US3698964A - Oxidation-resistant articles of an iron base alloy containing chromium and aluminum and/or silicon - Google Patents

Oxidation-resistant articles of an iron base alloy containing chromium and aluminum and/or silicon Download PDF

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US3698964A
US3698964A US86768A US3698964DA US3698964A US 3698964 A US3698964 A US 3698964A US 86768 A US86768 A US 86768A US 3698964D A US3698964D A US 3698964DA US 3698964 A US3698964 A US 3698964A
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oxidation
silicon
alloys
chromium
aluminum
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US86768A
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Elmer J Caule
Philip R Sperry
Michael J Pryor
James A Ford
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Olin Corp
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/34Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium

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  • a class of alloys is described in this invention which are essentially low alloys of Fe and which have oxidation resistance significantly greater than achieved by the stainless steels in the temperature range from 500 to 1000 C.
  • FIG. 1 is a plot of weight gain in micrograms per square centimeters observed having 2% chromium-3% aluminum alloy exposed to temperatures of 250 800 C. for two hours;
  • FIG. 2 is a plot of weight gain in micrograms per square centimeter for type 301 stainless steel (17 chromium, 7 nickel) against temperatures in degrees C also after exposure to these temperatures for a period of two hours; and
  • FIG. 3 is a plot of weight gain in micrograms per square centimeter against temperatures after exposure of a 3% chromium-2% silicon alloy to temperatures from 250-800 C. for two hours.
  • FIG. 3 is a plot for the iron-chromium-silicon alloy of the present invention showing weight gains in micrograms per square centimeter against temperature after the alloy having the composition 3.0% chromium, 2.0% silicon shown was heated for two hours in the temperature range of 250 to 800 C. It is apparent that the alloy had much lower weight gains than the type 301 stainless steels shown in FIG. 2 in the 500 to 800 C. temperature range. In fact, from this data, it is apparent that weight gains below 50 micrograms per square centimeter are assured for the entire temperature range.
  • alloys of the present invention are considerably less expensive than alloys containing chromium in amounts of at least 11%; for example, 18 chromium-8 nickel is commonly used.
  • the Fe-base alloys of the present invention may be processed according to ordinary Fc-base melting, casting, and hot and cold working procedures.
  • the alloys of the present invention do not require specialized equipment or technology.
  • the alloys of the present invention may be vacuum cast, homogenized, for example, at 1800 F., hot rolled to approximately 0.200 inch, with a reheat to 1800 R, if desired, scalped, and cold rolled without interannealing from 0.20 gage to 0.015.
  • the steel to be used in the present invention does not, however, require vacuum casting. Ordinary steel making procedures may be used such as blast furnace treatment with either open hearth or LD process reduction of the carbon content, as is well known in the art.
  • the resulting composition of the alloys may be as follows: phosphorus and sulfur, 0.04 max. each, manganese may be up to 1.5%, preferably up to 0.2%, copper may be present as high as 2%, but preferably not more than 0.5%, others, including nickel, molybdenum, vanadium, and other alloying elements commonly present in low alloy steels may be present up to 0.20%.
  • the carbon content may range as high as 2%, for some applications requiring very high wear resistance. However, the carbon content is preferably not more than about 1%. Furthermore, the most preferred range of carbon is from 0.01 to 0.25%. It is expected that the latter range will have the most general application.
  • the alloys of the present invention are highly resistant to atmospheric oxidation and tarnishing after first being exposed to high temperature air oxidation for 5 minutes to 100 hours at 400 to 1000 C., preferably 600 to 1000 C. For example, two hours at 800 C. has been found to be very satisfactory.
  • An oxidation and tarnish resistant article consisting essentially of an iron base alloy consisting of chromium from 1 to 5%, a material selected from the group consisting of aluminum from 1 to 4%, silicon from 1 to 4% and mixtures thereof, phosphorus 0.04% max., sulfur 0.04% max., manganese up to 1.5%, copper up to 2%, carbon up to 2%, others up to 0.20%, balance iron, said alloy of said article having a substantially colorless and adherent oxide film and having significantly greater oxidation resistance than stainless steels in the 500 to 1000 C. temperature range.
