US3853603A - Method for the chromizing of iron or ferrous alloy articles - Google Patents

Method for the chromizing of iron or ferrous alloy articles Download PDF

Info

Publication number
US3853603A
US3853603A US00306197A US30619772A US3853603A US 3853603 A US3853603 A US 3853603A US 00306197 A US00306197 A US 00306197A US 30619772 A US30619772 A US 30619772A US 3853603 A US3853603 A US 3853603A
Authority
US
United States
Prior art keywords
percent
iron
treating material
chromium
powdery
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US00306197A
Inventor
M Obayashi
J Endo
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toyota Central R&D Labs Inc
Original Assignee
Toyota Central R&D Labs Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toyota Central R&D Labs Inc filed Critical Toyota Central R&D Labs Inc
Application granted granted Critical
Publication of US3853603A publication Critical patent/US3853603A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/28Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
    • C23C10/34Embedding in a powder mixture, i.e. pack cementation
    • C23C10/36Embedding in a powder mixture, i.e. pack cementation only one element being diffused
    • C23C10/38Chromising
    • C23C10/40Chromising of ferrous surfaces
    • C23C10/42Chromising of ferrous surfaces in the presence of volatile transport additives, e.g. halogenated substances

Definitions

  • ABSTRACT A method for the chromizing of iron of ferrous alloy articles in powdery treating material comprising packing said iron or ferrous alloy articles in the mixed pow ders of sodium potassium or ammonium tetrafluoroborate and metallic chromium or ferrochromium and heating said articles within said mixed powders, thereby forming iron-chromium solid solution layers or chromium carbide layers on the surfaces of said articles.
  • the method of this invention can be performed without employing non-oxidative atmosphere.
  • This invention relates to the chromizing of iron and ferrous alloys including iron, steel and alloy steels, and
  • the powdery treating material is composed of chromium or ferrochromium powder and ammonium chloride powder, and iron or ferrous alloy to be treated is buried into the powdery treating material, and then it is heated at a high temperature near 1,000C in the hydrogen atmosphere or in the atmosphere of non-oxidation.
  • the high temperature treatment is, however, objectionable in view of the deterioration of the propaties of iron and ferrous alloy themselves and also the non-oxidation atmosphere makes the treatment complex and costly.
  • FIG. 1 is a micro photographic representation showing a chromium carbide layer on medium-carbon steel, which is formed according to Example 1;
  • FIGS. 2 to 4 are graphs obtained in Example I and showing the effects of the content of potassium tetrafluoroborate (KBF in the treating material, the heating temperature and the heating time on the thickness of chromium carbide layer formed on the surface of medium carbon steel.
  • FIG. 5 is a graph obtained in Example 2 and showing conditions, i.e. treating temperature and the content of potassium tetrafluorobor'ate, for forming the chromium carbide layer on the surface of a high carbon steel.
  • FIG. 6 is a micro photographic representation showing a chromium carbide layer on high carbon steel which is formed according to Example 2;
  • FIGS. 7 to 9 are graphs obtained in Example 3 and showing the effects of the content of KBF. in the treating material, the heating temperature and the heating time on the thickness of an iron-chromium solid solution layer formed on the surface of low carbon steel.
  • FIG. 10 is a micro photographic representation showing an iron-chromium solid solution layer on low carbon steel, which is formed according to Example 3;
  • FIGS. 11 and 12 are graphs obtained in Example 4 and showing the effects of the content of KBF, in the treating material and the heating temperature on the thickness of a layer formed on the surface of low carbon steel.
  • FIG. 13 is a micro photographic representation show ing a chromium carbide layer on low carbon ateel, which is formed according to Example 4;
  • FIG. 14 is a micro photographic representation showing a chromium carbide layer on pure iron is formed according to Example 5;
  • the present invention is directed to an improved pack method for the chromizing of iron and ferrous alloys and is characterized to use the mixed powders of sodium potassium and ammonium tetrafluoroborate and metallic chromium or ferro-chromium as the treating material.
  • the method of the present invention comprises preparing the mixed powders composed of said tetrafluoroborate and metallic chromium or ferrochromium, packing iron and ferrous alloy articles such as, iron, steel or alloy steel articles in said mixed powders and heating the articles within said mixed powders so as to form chromium carbide layers or iron-cromium solid solution layer on the surfaces of the articles.
  • a chromium carbide layer or an iron-chromium solid so lution layer can be definitely formed on the surface of the article.
  • the thus formed layer represent a high value of hardness and superior resistance performance against corrosion and oxidation.
  • the method according to this invention is thus highly suitable forthe surface treatment of tools, dies and parts for many kinds of equipments. It is highly productive, and it has been ascertained that the layer thus obtained is strongly and tightly bonded to the surface of mother article and has, in addition, a dense and continuous structure, thus obviating substantially the above mentioned various conventional drawbacks.
  • powdery treating material mixed powders of tetrafluoroborate, i.e. potassium tetrafluoroborate (KBFq), sodium tetrafluoroborate (NaBF and ammonium tetrafluoroborate (NI-I BF and metallic chromium orferrochromium are used.
  • the ferrochromium include low carbon ferrochromium and high carbon ferrochromium.
  • One or more than one kind of sodium potassium or ammonium tetrafluoroborates can be used in the powdery treating material.
  • both metallic chromium and ferrochromium can be added in the powdery treating material. It is preferable that these powders are selected to be 40 mesh or finer.
  • the powdery tetrafluoroborate may be added to the treating material in a quantity between. about 0.5 to percent by weight (hereinafter percent means percent by weight). With use of less quantity of tetrafluoroborate than 0.5 percent, the formation of the chromium carbide layer or the like would not be uniform and would be too slow to be accepted for the practical purpose.
  • the quantity of the tetrafluoroborate is between 1 to 20 percent.
  • the remainder of the treating material is powdery metallic chromium or ferrochromium, namely the metallic chromium or ferrochromium may be mixed in a quantity between 20 to 99.5 percent and preferably in a quantity between 80 to 99 percent.
  • inactive powdery substance having a high melting point such as alumina (A1 silica (SiO Boron nitride (BN), chr'omic oxide (Cr O and the like can be added up to the same quantity as that of the treating material.
  • alumina A1 silica (SiO Boron nitride (BN), chr'omic oxide (Cr O and the like can be added up to the same quantity as that of the treating material.
  • the heating temperature may be selected within the ture below 550C, the adequate thick chromium carbide or the like layer can not be formed on the surface of the article treated, and in the case that a temperature over I ,l200C is selected, the powdery treating material would become to be sintered and the article treated would become one body with the treating material. At this time, the property of alloy forming the article would be worsened.
  • the preferable range of the heatin the atmosphere of non-oxidation gas but the method can be carried into effect either under air atmosphere or inert gas atmosphere As the iron or ferrous alloy to be treated, iron, iron steel and alloy steels can be treated successfully.
  • chromium carbide layer and ironchromium solid solution layer are formed on the surfaces of iron and ferrous alloy. And each of said layers can be selectively formed by selectively using proper ferrous alloy and proper treating material.
  • the kind of the layer depends on the content of carbon in the ferrous alloy to be treated and in the ferrochromium of the powdery treating material. In the case that ferrous alloy to be treated contains more than 0.1 percent carbon, the layer formed on the surface of said ferrous alloy would be chromium carbide. And if the ferrochromium of the powdery treating material contains more than 1 percent carbon, the layer formed may be chromium carbide. In other cases, iron or ferrous alloy contains not more than 0.1 percent of carbon and the ferrochromium of the powdery treating material contains not more than 1 percent of carbon, the layer formed would be iron-chromium solid' solution.
  • the following table shows the combinations of the objects of the treatment, the kind of layer formed, the kind of metal in the powdery treating material and the kind of iron or ferrous alloy to be treated.
  • low carbon steel medium carbon steel high carbon steel ferrochromium torsion may be liable to occur in the articles by virtue of the transformation of ferrous alloy, which distortion must naturally be avoided by lowering the adopted higher heating temperature below 800C.
