US3272665A - Molybdate coatings on aluminum and aluminum base alloys - Google Patents

Molybdate coatings on aluminum and aluminum base alloys Download PDF

Info

Publication number
US3272665A
US3272665A US275225A US27522563A US3272665A US 3272665 A US3272665 A US 3272665A US 275225 A US275225 A US 275225A US 27522563 A US27522563 A US 27522563A US 3272665 A US3272665 A US 3272665A
Authority
US
United States
Prior art keywords
aluminum
molybdate
base alloys
temperature
particles
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US275225A
Inventor
Romans Harmon Brown
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Reynolds Metals Co
Original Assignee
Reynolds Metals Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Reynolds Metals Co filed Critical Reynolds Metals Co
Priority to US275225A priority Critical patent/US3272665A/en
Application granted granted Critical
Publication of US3272665A publication Critical patent/US3272665A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • C23C22/00—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C22/05—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions
    • C23C22/06—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH less than 6
    • C23C22/40—Chemical surface treatment of metallic material by reaction of the surface with a reactive liquid, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using aqueous solutions using aqueous acidic solutions with pH less than 6 containing molybdates, tungstates or vanadates
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2982—Particulate matter [e.g., sphere, flake, etc.]
    • Y10T428/2991—Coated

Definitions

  • This invention relates to the protection of the surfaces of aluminum and aluminum base alloys against corrosion. More particularly, the invention concerns the protection of particles and sheet or strip by treatment of the surfaces thereof with alkali metal molybdate solutions at elevated temperature and pressure.
  • aluminum and aluminum base alloys are subject to corrosion by brines and other corrosive agents.
  • small generally spherical particles of aluminum or aluminum base alloys are employed as propping agents for creating or enlarging well fractures, it has been observed that the life of such agents is sometimes shortened by corrosion induced by conditions of moisture within the well, and/or by the direct action of oil well brines and other corrosive compositions encountered in subsurface work.
  • Such aluminum particles are of a size lying generally between about 0.03 and about 0.25 inch in diameter, thus possessing a high surface area which makes them particularly susceptible to corrosion.
  • Such treatments provide a molybdate coating on the aluminum surface which is relatively thin, porous and low in abrasion resistance, and the protection provided by such conventional molybdate coatings on aluminum surfaces would not be adequate for protection of aluminum particles used as propping agents in oil wells or the like having the corrosioninducing conditions sometimes encountered in such wells.
  • the alkali metal is preferably sodium or potassium, but may include other alkali metals such as lithium, caesium and rubidium.
  • the concentration of the alkali metal molybdate solution should be at least about 4% by weight in order to provide enough molybdate in a conveniently limited amount of solution, and can be increased to any amount, although 5% by weight is generally preferred.
  • Treatment is carried out, in accordance with the invention, under pressure in a suitable pressure vessel, such as an autoclave, so as to maintain the treating solution and the metal surface being treated at a temperature between about 325 F. and about 400 F., preferably about 350 F. While the temperature can be raised to a figure higher than indicated, about 400 F. represents a practical upper limit in order to avoid converting the metal surface to oxide by action of hot water, to an undesirable extent.
  • a suitable pressure vessel such as an autoclave
  • the pressure may be varied according to known practice by the increase of temperature, or it may be raised further by the introduction of carbon dioxide or other inert gas. Some pressure may also be achieved by the presence of gas generated in the course of the treatment. For the production of a good coating, the pressure will be above about 275 pounds per square inch, and about 300 psi. is preferred, but there is no upper limit.
  • the period of treatment will very somewhat according to the size of the surface of the aluminum or aluminum base alloy, but should in general range from about 2 to about 24 hours.
  • For the treatment of propping agent a minimum of about 16 hours at 350 F. is preferred, but this may be shortened to 6 hours in presence of carbon dioxide under pressure.
  • the monohydrate coating appears to be accompanied by an adsorption phenomenon whereby alkali metal molybdate is adsorbed and remains in anhydrous form in the oxide coating. This is demonstrated by the observation that the adsorbed alkali metal molybdate cannot be removed from the oxide by leaching with water, although it is ordinarily quite soluble. From another point of View, the oxide-molybdate coating formed at elevated temperature and pressure closes cavities on the metal surface, and because of its greater thickness as well, affords increased protection to the metal against corrosive influences.
