WO2014162196A2 - Stainless steel and method of manufacturing the same - Google Patents
Stainless steel and method of manufacturing the same Download PDFInfo
- Publication number
- WO2014162196A2 WO2014162196A2 PCT/IB2014/000473 IB2014000473W WO2014162196A2 WO 2014162196 A2 WO2014162196 A2 WO 2014162196A2 IB 2014000473 W IB2014000473 W IB 2014000473W WO 2014162196 A2 WO2014162196 A2 WO 2014162196A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- stainless steel
- superficial layer
- chromium
- base material
- layer
- 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.)
- Ceased
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F21/00—Constructions of heat-exchange apparatus characterised by the selection of particular materials
- F28F21/08—Constructions of heat-exchange apparatus characterised by the selection of particular materials of metal
- F28F21/081—Heat exchange elements made from metals or metal alloys
- F28F21/082—Heat exchange elements made from metals or metal alloys from steel or ferrous alloys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/011—Layered products comprising a layer of metal all layers being exclusively metallic all layers being formed of iron alloys or steels
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/74—Methods of treatment in inert gas, controlled atmosphere, vacuum or pulverulent material
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/74—Methods of treatment in inert gas, controlled atmosphere, vacuum or pulverulent material
- C21D1/773—Methods of treatment in inert gas, controlled atmosphere, vacuum or pulverulent material under reduced pressure or vacuum
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/004—Heat treatment of ferrous alloys containing Cr and Ni
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/54—Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/06—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases
- C23C10/08—Solid state diffusion of only metal elements or silicon into metallic material surfaces using gases only one element being diffused
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/60—After-treatment
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/04—Treatment of selected surface areas, e.g. using masks
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
- C23C8/08—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
- C23C8/24—Nitriding
- C23C8/26—Nitriding of ferrous surfaces
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/80—After-treatment
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features
- F01N13/16—Selection of particular materials
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/001—Austenite
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N2510/00—Surface coverings
- F01N2510/08—Surface coverings for corrosion prevention
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N2510/00—Surface coverings
- F01N2510/10—Surface coverings for preventing carbon deposits, e.g. chromium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N2530/00—Selection of materials for tubes, chambers or housings
- F01N2530/02—Corrosion resistive metals
- F01N2530/04—Steel alloys, e.g. stainless steel
Definitions
- the invention relates to a stainless steel and a method of manufacturing the same.
- the invention relates to a stainless steel suitable for exhaust system component that require anticorrosion against both of general corrosion and local corrosion, and a method of manufacturing the same.
- the present invention provides a low cost stainless steel that can be used for a long time also under an environment where both of the general corrosion and the local corrosion occur and a method of manufacturing the same.
- a stainless steel that contains cliromium and other alloying elements as a plurality of alloying elements includes: a base material layer, the base material layer including chromium at a specified cliromium content necessary for forming a passive film or more; and a superficial layer, the superficial layer including cliromium at a lower chromium content than that the chromium content contained in the base material layer, and the superficial layer including the other alloying elements at a same content of the other alloying element as the content of the other alloying element contained in the base material layer.
- a superficial layer becomes a sacrificing layer against the local conosion by significantly reducing only a chromium content in the superficial lay er than that of the base material layer.
- the corrosion resistance against the local corrosion can be imparted to the superficial layer. Accordingly, sufficient corrosion resistance against both of the general corrosion and the local corrosion such as the pitting corrosion can be shown, without increasing an alloying element or applying a surface treatment.
- the chromium content contained in the superficial layer may be low er than the specified chromium content.
- a stainless steel includes: a base material layer, the base material layer including chromium and other al loying element as a plurality of alloying elements; and a superficial layer, the superficial layer including the chromium and other alloying element as a plurality of alloying elements, the chromium content contained in the superficial layer being less than the specified chromium content necessary for forming a passive film, a difference between the chromium content contai ned in the base material layer and the chromium content contained in the superficial layer being larger than a difference between the content of the other alloying element contained in the base material layer and the content of the other alloying element contained in the superficial layer.
- the stainless steel since the stainless steel has the chromium content of the superficial layer, which is less than the specified chromium content necessary for forming a passive fi lm, the passive film is not formed in the superficial layer and the corrosion resistance against the general corrosion is degraded. However, the local corrosion such as the pitting corrosion which proceeds with defects as a starting point on the assumption of a strong film in the outermost surface can be suppressed from occurring. On the other hand, in the base material layer, since the chromium content capable of forming and regenerating a passive film is secured, the corrosion can effectively be suppressed from proceeding.
- the superficial layer can be a sacrificing layer against the local corrosion by significantly reducing only the chromium content in the superficial layer than that in the base material layer.
- the corrosion resistance to the local corrosion can be imparted to the superficial layer. Accordingly, sufficient corrosion resistance against both of the general corrosion and the local corrosion such as the pitting corrosion can sufficiently be shown without increasing an amount of alloying element or applying surface treatment.
- the other al loy ing element may be an additional element for improving the corrosion resistance of each of the base material layer and the superficial layer.
- the corrosion resistance in the superficial layer can be obtained by the other alloying elements and an advance speed of the general corrosion can be suppressed.
- the chromium content contained in the superficial layer may be less than 1 1 %.
- a passive fi lm is not substantial ly formed, and the corrosion resistance against the general corrosion is degraded thereby.
- the local corrosion such as the pitting corrosion that proceeds w ith defects as a starting point on the assumption of existence of a strong film on the outermost surface can effectively be suppressed from occurring.
- the superficial layer may form a part of an inner wall surface of an exhaust path of an internal combustion engine, and an exhaust system component may be formed w ith the base material layer and the superficial layer.
- a method of manufacturing a stainless steel comprising: preparing a stainless steel raw material that includes a base material layer and a superficial layer, both of which include chromium and other alloying elements as a plurality of alloying elements : disposing at least the superficial layer of the stainless steel raw material under a low pressure environment, the low pressure env ironment is an environment of lower pressure than atmospheric pressure; and heating at least the superficial layer of the stainless steel raw material to a treatment temperature is higher than a vaporizing temperature of the chromium under the low pressure environment and lower than vaporizing temperatures of the other alloying elements under the low pressure environment.
