US3837848A - Method of making tools by impregnating a steel skeleton with a carbide, nitride or oxide precursor - Google Patents
Method of making tools by impregnating a steel skeleton with a carbide, nitride or oxide precursor Download PDFInfo
- Publication number
- US3837848A US3837848A US00156029A US15602971A US3837848A US 3837848 A US3837848 A US 3837848A US 00156029 A US00156029 A US 00156029A US 15602971 A US15602971 A US 15602971A US 3837848 A US3837848 A US 3837848A
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- United States
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- percent
- skeleton
- pores
- alloys
- steel
- 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
- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 35
- 239000010959 steel Substances 0.000 title claims abstract description 35
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 10
- 150000004767 nitrides Chemical class 0.000 title claims description 12
- 239000002243 precursor Substances 0.000 title description 3
- 239000011148 porous material Substances 0.000 claims abstract description 51
- 239000002245 particle Substances 0.000 claims abstract description 24
- 238000011049 filling Methods 0.000 claims abstract description 10
- 238000000034 method Methods 0.000 claims description 54
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 32
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 30
- 229910052751 metal Inorganic materials 0.000 claims description 24
- 239000002184 metal Substances 0.000 claims description 24
- 238000005245 sintering Methods 0.000 claims description 21
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 claims description 20
- 238000000137 annealing Methods 0.000 claims description 19
- 239000012768 molten material Substances 0.000 claims description 18
- 229910052757 nitrogen Inorganic materials 0.000 claims description 16
- 239000000463 material Substances 0.000 claims description 15
- 229910045601 alloy Inorganic materials 0.000 claims description 14
- 239000000956 alloy Substances 0.000 claims description 14
- 239000000843 powder Substances 0.000 claims description 13
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 12
- 229910052799 carbon Inorganic materials 0.000 claims description 12
- 238000007598 dipping method Methods 0.000 claims description 12
- 238000005470 impregnation Methods 0.000 claims description 12
- 239000011777 magnesium Substances 0.000 claims description 11
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 9
- 229910052742 iron Inorganic materials 0.000 claims description 9
- 239000001301 oxygen Substances 0.000 claims description 9
- 229910052760 oxygen Inorganic materials 0.000 claims description 9
- 229910021364 Al-Si alloy Inorganic materials 0.000 claims description 8
- 229910018575 Al—Ti Inorganic materials 0.000 claims description 8
- 239000000945 filler Substances 0.000 claims description 8
- 230000015572 biosynthetic process Effects 0.000 claims description 6
- 229910001092 metal group alloy Inorganic materials 0.000 claims description 5
- 239000010936 titanium Substances 0.000 claims description 5
- 229910052782 aluminium Inorganic materials 0.000 claims description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 4
- 150000002739 metals Chemical class 0.000 claims description 4
- 150000003839 salts Chemical class 0.000 claims description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 3
- 229910000676 Si alloy Inorganic materials 0.000 claims description 3
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 3
- UQZIWOQVLUASCR-UHFFFAOYSA-N alumane;titanium Chemical compound [AlH3].[Ti] UQZIWOQVLUASCR-UHFFFAOYSA-N 0.000 claims description 3
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 claims description 3
- 150000004645 aluminates Chemical class 0.000 claims description 3
- 229910052749 magnesium Inorganic materials 0.000 claims description 3
- 238000009827 uniform distribution Methods 0.000 claims description 3
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 claims description 2
- 150000004760 silicates Chemical class 0.000 claims description 2
- 239000007769 metal material Substances 0.000 abstract description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 20
- 239000011651 chromium Substances 0.000 description 14
- 239000011572 manganese Substances 0.000 description 11
- 229910052759 nickel Inorganic materials 0.000 description 6
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 5
- 229910052804 chromium Inorganic materials 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 239000010955 niobium Substances 0.000 description 5
- 239000000919 ceramic Substances 0.000 description 4
- 239000010941 cobalt Substances 0.000 description 4
- 229910017052 cobalt Inorganic materials 0.000 description 4
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 4
- 238000001125 extrusion Methods 0.000 description 4
- 239000000835 fiber Substances 0.000 description 4
- 238000002844 melting Methods 0.000 description 4
- 230000008018 melting Effects 0.000 description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 3
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 229910052748 manganese Inorganic materials 0.000 description 3
- 239000002994 raw material Substances 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- 239000000725 suspension Substances 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 229910052721 tungsten Inorganic materials 0.000 description 3
- 239000010937 tungsten Substances 0.000 description 3
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 2
- PHFQLYPOURZARY-UHFFFAOYSA-N chromium trinitrate Chemical group [Cr+3].[O-][N+]([O-])=O.[O-][N+]([O-])=O.[O-][N+]([O-])=O PHFQLYPOURZARY-UHFFFAOYSA-N 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 239000013067 intermediate product Substances 0.000 description 2