  • Aluminum and aluminum base alloy particles having the improved coating produced in accordance with the method of the invention can be used successfully as propping agents in oil wells having severe conditions.
  • the treatment process is also applicable to the protection of aluminum and aluminum base alloys in particle form intended for other purposes, for example, protection is afforded to such particles against corrosive tap water.
  • the treatment of the invention is also suitable for the protection of aluminum and aluminum base alloys in the form of sheet and strip, and here a much shorter treatment time is sufficient, for example as little as two hours.
  • Example 1 10 lbs. of aluminum shot having a generally spherical shape, and averaging about 0.1 inch in diameter, were immersed in a aqueous solution of sodium molybdate in an autoclave and reacted for 24 hours under pressure sufficient to maintain the temperature of the mixture in the autoclave at about 350 F. at the end of the treatment, the aluminum shot was removed and treated with a simulated well brine solution at a temperature of 300 F. for 28 days. No perceptible corrosion of the surfaces of the particles was observed.
  • Example 2 When the treatment and test of Example 1 is repeated except for substitution of potassium molybdate for sodium molybdate, substantially the same results are obtainable.
  • Example 3 The treatment described in Example 1 was carried out under a pressure of 275 p.s.i. obtained by adding Dry Ice to the autoclave at 350 F. for a period of six hours.
  • Example 4 A sheet of alloy 5052 having a thickness of 0.008 inch was treated for 2 hours as described in Example 3.
  • Method for protecting the surface of aluminum and aluminum base alloys against corrosion which comprises immersing said surface in an aqueous solution consisting essentially of water and at least about 4% by Weight of an alkali metal molybdate at a temperature between about 325 and about 400 F. for a period of at least 2 hours under pressure sufficient to maintain the solution and the metal surface at said temperature.
  • Method for protecting the surface of aluminum and aluminum base alloys against corrosion which comprises immersing said surface in an aqueous solution consisting essentially of water at least about 4% by weight of an alkali metal molybdate at a temperature between about 325 and about 400 F. for a period of at least 2 hours at a pressure of at least 275 pounds per square inch.
  • Method for protecting the surface of aluminum and aluminum base alloys against corrosion which comprises immersing said surface in an aqueous solution consisting essentially of water and at least about 4% by weight of an alkali metal molybdate at a temperature between about 325 and about 400 F. for a period of at least two hours in presence of carbon dioxide gas under pressure sufficient to maintain the solution and the metal surface at said temperature.
  • Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines which comprises immersing said particles in an aqueous solution consisting essentially of water and at least about 4% by weight of an alkali metal molybdate at a temperature between about 325 and about 400 F. for a period of at least 16 hours under pressure sufficient to maintain the solution and the metal surface at said temperature.
  • Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines which comprises immersing said particles in an aqueous solution consisting essentially of water and at least about 4% by weight of an alkali metal molybdate at a temperature between about 325 and about 400 F. for a period of at least 16 hours under pressure of at least 275 pounds per square inch.
  • Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines which comprises immersing said particles in an aqueous solution consisting essentially of water and at least about 4% by weight of sodium molybdate at a temperature between about 325 and about 400 F. for a period of at least 16 hours under pressure of at least 275 pounds per square inch.
  • Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines which comprises immersing said particles in an aqueous solution consisting essentially of water and at least about 4% by weight of potassium molybdate at a temperature between abuot 325 and about 400 F. for a period of at least 16 hours under pressure of at least 275 pounds per square inch.
  • Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines which comprises immersing said particles in an aqueous solution consisting essentially of water and about 5% by weight of sodium molybdate at a temperature of about 350 F. for a period of at least 16 hours under pressure sufficient to maintain said temperature.
  • Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines which comprises immersing said particles in an aqueous solution consisting essentially of water and about 5% by weight of potassium molybdate at a temperature of about 350 F. for a period of at least 16 hours under pressure sulficient to maintain said temperature.
  • Method for protecting particles of aluminum and aluminum base alloys against corrosion which comprises immersing said particles in an aqueous solution consisting essentially of water and about 5% by weight of sodium molybdate at a temperature of about 350 F. and a pressure of about 275 pounds per sq. inch in presence of carbon dioxide gas for about 6 hours.