  • the heating time period depends upon the thickness of the carbide or the like layer to be formed.
  • the heating shorter than 30 minutes will, however, provide no practically acceptable information of said layer, although the final determination of the heating time period depends upon the heating temperature.
  • the thickness of said layer With increase of the heating time period, the thickness of said layer will be increased correspondingly.
  • an acceptable thickness of the layer can be realized within 30 hours or shorter time period.
  • the most preferable range of the heating time period will be 2 to-10 hours.
  • the microphotograph shown in FIG. 1 was taken from the specimen which was treated at 950C for 8 hours within the treating material composed of 3% 'KBF, and 97 percent low carbon ferrochromium.
  • said thickness gradually increases as each of the heating temperature and the heating time increases.
  • chromium carbide is formed by means of treating medium carbon steel in the mixed powder of low carbon ferrochromium and KBF., and the chromium layer of adequate thickness can be obtained by using a powdery treating material containing 1 to percent KBF EXAMPLE 2
  • specimens made of high carbon steel JIS 8K3, C: 1.00 1.10 percent, Si: less than 0.35 percent, Mn: less than 0.50 percent, Pz'less than 0.030 percent, S: less than 0.030 percent, balance of iron
  • FIG. 5 The result of the observation, whether chromium carbide layer was formed or V not, is shown in FIG. 5 with the relation of the treating conditions.
  • the ordinate and the abscissa represent the heating temperature and the content of KBF, in the treating material respectively, and the dot marks indicate that the chromium carbide layer of .a few microns for more in thickness was formed by the condition shown with each of said dot marks.
  • the treating temperature may be 600C or higher than 600C.
  • the microphotograph shown in FIG. 6 was taken from the specimen which was treated at 700C for 4 hours within the'treating material composed of 80% KBF, and 20 percent low carbon ferrochromium.
  • the microphotograph show the typical chromium carbide layer formed according to this Example.
  • EXAMPLE 3 By the same manner described in Example 1, specimens .made of low carbon steel (carbon content is about 0.05 percent). were treated at a temperature ranging from 900C to 1100C for 2 to hours in the powdery treating materials composed of 0.5 to 15% KBF, and 85 to,99.5 percent low carbon ferrochromium. Then, all of the specimens treated were cut and observed by a microscope. A few of the specimens were also treated by X-ray diffraction, by an X-ray micro analyzer and by a Vickers hardness tester. And it was recognized that an iron-chromium solid solution layer was formed within each of said speimens.
  • the content of chromium in said iron-chromium solid solution layer is 40 percent at the surface of said layer and decrease according to the distance from the surface. Also Hv 230 was measured on said layer.
  • the typical non-chromium solid solution layer formed according to this Example is shown in FIG. 10. The microphotograph shown in FIG. l0 was taken-from the speci men which was treated at 1,050C for 8 hours within the treating material composed of 3% KBF, and 97 percent low carbon ferrochromium.
  • FIGS. 7 to 9 are graphs obtained in this Example and showing the effects of the content of KBF, in the treating material, the heating temperature and the heating time on the thickness 'of the iron-chromium solid solution layer formed on the surface of low carbon steel.
  • the thickness of the layer formed decreases from about micron to 50 micron according to increasing the content of KBF, from 0.5 to 5 percent, the thickness of the layer becomes a constant value, 50 micron, in the higher content of KBF, than 5%.
  • the thickness of the layer increases rapidly according to increasing each of the heating temperature and time as shown in FIGS. 8 and 9 respectively.
  • EXAMPLE 4 Specimens made of low carbon steel (carbon content is about 0.05 percent) were treated at a temperature between 900 and 1150C for 5 hours in the powdery treating materials composed of 0.5 to 10% KBF and to 99.5 percent of high carbon ferrochromium (67 percent chromium, 4.9 percent carbon and the balance of iron) of mesh. All the specimens were cut and tested as same as the specimens in the Examples 1 to 3. In this Example two kinds of layer, the iron chromium solid solution layer and chromium carbide layer, were formed respectively.
  • the powdery treating material containing 1 percent or lower than 1% of the high carbon ferrochromium gave the iron chromium solid solution layer and the powdery treating material containing 2 percent or higher than 2 percent of the
  • the effects of the content of KBF, in the treating ma- I terial and of the heating temperature are shown in FIGS. 11 (obtained from the specimens treated at l,000C for 5 hours) and 12 (obtained from the specimens treated for 5 hours in the powdery treating material containing 10% KBF
  • the thickness of the layer formed decreases rapidly from about 38' micron to about 10 micron, according to increasing the content of KBF, from 0.5 to 2 percent and becomes a constant value, about 5 micron, in the higher content of KBF, than 2 percent.
  • the thickness of the layer formed' shows almost a constant value, about 5 micron at a temperature from 900 to 1000C and the thickness of the layer increases gradually according to increasing the heating temperature as shown in FIG. 12.
  • FIG. 13 As a typical layer formed in this Example, a microphotograph is shown in FIG. 13, which was taken from the specimen treated at 1,050 C for 5 hours in the powcarbon ferrochromium is employed as one of the essential elements of the treating material, the carbon of said ferrochromium'is introduced together with chromium into the low carbon steel during the treatment, and then chromium carbide layer can be formed even though the low carbon steel does not contain equough carbon to form the carbide.
  • the content of mation of thecarbide Namely the low content of KER, gives an iron-chromium solid solution layer, and the high content of KBF gives the chromium carbide layer.
  • Example 4 By the same manner described in Example 4, a specimen made of pure iron was treated at 1,150C for 5 hours in the powdery treating material composed of KBF and high carbon ferrochromium. By this treatment, a layer shown in FIG. 14 was formed. And it was recognized that the layer is chromium carbide.
  • treating material composed of 87 percent low carbon ferrochromium (65 percent chromium, 0.06 1 percent carbon and the balance of iron) of -l00 mesh, of 3 percent of KBF of 200 mesh and of 10 percent A1 0 of 325 mesh; b. treating material composed of 57 percent low carbon ferrochromium of l00 mesh, of 3 percent KBF of 200 mesh and of 40% SiO of 325 mesh;
  • treating material composed of 87 percent low carbon'ferrochromium of 100 mesh, of 3% KBF, of 200 mesh and 10% BN of 325 mesh.
  • a specimen made of low carbon steel was treated at 1,050C for 8 hours in the'following treating material (d) treating material composed of 87 percent low carbon ferrochromium of 100 mesh, of 3% KBR, of 200 mesh and of 10%'Cr O of 325 mesh.
  • treating material composed of 90 percent metallic chromium of --100 mesh and of 10% NaBF of l00 mesh;
  • treating material composed of 90 percent metallic KBF in the powdery treating material effects the forchromium of -l00 mesh and of 10% NH BF of 200 mesh;
  • a chromium carbide layer of about 15 micron in thickness was formed on each of said specimens.
  • treating material composed of 57 percent low carbon ferrochromium of l 00 mesh, of 3% KBF, of 200 mesh and of SiO of 250 mesh, treating temperature and time being 1,000C and 8 hours 3 5 respectively.
  • the specimen treated under the treating condition of (a) was formed a chromium carbide layer of about 13 microns in thickness, and the specimen treated under the treating condition of (b) was formed a chromium carbide layer of about 15 microns in thickness.
  • a method for the chromizing'of an iron or ferrous alloy article in powdery treating material comprising the steps of packing said article in the powdery treating 5 material consisting essentially of 0.5 to percent by weight of one member selected from the group consisting of potassium tetrafluoroborate, sodium tetrafluoroborate, ammonium tetrafluoroborate and the mixture thereof and 20 to 99.5 percent by weight of one member selected from the group consisting of metallic chromium, ferrochromium and the mixture thereof, heating said ferrous metal article within said powdery treating material at a temperature between 550 and 1,200C for 1 to 30 hours, and taking said article out of said powdery treating material, thereby forming a chromized layer on thesurface of said article.
  • a method according to claim 1, wherein said article is made of one selected from the group consisting of iron, steel and alloy steels.
  • said article is made of one member selected from the group consisting of pure iron and low carbon steel containing up to 0.1 percent by weight of carbon and said powdery percent of carbon and the mixture thereof.