- chromium is gradually vaporized from the superficial layer by heating the superficial layer of the stainless steel material at a treatment temperature that is higher than a vaporizing temperature of the chromium and lower than vaporizing temperatures of the other alloying elements under the low pressure environment. Therefore, a dechromization process in which in accordance w ith a treatment time of depressurization and heating, the chromium content in the superficial layer can be set lower than the chromium content in the base material layer proceeds.
- a stainless steel having a hybrid structure in which the superficial layer becomes an alloy steel that is strong against the local corrosion such as the pitting corrosion and contains other al loying elements, and the base material layer is strong against the general corrosion is manufactured.
- a high con osion resistant stainless steel that can be used for a long term even under an environment w here both of the general corrosion and the local corrosion may occur can be obtained.
- a method of manufacturing a stainless steel comprising: preparing a stainless steel raw material that includes a base material layer containing chromium and other alloying elements as a plurality of alloying elements and a superficial layer that includes chromium and other alloying elements as a plurality of alloying elements; heating at least the superficial layer of the stainless steel raw material at a predetennined temperature; and exposing at least the superficial layer of the stainless steel raw material under an env ironment that is an environment of lower vapor pressure than a vapor pressure of the chromium under the predetennined temperature and higher than vapor pressures of the other alloying elements under the predetermined temperature.
- a dechromization treatment proceeds, in which the chromium content contained in the superficial layer can be set lower than the chromium content contained in the base material layer corresponding to a treatment time of depressurization and heating under a high temperature and lo pressure environment.
- a method of manufacturing a low cost stainless steel that can show sufficient corrosion resistance against both of the general corrosion and the local corrosion such as the pitting corrosion can be obtained without increasing an amount of the alloying element and w ithout applying the surface treatment.
- a stainless steel having a hybrid structure in which the superficial layer becomes an alloy lay er that is strong to the local corrosion such as the pitting corrosion and contains other alloying elements and the base material layer is strong against the general corrosion is manufactured.
- the stainless steel raw material is dechromized in the ranges of the heating temperature and reduced pressure that are on a gas phase side from a vapor pressure curve of chromium in a vapor pressure diagram of metal and on a gas phase and solid phase side of the other alloying elements.
- the content of the other alloying element contained in the superficial layer is the same as those of the base material layer, and the chromium content contained in the superficial layer is lower than the chromium content in the base material layer.
- FIG. 1 is a diagram for describing a rough structure of a stainless steel according to an embodiment of the present inv ention and a corrosion resistance thereof;
- FIG. 2 is a diagram for describing a change of a chromium concentration distribution corresponding to a depth from an outermost surface due to a difference in a heat treatment condition during a dechromization process according to the embodiment of the present invention and a chromium concentration distribution for each thereof;
- FIG. 3A is a diagram for describing a dechromization treatment of a stainless steel according to the embodiment of the present inv ention:
- FIG. 3 B is a graph that shows a chromium concentration distribution corresponding to a depth after the dechromization process according to the embodiment
- FIG. 3C is a graph that shows concentration distributions of other alloying elements after the dechromization treatment according to the embodiment.
- FIG. 4 is a schematic configuration diagram of a dechromization treatment system for perfomiing a method of manufacturing a stainless steel according to the embodiment of the present invention:
- FIG. 5 is a vapor pressure curve il lustrating a treatment condition of the dechromization treatment according to the embodiment of the present invention.
- FIG. 6 is a flowchart that shows a rough process of the dechromization treatment of the stainless steel according to the embodiment of the present invention.
- FIG. 7 is a list of treatment conditions and test results, in which heat treatment conditions of a plurality of examples according to the embodiment of the present invention and test results of the corrosion resistance thereof are shown by comparing with comparative examples;
- FIG. 8A is a graph that shows a concentration distribution for each of alloying elements corresponding to a depth from a surface after the dech omization treatment of the embodiment of the present invention:
- FIG. 8B is a graph that shows a concentration distribution for each of alloying elements corresponding to a depth from a surface after heat treatment of comparative example:
- FIG. 9 is a diagram for describing corrosion test results of Examples 1 to 3 and Comparativ e Examples 1 to 6 of the present invention.
- FIG. 1 to FIG. 9 are diagrams for describing a stainless steel according to one embodiment of the present inv ention and a method of manufacturing the same.
- the stainless steel according to the present embodiment includes chromium and other alloying elements, all of which are not shown in FIG. 1 as a plurality of alloying elements, and has SUS 31 6L (JIS Standard) that is an austenitic stainless steel, for example, as a raw material (host material ).
- SUS 31 6L JIS Standard
- a stainless steel 10 As shown in FIG. 1 . a stainless steel 10 according to the present embodiment includes a base material layer 1 1 in which chromium is contained at a specified chromium content necessary for forming a passiv e film or more and a superficial layer 12 hav ing a predetermined layer thickness, which is integrally formed w ith the base material layer 1 1 .
- the superficial layer 1 2 forms a part of an inner wall surface of an exhaust path of an internal combustion engine, for example, a part of an inner wall surface of an EGR gas path which has an EGR cooler, and the base material layer 1 1 and the superficial layer 1 2 form an exhaust system component.
- the stainless steel of the present invention may be one that is used for other exhaust system components other than the EGR cooler, and may be one that is used for other than exhaust system components.
- the base material layer 1 1 is a layer of a raw material of the stainless steel 10, for example. SUS 16L as it is. and includes, in addition to chromium ( Cr) and iron ( Fe ). other alloying elements such as nickel (Ni ). molybdenum (Mo) and nitrogen (N) each at a predetermined content.
- the base material layer 1 1 includes 1 7.3 1 wt° o of chromium (Cr). I 2.09wi% of nickel (Ni). 2.05wt% of molybdenum (Mo). of nitrogen (N) and the balance of iron (Fe).
- ° ⁇ o. wl°/o is used as mass percent, and an element may simply be referred to by an element symbol .
- the superficial layer 1 2 is obtained by applying a dechromization treatment (see FIG. 3A ) described below in the range of a predetermined depth from a surface side thereof with respect to a ra material of the stainless steel 1 0.
- the chromium content in the superficial layer 12 is lower than the chromium content of the base material layer 1 1 .
- the content of each of the other alloy ing elements such as nickel (Ni), moly bdenum (Mo) and nitrogen (N ) contained in the stainless steel of the raw material is the same as that of the base material layer 1 1 .
