US3074828A - Exothermic heated metal for heat treating and forming - Google Patents
Exothermic heated metal for heat treating and forming Download PDFInfo
- Publication number
- US3074828A US3074828A US5594A US559460A US3074828A US 3074828 A US3074828 A US 3074828A US 5594 A US5594 A US 5594A US 559460 A US559460 A US 559460A US 3074828 A US3074828 A US 3074828A
- Authority
- US
- United States
- Prior art keywords
- metal
- forming
- panel
- composition
- temperature
- 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 57
- 239000002184 metal Substances 0.000 title claims description 57
- 239000000203 mixture Substances 0.000 claims description 43
- 238000000034 method Methods 0.000 claims description 24
- 238000010791 quenching Methods 0.000 claims description 12
- 238000010438 heat treatment Methods 0.000 claims description 11
- 230000000171 quenching effect Effects 0.000 claims description 10
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 31
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 24
- 239000010936 titanium Substances 0.000 description 23
- 229910052719 titanium Inorganic materials 0.000 description 22
- 238000000576 coating method Methods 0.000 description 12
- 229910052749 magnesium Inorganic materials 0.000 description 12
- 239000011777 magnesium Substances 0.000 description 12
- 239000011248 coating agent Substances 0.000 description 10
- 239000000843 powder Substances 0.000 description 10
- QFXZANXYUCUTQH-UHFFFAOYSA-N ethynol Chemical group OC#C QFXZANXYUCUTQH-UHFFFAOYSA-N 0.000 description 8
- 239000003721 gunpowder Substances 0.000 description 8
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 8
- 238000002844 melting Methods 0.000 description 5
- 230000008018 melting Effects 0.000 description 5
- 229910002651 NO3 Inorganic materials 0.000 description 4
- NHNBFGGVMKEFGY-UHFFFAOYSA-N Nitrate Chemical compound [O-][N+]([O-])=O NHNBFGGVMKEFGY-UHFFFAOYSA-N 0.000 description 4
- 239000004568 cement Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 239000002002 slurry Substances 0.000 description 3
- 229910000861 Mg alloy Inorganic materials 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000004880 explosion Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 235000011837 pasties Nutrition 0.000 description 2
- 239000000779 smoke Substances 0.000 description 2
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical group O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 1
- SGTNSNPWRIOYBX-UHFFFAOYSA-N 2-(3,4-dimethoxyphenyl)-5-{[2-(3,4-dimethoxyphenyl)ethyl](methyl)amino}-2-(propan-2-yl)pentanenitrile Chemical compound C1=C(OC)C(OC)=CC=C1CCN(C)CCCC(C#N)(C(C)C)C1=CC=C(OC)C(OC)=C1 SGTNSNPWRIOYBX-UHFFFAOYSA-N 0.000 description 1
- WTFUTSCZYYCBAY-SXBRIOAWSA-N 6-[(E)-C-[[4-[2-(2,3-dihydro-1H-inden-2-ylamino)pyrimidin-5-yl]piperazin-1-yl]methyl]-N-hydroxycarbonimidoyl]-3H-1,3-benzoxazol-2-one Chemical group C1C(CC2=CC=CC=C12)NC1=NC=C(C=N1)N1CCN(CC1)C/C(=N/O)/C1=CC2=C(NC(O2)=O)C=C1 WTFUTSCZYYCBAY-SXBRIOAWSA-N 0.000 description 1
- 241001416092 Buteo buteo Species 0.000 description 1
- 241000023467 Composia Species 0.000 description 1
- 244000171022 Peltophorum pterocarpum Species 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 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
- 238000010276 construction Methods 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000009472 formulation Methods 0.000 description 1
- 239000003517 fume Substances 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 239000004922 lacquer Substances 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000009740 moulding (composite fabrication) Methods 0.000 description 1
- 231100000956 nontoxicity Toxicity 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 239000000344 soap Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- -1 titanium hydride Chemical compound 0.000 description 1
- 229910000048 titanium hydride Inorganic materials 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
Definitions
- the cooling is not uniform, in that the edges cool faster than the center and the quenching does not give a uniform product.
- present forming methods wherein the object to be formed is heated in a bath and then transferred to a press or the like for forming.
- the non-uniform cooling has deleterious effects on the properties of the final formed object.
- the present invention provides a method of heating metal prior to treatment or forming which obviates the hereinbefore mentioned difliculties.
- An object of the present invention is to provide a method of and compositions for heating metal.
- Another object is to provide a method of metal forming.
- Still another object is to pro vide a method of heat treating only a portion of an object.
- Another object is to provide a method of heating and forming metal wherein the outer edges of the metal remain at substantially the same temperature as the center as the object is moved from the heating area to the forming area.
- Still another object is to provide a method of treating a metallic object such as a sheet or the like wherein the heating and forming or quenching occur consecutively in the same area.
- Another object is to provide novel compositions which when applied to metal and ignited, heat the metal to a desired predetermined temperature.