Abstract

A method for the chromizing of iron of ferrous alloy articles in powdery treating material comprising packing said iron or ferrous alloy articles in the mixed powders of sodium potassium or ammonium tetrafluoroborate and metallic chromium or ferrochromium and heating said articles within said mixed powders, thereby forming iron-chromium solid solution layers or chromium carbide layers on the surfaces of said articles. The method of this invention can be performed without employing non-oxidative atmosphere.

Description

nie States i tent [191 Obayashi et a1.
[ METHOD FOR THE CHROMIZING OF IRON OR FERROUS ALLOY ARTICLES [75] Inventors: Mikio Obayashi; Junji Endo, both of Nagoyashi, Japan [73] Assignee: Kabushiki Kaisha Toyota Chuo Kenkyusho, Nagoyashi, Japan [22] Filed: Nov. 14, 1972 [21] Appl. No.: 306,197
[30] Foreign Application Priority Data Nov 16, 1971 Japan 46-91151 [52] U.S. Cl..... l17/l07.2 P, 117/106 C, 117/130 R [51] Int. Cl. C23c 9/02 [58] Field of Search 117/1072 P, 130 R, 106 C [5 6] References Cited UNITED STATES PATENTS 3,163,553 12/1964 Commandayetal ..ll7/lO7.2PX
3,257,230 6/1966 Wachtell et a1. 117/1072 P Primary Examiner-Leon D. Rosdol Assistant Examinerl-larris A. Pitlick Attorney, Agent, or Firm-Wenderoth, Lind & Ponack [57] ABSTRACT A method for the chromizing of iron of ferrous alloy articles in powdery treating material comprising packing said iron or ferrous alloy articles in the mixed pow ders of sodium potassium or ammonium tetrafluoroborate and metallic chromium or ferrochromium and heating said articles within said mixed powders, thereby forming iron-chromium solid solution layers or chromium carbide layers on the surfaces of said articles. The method of this invention can be performed without employing non-oxidative atmosphere.
8 Claims, 14 Drawing Figures PATENTEI, LEI I (H974 SHEET 2 0F 5 LII? 0 GIINTENT ITF IIBEI "/0 I E E: a 52;:
QM m A z. a $2: 5 @525 TREATING TIME I HRS.)
mm r
mmme TEMPERATURE c a 0 o o o 0 1020 304050601086 sin commoruam /o) THICKNESS 0F LAYER 00mm or m (94 IIlI] THIIIIINESS TIE LAYER I I U lv l I l 1 l I] 900 950 I000 I050 I100 I150 TREATING TEMPERATURE ("C I IIIII 5 B0- 0 2 so 0 TREATING TIME IIIIIS.)
PAEENEEE 5.853.603
srmsnrs Y'FG 40 I BGHTENT 01 11814 1 F IGJZ IRE TEMPERATURE (0 1 METHOD FOR THE CHROMIZING OF IRON OR FERROUS ALLOY ARTICLES This invention relates to the chromizing of iron and ferrous alloys including iron, steel and alloy steels, and
'more particularly it relates to the chromizing of iron and ferrous alloys packed in powdery treating material.
its corrosion resistance, its oxidation resistance and its wear resistance. And many different kinds of methods for the chromizing of iron and ferrous alloy have been suggested heretofore. The most commonly used method in practice is the so-called pack method by which iron and ferrous alloy to be treated is heated in powdery treating material- In this pack method, the powdery treating material is composed of chromium or ferrochromium powder and ammonium chloride powder, and iron or ferrous alloy to be treated is buried into the powdery treating material, and then it is heated at a high temperature near 1,000C in the hydrogen atmosphere or in the atmosphere of non-oxidation. The high temperature treatment is, however, objectionable in view of the deterioration of the propaties of iron and ferrous alloy themselves and also the non-oxidation atmosphere makes the treatment complex and costly.
It is an object .of this invention to provide an improved method for the chromizing of iron and ferrous alloy articles.
It is'another object of this invention to provide a method for the chromizing, which is simple in practice and less expensive.
. It is still another object of this invention to provide a powdery treating material that is capable of the chromizing in the air and at a relatively low temperature.
' It is a still further object of this invention to provide a powdery treating material that forms a chromium carbide layer or iron-chromium solid solution layer on the surface of an iron or ferrous alloy article.
Other, objects of the invention will appear hereinaftern The novel features that are considered characteristic of the invention are set forth with particularity in the appended claims. The invention, itself, as to its method of operation, together with additional objects and advantages thereof, will best be understood from the following description of specific embodiments when read in connection with the accompanying drawings, in which:
FIG. 1 is a micro photographic representation showing a chromium carbide layer on medium-carbon steel, which is formed according to Example 1;
FIGS. 2 to 4 are graphs obtained in Example I and showing the effects of the content of potassium tetrafluoroborate (KBF in the treating material, the heating temperature and the heating time on the thickness of chromium carbide layer formed on the surface of medium carbon steel.
FIG. 5 is a graph obtained in Example 2 and showing conditions, i.e. treating temperature and the content of potassium tetrafluorobor'ate, for forming the chromium carbide layer on the surface of a high carbon steel.
FIG. 6 is a micro photographic representation showing a chromium carbide layer on high carbon steel which is formed according to Example 2;
FIGS. 7 to 9 are graphs obtained in Example 3 and showing the effects of the content of KBF. in the treating material, the heating temperature and the heating time on the thickness of an iron-chromium solid solution layer formed on the surface of low carbon steel.
FIG. 10 is a micro photographic representation showing an iron-chromium solid solution layer on low carbon steel, which is formed according to Example 3;
FIGS. 11 and 12 are graphs obtained in Example 4 and showing the effects of the content of KBF, in the treating material and the heating temperature on the thickness of a layer formed on the surface of low carbon steel.
FIG. 13 is a micro photographic representation show ing a chromium carbide layer on low carbon ateel, which is formed according to Example 4;
FIG. 14 is a micro photographic representation showing a chromium carbide layer on pure iron is formed according to Example 5;