- 239000010410 layer Substances 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 239000011733 molybdenum Substances 0.000 description 2
- 230000000802 nitrating effect Effects 0.000 description 2
- 239000012299 nitrogen atmosphere Substances 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 235000019353 potassium silicate Nutrition 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- NTHWMYGWWRZVTN-UHFFFAOYSA-N sodium silicate Chemical compound [Na+].[Na+].[O-][Si]([O-])=O NTHWMYGWWRZVTN-UHFFFAOYSA-N 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000002344 surface layer Substances 0.000 description 2
- 229910052720 vanadium Inorganic materials 0.000 description 2
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 229920002411 Pearloid Polymers 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910001315 Tool steel Inorganic materials 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- CXOWYMLTGOFURZ-UHFFFAOYSA-N azanylidynechromium Chemical compound [Cr]#N CXOWYMLTGOFURZ-UHFFFAOYSA-N 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 238000003763 carbonization Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 150000001805 chlorine compounds Chemical class 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 210000003298 dental enamel Anatomy 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000004519 grease Substances 0.000 description 1
- 229910001385 heavy metal Inorganic materials 0.000 description 1
- 238000001192 hot extrusion Methods 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 229910000734 martensite Inorganic materials 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 238000005272 metallurgy Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000011368 organic material Substances 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 239000010451 perlite Substances 0.000 description 1
- 235000019362 perlite Nutrition 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000008207 working material Substances 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/07—Alloys based on nickel or cobalt based on cobalt
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/24—After-treatment of workpieces or articles
- B22F3/26—Impregnating
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C33/00—Making ferrous alloys
- C22C33/02—Making ferrous alloys by powder metallurgy
- C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
- C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
- C22C33/0285—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with Cr, Co, or Ni having a minimum content higher than 5%
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12014—All metal or with adjacent metals having metal particles
- Y10T428/1216—Continuous interengaged phases of plural metals, or oriented fiber containing
Definitions
- Another known method for making form parts of high hot strength or high temperature resistance and high hot hardness uses metal powder as raw material and frequently high melting oxides are added. The powder or mixture of powders is then compressed into porous blocks or billets, which are subsequently sintered to obtain high density. Sintering is to occur at high temperatures. Alternatively, hot pressing or hot extrusion is used for forming and condensing the parts to be made. In either case, it is deemed desirable to obtain a product having a high density.
- the non-metallic parts, and preferably also the metal powder should be very fine in order to obtain a finally dispersed and essentially uniform distribution of the inclusion. As with present day knowledge, this is believed to result in parts of high strength.
- the present invention is based on development and investigations that have been conducted independently from the foregoing and were particularly directed to the making of tools and dies to be used for hot working. It is important that the material worked with is considerably cheaper than the known alloys on nickel and cobalt basis. These developments have led to the result that, for example, a porous die or mold for extrusion, e.g., of steel pipes, and having a nitrogen content of about 1 percent could be made from chromium steel powder, having a longer service life than known dies and molds. Moreover, the product (e.g., pipe) had a better surface texture when such particular die was used.
- the known materials do not have that property or only to a very unsatisfactory degree.
- tool steel and martensitic aging steel as used to an increasing extent are very hard at temperatures up to about 550 C, but their strength decreases rapidly above that temperature. Above 550 C one uses exclusively the usually austenitic alloys having nickel or cobalt basis as was mentioned above but it was also stated above, that these alloys do not have the sufficient strength at lower temperature, and that was found to be detrimental for overall wear and life.
- tools or dies to be used for hot forming of metal such as a press or rolling mandrel or a die of an extrusion molding machine or the like in the following manner.
- the tool or die is made as a skeleton with a penetrating and all-pervading network of pores but at a total volume of pores less than 50 percent, preferably about 20 to 30 percent.
- Metal to be used here is to have high hot strength and high temperature resistance.
- the pores are to be filled with a non-metallic, an-organic material as completely as possible, and having significant hardness particularly below 650 C, so as to render the tool practically undeformable.
- the mechanical properties are determined in the lower temperature range predominantly by the non-metallic component, while for temperatures above 650 C, the metal component of the skeleton determines predominantly these properties.