- Another object is to provide a method of heating metal which is more economical than present methods.
- Still another object is to provide exothermic compositions which when coated on metal objects and burned impart desired predetermined temperatures to the metal object.
- Th present invention provides a method of heating metal prior to forming or heat treatment.
- the invention further consists in the compositions hereinafter described and claimed for use in the present process.
- an exothermic or heat producing inflammable composition (more fully disclosed hereinafter) is applied in a desired thickness to a metal object which is to be formed or treated.
- the composition is ignited near the center of the area covered by the composition so that it burns toward the periphery and there by heats the object uniformly.
- the center of the object retains heat and since the outer edges are heated last, they also stay at the desired temperature while the object is moved to a quench or forming machine.
- the inflammable composition can be applied to the metal by spraying, by a brush or roller, or it the sheet is very thin, a printing process can be used. Successive coats of material can be applied to build up the layer to the desired thickness. .
- the thickness of the various compositions is dependent upon the time of burning desired, which in turn controls the temperature to which the metal is heated. In other words, the thicker the composition the longer it burns and the higher the temperature which is induced into the metal. 7
- the temperature of the heated metal object must be high enough for forming or heat treating, and it must be below the melting point of the particular metal to which it is applied.
- the objects are treated with compositions which will induce temperatures of from about 300 F. to about 1100 F. in the object.
- the most desirable burning rate is about 1 linear foot per second, to prevent explosion and provide rapid heating. This enables the center of the coated area to remain hot while the coat burns toward the outside edges.
- the composition can be ignited at any suitable temperature, but for safety purposes it is desired that the ignition temperature b above that of a wood or paper flame.
- the quenching and forming steps can take Place in any suitable manner which is presently known to the art.
- the method of substantially instantaneous quenching shown in U.S. Patent No. 2,838,788 is the preferred quenching method.
- the present composition includes a metal powder and a carrier, as an igniter and/or a suitable vehicle.
- the preferred compositions include a metal powder and both an igniter and a vehicle, particularly a major portion of a metal powder and a minor portion of an igniter together with suflicient vehicle to form a thick pasty consistency.
- the metal powders suitable are aluminum, magnesium, titanium and titanium hydride. Powdered magnesium is preferred because it ignites and burns better than other metallic powders. Also magnesium is non-sparking, has a lower melting point than other metal powders, and presents no toxicity hazards. To facilitate burning, the metals should be 325 mesh or finer.
- igniter is gunpowder, while other commercially available igniter and fuse materials are sold by Universal Match Corporation of St. Louis, Missouri, and others.
- the vehicle which is most suitable is clear nitrate dope similar to the material sold for use in the construction of model airplanes.
- Other vehicles that may be used to give varying temperatures in the metal include collodion, rubber cement, water and wet paper towels, lacquer thinner, Johnsons #ll'l lubrication wax, and materials from the Dennis Chemical Company, St. Louis, Missouri, known as Flame Adhesive, and Ignition Coatings F350. 119A and 1 350-1193. It is desirable that the vehicle be water soluble, particularly when magnesium powders are used, since water enhances the burning action of magnesium.
- the present invention is applicable to any metal object or sheet, but is particularly suited to treating pure titanium and magnesium alloy sheets in the aircraft industry.
- the preferred composition includes eight parts of 325 mesh magnesium powder and one part gunpowder mixed with enough clear nitrate dope to form a thick paste. When this composition is applied to a titanium sheet 0.040" thick in a 4;" coating and ignited, the temperature of the treated side reaches 1100 F. and the untreated side reaches a temperature of 900-1000 F.
- the coatings can be applied to one or to both sides of the object to be heated. Furthermore, if only a portion of an object is to be heat treated, the composition can be applied to that portion only. This is suitable in providing hardened bearing areas which presently require insert bushings or the like.
- the temperatures are measured with Tempil-sticks' ranging in temperature from 300 F. to 1100 F.
- the inflammable composia tions are coated on titanium sheet 0.040" x 3 x 6" and magnesium alloy sheet 0.032 x 3" x 6".
- the invention is applicable to heating other objects, particularly metallic objects, but the titanium and magnesium sheets were used for convenience.
- Example 1 Magnesium powder (150 microns) is mixed with collodion and brushed on titanium panel, ignited with a match, and water is sprayed on the burning magnesium.
- the temperature on the uncoated side of the panel is from 500 to 700 F.
- Example 2 Magnesium powder (150 microns) is spread generously on a titanium panel, water is poured on the panel and the water and powder are stirred to make a slurry. The coating is ignited by an oxy-acetylene flame. The magnesium powder burns vigorously, and a temperature of 1100 F. is induced on the coated side of the panel, and a temperature of 1000 F. is induced on the uncoated side of the panel.
- Example 3 8 parts of magnesium powder (150 microns) plus 1 part of gunpowder are mixed with enough rubber cement to form a slurry and applied by brush to one side of a titanium panel. Water is sprayed on the ignited magnesium powder and results in temperatures of 300 F. and 500 F. on the uncoated and the coated sides of the panel respectively.