- the chromium content in the superficial layer 1 2 is usually set low to a degree such that a passive film that is naturally fomied on the outermost surface of the stainless steel cannot be substantial ly formed, and the specified chromium content necessary for forming the passive film is less than 1 l wi%, for example. This corresponds to the lower limit chromium content necessary for a passive film to be naturally formed or to be self-repaired.
- the specified chromium content is set to 1 1 %.
- the specified chromium content may be set to another value close to 1 1 %, for example, 1 1 .5% or 1 2%, or 10.5% the same or less than that.
- the chromium content in the superficial layer 1 2 increases corresponding to a depth from the outermost surface layer of the superficial layer 1 2. Further, in a main portion 1 l a (a host material portion) of the base material layer 1 1 , in w hich a depth from a surface becomes a specified depth d l or more, the chromium content is nearly constant. That is. the main portion 1 1 a (a host material portion) of the base material layer 1 1 corresponds to a host material region where contents of iron (Fe) and chromium (Cr) are approximately constant. On the other hand, in a portion l i b on the superficial layer side of the base material layer 1 1 .
- the chromium content changes to be larger in accordance w ith the depth from the outennost surface in the range of a SUS region (stainless region) w here the chromium content is larger than in the superficial layer 1 2 and smaller than in the main portion 1 l a of the base material layer 1 1 .
- a change rate of the chromium content conesponding to the depth from the outermost surface is different between the superficial layer 1 2 and the portion l i b on the superficial layer side of the base material layer 1 1 . That is. the change rate of the chromium content corresponding to a depth from the outermost surface layer in the superficial layer 1 2 (amount of change of the chromium content/amount of unit change of depth from an outennost surface) is larger than the change rate of the chromium content in the base material layer 1 1 corresponding to a depth from the outermost surface.
- the superficial layer 12 has the chromium content that is less than the specified chromium content necessary for forming the passive film.
- a difference of the chromium content between the base material layer 1 1 and the superficial layer 1 2 is larger than a difference of contents of other al loying elements between the base material layer 1 1 and the superficial layer 1 2.
- alloying elements such as nickel Ni ) and molybdenum ( Mo ) which are contained at the same content in both of the base material layer 1 1 and the superficial layer 12 are additional elements that can contri bute to improve the corrosion resistance of each of the base material layer 1 1 and the superficial layer 1 2.
- the corrosion resistance against the local con'osion can be imparted to the superficial layer 1 2 w hile remaining high con'osion resistance against the general corrosion as the stainless steel in the base material layer 1 1 can be formed.
- the superficial layer 1 2 is degraded in the con-osion resistance against the general corrosion by reducing the chromium content in the proximity of a surface.
- the superficial layer 1 2 has a certain degree of corrosion resistance against the general con'osion because it contains alloying elements (Ni. Mo) having high con'osion resistance as other alloying elements.
- a dechromization treatment for forming a stainless steel 10 from a stainless steel raw material thereof will be described.
- a stainless steel raw material is taken as a SUS 3 1 6L. which has a low carbon content and contains molybdenum (Mo).
- Mo molybdenum
- other stainless steels for example, a SUS304 that is more general stainless steel can be used.
- the stainless steel ra material is cal led a workpiece W (see FIG. 4).
- Tlie orkpiece W is formed into a raw material shape such as a plate or a flat piping, and becomes a raw material for exhaust system components having a large area exhaust contact surface in an exhaust system of an internal combustion engine and for components used in an exhaust contact portion of an EGR cooler for cooling an exhaust gas. for example. Further, by masking a portion other than a target portion of the dechromization treatment, the dechromization treatment of the workpiece ⁇ V can be applied only on a target poilion of the dechromization process, and also only the inside of the w orkpiece W can be processed.
- the w orkpiece W includes, as show n in FIG. 2 w ith a bracketed mark, a base material layer portion L I and the superficial layer portion L2 corresponding to the base material layer 1 1 and the superficial layer 1 2 of the stainless steel 10.
- the w orkpiece ⁇ V is subjected to the dechromization treatment using a dechromization treatment system 30 such as shown in FIG. 4 and the stainless steel 10 is obtained.
- the dechromization treatment system 30 is constructed by including an inert gas feeder 3 1 , a vacuum heating furnace 33 and a vacuum exhaust device 36.
- the inert gas feeder 3 1 includes an inert gas bomb 3 1 a in w hich an inert gas. for example, a nitrogen gas ( ⁇ ;) is compressed and filled, a feed control unit 3 1 b for feeding the nitrogen gas from the inert gas bomb 3 1 a into the vacuum heating furnace 33, and an atmosphere sensor 3 1 c exposed in the vacuum heating furnace 33.
- a nitrogen gas ⁇ ;
- a feed control unit 3 1 b for feeding the nitrogen gas from the inert gas bomb 3 1 a into the vacuum heating furnace 33
- an atmosphere sensor 3 1 c exposed in the vacuum heating furnace 33.
- the inert gas bomb 3 1 a is configured such that the inert gas, for example, the nitrogen (N 2 ) gas can continuously be fed to a feed control unit 3 1 b side in the range of required feeding pressure and flow rate.
- the inert gas may be other gas other than nitrogen gas, for example, an argon (Ar) gas.
- the feed control unit 3 1 b is, though not detailed in the draw ing, composed of a control valve and a control mechanism for variably controlling an opening thereof.
- the atmosphere sensor 3 1 c is constructed by including an oxygen sensor that detects an oxygen concentration in the vacuum heating furnace 33, for example.
- the feed control unit 3 1 b changes a feed amount of the nitrogen (N 2 ) gas based on detected information of the atmosphere sensor 3 1 c according to a dechromization treatment condition determined in advance, for example.
- N 2 nitrogen
- the vacuum heating furnace 33 forms a dechromization treatment chamber 32 having a predetermined volume capable of housing the orkpiece W inside thereof, a gas inlet port 32a to the dechromization treatment chamber 32 and a gas outlet port 32b from the dechromization treatment chamber 32 to the vacuum exhaust device 36. Further, to the vacuum heating furnace 33 , a heating device 34 is installed and a support dev ice 35 that supports the workpiece W in the dechromization treatment chamber 32 is disposed.