- the particular tool or die, made in that manner, particularly with a total pore volume of less than 50 percent, has these pores filled with nonmetallic material either completely or only in zones of the tool engaging later the material to be worked; these zones may have a depth of about 5 to 10 mm, as filled with the non-metallic inclusion, while the remainder (interior) of the tool, has a relative density of percent and above.
- the raw material, from which to make the tools or dies may be comprised of small particles of any form, such as flakes, shavings, powder, fibers, cuttings or the like. These particles are compressed and sintered, and the resulting porous part has the shape of the tool or die to be made.
- a metallic body is produced penetrated by a continuous, allpervating network of pores, and that is actually the basis for defining the body as a skeleton. It is this a random type frame and support microstructure made of material of high temperature resistance.
- a heat resisting steel alloy that could be used in accordance with the invention has composition shown in the following table.
- Example Carbon max. 0.5 0.05 Silicon 0.2 2.0 l4 Manganese 0.3 l5 0.6 Chromium l 25 13 Nickel 4 2O l3 Tungsten up to l0 l4 Vanadium up to 2 l lron remainder remainder.
- the following elements could be added to further increase hot strength:
- Example Carbon max 0.5 0.02 Silicon 0.2 2.0 0.7 Manganese 0.3 l5 [.3 Chromium l0 25 25 Nickel 4 20 13.5 Tungsten up to 3.3 Vanadium up to Nitrogen 0.2 3.0 1.62 Iron remainder remainder A heat resisting nickel alloy may, for example, be made in accordance with Table C.
- At least 57 A heat resisting cobalt alloy may be made in accordance with Table D.
- the metal particles are poured into a mold and condensed subsequently. It is usually of advantage to sinter the pressed form so that the metal parts engage more intimately so as to establish an integral body.
- the porous skeleton may be particularly treated in order to increase the hot strength and heat resistance; for example, there may be provided carbonization, nitrating or cold working.
- the relative density of the skeleton is variable over a large range and may actually range from about 4 percent, if shavings are used, up to 90 percent for very fine powder or the like. Preferably, the relative density ranges from 60 to percent.
- the metallic skeleton body has in each of these cases a network of pores which are more or less interconnected and penetrate the body throughout. They are now to be filled so that, in effect, a second network be produced, which, in turn, is penetrated by the metallic skeleton. This second and, in fact, coherent network of filler material is produced by infiltration, impregnating or the like. This may be combined with an annealing process, for example, upon sintering the metal skeleton body, but impregnation could be carried out in a separate process.
- the melted, i.e., liquified, material that is to penetrate the pores of the skeleton may have already the final composition or it is an intermediate product that reacts chemically with some element of the skeleton body so that, in fact, the final product is composed of a second non-metallic, inorganic network that has become integral with the porous skeleton as originally produced.
- silicate water glass, glass, enamel or the like.
- other salts such as chlorides or aluminates, can be used.
- Molten metal or a metal alloy can be used also for impregnation, such as aluminum, magnesium, individually or an aluminum silicon alloy or an aluminum titanium alloy.
- impregnating metals penetrate the pores of the skeleton body and are changed into non-metallic compounds within the pores. For example, these metals are caused to react with carbon, oxygen and/or nitrogen, so as to produce carbides, oxides or nitrides. These reactions require some annealing.
- the reaction material carbon etc.
- carbon or nitrogen may be present prior to impregnation in the metal part of the skeleton, or oxygen may be formed on the surface of the pores, for example, as an oxide skin of the metal of the porous skeleton body.
- the skeleton can be treated with a watery solution from which salt or an oxide thereof has precipitated, and the oxygen thereof will react subsequently with metal caused to penetrate the pores.
- Including the reaction material in or on the pores of the skeleton is also applicable if the skeleton body is subsequently impregnated with silicate, e.g., for improving the wettability or for reducing viscosity of the principle impregnating material, or the softening point after impregnating is to be increased.
- the tool is to be used at a temperature, generally, that is below the melting point of the non-metallic material that penetrates the pores of the skeleton; however, for a short period of time, operating temperature may be somewhat above that melting point, particularly if the strength of the metallic skeleton is sufficient to sustain that hot temperature.
- the heat of fusion serves as local heat sink and the improved thermal conduction facilitates withdrawal and transfer of heat from the surface of the tool that is subjected immediately to the hot working temperature.
- the non-metallic material in the network of pores must not react chemically, at least not strongly react chemically, during subsequent use with material worked by the tool or die, nor must subsequent exposure of the tool or die to a working material cause the removal of the non-metallic material from the pores in the metallic skeleton.