- Example 4 8 parts of magnesium powder (150 microns) plus 2 parts of gunpowder are mixed with enough rubber cement to form a thick paste, applied by brush to one side of a titanium panel, and ignited by an oxy-acetylene flame. The magnesium burns slowly inducing temperatures of 300 F. to 500 F. in the panel.
- Example 5 4 parts of magnesium powder (150 microns) plus 1 part of gunpowder are mixed with enough dope to form a thick paste, applied by brush to one side of a titanium panel, and ignited by an oxy-acetylene flame. The rather slow burning time is 5 minutes resulting in temperatures of 900 F. on uncoated side of the panel and 1100 F. on the coated side.
- Example 6 Magnesium powder (150 microns) is mixed with enough rubber cement to form a slurry and brushed on one side of a magnesium panel in a layer 0.010" thick. When the coating is burned, the temperature on the coated side of the panel is 300 F.
- Example 7 A wet piece of paper towel is placed on one side of a magnesium panel, the panel is then dipped in magnesium powder (150 microns), and ignited by an oxyacetylene flame. The magnesium powder burns slow 1y, resulting in temperatures of 300 F. and 500 F. Burning also leaves a black residue on the panel which is easily removed with soap and water.
- Example 8 Two pieces of paper towel are thoroughly wetted and placed on each side of a titanium panel. The panel is dipped in a can of magnesium powder 150 microns), tapped to knock off the excess magnesium powder, and ignited by an oxy-acetylene flame. The magnesium powder burns very vigorously and rapidly. The temperature on the bottom side of the panel is 1000 F., and the temperature on the top side is 1100 F.
- Example 9 One part of magnesium powder microns) is thoroughly mixed with 1 part of a carrier (Igniter of Univer sal Match Corporation) and brushed on one side of a titanium panel in a coating approximately & thick, dried for /2 hour, fused and ignited with a fuse match. The composition burns very vigorously and rapidly, and the temperature on the uncoated side of the panel is 1000 F.
- a carrier Igniter of Univer sal Match Corporation
- Example 10 A thin coat (.010) of a mixture of 1 part magnesium powder (150 microns) and 1 part of a carrier (Igniter of Universal Match Corporation) is applied by brush to one side of a titanium panel, dried 15 minutes, and ignited with oxy-acetylene flame. The temperature on the coated side of the panel is 500 F.
- Example 11 A coating of 1 part of magnesium powder (150 microns) and 1 part of a carrier (Igniter of Universal Match Corporation) is applied by brush to one side of a titanium panel, dried for /2 hour, and ignited by means of oxy-acetylene flame. The temperature on the coated side of the panel is 700 F., while the temperature on the uncoated side of the panel is 600 F.
- a carrier Igniter of Universal Match Corporation
- Example 12 Four parts of magnesium powder and 1 part of gunpowder are mixed with enough Dennis flame adhesive and thinner to make a pasty consistency and brushed on one side of a titanium panel, fused and ignited. The composition burns with the issuance of large yellow flame and lack smoke, and induces a temperature on the uncoated side of the panel of 500 F.
- Example 13 One part of magnesium powder (150 microns) and 1 part of titanium powder are mixed thoroughly with lubricating wax, applied to one side of a titanium panel, dried, and ignited by means of an oxy-acetylene flame. The composition burns with sulficient heat to induce temperatures of 500 F. on the coated side of the panel and 300 F. on the uncoated side of the panel.
- compositions which can be used to heat metal bodies to desired predetermined temperatures particularly temperatures of from about 300 F. to about 1100 F.
- the panels can be formed in any desired forming machine, or they can be quenched, treated or the like. Particularly, the heated panels can be substantially instantaneously quenched in an apparatus as shown in U.S. Patent No. 2,838,788.
- compositions burn with the emission of thick smoke and fumes and suitable safety provisions should be made for the elimination of these.
- a method of heat treating metal objects comprising the steps of positioning a metal object coated with an inflammable composition in a treatment tank, burning ofi the composition leaving the metal object at a desired temperature level for heat treating, and quenching the metal in the same tank in which it is heated.
- a method of heat treating sheet titanium metal including the steps of coating the sheet titanium with an inflammable composition, said composition including about eight parts powdered 325 mesh magnesium, about one part gunpowder, and enough clear nitrate dope to make a thick paste, positioning the coated sheet in a treating tank, burning the composition to heat the sheet titanium to a desired predetermined temperature of from about 300 F. .to about 1100 F., and substantially instantaneously quenching the heated sheet titanium.
- a method of forming metal including the steps of burning off a film of an inflammable composition coated on the metal to heat the metal to a temperature substantially below its melting point, and forming the heated metal.
- a method of forming sheet metal comprising the steps of coating the sheet metal with a film of an inflammable composition, burning off the composition to heat the metal to a forming temperature substantially below its melting point, and forming the heated metal.