Landscapes

  • Chemical & Material Sciences (AREA)
  • General Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Treatment Of Metals (AREA)
  • Preventing Corrosion Or Incrustation Of Metals (AREA)

Description

United States Patent 3,272,665 MULYBDATE COATINGS 0N ALUMINUM AND ALUMINUM BASE ALLOYS Harmon Brown Romans, Henrico County, Va., assignor to Reynolds Metals Company, Richmond, Va., a corporation of Virginia No Drawing. Filed Apr. 24, 1963, Ser. No. 275,225 13 Claims. (Cl. 148-627) This application is a continuation-in-part of application Serial No. 236,682, filed November 8, 1962, and now abandoned.
This invention relates to the protection of the surfaces of aluminum and aluminum base alloys against corrosion. More particularly, the invention concerns the protection of particles and sheet or strip by treatment of the surfaces thereof with alkali metal molybdate solutions at elevated temperature and pressure.
It is known that aluminum and aluminum base alloys are subject to corrosion by brines and other corrosive agents. Where small generally spherical particles of aluminum or aluminum base alloys are employed as propping agents for creating or enlarging well fractures, it has been observed that the life of such agents is sometimes shortened by corrosion induced by conditions of moisture within the well, and/or by the direct action of oil well brines and other corrosive compositions encountered in subsurface work. Such aluminum particles are of a size lying generally between about 0.03 and about 0.25 inch in diameter, thus possessing a high surface area which makes them particularly susceptible to corrosion. In fracturing operations, they are suspended in hydraulic fracture liquids which are pumped into the well to create or enlarge flow channels extending from the well bore into contiguous formations. Such particles, when unprotected, may under some conditions corrode to form a solid mass, resulting in expense of removal and loss of material.
In accordance with the present invention there is provided a novel method of treatment of the surfaces of aluminum and aluminum base alloys, both in the form of particles and of sheets or strip, as well as novel treated materials, whereby effective protection against corrosion of these materials can be obtained for extended periods, thereby greatly increasing the useful life of these materials.
It has been known to treat aluminum surfaces in general with aqueous solutions of sodium or potassium molybdate by immersion for relatively short periods (e.g., 5 to 60 minutes), at relatively low temperatures (e.g., room temperature up to the boiling point of a saline Water solution), and at relatively low pressures (e.g., atmospheric pressure or up to about 15 psi. above atmospheric pressure), using concentrations of about 0.5% to about 6% of the molybdate by weight. Such treatments provide a molybdate coating on the aluminum surface which is relatively thin, porous and low in abrasion resistance, and the protection provided by such conventional molybdate coatings on aluminum surfaces would not be adequate for protection of aluminum particles used as propping agents in oil wells or the like having the corrosioninducing conditions sometimes encountered in such wells.
In accordance with the present invention, however, it has been found that aluminum and aluminum base alloy surfaces can be successfully treated with aqueous solutions of alkali metal molybdates under different conditions which will produce a coating onthe surfaces which is not only thicker but also substantially nonporous and more abrasion resistant than the coating produced with molybdate using conventional conditions.
For the purposes of the invention, the alkali metal is preferably sodium or potassium, but may include other alkali metals such as lithium, caesium and rubidium.
3,272,665 Patented Sept. '13, 1966 The concentration of the alkali metal molybdate solution should be at least about 4% by weight in order to provide enough molybdate in a conveniently limited amount of solution, and can be increased to any amount, although 5% by weight is generally preferred.
Treatment is carried out, in accordance with the invention, under pressure in a suitable pressure vessel, such as an autoclave, so as to maintain the treating solution and the metal surface being treated at a temperature between about 325 F. and about 400 F., preferably about 350 F. While the temperature can be raised to a figure higher than indicated, about 400 F. represents a practical upper limit in order to avoid converting the metal surface to oxide by action of hot water, to an undesirable extent.
The pressure may be varied according to known practice by the increase of temperature, or it may be raised further by the introduction of carbon dioxide or other inert gas. Some pressure may also be achieved by the presence of gas generated in the course of the treatment. For the production of a good coating, the pressure will be above about 275 pounds per square inch, and about 300 psi. is preferred, but there is no upper limit.
The period of treatment will very somewhat according to the size of the surface of the aluminum or aluminum base alloy, but should in general range from about 2 to about 24 hours. For the treatment of propping agent a minimum of about 16 hours at 350 F. is preferred, but this may be shortened to 6 hours in presence of carbon dioxide under pressure.