Broadly, the present invention is directed to an improved pack method for the chromizing of iron and ferrous alloys and is characterized to use the mixed powders of sodium potassium and ammonium tetrafluoroborate and metallic chromium or ferro-chromium as the treating material. Namely, the method of the present invention comprises preparing the mixed powders composed of said tetrafluoroborate and metallic chromium or ferrochromium, packing iron and ferrous alloy articles such as, iron, steel or alloy steel articles in said mixed powders and heating the articles within said mixed powders so as to form chromium carbide layers or iron-cromium solid solution layer on the surfaces of the articles. It has been found upon carrying out a large number of practical experiments that in this way, a chromium carbide layer or an iron-chromium solid so lution layer can be definitely formed on the surface of the article. The thus formed layer represent a high value of hardness and superior resistance performance against corrosion and oxidation. The method according to this invention is thus highly suitable forthe surface treatment of tools, dies and parts for many kinds of equipments. It is highly productive, and it has been ascertained that the layer thus obtained is strongly and tightly bonded to the surface of mother article and has, in addition, a dense and continuous structure, thus obviating substantially the above mentioned various conventional drawbacks.
As powdery treating material, mixed powders of tetrafluoroborate, i.e. potassium tetrafluoroborate (KBFq), sodium tetrafluoroborate (NaBF and ammonium tetrafluoroborate (NI-I BF and metallic chromium orferrochromium are used. Here the ferrochromium include low carbon ferrochromium and high carbon ferrochromium. One or more than one kind of sodium potassium or ammonium tetrafluoroborates can be used in the powdery treating material. Also both metallic chromium and ferrochromium can be added in the powdery treating material. It is preferable that these powders are selected to be 40 mesh or finer. The powdery tetrafluoroborate may be added to the treating material in a quantity between. about 0.5 to percent by weight (hereinafter percent means percent by weight). With use of less quantity of tetrafluoroborate than 0.5 percent, the formation of the chromium carbide layer or the like would not be uniform and would be too slow to be accepted for the practical purpose.
Too much addition of the fluoroborate than 80 percent wide range from 550 to 1200C. At a heating tempera- Therefore, the treating material is solidified after the treating process and it will be difficult to take the article treated out of the treating material and the treating material will be unusable repeatedly, and besides the surface condition of the article will not be well. Preferably, the quantity of the tetrafluoroborate is between 1 to 20 percent. The remainder of the treating material is powdery metallic chromium or ferrochromium, namely the metallic chromium or ferrochromium may be mixed in a quantity between 20 to 99.5 percent and preferably in a quantity between 80 to 99 percent. In order to prevent the solidification of the treating material inactive powdery substance having a high melting point such as alumina (A1 silica (SiO Boron nitride (BN), chr'omic oxide (Cr O and the like can be added up to the same quantity as that of the treating material.
The heating temperature may be selected within the ture below 550C, the adequate thick chromium carbide or the like layer can not be formed on the surface of the article treated, and in the case that a temperature over I ,l200C is selected, the powdery treating material would become to be sintered and the article treated would become one body with the treating material. At this time, the property of alloy forming the article would be worsened. The preferable range of the heatin the atmosphere of non-oxidation gas, but the method can be carried into effect either under air atmosphere or inert gas atmosphere As the iron or ferrous alloy to be treated, iron, iron steel and alloy steels can be treated successfully.
According to the method of the present invention,
two kinds of layers, chromium carbide layer and ironchromium solid solution layer are formed on the surfaces of iron and ferrous alloy. And each of said layers can be selectively formed by selectively using proper ferrous alloy and proper treating material. Generally, the kind of the layer depends on the content of carbon in the ferrous alloy to be treated and in the ferrochromium of the powdery treating material. In the case that ferrous alloy to be treated contains more than 0.1 percent carbon, the layer formed on the surface of said ferrous alloy would be chromium carbide. And if the ferrochromium of the powdery treating material contains more than 1 percent carbon, the layer formed may be chromium carbide. In other cases, iron or ferrous alloy contains not more than 0.1 percent of carbon and the ferrochromium of the powdery treating material contains not more than 1 percent of carbon, the layer formed would be iron-chromium solid' solution.
The following table shows the combinations of the objects of the treatment, the kind of layer formed, the kind of metal in the powdery treating material and the kind of iron or ferrous alloy to be treated.
low carbon steel medium carbon steel high carbon steel ferrochromium torsion may be liable to occur in the articles by virtue of the transformation of ferrous alloy, which distortion must naturally be avoided by lowering the adopted higher heating temperature below 800C.
The heating time period depends upon the thickness of the carbide or the like layer to be formed. The heating shorter than 30 minutes will, however, provide no practically acceptable information of said layer, although the final determination of the heating time period depends upon the heating temperature. With increase of the heating time period, the thickness of said layer will be increased correspondingly. In practice, an acceptable thickness of the layer can be realized within 30 hours or shorter time period. The most preferable range of the heating time period will be 2 to-10 hours.