- the dechromization treatment chamber 32 in the vacuum heating furnace 33 is thermally shielded from a space outside of the furnace by a heat-shielding wall that is not shown in the drawing and the workpiece W can be removed and inserted through the workpiece inlet port. Further, the gas inlet port 32a can reduce air (oxygen) in the dechromization treatment chamber 32 by introducing a nitriding gas into the inside of the dechromization treatment chamber 32 when the nitriding gas is fed from the inert gas feeder 3 1 .
- the heating device 34 includes a heater 34a for heating the inside of the dechromization treatment chamber 32. a temperature sensor 34b for detecting a temperature of the inside of the dechromization treatment chamber 32, and a heating control unit 34c for variably controlling an output of the heater 34a based on the heating condition w here the heating temperature is set in advance and a detected temperature of the temperature sensor 34b.
- the heater 34a is embedded in an inner wall portion that extends to a broad range of the inner wall surface of the v acuum heating furnace 33 for example, and uniformly heats the inside of the dechromization treatment chamber 32, in particular, a space portion that is a region where the workpiece W is disposed. Further, the temperature sensor 34b detects a gas temperature of the inside of the dechromization treatment chamber 32, in particular, in the proximity of a portion where the workpiece W is subjected to the dechromization treatment or a temperature of the workpiece W.
- the support device 35 supports the workpiece W in a state that can be dechromized in the dechromization treatment chamber 32 and can have an optional shape such as a table, a frame, a basket, or a hook, which supports at least one workpiece by many points. Further, the support device 35 may have a transportation function in combination, by which the workpiece W can be moved in a predetermined direction.
- the vacuum exhaust device 36 is disposed on a dow n-stream side (exhaust side) of the vacuum heating furnace 33 and composed of a vacuum pump for discharging air w hich intruded into the dechromization treatment chamber 32 during the installation of the workpiece W, a nitrogen gas from the inert gas feeder 3 1 , and a residual gas after the dechromization treatment in the dechromization treatment chamber 32.
- the heating dev ice 34 is vacuum-exhausted by the vacuum exhaust device 36 to a low pressure of an extent such that compounds such as oxide or nitride of chromium are not substantially generated in the dechromization treatment chamber 32 of the vacuum heating furnace 33. Then, the heating device 34 can heat the workpiece W when at least the superficial portion L2 of the workpiece W is disposed under a low pressure environment hav ing pressure lower than the atmospheric pressure. Further, the heating device 34 can heat the workpiece W at a treatment temperature that is higher than a vaporizing temperature of chromium (hereinafter, simply referred to also as Cr) under the low pressure env ironment and lower than a vaporizing temperature of other alloying elements (for example. Ni, Mo, Fe) under the lo pressure environment.
- Cr vaporizing temperature of chromium
- the heating device 34 can carry out the dechromization treatment in which a chromium content in a superficial portion L2 is set lower than a chromium content in the base material layer portion L I with the contents of the other alloy ing elements such as Ni. Mo. Fe of the workpiece W in the superficial portion L2 maintaining the same as those in in the base material layer portion L I .
- a pressure range of vacuum used in the vacuum heating furnace 33 is set to a range from pressure P I where a degree of vacuum is relatively high to pressure P2 where the degree of vacuum is relativ ely lo (P 1 ⁇ 1 .Ox 10 [Pa] ⁇ P2).
- a unit of temperature is denoted by [K] , However, in the follow ing description. [°C] is used from the v iewpoint of convenience.
- a temperature at which the vapor pressure becomes about 1 .0 x 10 "2 [Pa] is taken as a vaporizing temperature, then, the vaporizing temperature of Cr is 1205 [°C], the heating temperature t l is about 1000 [°C], for example, and the heating temperature t2 is about 1 300 [°C], for example.
- a dechromization layer in which the shal lower the depth from the outermost surface is. the lower the Cr content is. and as the depth from the outermost surface increases, the Cr content gradually increases can be formed.
- a dechromization layer where as the depth from the outermost surface increases, the Cr content gradually increases can be formed.
- a treatment speed of the dechromization treatment can be control led.
- the pressure in the vacuum heating furnace 33 is increased to the pressure P2 side in the range of the w orking pressure (the vacuum is lowered) or the heating temperature is lowered to the t l side in the range of variable control of the pressure and temperature in the vacuum heating furnace 33 show n by cross-hatching in FIG. 5, as shown with a solid line in FIG. 2, a layer thickness (depth ) of the superficial layer portion L2 corresponding to the superficial layer 12 can be reduced.
- the method of manufacturing a stainless steel of the present embodiment inc ludes a preparation step S I .
- a vacuum exhausting step S2 a heating step S3 , a dechromization layer growth step S4 due to holding of low pressure and high temperature, and a cooling step S5.
- a stainless steel ra material including a base material layer portion L I that contains chromium and other al loying elements as a plurality of al loy ing elements in a layer and a superficial layer portion L2 that contains chromium and other alloying elements as a plurality of alloying elements in a layer is prepared as a w orkpiece W.
- a workpiece W is a part of an EGR cooler, an article before the dechromization treatment of a heat exchange pipe, for example, a plurality of workpieces W forms at least an inner peripheral wall surface part of a heat exchange pipe with a stainless steel.
- each of the workpieces W is cleansed and an oil component (in particular, carbon (C )) on a surface of the superficial layer portion L2 is removed such that a Cr compound is not formed.
- the respective w orkpieces W may be carried in the vacuum heating furnace 33 in a state where a portion other than the target portion of the dechromization treatment is masked.
- the inside of the vacuum heating furnace 33 into which the workpiece W is carried in is evacuated by the vacuum exhaust device 36. and at least the superficial layer portion L2 of the workpiece W is disposed under a low pressure environment having pressure lower than the atmospheric pressure.
- the inside of the vacuum heating furnace 33 into w hich the workpiece W is carried in is heated to a treatment temperature that is higher than the vaporizing temperature of chromium under the low pressure environment and is lower than vaporizing temperatures of other alloying elements under the low pressure environment.
- the heating step can be carried out in parallel w ith the vacuum exhausting step or the steps may be partially overlapped w ith each other.
- a heating state at the treatment temperature described above is maintained for a predetermined heating time.
