waves and high-strain-rate phenomena in metals: concepts and applications | |
| US3081498A (en) | Explosive method of powder compaction | |
| US3493353A (en) | Metal composites with low-melt content bonds | |
| US3238071A (en) | Process of treating explosively clad metals | |
| US3282743A (en) | Process for relieving residual stresses in metals | |
| Rohde et al. | The dynamic yield behavior of annealed and cold-worked Fe-0.17 pct Ti alloy | |
| JPS63166953A (en) | Blasting treatment for hot dip galvanized-type steel sheet | |
| Inoue et al. | Texture, tensile properties and press formability of Mg-3Al-1Zn/Ti clad sheets produced by roll-bonding | |
| Mamalis et al. | A consolidation mechanism for the compaction of copper powder at high pressures | |
| Raghukandan et al. | An experimental investigation on the effect of h/D ratio on dynamic form—Cladding of domes | |
| CN212311143U (en) | Copper-titanium-aluminum metal explosive welding composite board | |
| Vingsbo et al. | On the dislocation density of a fatigued α-iron | |
| SU1052277A1 (en) | Method of producing coats | |
| Sanders et al. | Correlation of Microstructural Features With Low-Cycle Fatigue and Corrosion Behavior in Aluminum-Zinc-Magnesium Single Crystals | |
| Messerschmidt et al. | X‐ray topographic in‐situ observation of slip band propagation in MgO single crystals | |
| AT233913B (en) | Process for the production of metal composite bodies |