It is not necessary to carry out the method according to this invention in the atmosphere of hydrogen gas or EXAMPLE 1 Several kinds of powdery treating materials composed of to 99 percent low carbon ferrochromium (65 percent chromium, 0.06 percent carbon and the balance of iron powder of 200 mesh and the balance of KBF, of 200 mesh were introduced into in each of iron containers of 50 mm inner diameter and 40 mm height, and then specimens, 5 mm thick, 10 mm wide and 10 mm long, made of medium carbon steel (118 855C; C 0.52 0.58 percent, Si: 0.15 0.35 percent, Mn: 0.60 0.90 percent, P: less than 0.030 percent, S less than 0.035 percent, balance of iron) were packed in each of said treating material in said container and were heated in the air at a different temperature between 900 and l,050C for 2 to 15 hours, then they were cooled in the air. All of the specimens were cut to be observed their cross sections by a microscope. A few of the specimens were also tested by X-ray diffraction. And it was recognized that a chromium carbide layer was formed on the surface of each of said specimens, and it was confirmed that said layer is composed of the chromium carbide such as Cr Co or Cr-,C And also Vickers hardness of said layer was measured about y s Hv 1,800, equal to the bulk of the chromium carbide.
The microphotograph shown in FIG. 1; was taken from the specimen which was treated at 950C for 8 hours within the treating material composed of 3% 'KBF, and 97 percent low carbon ferrochromium. The
ances, from 1 to. 10. percent in the content of KBF,.
However, as shown in FIGS. 2 and 3, said thickness gradually increases as each of the heating temperature and the heating time increases.
According to the embodiment described above, it is apparent that chromium carbide is formed by means of treating medium carbon steel in the mixed powder of low carbon ferrochromium and KBF.,, and the chromium layer of adequate thickness can be obtained by using a powdery treating material containing 1 to percent KBF EXAMPLE 2 By the same manner described in Example 1, specimens made of high carbon steel (JIS 8K3, C: 1.00 1.10 percent, Si: less than 0.35 percent, Mn: less than 0.50 percent, Pz'less than 0.030 percent, S: less than 0.030 percent, balance of iron) were treated at a temperature between 600 and 1050C for 4 hours in the powdery treating materials composed of 20 to 98 percent of low carbon ferrochromium and 2 to 80 percent of KBF Then, all of the specimens treated were cut and observed by a microscope. The result of the observation, whether chromium carbide layer was formed or V not, is shown in FIG. 5 with the relation of the treating conditions. In FIG. 5, the ordinate and the abscissa represent the heating temperature and the content of KBF, in the treating material respectively, and the dot marks indicate that the chromium carbide layer of .a few microns for more in thickness was formed by the condition shown with each of said dot marks. As known from the figure, in order to form an adequate thickness of the layer, the treating temperature may be 600C or higher than 600C.
The microphotograph shown in FIG. 6 was taken from the specimen which was treated at 700C for 4 hours within the'treating material composed of 80% KBF, and 20 percent low carbon ferrochromium. The microphotograph show the typical chromium carbide layer formed according to this Example.
EXAMPLE 3 By the same manner described in Example 1, specimens .made of low carbon steel (carbon content is about 0.05 percent). were treated at a temperature ranging from 900C to 1100C for 2 to hours in the powdery treating materials composed of 0.5 to 15% KBF, and 85 to,99.5 percent low carbon ferrochromium. Then, all of the specimens treated were cut and observed by a microscope. A few of the specimens were also treated by X-ray diffraction, by an X-ray micro analyzer and by a Vickers hardness tester. And it was recognized that an iron-chromium solid solution layer was formed within each of said speimens. The content of chromium in said iron-chromium solid solution layer is 40 percent at the surface of said layer and decrease according to the distance from the surface. Also Hv 230 was measured on said layer. The typical non-chromium solid solution layer formed according to this Example is shown in FIG. 10. The microphotograph shown in FIG. l0 was taken-from the speci men which was treated at 1,050C for 8 hours within the treating material composed of 3% KBF, and 97 percent low carbon ferrochromium.
FIGS. 7 to 9 are graphs obtained in this Example and showing the effects of the content of KBF, in the treating material, the heating temperature and the heating time on the thickness 'of the iron-chromium solid solution layer formed on the surface of low carbon steel.
. As shown in FIG. 7, the thickness of the layer formed decreases from about micron to 50 micron according to increasing the content of KBF, from 0.5 to 5 percent, the thickness of the layer becomes a constant value, 50 micron, in the higher content of KBF, than 5%. With regard to the heating temperature and the heating time, the thickness of the layer increases rapidly according to increasing each of the heating temperature and time as shown in FIGS. 8 and 9 respectively.
EXAMPLE 4 Specimens made of low carbon steel (carbon content is about 0.05 percent) were treated at a temperature between 900 and 1150C for 5 hours in the powdery treating materials composed of 0.5 to 10% KBF and to 99.5 percent of high carbon ferrochromium (67 percent chromium, 4.9 percent carbon and the balance of iron) of mesh. All the specimens were cut and tested as same as the specimens in the Examples 1 to 3. In this Example two kinds of layer, the iron chromium solid solution layer and chromium carbide layer, were formed respectively. The powdery treating material containing 1 percent or lower than 1% of the high carbon ferrochromium gave the iron chromium solid solution layer and the powdery treating material containing 2 percent or higher than 2 percent of the The effects of the content of KBF, in the treating ma- I terial and of the heating temperature are shown in FIGS. 11 (obtained from the specimens treated at l,000C for 5 hours) and 12 (obtained from the specimens treated for 5 hours in the powdery treating material containing 10% KBF As shown in FIG. 11, the thickness of the layer formed decreases rapidly from about 38' micron to about 10 micron, according to increasing the content of KBF, from 0.5 to 2 percent and becomes a constant value, about 5 micron, in the higher content of KBF, than 2 percent. With regard to the heating temperature, the thickness of the layer formed'shows almost a constant value, about 5 micron at a temperature from 900 to 1000C and the thickness of the layer increases gradually according to increasing the heating temperature as shown in FIG. 12.