- the inside of the vacuum heating furnace 33 is heated to a treatment temperature that is higher than the vaporizing temperature of Cr or lower than the vaporizing temperatures of other alloying elements such as Ni and the like under the low pressure environment, or the inside of the vacuum heating furnace 33 is depressurized.
- the high temperature heating state at a predetermined heating temperature between the heating temperature t l and t2. to a pressure that is the vapor pressure of Cr or less and higher than the vapor pressures of other al loying elements such as Ni and the like corresponding to the heating temperature.
- the dechromization treatment of the workpiece W is performed in the range of the heating temperature and the reduced pressure, which is on a gas phase side from a vapor pressure curve of chromium and on a gas phase/solid phase side of the other alloying elements in the vapor pressure curve shown in FIG. 5.
- the dechromization layer growth step the high temperature heating state under the low pressure environment as described above is established, and. as shown in FIG. 3A, chromium atoms (Cr shown by encircling with a circle in the drawing) gradually v olatilize from a surface of the superficial layer portion L2 of the workpiece W. thus the dechromization treatment is performed.
- the chromium content in the superficial layer portion L2 is set to the content that is lower than the chromium content in the base material layer portion L I corresponding to the depth from the outermost surface such that the chromium content becomes lower the closer to the outermost surface of the superficial layer portion L2 while maintaining the contents of other elements in the superficial layer portion L2 of the workpiece W the same as that of the base material layer portion L I .
- the heating time in the heating step and dechromization layer growth step in the range of the variable control of the pressure and temperature in the vacuum heating furnace 33 show n w ith cross-hatching in FIG. 5. the pressure and heating temperature in the vacuum heating furnace 33 are controlled.
- the depth of the dechromization treatment corresponding to the layer thickness (depth) of the superficial layer portion L2 and the change rate of the chromium content corresponding to the depth from the surface thereof can be adjusted.
- a temperature of the superficial layer portion L2 and the like of the w orkpiece W is gradually decreased by natural heat dissipation, and a series of dechromization treatment comes to an end w hen a temperature of the workpiece W reaches a specified cooling completion temperature. Then, the workpiece W is taken out of the vacuum heating furnace 33 in a state of a stainless steel 10 in w hich the workpiece W has a superficial layer 12 in which only Cr content is decreased w ith respect to the base material layer 1 1 that is a host material.
- the dechromization treatment is performed, in w hich only chromium is vaporized and volatilized by considering a difference of vapor pressures of a plurality of alloying elements in the workpiece W. That is. after carbon contained in an oil component on a surface of the workpiece W is removed such that a Cr compound is not formed, the range (the range of cross-hatching) of heating temperature and reduced , pressure that is on a gas phase side than from the vapor pressure curve of chromium in the vapor pressure curve shown in FIG. 5 is specified, the stainless steel raw material is heated under low pressure and high temperature, and the dechromization treatment is carried out thereby.
- the workpiece W processed by the dechromization treatment becomes the stainless steel 10 described above, and, in the superficial layer 1 2 thereof, the chromium concentration is reduced by vaporizing the Cr element among the constituent elements of the stainless steel raw material . Therefore, the superficial layer 12 serves as a sacrificing layer in w hich the corrosion resistance (corrosion resistance, anticorrosion property) against the general corrosion is degraded.
- the superficial layer 1 2 becomes a sacrificing layer against the local corrosion by significantly reducing only the chromium content in the superficial layer 12 than that in the base material layer 1 1 , with the high corrosion resistance against the general corrosion remained in the base material layer 1 1 as a stainless steel, the corrosion resistance against the local corrosion can be imparted to the superficial layer 1 2.
- the superficial layer 1 2 of which chromium content is lower than the content of the base material layer 1 1 serv es as a sacrificing layer against the local corrosion, and. since the base material layer 1 1 of a lower lav er thereof is a stainless steel layer hav ing a high chromium content, the corrosion resistance can be secured in two steps.
- the superficial layer 12 that becomes a sacrificing layer can readily .be formed. Accordingly, there is no need of a complicated passivation treatment. and there is no need of adopting a super stainless such as SUS836 in which an alloying metal (such as Ni and the like ) is increased, or adding a surface treatment such as cold spraying or plating.
- the contents of other alloying elements that are additional elements for improving the corrosion resistance other than chromium are maintained in the same level as in the base material layer 1 1 also in the superficial layer 1 2 that becomes a sacrificing layer.
- the corrosion resistance 'anticorrosion property in both of the superficial layer 1 2 and the base material layer 1 1 can be improved, and the proceeding speed of the general corrosion in the superficial layer 1 2 can effectively be suppressed.
- the chromium content in the superficial layer 1 2 increases corresponding to a depth from the outermost surface and the chromium content in a main portion 1 l a of the base material layer 1 1 is constant. Further, in a SUS region portion 1 l b on a superficial layer 1 2 side of the base material layer 1 1 , the chromium content changes in the range that is larger than in the superficial layer 1 2 and smaller than in the main portion 1 1 a of the base material layer 1 1 . Therefore, the corrosion resistance against the local corrosion in the superficial layer 12 and the corrosion resistance against the general corrosion in the base material layer 1 1 can surely be combined.
- the change rate of the chromium content corresponding to a depth from the outermost surface is different between the superficial layer 1 2 and the SUS region portion l i b on the superficial layer 1 2 side of the base material layer 1 1 . Therefore, when a thickness of the superficial layer 1 2 up to the main portion 1 l a of the base material layer 1 1 changes as the general corrosion proceeds, the chromium content in the proximity of the outermost surface of the superficial layer 1 2 can be adj usted to be a chromium content value adequate for anticorrosion at each of depths from the outermost surface corresponding to a thickness thereof.
- the stainless steel of the present embodiment is used as an exhaust system component, since condensed w ater containing an exhaust component is generated or condensed, the component is used under an environment w here the general coiTosion and the local corrosion such as the pitting corrosion are likely to occur.
- the stainless steel of the present embodiment is used in the exhaust system component, a low cost exhaust system component that can sufficiently sho the corrosion resistance against both of the general corrosion and the local corrosion such as the pitting corrosion can be obtained.
- the superficial layer 1 2 is subjected to the dechromization treatment by heating the superficial layer portion L2 of the workpiece W at a treatment temperature that is higher than a vaporizing temperature of chromium and low er than the vaporizing temperatures of other alloying elements under the low pressure environment.