- a method of forming sheet titanium metal including the steps of coating the sheet titanium with an inflammable composition, said composition including about eight parts powdered 325 mesh magnesium, about one part gunpowder and enough clear nitrate dope to make a thick paste, positioning the coated sheet in a forming machine, igniting the composition at the approximate center thereof, burning the composition from the center outwardly toward the outer periphery of the sheet at the rate of about 1 linear foot per second to maintain the entire sheet at about the desired predetermined forming temperature, and forming the heated sheet.
- an inflammable composition said composition including about eight parts powdered 325 mesh magnesium, about one part gunpowder and enough clear nitrate dope to make a thick paste
- positioning the coated sheet in a forming machine positioning the coated sheet in a forming machine, igniting the composition at the approximate center thereof, burning the composition from the center outwardly toward the outer periphery of the sheet at the rate of about 1 linear foot per second to maintain the entire sheet at about the desired predetermined forming
- a method of heat treating metal including the steps of burning off a film of an inflammable composition previously coated on the metal to heat the metal to a temperature substantially below its melting point, and thereafter substantially instantaneously quenching the heated metal.
- a method of heat treating metal objects comprising the steps of coating a metal object with an inflammable composition, positioning the coated object in a treatment tank, burning off the composition to raise the temperature of the object to a desired level for heat treating, and substantially instantaneously quenching the metal object in the same tank in which it is heated.
- a method of forming sheet metal including the steps of coating a metal sheet with an inflammable composition, positioning the coated sheet in forming apparatus, igniting the coated sheet, burning ofi the inflammable composition to heat the sheet to forming temperature in the forming apparatus, and forming the heated sheet in the forming apparatus.
Landscapes
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Air Bags (AREA)
Description
United States Patent Ofiflce 3,074,828 Patented Jan. 22, 1953 3,074,828 EXGTHERMEC HEATED METAL FGR HEAT TREATING AND F06 Harry M. Griiffin, Chesterfield, Mo, and August R. Save,
New York, N 31., asslgnors to McDonnell Aircraft Corporation, St. Louis, Mo, a corporation of Maryland No Drawing. Filed Feb. 1, 1960, Ser. No. 5,594 9 Claims. (Cl. 148-43.
' time that it leaves the heat bath until it reaches the quench tank. The cooling is not uniform, in that the edges cool faster than the center and the quenching does not give a uniform product. The same is true of present forming methods wherein the object to be formed is heated in a bath and then transferred to a press or the like for forming. The non-uniform cooling has deleterious effects on the properties of the final formed object.
The present invention provides a method of heating metal prior to treatment or forming which obviates the hereinbefore mentioned difliculties. An object of the present invention is to provide a method of and compositions for heating metal. Another object is to provide a method of metal forming. Still another object is to pro vide a method of heat treating only a portion of an object. Another object is to provide a method of heating and forming metal wherein the outer edges of the metal remain at substantially the same temperature as the center as the object is moved from the heating area to the forming area.
Still another object is to provide a method of treating a metallic object such as a sheet or the like wherein the heating and forming or quenching occur consecutively in the same area.
Another object is to provide novel compositions which when applied to metal and ignited, heat the metal to a desired predetermined temperature.
Another object is to provide a method of heating metal which is more economical than present methods.
Still another object is to provide exothermic compositions which when coated on metal objects and burned impart desired predetermined temperatures to the metal object.
These and other objects and advantages will become apparent hereinafter.
Th present invention provides a method of heating metal prior to forming or heat treatment. The invention further consists in the compositions hereinafter described and claimed for use in the present process.
In the present invention, an exothermic or heat producing inflammable composition (more fully disclosed hereinafter) is applied in a desired thickness to a metal object which is to be formed or treated. The composition is ignited near the center of the area covered by the composition so that it burns toward the periphery and there by heats the object uniformly. The center of the object retains heat and since the outer edges are heated last, they also stay at the desired temperature while the object is moved to a quench or forming machine.
The inflammable composition can be applied to the metal by spraying, by a brush or roller, or it the sheet is very thin, a printing process can be used. Successive coats of material can be applied to build up the layer to the desired thickness. .The thickness of the various compositions is dependent upon the time of burning desired, which in turn controls the temperature to which the metal is heated. In other words, the thicker the composition the longer it burns and the higher the temperature which is induced into the metal. 7 The temperature of the heated metal object must be high enough for forming or heat treating, and it must be below the melting point of the particular metal to which it is applied. Preferably, the objects are treated with compositions which will induce temperatures of from about 300 F. to about 1100 F. in the object.
The most desirable burning rate is about 1 linear foot per second, to prevent explosion and provide rapid heating. This enables the center of the coated area to remain hot while the coat burns toward the outside edges.