  • An article according to claim 1 containing copper in an amount up to 0.5%.
  • An article according to claim 1 containing carbon in an amount up to 1%.

Abstract

IRON BASE ALLOYS WITH ALLOYING ADDITIONS OF CHROMIUM AND ALUMINUM AND/OR SILICON ARE DESCRI BED WHICH EXHIBIT UNIQUE AND UNEXPECTEDLY LOW WEIGHT GAINS WHEN EXPOSED TO OXIDIZING ENVIRONMENTS. ONE OF THE MAJOR ADVANTAGES OF THE GROUP OF ALLOYS DESCRIBED HEREIN LIES IN THEIR MODERATE COST, ESPECIALLY AS COMPARED TO OTHER OXIDATION RESISTANT FE-BASE ALLOYS SUCH AS THE VARIOUS GRADES OF STAINLESS STEEL CONTAINING AT LEAST 11% CHROMIUM. THE OXIDATION RESISTANCE IS IMPARTED TO THESE ALLOYS THROUGH THE FORMATION OF A TENACIOUS COMPACT OXIDE FILM CONSISTING ESSENTIALLY OF OXIDES OF THE ALLOYING ADDITIONS.

Description

Oct. 17, 1972 J, CAULE ET AL 3,698,964
OXIDATION-RESISTANT ARTICLE OF AN IRON BASE ALLOY CONTAINING CHROMIUM AND ALUMINUM AND/OR SILICON Original Filed Aug. 8, 1968 3 Sheets-Sheet l Q: E 2 t2 a N 1 I e I Q 3 5 WJ/ SVVVHQO/J/W NW9 lHQ/J/M INVENTORS.
ELMER J. CA ULE PHIL /P R. SPERRY M/CHALL J PRYOR JAMES A. FORD ATTORNEY Oct. 17, 1972 J, c u ETAL 7 3,698,964 OXIDATION-RESISTANT ARTICLE OF AN IRON BASE ALLOY CONTAINING CHROMIUM AND ALUMINUM AND/0R SILICON Original Filed Aug. 8, 1968 3 Sheets-Sheet 2 QQQ M B 9 H J. 9 I 8w W m d w m w 0% W 7- 1. 8w
INVENTORS ELMERJ. CAULE PHIL/P R. SPERRY MICHAEL J. PRVOR ATTORNEY Oct. 17, 1972 5,1, c u ETAL 3,698,964
OXIDATION-RESISTANT ARTICLE OF AN IRON BASE ALLOY CONTAINING CHROMIUM AND ALUMINUM AND/OR SILICON Original Fixed Aug. 8, 1968 5 Sheets-Sheet 3 cox,
QQQ
w EEYQQQSH INVENTORS EVR 0 Mg m F J.$J.A. m WMM H A MJ ATTORNEY United States Patent 3,698,964 OXIDATION-RESISTANT ARTICLES OF AN IRON BASE ALLOY CONTAINING CHROMIUM AND ALUMINUM AND/OR SILICON Elmer J. Caule, New Haven, Philip R. Sperry, North Haven, Michael J. Pryor, Woodbridge, and James A. 50rd, North Haven, Conn., assignors to Olin Corporaon Original application Aug. 8, 1968, Ser. No. 751,311. Divided and this application Nov. 4, 1970, Ser. No. 86,768
Int. Cl. C22c 39/06, 39/14 US. Cl. 148-315 6 Claims ABSTRACT OF THE DISCLOSURE Iron base alloys with alloying additions of chromium and aluminum and/or silicon are described which exhibit unique and unexpectedly low weight gains when exposed to oxidizing environments. One of the major advantages of the group of alloys described herein lies in their moderate cost, especially as compared to other oxidation resistant Fe-base alloys such as the various grades of stainless steel containing at least 11% chromium. The oxidation resistance is imparted to these alloys through the formation of a tenacious compact oxide film consisting essentially of oxides of the alloying additions.
CROSS REFERENCE TO RELATED APPLICATION This application is a division of copending application Ser. No. 751,311, filed Aug. 8, 1968, for Oxidation Resistant Iron Base Alloy Containing Chromium and Aluminum and/or Silicon, by Elmer J. Caule, Philip R. Sperry, Michael J. Pryor and James A. Ford, now abandoned.