- the superficial layer 1 2 can be dechromized.
- the chromium content of the superficial layer 1 2 can be set lower than the chromium content of the base material layer 1 1 corresponding, to treatment times of depressurization and heating.
- the superficial layer 12 that becomes a sacrificing layer against the local corrosion can be readily formed by applying the dechromization treatment to the superficial portion L2. thus, also a complicated passive film treatment and the like become unnecessary.
- a manufacturing method of a low cost stainless steel that can sho sufficient corrosion resistance against both of the general corrosion and the local corrosion such as the pitting corrosion can be obtained.
- a stainless steel having a hybrid structure, in which the superficial layer 1 2 is an al loy steel that is strong against the local corrosion such as the pitting corrosion and contains other alloying elements and the base material layer 1 1 is strong against the general corrosion can be manufactured.
- the superficial layer 1 2 is an al loy steel that is strong against the local corrosion such as the pitting corrosion and contains other alloying elements and the base material layer 1 1 is strong against the general corrosion
- a plurality of test pieces was cut out from a raw material configuring the stainless steel 1 0, on a surface of each of thereof, a corrosion solution L (see FIG. 1 ) equivalent with or more than strong acidic condensed w ater containing an exhaust gas component of an internal combustion engine was dropped. Thereafter, the test piece was dried, and a corrosion test where the test piece was left under a high temperature and high humidity environment was carried out. Then, the test pieces of one example were cleansed, and a pitting corrosion depth (maximum erosion depth) of each thereof was measured.
- a table in FIG. 7 shows heat treatment conditions of a plurality of Examples and Comparativ e Examples and results of the corrosion test thereof in comparison.
- No. 1 to 9 each in the table of FIG. 7 shows a test piece number
- No. 1 and No. 5 to No. 9 each shows Comparative Examples 1 to 6.
- Example 1 represented by No. 2.
- the dechromization treatment was applied on the superficial layer portion L2 of the workpiece W that was formed of SUS316L at a treatment temperature of 1200 [°C] and a treatment pressure of 1 .0 ⁇ 10 "2 [Pa] for about 2 hours, and the superficial layer 12 having a lay er thickness of 20 ⁇ , in which the chromium content was reduced was formed.
- Example 2 represented by No. 3, the dechromization treatment was applied on the superficial layer portion L2 of the workpiece W that was fonned of SUS3 16L at a treatment temperature of 1250 [°C] and a treatment pressure of 1 .0 x 10 "2 [Pa] for about 1 hour, and the superficial layer 12 having a layer thickness of 20 ⁇ , in which the chromium content was reduced was formed. [0098J In this case, as shown in FIG. 8A, the chromium content in the superficial layer portion L2 of the workpiece W was reduced.
- nickel ( i) and iron (Fe) that are other alloying elements in the superficial layer portion L2 were the same as those in the base material layer portion L I ( SUS3 1 6L that is a low carbon stainless steel ). Further, also carbon (C) w as the same as in the base material layer portion L I .
- Example 3 represented by No. 4, the dechromization treatment was applied on the superficial layer portion L2 of the workpiece W that was formed of SUS3 16L at a treatment temperature of 1 300 [°C] and a treatment pressure of 1 .0 ⁇ 10 "2 [Pa] for about 1 hour, and the superficial layer 1 2 having a layer thickness of 20 ⁇ . in which the chromium content was reduced was formed.
- Comparative Example 1 represented by No. 1 , .the dechromization treatment was not applied on the superficial layer portion L2 of the workpiece W formed of a SUS3 16L and both of the superficial portion L2 and the base material layer portion L I were remained as the raw material of the SUS3 16L.
- Comparative Example 2 represented by No. 5. a low pressure- and high-temperature heat treatment was applied on the superficial layer portion L2 of the workpiece W formed of a SUS3 16L at a treatment temperature of 900 [°C] and a treatment pressure of 1 .0 ⁇ 10 '2 [Pa] for about 1 hour.
- Comparative Example 3 represented by No. 6. a high-temperature heat treatment at a relatively low pressure was applied on the superficial layer portion L2 of the workpiece W formed of a SUS3 1 6L with a treatment temperature set at 1 250 [°C] and a treatment pressure set at 1 .0 ⁇ 10 3 [Pa] for about 1 hour.
- Comparative Example 4 represented by No. 7. a low-pressure and high-temperature heat treatment was applied on the superficial layer portion L2 of the workpiece W formed of a SUS3 16L with a treatment temperature set at 1 200 [°C] and a treatment pressure set at 1 .0 l O 1 [Pa] for about 1 hour.
- Example 4 all of the test pieces were appeared to be improved compared with Comparative Example 1 . However, among main corrosion pittings pt l to pt8 generated on surfaces of the test pieces, some thereof had the pitting corrosion depths exceeding 100 ⁇ , that is. the corrosion resistance against the pitting corrosion was insufficient.
- Comparative Example 5 represented by No. 8, a normal nitriding treatment was applied on the superficial layer portion L2 of the workpiece W formed of a SUS3 16L with a treatment temperature set at 1 200 [°C] and a treatment pressure set at 1 .0 x l O 5 [Pa] .
- the chromium content in the superficial layer portion L2 of the workpiece W was decreased.
- FIG. 8 also each of contents of nickel (Ni) and iron (Fe) that are other alloying elements in the superficial layer portion L2 w as decreased.
- Example 6 the pitting corrosion depths of the main corrosion pittings pt l to pt8 that were generated on surfaces of the test pieces exceeded 100 ⁇ , that is. the corrosion resistance against the pitting corrosion was insufficient.
- the vacuum heating furnace 33 was used to form a low pressure environment that can be heated to a high temperature. However, by heating the workpiece to a high temperature under other low pressure env ironment that does not generate a compound, only Cr in the material can be released outside of the material.
- a heating state at a predetermined treatment temperature is held for a predetermined heating time, and under the state, the inside of the vacuum heating furnace 33 is heated to a treatment temperature that is higher than the vaporizing temperature of Cr and lower than the vaporizing temperatures of other alloying elements such as Ni and the like under a low pressure environment.