- the tool made in accordance with the present invention differs from the form parts made in accordance with known impregnating methods. It should be mentioned that impregnating a porous metal skeleton with a liquidous metal such as copper is known, however, in that case, two intertwining metal networks are produced. Also, it is known to penetrate metallic skeletons with grease or oil or with watery solutions, but penetration and impregnation in this case has an entirely different purpose. The resulting form parts are not comparable in any way with the tools made in accordance with the present invention.
- Texture and microstructure consisted actually almost completely of so-called nongenuine nitrogen perlite or nitrogen pearloid having a finely laminated texture composition of chromium nitrate Cr N and an austenitic base. That body had high temperature resistance and hot strength.
- This annulus constituted the skeleton and was placed into a vacuum furnace, above a supply of silicate (water glass), and was heated together therewith to a temperature of l,000 to 1,050 C using a nitrogen atmosphere at about 600 torr (or about 1 16 pounds per square inch). The viscosity of the silicate was sufficiently low for that temperature.
- the furnace was evacuated and the skeleton was dipped into the molten silicate. Again, the furnace was filled with nitrogen at a pressure of 700 torr. The annulus remained submerged in the molten silicate for about minutes, while molten, low viscosity silicate penetrated the pores of the annulus. Thereafter, the annulus was removed from the silicate but not from the furnace. Heat was maintained in the furnace for about l0 minutes longer, before being turned off. This, then, completed the making of a die to be used for extrusion molding.
- Method of making a tool comprising the steps of compressing and sintering chromium-nickel-steel particles to obtain a porous skeleton of not more than 50 percent pore volume; sintering the skeleton; nitrating the skeleton to obtain chromium-nitride with at least 1 percent N in the skeleton; impregnating the skeleton with molten silicate to fill at least some of the pores and annealing the skeleton in a nitrogen atmosphere.
- Method as in claim 1 providing surface zones of the skeleton with a relatively high porosity for a depth of about 5 to 10 millimeter, the interior having relative density of at least 90 percent, and filling only the surface zones with said molten material.
- the method of making a tool comprising the steps of making a skeleton by compressing steel particles such as powder or flaky shavings to form a porous skeleton penetrated by a continuous network of pores of total volume not exceeding 50 percent, said steel parti cles containing at least one element selected from the group consisting of carbon, nitrogen and oxygen;
- a molten material selected from the group consisting of silicates, metals and metal alloys having an affinity to said carbon, nitrogen and oxygen to form respectively a carbide, nitride or oxide, for a period sufficient to cause the molten material to penetrate the pores; and
- Method as in claim 3 providing the porous metal alloy with an approximately uniform distribution of pores and a pore volume of about 20 to 30 percent.
- Method as in claim 3 providing surface zones of the skeleton with a relatively high porosity for a depth of about 5 to 10 millimeter, the interior having relative density of at least 90 percent, and filling only the surface zones with said molten material.
- the filler being formed by dipping the skeleton into one of the materials selected from the group consisting of molten aluminum, magnesium, aluminum-silicon alloys and aluminum-titanium alloys.
- the particles further include up to 2 percent Nb, up to 3 percent Mo, up to 0.03 percent BZr, the iron content being lower accordingly.
- the tiller made by dipping the skeleton into a molten material selected from the group consisting of silicate, Mg; Al; Al-Si alloys; or Al-Ti alloys for impregnation; and annealing the impregnated skeleton.
- the skeleton made by compressing and sintering particles comprising up to 0.5 percent C; 0.2 to 2.0 percent Si; 0.3 to 15 percent Mn; 10 to 25 percent Cr; 4 20 percent Ni; up to 10 percent W; up to 2 percent V; 0.2 to 3.0 percent N, the remainder Fe.
- the filler made by dipping the skeleton into a molten material selected from the group consisting of silicate; Mg; Al; Al-Si alloys; or Al-Ti alloys for impregnation; and annealing the impregnated skeleton.
- a molten material selected from the group consisting of silicate; Mg; Al; Al-Si alloys; or Al-Ti alloys for impregnation; and annealing the impregnated skeleton.
- the skeleton made by compressing and sintering steel particles comprising up to 0.3 percent C; up to 2 percent Si; up to 4.0 percent Mn; up to 22 percent Cr; up to 20 percent Mo; up to 8 percent W; up to l8 percent Co; up to 4 percent Ti; up to percent Al; up to 20 percent Fe; the remainder Ni, but at least 40 percent.