BACKGROUND OF THE INVENTION It has long been an objective of the art to achieve a low cost Fe-base alloy with oxidation resistance superior to that exhibited by the stainless steels containing more than 11% chromium. Presently, the only known method for providing such oxidation resistance relies in the formation of an adherent Cr O surface layer; this requires large amounts of Cr in solid solution; in fact, it has been shown that a minimum of about 11 weight percent Cr is necessary to provide the very excellent oxidation resistance characteristics of stainless steels.
It is an object of the present invention to provide alloys which are less expensive than stainless steels.
It is another object of the present invention to provide alloys which give equal, or superior, oxidation and corrosion resistance when compared to stainless steels in the 500 to 1000 C. temperature range.
It is another object of the present invention to provide alloys which do not require special processing techniques or equipment.
Other objects and advantages will become apparent to those skilled in the art as a detailed description of a particular embodiment proceeds and with reference to the drawings which form a part hereof.
SUMMARY OF THE INVENTION A class of alloys is described in this invention which are essentially low alloys of Fe and which have oxidation resistance significantly greater than achieved by the stainless steels in the temperature range from 500 to 1000 C.
This unusual oxidation resistance is achieved through 3,698,964 Patented Oct. 17, 1972 the addition of combinations of chromium and aluminum and/or silicon alloying elements. Specifically, extensive research has shown that the combination of Al and/ or Si in a high purity Fe-base provides unusual and unexpected oxidation behavior in a high temperature air environment when used with 1 to 5% chromium. It has been shown that over the composition range of 1-5%- Cr and 1-4% Si and/or 1-4%.. Al, oxidation weight gain of the alloys of this invention is on the order of 20 times less than that experienced by stainless steels.
BRIEF DESCRIPTION OF THE DRAWINGS In the accompanying drawings:
'FIG. 1 is a plot of weight gain in micrograms per square centimeters observed having 2% chromium-3% aluminum alloy exposed to temperatures of 250 800 C. for two hours; FIG. 2 is a plot of weight gain in micrograms per square centimeter for type 301 stainless steel (17 chromium, 7 nickel) against temperatures in degrees C also after exposure to these temperatures for a period of two hours; and
FIG. 3 is a plot of weight gain in micrograms per square centimeter against temperatures after exposure of a 3% chromium-2% silicon alloy to temperatures from 250-800 C. for two hours.
DETAILED DESCRIPTION As shown in FIG. 1, the combination of 3% Al and 2% Cr produces a unique and unusual reversal in oxidation weight gain in the temperature range of 600 to 900 C. Weight gains below micrograms per square centimeter are obtained at temperatures of 700 to 800 C. This is in distinct contrast to the oxidation weight gain exhibited by stainless steel (type 301-17 chromium, 7 nickel) shown in FIG. 2 over the same temperature range.
The oxide films produced in this temperature range are nearly colorless and adherent. On the other hand, certain (type 301) stainless steels begin to form nonadherent scales at the higher temperatures, i.e., 900 C. This unique and distinct reversal in oxidation weight gain occurs over the range of chemistry given above, for 15% Cr and Al and/or Si at l-4%.
FIG. 3 is a plot for the iron-chromium-silicon alloy of the present invention showing weight gains in micrograms per square centimeter against temperature after the alloy having the composition 3.0% chromium, 2.0% silicon shown was heated for two hours in the temperature range of 250 to 800 C. It is apparent that the alloy had much lower weight gains than the type 301 stainless steels shown in FIG. 2 in the 500 to 800 C. temperature range. In fact, from this data, it is apparent that weight gains below 50 micrograms per square centimeter are assured for the entire temperature range.
The decrease in the weight gain with temperature is believed to result from the formation of alumina, A1 0 together with complexes such as Fe0.Al O When silicon is present in addition to aluminum, the silicon appears to stimulate the formation of these compounds in a manner not clearly understood.
In the case of silicon alloyed with chromium, the silicon stimulates the formation of chromium oxide compounds in a manner not clearly understood.
It will be apparent that the alloys of the present invention are considerably less expensive than alloys containing chromium in amounts of at least 11%; for example, 18 chromium-8 nickel is commonly used.