- the inside of the vacuum heating furnace 33 is depressurized to a pressure that is the vapor pressure of Cr or less and higher than vapor pressures of other alloying elements such as Ni and the like corresponding to the heating temperature in a high-temperature heating state at a predetermined heating temperature between the heating temperature tl and t2.
- optional one or both thereof may appropriately be selected, or may be combined under different conditions (temperature and pressure).
- the SUS316L was used as a stainless steel raw material that configures the workpiece W.
- the base material layer 1 1 (1 1 ') that includes a SUS region portion l i b (1 lb') on a superficial layer side, in which the chromium content is lower than that of the main portion 1 1 a ( 1 1a') and higher than the specified chromium content, and the main portion 1 1a (1 1a') that is a host material was disposed.
- both of the superficial layer portion L2 (L2') of the workpiece W corresponding to the superficial layer 12 of the stainless steel 10 and the SUS region portion Li b (L i b' ) on the superficial layer side of the base material layer portion L I (L l ) may be dechromized to be less than the specified chromium content necessary to form a passive film. Further, by variably controlling the dechromization treatment condition, the change rate of the chromium content corresponding to a thickness of the superficial layer 12 and a depth from the outermost surface may be changed stepwise.
- the thickness of the superficial layer 12 is changed, when the heat treatment condition such as a reduced pressure and a heating temperature (maintaining at a Cr vapor pressure or less or a Cr vaporizing temperature or more) is set to a high temperature and a short time, layer thicknesses of the superficial layer portion L2 that becomes the superficial layer 12 and the SUS region 1 l b on the superficial layer side of the base material layer 1 1 and a portion L i b on the superficial layer side become smaller.
- the heat treatment condition such as a reduced pressure and a heating temperature (maintaining at a Cr vapor pressure or less or a Cr vaporizing temperature or more)
- a heating temperature maintaining at a Cr vapor pressure or less or a Cr vaporizing temperature or more
- the layer thicknesses of the superficial layer portion L2' that becomes the superficial layer 12 and the SUS layer of the base material layer 1 1 and a portion L i b' on the superficial layer side tend to be larger.
- the present invention can provide a low cost stainless steel that can be used for a long time under an environment where both of the general corrosion and the local corrosion occur, and a method of manufacturing the low cost stainless steel.
- the present invention like this is useful at large for a stainless steel suitable for exhaust system components for which the corrosion resistance against both of the general corrosion and the local corrosion such as the pitting corrosion are required and a method of manufacturing the same.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Crystallography & Structural Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Physical Vapour Deposition (AREA)
Abstract
Description
Claims
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201480018776.4A CN105247081B (en) | 2013-04-04 | 2014-04-02 | Stainless steel and its manufacturing method |
| DE112014001812.0T DE112014001812B4 (en) | 2013-04-04 | 2014-04-02 | Stainless steel and method of making same |
| US14/782,156 US10619950B2 (en) | 2013-04-04 | 2014-04-02 | Stainless steel and method of manufacturing the same |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2013078750A JP5842854B2 (en) | 2013-04-04 | 2013-04-04 | Stainless steel and manufacturing method thereof |
| JP2013-078750 | 2013-04-04 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| WO2014162196A2 true WO2014162196A2 (en) | 2014-10-09 |
| WO2014162196A3 WO2014162196A3 (en) | 2015-12-10 |
Family
ID=50829210
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/IB2014/000473 Ceased WO2014162196A2 (en) | 2013-04-04 | 2014-04-02 | Stainless steel and method of manufacturing the same |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US10619950B2 (en) |
| JP (1) | JP5842854B2 (en) |
| CN (1) | CN105247081B (en) |
| DE (1) | DE112014001812B4 (en) |
| WO (1) | WO2014162196A2 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20200232376A1 (en) * | 2019-01-17 | 2020-07-23 | Tenneco Automotive Operating Company Inc. | Diffusion Surface Alloyed Metal Exhaust Component |
| CN111740300A (en) * | 2020-05-22 | 2020-10-02 | 合肥圣达电子科技实业有限公司 | Manufacturing process of packaging shell for high-power laser |
| CN115287596B (en) * | 2022-07-22 | 2023-10-24 | 江苏襄宿新材料有限公司 | Preparation method of chromium alloy layer on stainless steel |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0254740A (en) | 1988-08-19 | 1990-02-23 | Kobe Steel Ltd | Steel material and tube for absorption thermal apparatus having excellent corrosion resistance |
| JPH04131321A (en) | 1990-09-25 | 1992-05-06 | Toshiba Corp | Surface reformed member and production thereof |
| JP2001234300A (en) | 2000-02-28 | 2001-08-28 | Kawasaki Steel Corp | Austenitic stainless steel sheet excellent in pickling properties of stainless processed products and method for producing the same |
| JP2012170961A (en) | 2011-02-18 | 2012-09-10 | Jfe Steel Corp | Stainless steel excellent in corrosion resistance |
Family Cites Families (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1306690A (en) * | 1919-06-17 | Alexander edwin gillespie | ||
| US3623901A (en) * | 1968-11-18 | 1971-11-30 | Bethlehem Steel Corp | Formation of chromium-containing coatings on both sides of steel strip with one coated side having a bright finish |
| US3904378A (en) * | 1971-07-14 | 1975-09-09 | Armco Steel Corp | Steel clad stainless composite article |
| KR910003538B1 (en) * | 1986-03-04 | 1991-06-04 | 가와사끼 세이데쓰 가부시끼가이샤 | Martensitic stainless steel sheet having improved oxidation resistance workability and corrosion resistance |
| JPH02259085A (en) * | 1989-03-31 | 1990-10-19 | Nippon Steel Corp | Exhaust steel pipe for internal combustion engine excellent in corrosion resistance |