The composition can be ignited at any suitable temperature, but for safety purposes it is desired that the ignition temperature b above that of a wood or paper flame. The quenching and forming steps can take Place in any suitable manner which is presently known to the art. The method of substantially instantaneous quenching shown in U.S. Patent No. 2,838,788 is the preferred quenching method.
The present composition includes a metal powder and a carrier, as an igniter and/or a suitable vehicle. The preferred compositions include a metal powder and both an igniter and a vehicle, particularly a major portion of a metal powder and a minor portion of an igniter together with suflicient vehicle to form a thick pasty consistency.
The metal powders suitable are aluminum, magnesium, titanium and titanium hydride. Powdered magnesium is preferred because it ignites and burns better than other metallic powders. Also magnesium is non-sparking, has a lower melting point than other metal powders, and presents no toxicity hazards. To facilitate burning, the metals should be 325 mesh or finer.
The most suitable igniter is gunpowder, while other commercially available igniter and fuse materials are sold by Universal Match Corporation of St. Louis, Missouri, and others.
The vehicle which is most suitable is clear nitrate dope similar to the material sold for use in the construction of model airplanes. Other vehicles that may be used to give varying temperatures in the metal include collodion, rubber cement, water and wet paper towels, lacquer thinner, Johnsons #ll'l lubrication wax, and materials from the Dennis Chemical Company, St. Louis, Missouri, known as Flame Adhesive, and Ignition Coatings F350. 119A and 1 350-1193. It is desirable that the vehicle be water soluble, particularly when magnesium powders are used, since water enhances the burning action of magnesium.
The present invention is applicable to any metal object or sheet, but is particularly suited to treating pure titanium and magnesium alloy sheets in the aircraft industry. The preferred composition includes eight parts of 325 mesh magnesium powder and one part gunpowder mixed with enough clear nitrate dope to form a thick paste. When this composition is applied to a titanium sheet 0.040" thick in a 4;" coating and ignited, the temperature of the treated side reaches 1100 F. and the untreated side reaches a temperature of 900-1000 F.
The coatings can be applied to one or to both sides of the object to be heated. Furthermore, if only a portion of an object is to be heat treated, the composition can be applied to that portion only. This is suitable in providing hardened bearing areas which presently require insert bushings or the like.
The temperatures are measured with Tempil-sticks' ranging in temperature from 300 F. to 1100 F.
In the following examples, the inflammable composia tions are coated on titanium sheet 0.040" x 3 x 6" and magnesium alloy sheet 0.032 x 3" x 6". As mentioned, the invention is applicable to heating other objects, particularly metallic objects, but the titanium and magnesium sheets were used for convenience.
The following examples are intended to illustrate certain practical formulations, however certain modifications of these examples can be utilized with different metals and different temperatures.
Example 1 Magnesium powder (150 microns) is mixed with collodion and brushed on titanium panel, ignited with a match, and water is sprayed on the burning magnesium. The temperature on the uncoated side of the panel is from 500 to 700 F.
Example 2 Magnesium powder (150 microns) is spread generously on a titanium panel, water is poured on the panel and the water and powder are stirred to make a slurry. The coating is ignited by an oxy-acetylene flame. The magnesium powder burns vigorously, and a temperature of 1100 F. is induced on the coated side of the panel, and a temperature of 1000 F. is induced on the uncoated side of the panel.
Example 3 8 parts of magnesium powder (150 microns) plus 1 part of gunpowder are mixed with enough rubber cement to form a slurry and applied by brush to one side of a titanium panel. Water is sprayed on the ignited magnesium powder and results in temperatures of 300 F. and 500 F. on the uncoated and the coated sides of the panel respectively.
Example 4 8 parts of magnesium powder (150 microns) plus 2 parts of gunpowder are mixed with enough rubber cement to form a thick paste, applied by brush to one side of a titanium panel, and ignited by an oxy-acetylene flame. The magnesium burns slowly inducing temperatures of 300 F. to 500 F. in the panel.
Example 5 4 parts of magnesium powder (150 microns) plus 1 part of gunpowder are mixed with enough dope to form a thick paste, applied by brush to one side of a titanium panel, and ignited by an oxy-acetylene flame. The rather slow burning time is 5 minutes resulting in temperatures of 900 F. on uncoated side of the panel and 1100 F. on the coated side.
Example 6 Magnesium powder (150 microns) is mixed with enough rubber cement to form a slurry and brushed on one side of a magnesium panel in a layer 0.010" thick. When the coating is burned, the temperature on the coated side of the panel is 300 F.
Example 7 A wet piece of paper towel is placed on one side of a magnesium panel, the panel is then dipped in magnesium powder (150 microns), and ignited by an oxyacetylene flame. The magnesium powder burns slow 1y, resulting in temperatures of 300 F. and 500 F. Burning also leaves a black residue on the panel which is easily removed with soap and water.
Example 8 Two pieces of paper towel are thoroughly wetted and placed on each side of a titanium panel. The panel is dipped in a can of magnesium powder 150 microns), tapped to knock off the excess magnesium powder, and ignited by an oxy-acetylene flame. The magnesium powder burns very vigorously and rapidly. The temperature on the bottom side of the panel is 1000 F., and the temperature on the top side is 1100 F.