The Fe-base alloys of the present invention may be processed according to ordinary Fc-base melting, casting, and hot and cold working procedures. The alloys of the present invention do not require specialized equipment or technology.
For example, the alloys of the present invention may be vacuum cast, homogenized, for example, at 1800 F., hot rolled to approximately 0.200 inch, with a reheat to 1800 R, if desired, scalped, and cold rolled without interannealing from 0.20 gage to 0.015.
The steel to be used in the present invention does not, however, require vacuum casting. Ordinary steel making procedures may be used such as blast furnace treatment with either open hearth or LD process reduction of the carbon content, as is well known in the art. The resulting composition of the alloys may be as follows: phosphorus and sulfur, 0.04 max. each, manganese may be up to 1.5%, preferably up to 0.2%, copper may be present as high as 2%, but preferably not more than 0.5%, others, including nickel, molybdenum, vanadium, and other alloying elements commonly present in low alloy steels may be present up to 0.20%. The carbon content may range as high as 2%, for some applications requiring very high wear resistance. However, the carbon content is preferably not more than about 1%. Furthermore, the most preferred range of carbon is from 0.01 to 0.25%. It is expected that the latter range will have the most general application.
As a further superior feature of these alloys, it has been found that the alloys of the present invention are highly resistant to atmospheric oxidation and tarnishing after first being exposed to high temperature air oxidation for 5 minutes to 100 hours at 400 to 1000 C., preferably 600 to 1000 C. For example, two hours at 800 C. has been found to be very satisfactory.
It has also been found that these alloys are resistant to contaminated atmospheres containing sulfur and/ or water vapor and/or carbon monoxide-dioxide combinations. These atmospheres are representative of most hydrocarbon combustion gases.
It is to be understood that the invention is not limited to the illustrations described and shown herein which are deemed to be merely illustrative of the best modes of carrying out the invention, and which are susceptible of modifications of form, size, arrangement of parts and detail of operation, but rather is intended to encompass all such modifications which are within the spirit and scope of the invention as set forth in the appended claims.
What is claimed is:
1. An oxidation and tarnish resistant article consisting essentially of an iron base alloy consisting of chromium from 1 to 5%, a material selected from the group consisting of aluminum from 1 to 4%, silicon from 1 to 4% and mixtures thereof, phosphorus 0.04% max., sulfur 0.04% max., manganese up to 1.5%, copper up to 2%, carbon up to 2%, others up to 0.20%, balance iron, said alloy of said article having a substantially colorless and adherent oxide film and having significantly greater oxidation resistance than stainless steels in the 500 to 1000 C. temperature range.
2. An article according to claim 1 wherein said material is aluminum and wherein a reversal occurs in the plot of oxidation weight gain against temperature in the 600 to 1000 C. range.
3. An article according to claim 1 wherein said material is silicon.
4. An article according to claim 1 containing manganese in an amount up to 0.2%
5. An article according to claim 1 containing copper in an amount up to 0.5%.
6. An article according to claim 1 containing carbon in an amount up to 1%.
References Cited UNITED STATES PATENTS 1,166,342 12/1915 Field -128 A 3,144,362 8/1964 Bradd 75-124 X 2,763,544 9/1956 Wagner 75--124 X 2,770,563 11/1956 Herzog 75-124 X 2,941,883 6/1960 Ida 75--124 3,031,392 4/1962 Ida 75124 X L. DEWAYNE RUTLEDGE, Primary Examiner J. E. LEGR-U, Assistant Examiner U.S. Cl. X.R.