- Method as in claim 12 dipping the skeleton into one of the molten materials selected from the group consisting of silicate; Mg; Al; Al-Si alloys, and Al-Ti alloys for impregnation; and annealing the impregnated skeleton.
- the skeleton made by compressing and sintering steel particles comprising up to 0.60 percent C; up to 1 percent Si; 0.5 3 percent Mn; 10 22 percent Cr; 10 20 percent Ni; up to percent W; up to 4 percent Mo; up to 4 percent Nb; up to 4 percent Fe; N not exceeding a few percent; remainder Co, at least 22 percent.
- Method as in claim 14 dipping the skeleton into one of the molten materials selected from the group consisting of silicate; Mg; Al; Al-Si alloys; and Al-Ti alloys for impregnation; and annealing the impregnated skeleton.
- the steel of the particles compressed include at least one of the elements selected from the group consisting of carbon and nitrogen for the formation of carbide and nitride.
- Method of making a tool comprising the steps of compressing chromium-nickel-steel particles such as powder or flaky shavings to obtain a porous skeleton penetrated by a continuous network of pores of a total pore volume below 50 percent;
- a molten material selected from the group consisting of silicate, a salt such as a chloride and an aluminate.
- the chromiumnickel-steel comprises up to 0.5 percent C; 0.2 2.0 percent Si; 0.3 to 15 percent Mn; 10 25 percent Cr; 4 to 20 percent Ni; up to 10 percent W; and up to 2 percent V, the remainder being iron, all percentages by weight, the pore volume being about 20 to 30 percent:
- the chromiumnickel-steel comprises up to 0.5 percent C; 0.2 to 2.0 percent Si; 0.3 to 15 percent Mn; 10 to 25 percent Cr; 4-20 percent Ni; up to 10 percent W; up to 2 percent V; 0.2 to 3.0 percent N, remainder Fe.
- chromium-nickel-steel comprises up to 0.3 percent C; up to 2 percent Si; up to 4.0 percent Mn; up to 22 percent Cr; up to 20 percent Mo; up to 8 percent W; up to 18 percent Co; up to 4 percent Ti; up to 5 percent Al; up to 20 percent Fe; remainder Ni, but at least 40 percent.
- chromiumnickel-steel comprises up to 0.60 percent C; up to 1 percent Si; 0.5 3 percent Mn; 10 22 percent Cr; 10 20 percent Ni; up to 15 percent W; up to 4 percent Mo; up to 4 percent Nb; up to 4 percent Fe; N not exceeding a few percent; remainder Co, at least 22 percent.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Powder Metallurgy (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19702032814 DE2032814C (de) | 1970-06-29 | Werkzeug |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3837848A true US3837848A (en) | 1974-09-24 |
Family
ID=5775614
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00156029A Expired - Lifetime US3837848A (en) | 1970-06-29 | 1971-06-23 | Method of making tools by impregnating a steel skeleton with a carbide, nitride or oxide precursor |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3837848A (de) |
| AT (1) | AT305000B (de) |
| FR (1) | FR2099312A5 (de) |
| GB (1) | GB1354366A (de) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4738730A (en) * | 1986-02-18 | 1988-04-19 | Lindberg Corporation | Steam sealing for nitrogen treated ferrous part |
| RU2136479C1 (ru) * | 1998-06-01 | 1999-09-10 | Тульское государственное научно-исследовательское геологическое предприятие | Материал матриц алмазного и абразивного инструментов и способ его изготовления |
| US6110577A (en) * | 1997-02-14 | 2000-08-29 | Ngk Insulators, Ltd. | Composite material for heat sinks for semiconductor devices and method for producing the same |
| US20030136482A1 (en) * | 2002-01-23 | 2003-07-24 | Bohler Edelstahl Gmbh & Co Kg | Inert material with increased hardness for thermally stressed parts |
| EP1900835A1 (de) * | 2006-09-15 | 2008-03-19 | Haynes International, Inc. | Für die Festigkeitssteigerung durch Nitride geeignete Kobalt-Chrom-Eisen-Nickel-Legierungen |
| US7967605B2 (en) | 2004-03-16 | 2011-06-28 | Guidance Endodontics, Llc | Endodontic files and obturator devices and methods of manufacturing same |