As a typical layer formed in this Example, a microphotograph is shown in FIG. 13, which was taken from the specimen treated at 1,050 C for 5 hours in the powcarbon ferrochromium is employed as one of the essential elements of the treating material, the carbon of said ferrochromium'is introduced together with chromium into the low carbon steel during the treatment, and then chromium carbide layer can be formed even though the low carbon steel does not contain equough carbon to form the carbide. However, the content of mation of thecarbide. Namely the low content of KER, gives an iron-chromium solid solution layer, and the high content of KBF gives the chromium carbide layer.
EXAMPLE By the same manner described in Example 4, a specimen made of pure iron was treated at 1,150C for 5 hours in the powdery treating material composed of KBF and high carbon ferrochromium. By this treatment, a layer shown in FIG. 14 was formed. And it was recognized that the layer is chromium carbide.
EXAMPLE 6 Specimens made of high carbon steel JlS 8K3 (C:l.00l.l0 percent, Si: less than 0.35 percent, Mn: less than 0.50 percent, P: less than 0.030 percent, S: less than 0.030 percent) were treated at 1,000C for 5 hours in each of the following powdery treating materials (a), (b) and (c). i
a. treating material composed of 87 percent low carbon ferrochromium (65 percent chromium, 0.06 1 percent carbon and the balance of iron) of -l00 mesh, of 3 percent of KBF of 200 mesh and of 10 percent A1 0 of 325 mesh; b. treating material composed of 57 percent low carbon ferrochromium of l00 mesh, of 3 percent KBF of 200 mesh and of 40% SiO of 325 mesh;
c. treating material composed of 87 percent low carbon'ferrochromium of 100 mesh, of 3% KBF, of 200 mesh and 10% BN of 325 mesh.
A specimen made of low carbon steel was treated at 1,050C for 8 hours in the'following treating material (d) treating material composed of 87 percent low carbon ferrochromium of 100 mesh, of 3% KBR, of 200 mesh and of 10%'Cr O of 325 mesh.
The specimens treated in each of the treating material (a), (b) and (c) mentioned above were formed badly the formation of the layers.
EXAMPLE 7 '7 Specimens made of JIS 8K3 were treated at 1,000C
for 5 hours in each of the following treating materials;
a. treating material composed of 97 percent metallic chromium of l00 mesh and of 3% KBF of 200 mesh;
b. treating material composed of 97 percent metallic 5 chromium of l00 mesh and of 3% NaBF, of 100 mesh;
c. treating material composed of 90 percent metallic chromium of --100 mesh and of 10% NaBF of l00 mesh;
10 d. treating material composed of 90 percent metallic KBF in the powdery treating material effects the forchromium of -l00 mesh and of 10% NH BF of 200 mesh; Y e. treating material composed of 77 percent metallic chromium of 100 mesh, of 3% NaBF of -l00, mesh and of percent A1 0 of 325 mesh.
By the treatments described above, a chromium carbide layer of about 15 micron in thickness was formed on each of said specimens.
EXAMPLE 8 Specimens made of alloy steel (JIS SKDll: 1.5% c,
12% Cr, 1.0% M0, 0.4% V, and the balance of iron) being 1,050C and 8 hours respectively;
b. treating material composed of 57 percent low carbon ferrochromium of l 00 mesh, of 3% KBF, of 200 mesh and of SiO of 250 mesh, treating temperature and time being 1,000C and 8 hours 3 5 respectively.
The specimen treated under the treating condition of (a) was formed a chromium carbide layer of about 13 microns in thickness, and the specimen treated under the treating condition of (b) was formed a chromium carbide layer of about 15 microns in thickness.
What is claimed is:
l. A method for the chromizing'of an iron or ferrous alloy article in powdery treating material, comprising the steps of packing said article in the powdery treating 5 material consisting essentially of 0.5 to percent by weight of one member selected from the group consisting of potassium tetrafluoroborate, sodium tetrafluoroborate, ammonium tetrafluoroborate and the mixture thereof and 20 to 99.5 percent by weight of one member selected from the group consisting of metallic chromium, ferrochromium and the mixture thereof, heating said ferrous metal article within said powdery treating material at a temperature between 550 and 1,200C for 1 to 30 hours, and taking said article out of said powdery treating material, thereby forming a chromized layer on thesurface of said article.
2. A method according to claim 1, wherein an inactive powdery material selected from the group consisting of alumina, silica, boron nitride, chromium oxide and the mixture thereof is added to said powdery treating material.
3. A method according to claim 1, wherein said article is made of one selected from the group consisting of iron, steel and alloy steels.
4. A method according to claim 1, wherein said ferrochromium contains carbon.
5. A method according to claim 1, wherein said powdery treating material is of 40 mesh or finer.
LII
6. ,A method according to claim 1, wherein said arti- I cle is made of steel containing at least 0.1 percent by weight of carbon.
7. A method according to claim 1, wherein said ferrochromium contains more than 1 percent by weight of carbon.
8. A method according to claim 1, wherein said article is made of one member selected from the group consisting of pure iron and low carbon steel containing up to 0.1 percent by weight of carbon and said powdery percent of carbon and the mixture thereof.