4 Example 9 One part of magnesium powder microns) is thoroughly mixed with 1 part of a carrier (Igniter of Univer sal Match Corporation) and brushed on one side of a titanium panel in a coating approximately & thick, dried for /2 hour, fused and ignited with a fuse match. The composition burns very vigorously and rapidly, and the temperature on the uncoated side of the panel is 1000 F.
Example 10 A thin coat (.010) of a mixture of 1 part magnesium powder (150 microns) and 1 part of a carrier (Igniter of Universal Match Corporation) is applied by brush to one side of a titanium panel, dried 15 minutes, and ignited with oxy-acetylene flame. The temperature on the coated side of the panel is 500 F.
Example 11 A coating of 1 part of magnesium powder (150 microns) and 1 part of a carrier (Igniter of Universal Match Corporation) is applied by brush to one side of a titanium panel, dried for /2 hour, and ignited by means of oxy-acetylene flame. The temperature on the coated side of the panel is 700 F., while the temperature on the uncoated side of the panel is 600 F.
Example 12 Four parts of magnesium powder and 1 part of gunpowder are mixed with enough Dennis flame adhesive and thinner to make a pasty consistency and brushed on one side of a titanium panel, fused and ignited. The composition burns with the issuance of large yellow flame and lack smoke, and induces a temperature on the uncoated side of the panel of 500 F.
Example 13 One part of magnesium powder (150 microns) and 1 part of titanium powder are mixed thoroughly with lubricating wax, applied to one side of a titanium panel, dried, and ignited by means of an oxy-acetylene flame. The composition burns with sulficient heat to induce temperatures of 500 F. on the coated side of the panel and 300 F. on the uncoated side of the panel.
The foregoing examples show compositions which can be used to heat metal bodies to desired predetermined temperatures particularly temperatures of from about 300 F. to about 1100 F.
After the panels have been heated in the foregoing examples, the panels can be formed in any desired forming machine, or they can be quenched, treated or the like. Particularly, the heated panels can be substantially instantaneously quenched in an apparatus as shown in U.S. Patent No. 2,838,788.
Since most metal powder particles are covered with an insulating medium of molecular dimensions, they can accumulate frictional electricity. Therefore, shielding or grounding measures should be exercised when utilizing the present invention to prevent fire or explosion of the major mass of metal powder.
Also some of the compositions burn with the emission of thick smoke and fumes and suitable safety provisions should be made for the elimination of these.
This invention is intended to cover all changes and modifications of the examples of the invention herein chosen for purposes of the disclosure, which do not constitute departures from the spirit and scope of the invention.
We claim:
1. A method of heat treating metal objects comprising the steps of positioning a metal object coated with an inflammable composition in a treatment tank, burning ofi the composition leaving the metal object at a desired temperature level for heat treating, and quenching the metal in the same tank in which it is heated.
2. A method of heat treating sheet titanium metal including the steps of coating the sheet titanium with an inflammable composition, said composition including about eight parts powdered 325 mesh magnesium, about one part gunpowder, and enough clear nitrate dope to make a thick paste, positioning the coated sheet in a treating tank, burning the composition to heat the sheet titanium to a desired predetermined temperature of from about 300 F. .to about 1100 F., and substantially instantaneously quenching the heated sheet titanium.
3. A method of forming metal including the steps of burning off a film of an inflammable composition coated on the metal to heat the metal to a temperature substantially below its melting point, and forming the heated metal.
4. A method of forming sheet metal comprising the steps of coating the sheet metal with a film of an inflammable composition, burning off the composition to heat the metal to a forming temperature substantially below its melting point, and forming the heated metal.
5. A method of forming sheet titanium metal including the steps of coating the sheet titanium with an inflammable composition, said composition including about eight parts powdered 325 mesh magnesium, about one part gunpowder and enough clear nitrate dope to make a thick paste, positioning the coated sheet in a forming machine, igniting the composition at the approximate center thereof, burning the composition from the center outwardly toward the outer periphery of the sheet at the rate of about 1 linear foot per second to maintain the entire sheet at about the desired predetermined forming temperature, and forming the heated sheet.
6. A method of heat treating metal including the steps of burning off a film of an inflammable composition previously coated on the metal to heat the metal to a temperature substantially below its melting point, and thereafter substantially instantaneously quenching the heated metal.
7. A method of heat treating metal objects comprising the steps of coating a metal object with an inflammable composition, positioning the coated object in a treatment tank, burning off the composition to raise the temperature of the object to a desired level for heat treating, and substantially instantaneously quenching the metal object in the same tank in which it is heated.
8. A method of forming sheet metal including the steps of coating a metal sheet with an inflammable composition, positioning the coated sheet in forming apparatus, igniting the coated sheet, burning ofi the inflammable composition to heat the sheet to forming temperature in the forming apparatus, and forming the heated sheet in the forming apparatus.