| US11590571B2 (en) | 2019-10-25 | 2023-02-28 | Miba Sinter Austria Gmbh | Method for producing a sintered component |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE58908200D1 (de) * | 1988-02-25 | 1994-09-22 | Trw Motorkomponenten Gmbh & Co | Hartstofflegierung. |
| US5853506A (en) * | 1997-07-07 | 1998-12-29 | Ford Motor Company | Method of treating metal working dies |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2672426A (en) * | 1950-12-14 | 1954-03-16 | Mallory & Co Inc P R | Metal-ceramic bodies and method of making |
| US3031340A (en) * | 1957-08-12 | 1962-04-24 | Peter R Girardot | Composite ceramic-metal bodies and methods for the preparation thereof |
| US3201236A (en) * | 1962-08-24 | 1965-08-17 | Engelhard Ind Inc | Method of making metal bodies incorporated with non-metallic refractory material andproduct thereof |
| US3205565A (en) * | 1963-01-21 | 1965-09-14 | Clevite Corp | Sintered rubbing contact material and method for producing same |
| US3384464A (en) * | 1966-02-16 | 1968-05-21 | Mallory & Co Inc P R | Tungsten structures |
| US3419363A (en) * | 1967-05-01 | 1968-12-31 | Nasa | Self-lubricating fluoride-metal composite materials |
-
1971
- 1971-04-20 AT AT334971A patent/AT305000B/de not_active IP Right Cessation
- 1971-06-16 GB GB2808971A patent/GB1354366A/en not_active Expired
- 1971-06-23 US US00156029A patent/US3837848A/en not_active Expired - Lifetime
- 1971-06-25 FR FR7124190A patent/FR2099312A5/fr not_active Expired
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2672426A (en) * | 1950-12-14 | 1954-03-16 | Mallory & Co Inc P R | Metal-ceramic bodies and method of making |
| US3031340A (en) * | 1957-08-12 | 1962-04-24 | Peter R Girardot | Composite ceramic-metal bodies and methods for the preparation thereof |
| US3201236A (en) * | 1962-08-24 | 1965-08-17 | Engelhard Ind Inc | Method of making metal bodies incorporated with non-metallic refractory material andproduct thereof |
| US3205565A (en) * | 1963-01-21 | 1965-09-14 | Clevite Corp | Sintered rubbing contact material and method for producing same |
| US3384464A (en) * | 1966-02-16 | 1968-05-21 | Mallory & Co Inc P R | Tungsten structures |
| US3419363A (en) * | 1967-05-01 | 1968-12-31 | Nasa | Self-lubricating fluoride-metal composite materials |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4738730A (en) * | 1986-02-18 | 1988-04-19 | Lindberg Corporation | Steam sealing for nitrogen treated ferrous part |
| US6110577A (en) * | 1997-02-14 | 2000-08-29 | Ngk Insulators, Ltd. | Composite material for heat sinks for semiconductor devices and method for producing the same |
| US6479095B1 (en) | 1997-02-14 | 2002-11-12 | Ngk Insulators, Ltd. | Composite material for heat sinks for semiconductor devices and method for producing the same |
| RU2136479C1 (ru) * | 1998-06-01 | 1999-09-10 | Тульское государственное научно-исследовательское геологическое предприятие | Материал матриц алмазного и абразивного инструментов и способ его изготовления |
| US20030136482A1 (en) * | 2002-01-23 | 2003-07-24 | Bohler Edelstahl Gmbh & Co Kg | Inert material with increased hardness for thermally stressed parts |
| US7967605B2 (en) | 2004-03-16 | 2011-06-28 | Guidance Endodontics, Llc | Endodontic files and obturator devices and methods of manufacturing same |
| US10052173B2 (en) | 2004-03-16 | 2018-08-21 | Guidance Endodontics, Llc | Endodontic files and obturator devices and methods of manufacturing same |
| EP1900835A1 (de) * | 2006-09-15 | 2008-03-19 | Haynes International, Inc. | Für die Festigkeitssteigerung durch Nitride geeignete Kobalt-Chrom-Eisen-Nickel-Legierungen |
| US8075839B2 (en) | 2006-09-15 | 2011-12-13 | Haynes International, Inc. | Cobalt-chromium-iron-nickel alloys amenable to nitride strengthening |
| US11590571B2 (en) | 2019-10-25 | 2023-02-28 | Miba Sinter Austria Gmbh | Method for producing a sintered component |
Also Published As
| Publication number | Publication date |
|---|---|
| FR2099312A5 (de) | 1972-03-10 |
| AT305000B (de) | 1973-02-12 |
| GB1354366A (en) | 1974-06-05 |
| DE2032814A1 (de) | 1972-05-04 |
| DE2032814B2 (de) | 1972-05-04 |
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