Claims (8)

1. A METHOD FOR THE CHROMIZING OF AN IRON OR FERROUS ALLOY ARTICLE IN POWDERY TREATING MATERIAL, COMPRISING THE STEPS OF PACKING SAID ARTICLE IN THE POWDERY TREATING MATERIAL CONSISTING ESSENTIALLY OF 0.5 TO 80 PERCENT BY WEIGHT OF ONE MEMBER SELECTED FROM THE GROUP CONSISTING OF POTASSIUM TETRAFLUOROBORATE, SODIUM TETRAFLUOROBORATE, AMMONIUM TETRAFLUOROBORATE AND THE MIXTURE THEREOF AND 20 TO 99.5 PERCENT BY WEIGHT OF ONE MEMBER SELECTED FROM THE GROUP CONSISTING OF METALLIC
2. A method according to claim 1, wherein an inactive powdery material selected from the group consisting of alumina, silica, boron nitride, chromium oxide and the mixture thereof is added to said powdery treating material.
3. A method according to claim 1, wherein said article is made of one selected from the group consisting of iron, steel and alloy steels.
4. A method according to claim 1, wherein said ferrochromium contains carbon.
5. A method according to claim 1, wherein said powdery treating material is of 40 mesh or finer.
6. A method according to claim 1, wherein said article is made of steel containing at least 0.1 percent by weight of carbon.
7. A method according to claim 1, wherein said ferrochromium contains more than 1 percent by weight of carbon.
8. A method according to claim 1, wherein said article is made of one member selected from the group consisting of pure iron and low carbon steel containing up to 0.1 percent by weight of carbon and said powdery treating material consisting essentially of 0.5 to 80 percent by weight of one member selected from the group consisting of potassium tetrafluoroborate, sodium tetrafluoroborate, ammonium tetrafluoroborate and the mixture thereof and 20 to 99.5 percent by weight of one member selected from the group consisting of metallic chromium, ferrochromium containing up to 1 percent of carbon and the mixture thereof.
US00306197A 1971-11-16 1972-11-14 Method for the chromizing of iron or ferrous alloy articles Expired - Lifetime US3853603A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP46091151A JPS5120017B2 (en) 1971-11-16 1971-11-16