9. The method defined in claim 8 wherein the sheet metal is titanium.
References Cited in the file of this patent UNITED STATES PATENTS Re. 13,219 Chapman Mar. 21, 1911 934,711 Chapman Sept. 21, 1909 1,077,827 Fuller Nov. 4, 1913 1,799,945 Beck Apr. 7, 1931 1,815,691 Wilson July 21, 1931 1,849,056 Crawley Mar. 15, 1932 2,138,023 Buzzard et a1. Nov. 29, 1938 2,337,314 Deppeler Dec. 21, 1943 2,464,210 Cadwell Mar. 15, 1949 2,500,097 Soffel Mar. 7, 1950 2,680,063 Shapiro June 1, 1954 2,791,816 Pletsch May 14, 1957 2,816,012 Walton Dec. 10, 1957 2,889,238 Long et a1. June 2, 1959 2,898,253 Schneider et a1. Aug. 4, 1959 FOREIGN PATENTS 463,511 Great Britain Apr. 1, 1937 568,453 Great Britain Apr. 5, 1935
Claims (1)
1. A METHOD OF HEATING TREATING METAL OBJECTS COMPRISING THE STEPS OF POSITIONING A METAL OBJECT COATED WITH AN IN FLAMMABLE COMPOSITION IN A TREATMENT TANK, BURNING OFF THE COMPOSITION LEAVING THE METAL OBJECT AT A DESIRED TEMPERATURE LEVEL FOR HEAT TREATING, AND QUENCHING THE METAL IN THE SAME TANK IN WHICH IT IS HEATED.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US5594A US3074828A (en) | 1960-02-01 | 1960-02-01 | Exothermic heated metal for heat treating and forming |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US5594A US3074828A (en) | 1960-02-01 | 1960-02-01 | Exothermic heated metal for heat treating and forming |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3074828A true US3074828A (en) | 1963-01-22 |
Family
ID=21716658
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US5594A Expired - Lifetime US3074828A (en) | 1960-02-01 | 1960-02-01 | Exothermic heated metal for heat treating and forming |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3074828A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3355159A (en) * | 1962-05-23 | 1967-11-28 | British Aluminium Co Ltd | Apparatus for continuous heat treatment of sheet or strip material |
| US5127885A (en) * | 1990-12-24 | 1992-07-07 | Xerox Corporation | Endless metal belt with strengthened edges |
| US20160222498A1 (en) * | 2015-02-04 | 2016-08-04 | Spirit Aerosystems, Inc. | Localized heat treating of net shape titanium parts |
| TWI725532B (en) * | 2018-09-11 | 2021-04-21 | 美商美國禮來大藥廠 | Methods of treating psoriasis |
Citations (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US934711A (en) * | 1908-10-16 | 1909-09-21 | Frank Spencer Chapman | Soldering device. |
| US1077827A (en) * | 1911-05-06 | 1913-11-04 | Gen Electric | Process of treating tungsten. |
| US1799945A (en) * | 1927-05-20 | 1931-04-07 | Degussa | Process for heat treatment of metal articles |
| US1815691A (en) * | 1928-10-31 | 1931-07-21 | Western Electric Co | Method of heat treating metal parts |
| US1849056A (en) * | 1924-03-01 | 1932-03-15 | Forest Radio Company De | Electron discharge device |
| GB463511A (en) * | 1935-03-06 | 1937-04-01 | Wilhelm Klapproth | An improved process for coating pure and alloyed light metals with a firmly adhering protection against corrosion |
| US2138023A (en) * | 1935-11-14 | 1938-11-29 | Robert W Buzzard | Method of treating anodic coatings on magnesium and its alloys |
| US2337314A (en) * | 1943-04-08 | 1943-12-21 | Metal & Thermit Corp | Aluminothermic method and articles of manufacture |
| GB568453A (en) * | 1942-09-30 | 1945-04-05 | Ind De L Aluminium Sa | An improved method of welding metal bodies |
| US2464210A (en) * | 1945-01-29 | 1949-03-15 | Electric Railway Improvement Co | Welding materials and processes |
| US2500097A (en) * | 1947-10-14 | 1950-03-07 | Peter J Soffel | Exothermic composition for controlling the fluidity of castings |
| US2680063A (en) * | 1952-01-21 | 1954-06-01 | Us Army | Chemical heating composition |
| US2791816A (en) * | 1953-08-03 | 1957-05-14 | Exomet | Method of applying exothermic material to the hot-top of steel |
| US2816012A (en) * | 1955-04-04 | 1957-12-10 | Drackett Co | Heat-producing compositions |
| US2889238A (en) * | 1954-07-13 | 1959-06-02 | Solar Aircraft Co | Coating for cleaning and protecting metals |
| US2898253A (en) * | 1958-03-25 | 1959-08-04 | North American Aviation Inc | High temperature protective coating for metals |
-
1960
- 1960-02-01 US US5594A patent/US3074828A/en not_active Expired - Lifetime
Patent Citations (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US934711A (en) * | 1908-10-16 | 1909-09-21 | Frank Spencer Chapman | Soldering device. |