75-126 A, 126 B, 126 Q, 124, 14836
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Cited By (33)

* Cited by examiner, † Cited by third party
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US3905780A (en) * 1973-06-25 1975-09-16 Armco Steel Corp Oxidation-resistant low alloy steel with Al coating
US3909250A (en) * 1973-06-25 1975-09-30 Armco Steel Corp Oxidation-resistant ferrous alloy
US4141724A (en) * 1978-06-21 1979-02-27 United States Steel Corporation Low-cost, high temperature oxidation-resistant steel
US4299622A (en) * 1978-11-06 1981-11-10 Sony Corporation Magnetic alloy
US4398951A (en) * 1981-04-22 1983-08-16 Unisearch Limited Fermalloy(Fe-Mn-Al stainless steel)
US4491622A (en) * 1982-04-19 1985-01-01 Olin Corporation Composites of glass-ceramic to metal seals and method of making the same
US4500605A (en) * 1983-02-17 1985-02-19 Olin Corporation Electrical component forming process
US4524238A (en) * 1982-12-29 1985-06-18 Olin Corporation Semiconductor packages
US4542259A (en) * 1984-09-19 1985-09-17 Olin Corporation High density packages
US4570337A (en) * 1982-04-19 1986-02-18 Olin Corporation Method of assembling a chip carrier
US4577056A (en) * 1984-04-09 1986-03-18 Olin Corporation Hermetically sealed metal package
US4656499A (en) * 1982-08-05 1987-04-07 Olin Corporation Hermetically sealed semiconductor casing
US4682414A (en) * 1982-08-30 1987-07-28 Olin Corporation Multi-layer circuitry
US4769345A (en) * 1987-03-12 1988-09-06 Olin Corporation Process for producing a hermetically sealed package for an electrical component containing a low amount of oxygen and water vapor
US4775647A (en) * 1984-09-19 1988-10-04 Olin Corporation Sealing glass composite
US4784974A (en) * 1982-08-05 1988-11-15 Olin Corporation Method of making a hermetically sealed semiconductor casing
US4790977A (en) * 1987-09-10 1988-12-13 Armco Advanced Materials Corporation Silicon modified low chromium ferritic alloy for high temperature use
US4801488A (en) * 1984-09-19 1989-01-31 Olin Corporation Sealing glass composite
US4805009A (en) * 1985-03-11 1989-02-14 Olin Corporation Hermetically sealed semiconductor package
US4816216A (en) * 1985-11-29 1989-03-28 Olin Corporation Interdiffusion resistant Fe--Ni alloys having improved glass sealing
US4851615A (en) * 1982-04-19 1989-07-25 Olin Corporation Printed circuit board
US4853491A (en) * 1984-10-03 1989-08-01 Olin Corporation Chip carrier
US4862323A (en) * 1984-04-12 1989-08-29 Olin Corporation Chip carrier
US4866571A (en) * 1982-06-21 1989-09-12 Olin Corporation Semiconductor package
US4905074A (en) * 1985-11-29 1990-02-27 Olin Corporation Interdiffusion resistant Fe-Ni alloys having improved glass sealing property
US5007956A (en) * 1986-04-11 1991-04-16 Nippon Piston Ring Co., Ltd. Assembled cam shaft
US5014159A (en) * 1982-04-19 1991-05-07 Olin Corporation Semiconductor package
EP0658632A1 (en) * 1993-07-06 1995-06-21 Nippon Steel Corporation Steel of high corrosion resistance and steel of high corrosion resistance and workability
US5578265A (en) * 1992-09-08 1996-11-26 Sandvik Ab Ferritic stainless steel alloy for use as catalytic converter material
US5720920A (en) * 1993-07-06 1998-02-24 Nippon Steel Corporation Steel having excellent corrosion resistance and steel having excellent corrosion resistance and workability
US6149862A (en) * 1999-05-18 2000-11-21 The Atri Group Ltd. Iron-silicon alloy and alloy product, exhibiting improved resistance to hydrogen embrittlement and method of making the same
WO2010108528A1 (en) * 2009-03-26 2010-09-30 Federal-Mogul Burscheid Gmbh Nitratable steel material composition for producing piston rings and cylindrical sleeves
EP3261436A4 (en) * 2015-02-27 2018-07-25 Ecolab USA Inc. System and method for treating items with insecticide

Cited By (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3909250A (en) * 1973-06-25 1975-09-30 Armco Steel Corp Oxidation-resistant ferrous alloy