| JPH0313329A (en) * | 1989-06-13 | 1991-01-22 | Kawasaki Steel Corp | Sintered metal composite material excellent in corrosion resistance, dimensional accuracy and economical efficiency and preparation thereof |
| KR960014949B1 (en) * | 1992-02-25 | 1996-10-21 | 가와사끼 세이데쓰 가부시끼가이샤 | High chromium and high phosphosus ferritic stainless steel excellent in weatherproofness and rustproofness |
| JP3039630B2 (en) * | 1997-04-18 | 2000-05-08 | 新日本製鐵株式会社 | Low corrosion rate steel plate with low local corrosion |
| US5783622A (en) * | 1997-05-05 | 1998-07-21 | Armco Inc. | Precoated chromium alloyed steel with enhanced paint adhesion for exhaust applications |
| JPH11323504A (en) * | 1998-05-12 | 1999-11-26 | Nippon Steel Corp | Non-uniform structural corrosion-resistant stainless steel and its products |
| JP2000310161A (en) * | 1999-04-27 | 2000-11-07 | Isuzu Motors Ltd | EGR cooler |
| JP2003003211A (en) | 2001-06-19 | 2003-01-08 | Kanto Yakin Kogyo Co Ltd | Continuous heat-treatment method for metal under argon atmosphere |
| CN1280445C (en) | 2003-07-17 | 2006-10-18 | 住友金属工业株式会社 | Stainless steel and stainless steel pipe having resistance to carburization and coking |
| BRPI0318495B1 (en) * | 2003-09-05 | 2015-06-16 | Nippon Steel & Sumitomo Metal Corp | Welded pipe structure having improved resistance to stress corrosion cracking |
| AU2004325491B2 (en) * | 2004-12-07 | 2008-11-20 | Nippon Steel Corporation | Martensitic stainless steel pipe for oil well |
| JP2013053769A (en) | 2011-09-01 | 2013-03-21 | Toyota Motor Corp | Exhaust system component and method for forming surface layer of exhaust system component |
| US9028745B2 (en) * | 2011-11-01 | 2015-05-12 | Honeywell International Inc. | Low nickel austenitic stainless steel |
| DE102012002637B4 (en) * | 2012-02-10 | 2014-01-02 | Faurecia Emissions Control Technologies, Germany Gmbh | exhaust system |
-
2013
- 2013-04-04 JP JP2013078750A patent/JP5842854B2/en not_active Expired - Fee Related
-
2014
- 2014-04-02 DE DE112014001812.0T patent/DE112014001812B4/en active Active
- 2014-04-02 CN CN201480018776.4A patent/CN105247081B/en not_active Expired - Fee Related
- 2014-04-02 US US14/782,156 patent/US10619950B2/en not_active Expired - Fee Related
- 2014-04-02 WO PCT/IB2014/000473 patent/WO2014162196A2/en not_active Ceased
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0254740A (en) | 1988-08-19 | 1990-02-23 | Kobe Steel Ltd | Steel material and tube for absorption thermal apparatus having excellent corrosion resistance |
| JPH04131321A (en) | 1990-09-25 | 1992-05-06 | Toshiba Corp | Surface reformed member and production thereof |
| JP2001234300A (en) | 2000-02-28 | 2001-08-28 | Kawasaki Steel Corp | Austenitic stainless steel sheet excellent in pickling properties of stainless processed products and method for producing the same |
| JP2012170961A (en) | 2011-02-18 | 2012-09-10 | Jfe Steel Corp | Stainless steel excellent in corrosion resistance |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105247081A (en) | 2016-01-13 |
| JP2014201790A (en) | 2014-10-27 |
| US10619950B2 (en) | 2020-04-14 |
| DE112014001812T5 (en) | 2015-12-24 |
| WO2014162196A3 (en) | 2015-12-10 |
| US20160060720A1 (en) | 2016-03-03 |
| JP5842854B2 (en) | 2016-01-13 |
| DE112014001812B4 (en) | 2023-03-09 |
| CN105247081B (en) | 2017-09-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2365107B1 (en) | Process for coating an article | |
| US9988706B2 (en) | Automotive components formed of sheet metal coated with a non-metallic coating | |
| Badini et al. | Cyclic oxidation in burner rig of TiAlN coating deposited on Ti-48Al-2Cr-2Nb by reactive HiPIMS | |
| CN104862649B (en) | A kind of preparation method of titanium alloy surface gradient Ni/TiN composite modified layers | |
| WO2014162196A2 (en) | Stainless steel and method of manufacturing the same | |
| CN106637048A (en) | Preparation method of selective oxidation film at low dew point | |
| Resnina et al. | Functional properties of the multilayer NiTi alloy produced by wire arc additive manufacturing | |
| US20140322555A1 (en) | Process for producing a high-temperature protective coating and correspondingly produced component | |
| KR102261029B1 (en) | Nickel-based super alloy for diffusion bonding and method for diffusion bonding using the same | |
| Kong et al. | A novel bonding method of pure aluminum and SUS304 stainless steel using barrel nitriding | |
| CN108588366A (en) | A kind of heat treatment method of selective laser fusing forming 06Cr19Ni10 austenitic stainless steels | |
| CN103774085A (en) | High-nitrogen austenite layer in low-carbon alloy steel surface preparation and preparation method thereof | |
| CN103993258B (en) | Method for coating workpiece with complex inner cavity structure | |
| WO2012097976A1 (en) | Method to produce a hot formed part, and part thus formed | |
| CN107354424B (en) | A vapor-dip galvanizing pretreatment process for suppressing selective oxidation on the surface of high-strength steel sheets | |
| WO2014013788A1 (en) | Base material for hydrogen apparatus | |
| JP2014095105A (en) | Nitriding treatment method of exhaust system component | |
| Birol | Effect of post-oxidation treatment on thermal fatigue behaviour of plasma nitrided hot work tool steel at elevated temperatures | |
| CN105917149A (en) | Piston ring and production method therefor | |
| KR20160013131A (en) | Barrier coating for turbochargers | |
| RU2519356C2 (en) | Method of cyclic gas nitration of steel dies for hot forming | |
| US20160002775A1 (en) | Multilayer liner for chemical vapor deposition furnace | |
| RU2308541C1 (en) | Method of coating alloys | |
| JP2004190560A (en) | piston ring | |
| CN104233156A (en) | Heat treatment method for hot-dip aluminized coating |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 14726756 Country of ref document: EP Kind code of ref document: A2 |
|
| WWE | Wipo information: entry into national phase |
Ref document number: 14782156 Country of ref document: US |
|
| WWE | Wipo information: entry into national phase |
Ref document number: 1120140018120 Country of ref document: DE Ref document number: 112014001812 Country of ref document: DE |
|
| 122 | Ep: pct application non-entry in european phase |
Ref document number: 14726756 Country of ref document: EP Kind code of ref document: A2 |