| US1077827A (en) * | 1911-05-06 | 1913-11-04 | Gen Electric | Process of treating tungsten. |
| US1849056A (en) * | 1924-03-01 | 1932-03-15 | Forest Radio Company De | Electron discharge device |
| US1799945A (en) * | 1927-05-20 | 1931-04-07 | Degussa | Process for heat treatment of metal articles |
| US1815691A (en) * | 1928-10-31 | 1931-07-21 | Western Electric Co | Method of heat treating metal parts |
| GB463511A (en) * | 1935-03-06 | 1937-04-01 | Wilhelm Klapproth | An improved process for coating pure and alloyed light metals with a firmly adhering protection against corrosion |
| US2138023A (en) * | 1935-11-14 | 1938-11-29 | Robert W Buzzard | Method of treating anodic coatings on magnesium and its alloys |
| GB568453A (en) * | 1942-09-30 | 1945-04-05 | Ind De L Aluminium Sa | An improved method of welding metal bodies |
| US2337314A (en) * | 1943-04-08 | 1943-12-21 | Metal & Thermit Corp | Aluminothermic method and articles of manufacture |
| US2464210A (en) * | 1945-01-29 | 1949-03-15 | Electric Railway Improvement Co | Welding materials and processes |
| US2500097A (en) * | 1947-10-14 | 1950-03-07 | Peter J Soffel | Exothermic composition for controlling the fluidity of castings |
| US2680063A (en) * | 1952-01-21 | 1954-06-01 | Us Army | Chemical heating composition |
| US2791816A (en) * | 1953-08-03 | 1957-05-14 | Exomet | Method of applying exothermic material to the hot-top of steel |
| US2889238A (en) * | 1954-07-13 | 1959-06-02 | Solar Aircraft Co | Coating for cleaning and protecting metals |
| US2816012A (en) * | 1955-04-04 | 1957-12-10 | Drackett Co | Heat-producing compositions |
| US2898253A (en) * | 1958-03-25 | 1959-08-04 | North American Aviation Inc | High temperature protective coating for metals |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3355159A (en) * | 1962-05-23 | 1967-11-28 | British Aluminium Co Ltd | Apparatus for continuous heat treatment of sheet or strip material |
| US5127885A (en) * | 1990-12-24 | 1992-07-07 | Xerox Corporation | Endless metal belt with strengthened edges |
| US20160222498A1 (en) * | 2015-02-04 | 2016-08-04 | Spirit Aerosystems, Inc. | Localized heat treating of net shape titanium parts |
| US9951405B2 (en) * | 2015-02-04 | 2018-04-24 | Spirit Aerosystems, Inc. | Localized heat treating of net shape titanium parts |
| TWI725532B (en) * | 2018-09-11 | 2021-04-21 | 美商美國禮來大藥廠 | Methods of treating psoriasis |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US1924311A (en) | Insulating material | |
| US3074828A (en) | Exothermic heated metal for heat treating and forming | |
| US1823869A (en) | Coating of bodies with metal | |
| US1817888A (en) | Protective coating (alborizing) | |
| EP0003419A3 (en) | Isothermal forging lubricating composition and use thereof | |
| US2432465A (en) | Method of making metallic pigments | |
| DE825034C (en) | Mixture of substances for creating diffusion layers on metals and metal alloys | |
| US3135623A (en) | Surface treatment of steel billets to be extruded, and of extrusion tools | |
| DE2758393C2 (en) | Sheet metal lamination process | |
| US2138023A (en) | Method of treating anodic coatings on magnesium and its alloys | |
| DE766247C (en) | Process for coating metallic objects by melting on corrosion protection substances in powder form | |
| DE2002472A1 (en) | Tubular wire plasma arc spraying device | |
| JPS62280289A (en) | Fireproofing agent prepared from shell | |
| US1340245A (en) | Shotgun-shell | |
| US3006745A (en) | Catalyzed metal fuel | |
| JPS5421622A (en) | Burner material used cooking appliances | |
| US1795703A (en) | Method of coating bodies of iron, wood, or other material | |
| GB1281022A (en) | A process and apparatus when used for the application of corrosion-resisting coatings to rolled metal products | |
| GB1087580A (en) | Improvements relating to the coating of steel with nickel | |
| SU609599A1 (en) | Mixture for coating workpieces manufactured from metal powder | |
| US2683672A (en) | Vitreous enameling method and composition | |
| JPS5621302A (en) | Coatint method of fuse-bonding prevention insulating film on metal material | |
| US2676935A (en) | Nondiscoloring thermocoupling compound | |
| DE178521C (en) | ||
| US3193420A (en) | Catalyzed metal fuel containing a peroxide |