Publications (1)

Publication Number Publication Date
US3853603A true US3853603A (en) 1974-12-10

Family

ID=14018501

Family Applications (1)

Application Number Title Priority Date Filing Date
US00306197A Expired - Lifetime US3853603A (en) 1971-11-16 1972-11-14 Method for the chromizing of iron or ferrous alloy articles

Country Status (5)

Country Link
US (1) US3853603A (en)
JP (1) JPS5120017B2 (en)
CA (1) CA969454A (en)
DE (1) DE2255997C3 (en)
GB (1) GB1369344A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070172693A1 (en) * 2005-02-03 2007-07-26 Honda Motor Co., Ltd. Fe base alloy having layer and method for production thereof
WO2013070314A1 (en) * 2011-09-13 2013-05-16 Rexnord Industries, Llc Article with wear- resistant coating and method of forming same

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5836059B2 (en) * 1975-03-14 1983-08-06 新日本製鐵株式会社 Okugaimtosousyounotameno
US4232098A (en) * 1978-03-22 1980-11-04 Electric Power Research Institute, Inc. Sodium-sulfur cell component protected by a high chromium alloy and method for forming
FR2483468A2 (en) * 1980-05-29 1981-12-04 Creusot Loire IMPROVEMENT IN THE CHROMIZATION OF STEELS BY GAS
WO2005075699A1 (en) * 2004-02-03 2005-08-18 Honda Motor Co., Ltd. Fe BASE ALLOY HAVING LAYER AND METHOD FOR PRODUCTION THEREOF
DE102012204614A1 (en) * 2012-03-22 2013-09-26 Man Diesel & Turbo Se Manufacturing cast part used as cylinder heads for diesel engine, comprises introducing melted cast material into cavity of mold, solidifying cast material, and partially introducing additive into cast material to modify properties
CN104815980A (en) * 2015-03-26 2015-08-05 海门市金易焊接材料有限公司 Low-carbon ferrochromium powder

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3163553A (en) * 1958-10-27 1964-12-29 Chromizing Corp Process of diffusing metal into the surface of sheet metal
US3257230A (en) * 1964-03-24 1966-06-21 Chromalloy American Corp Diffusion coating for metals

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3163553A (en) * 1958-10-27 1964-12-29 Chromizing Corp Process of diffusing metal into the surface of sheet metal
US3257230A (en) * 1964-03-24 1966-06-21 Chromalloy American Corp Diffusion coating for metals

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070172693A1 (en) * 2005-02-03 2007-07-26 Honda Motor Co., Ltd. Fe base alloy having layer and method for production thereof
WO2013070314A1 (en) * 2011-09-13 2013-05-16 Rexnord Industries, Llc Article with wear- resistant coating and method of forming same

Also Published As

Publication number Publication date
GB1369344A (en) 1974-10-02
JPS5120017B2 (en) 1976-06-22
DE2255997A1 (en) 1973-05-24
DE2255997B2 (en) 1977-09-15
DE2255997C3 (en) 1978-05-24
CA969454A (en) 1975-06-17
JPS4855840A (en) 1973-08-06

Similar Documents

Publication Publication Date Title
DE2758618A1 (en) HIGH TEMPERATURE-RESISTANT, ABRASION-RESISTANT COATING COMPOSITION
US3853603A (en) Method for the chromizing of iron or ferrous alloy articles
US3837901A (en) Diffusion-coating of nickel-base superalloy articles
JP3017764B2 (en) Abrasion resistant composite roll and method for producing the same
US4090874A (en) Method for improving the sinterability of cryogenically-produced iron powder
US3719518A (en) Process of forming a carbide layer of vanadium, niobium or tantalum upon a steel surface
US4835011A (en) Yttrium enriched aluminide coatings
Mehan et al. Interaction between silicon carbide and a nickel-based superalloy at elevated temperatures
US3013875A (en) Method of manufacturing homogeneous carbides
US3861938A (en) Protective coating for metals
Knotek et al. Surface layers on cobalt base alloys by boron diffusion
JPS60181203A (en) Method for forming sintered layer on surface of metallic base body
EP0262774B1 (en) Wear-resistant sintered iron article
US4357182A (en) Chromization of steels by gas process
US3157532A (en) Methods of treating metallic powders
US5071473A (en) Uniform coarse tungsten carbide powder and cemented tungsten carbide article and process for producing same
Sands et al. The corrosion resistance of sintered austenitic stainless steel
US5000782A (en) Powder mixture for making yttrium enriched aluminide coatings
US4007302A (en) Case-hardening method for carbon steel
US3912827A (en) Method for forming a chromium carbide layer on the surface of an iron, ferrous alloy or cemented carbide article
US3885064A (en) Method for forming a chromium carbide layer on the surface of an iron, ferrous alloy or cemented carbide article
Glowacki et al. On some features of chromium carbide diffusion layer formation
US3874909A (en) Method for forming a carbide layer on the surface of an iron or ferrous alloy article
US3857725A (en) Method for forming an iron-manganese carbide layer on the surface of an iron base alloy article containing carbon
Khusid et al. Wear of carburized high chromium steels