US3905780A (en) * 1973-06-25 1975-09-16 Armco Steel Corp Oxidation-resistant low alloy steel with Al coating
US4141724A (en) * 1978-06-21 1979-02-27 United States Steel Corporation Low-cost, high temperature oxidation-resistant steel
US4299622A (en) * 1978-11-06 1981-11-10 Sony Corporation Magnetic alloy
US4398951A (en) * 1981-04-22 1983-08-16 Unisearch Limited Fermalloy(Fe-Mn-Al stainless steel)
US5014159A (en) * 1982-04-19 1991-05-07 Olin Corporation Semiconductor package
US4491622A (en) * 1982-04-19 1985-01-01 Olin Corporation Composites of glass-ceramic to metal seals and method of making the same
US4851615A (en) * 1982-04-19 1989-07-25 Olin Corporation Printed circuit board
US4570337A (en) * 1982-04-19 1986-02-18 Olin Corporation Method of assembling a chip carrier
US4866571A (en) * 1982-06-21 1989-09-12 Olin Corporation Semiconductor package
US4784974A (en) * 1982-08-05 1988-11-15 Olin Corporation Method of making a hermetically sealed semiconductor casing
US4656499A (en) * 1982-08-05 1987-04-07 Olin Corporation Hermetically sealed semiconductor casing
US4682414A (en) * 1982-08-30 1987-07-28 Olin Corporation Multi-layer circuitry
US4524238A (en) * 1982-12-29 1985-06-18 Olin Corporation Semiconductor packages
US4500605A (en) * 1983-02-17 1985-02-19 Olin Corporation Electrical component forming process
US4577056A (en) * 1984-04-09 1986-03-18 Olin Corporation Hermetically sealed metal package
US4862323A (en) * 1984-04-12 1989-08-29 Olin Corporation Chip carrier
US4775647A (en) * 1984-09-19 1988-10-04 Olin Corporation Sealing glass composite
US4542259A (en) * 1984-09-19 1985-09-17 Olin Corporation High density packages
US4801488A (en) * 1984-09-19 1989-01-31 Olin Corporation Sealing glass composite
US4853491A (en) * 1984-10-03 1989-08-01 Olin Corporation Chip carrier
US4805009A (en) * 1985-03-11 1989-02-14 Olin Corporation Hermetically sealed semiconductor package
US4816216A (en) * 1985-11-29 1989-03-28 Olin Corporation Interdiffusion resistant Fe--Ni alloys having improved glass sealing
US4905074A (en) * 1985-11-29 1990-02-27 Olin Corporation Interdiffusion resistant Fe-Ni alloys having improved glass sealing property
US5007956A (en) * 1986-04-11 1991-04-16 Nippon Piston Ring Co., Ltd. Assembled cam shaft
US4769345A (en) * 1987-03-12 1988-09-06 Olin Corporation Process for producing a hermetically sealed package for an electrical component containing a low amount of oxygen and water vapor
US4790977A (en) * 1987-09-10 1988-12-13 Armco Advanced Materials Corporation Silicon modified low chromium ferritic alloy for high temperature use
US5578265A (en) * 1992-09-08 1996-11-26 Sandvik Ab Ferritic stainless steel alloy for use as catalytic converter material
EP0658632A4 (en) * 1993-07-06 1995-11-29 Nippon Steel Corp Steel of high corrosion resistance and steel of high corrosion resistance and workability.
EP0658632A1 (en) * 1993-07-06 1995-06-21 Nippon Steel Corporation Steel of high corrosion resistance and steel of high corrosion resistance and workability
US5720920A (en) * 1993-07-06 1998-02-24 Nippon Steel Corporation Steel having excellent corrosion resistance and steel having excellent corrosion resistance and workability
US6149862A (en) * 1999-05-18 2000-11-21 The Atri Group Ltd. Iron-silicon alloy and alloy product, exhibiting improved resistance to hydrogen embrittlement and method of making the same
WO2010108528A1 (en) * 2009-03-26 2010-09-30 Federal-Mogul Burscheid Gmbh Nitratable steel material composition for producing piston rings and cylindrical sleeves
US8317938B2 (en) 2009-03-26 2012-11-27 Federal-Mogul Burscheid Gmbh Nitratable steel material composition for producing piston rings and cylindrical sleeves
EP3261436A4 (en) * 2015-02-27 2018-07-25 Ecolab USA Inc. System and method for treating items with insecticide
US11039612B2 (en) 2015-02-27 2021-06-22 Ecolab Usa Inc. System and method for treating items with insecticide

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