While it is desired not to be bound by any particular theory, it is believed that under the conditions of elevated temperature and pressure described above, formation takes place on the metal surface of an oxide coating which consists essentially of the alpha phase of aluminum oxide monohydrate Al O .H O, known as boehmite. This formation is confirmed by X-ray diffraction studies, which also reveal that using the conventional low temperature molybdate treatment, an oxide coating is produced having the form of an alpha phase of aluminum oxide trihydrate Al O .3H O (gibbsite). The monohydrate coating is not only thicker than the trihydrate coating, but it differs in crystal structure. Further, formation of the monohydrate coating appears to be accompanied by an adsorption phenomenon whereby alkali metal molybdate is adsorbed and remains in anhydrous form in the oxide coating. This is demonstrated by the observation that the adsorbed alkali metal molybdate cannot be removed from the oxide by leaching with water, although it is ordinarily quite soluble. From another point of View, the oxide-molybdate coating formed at elevated temperature and pressure closes cavities on the metal surface, and because of its greater thickness as well, affords increased protection to the metal against corrosive influences.
Aluminum and aluminum base alloy particles having the improved coating produced in accordance with the method of the invention can be used successfully as propping agents in oil wells having severe conditions. The treatment process is also applicable to the protection of aluminum and aluminum base alloys in particle form intended for other purposes, for example, protection is afforded to such particles against corrosive tap water.
The treatment of the invention is also suitable for the protection of aluminum and aluminum base alloys in the form of sheet and strip, and here a much shorter treatment time is sufficient, for example as little as two hours.
The presence of carbon dioxide, which may be added to the autoclave in the form of Dry Ice (solid CO provides increased pressure, and considerably shortens the time of treatment. Thus, a treatment time of 16 hours at 350 C. for aluminum particles can be shortened to 6 hours by adding carbon dioxide in the form of Dry Ice to the autoclave, which provides a rapid build-up of pressure to the required value.
The practice of the method of the invention is illustrated by the following examples:
Example 1 10 lbs. of aluminum shot having a generally spherical shape, and averaging about 0.1 inch in diameter, were immersed in a aqueous solution of sodium molybdate in an autoclave and reacted for 24 hours under pressure sufficient to maintain the temperature of the mixture in the autoclave at about 350 F. at the end of the treatment, the aluminum shot was removed and treated with a simulated well brine solution at a temperature of 300 F. for 28 days. No perceptible corrosion of the surfaces of the particles was observed.
Example 2 When the treatment and test of Example 1 is repeated except for substitution of potassium molybdate for sodium molybdate, substantially the same results are obtainable.
Example 3 The treatment described in Example 1 was carried out under a pressure of 275 p.s.i. obtained by adding Dry Ice to the autoclave at 350 F. for a period of six hours.
Example 4 A sheet of alloy 5052 having a thickness of 0.008 inch was treated for 2 hours as described in Example 3.
While present preferred embodiments of the invention, and methods of practicing the same, have been illustrated and described, it will be recognized that the invention may be otherwise variously embodied and practiced within the scope of the following claims.
What is claimed is:
1. Method for protecting the surface of aluminum and aluminum base alloys against corrosion which comprises immersing said surface in an aqueous solution consisting essentially of water and at least about 4% by Weight of an alkali metal molybdate at a temperature between about 325 and about 400 F. for a period of at least 2 hours under pressure sufficient to maintain the solution and the metal surface at said temperature.
2. Method for protecting the surface of aluminum and aluminum base alloys against corrosion which comprises immersing said surface in an aqueous solution consisting essentially of water at least about 4% by weight of an alkali metal molybdate at a temperature between about 325 and about 400 F. for a period of at least 2 hours at a pressure of at least 275 pounds per square inch.
3. Method for protecting the surface of aluminum and aluminum base alloys against corrosion which comprises immersing said surface in an aqueous solution consisting essentially of water and at least about 4% by weight of an alkali metal molybdate at a temperature between about 325 and about 400 F. for a period of at least two hours in presence of carbon dioxide gas under pressure sufficient to maintain the solution and the metal surface at said temperature.
4. Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines, which comprises immersing said particles in an aqueous solution consisting essentially of water and at least about 4% by weight of an alkali metal molybdate at a temperature between about 325 and about 400 F. for a period of at least 16 hours under pressure sufficient to maintain the solution and the metal surface at said temperature.
5. Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines, which comprises immersing said particles in an aqueous solution consisting essentially of water and at least about 4% by weight of an alkali metal molybdate at a temperature between about 325 and about 400 F. for a period of at least 16 hours under pressure of at least 275 pounds per square inch.
6. Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines, which comprises immersing said particles in an aqueous solution consisting essentially of water and at least about 4% by weight of sodium molybdate at a temperature between about 325 and about 400 F. for a period of at least 16 hours under pressure of at least 275 pounds per square inch.
7. Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines, which comprises immersing said particles in an aqueous solution consisting essentially of water and at least about 4% by weight of potassium molybdate at a temperature between abuot 325 and about 400 F. for a period of at least 16 hours under pressure of at least 275 pounds per square inch.
8. Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines, which comprises immersing said particles in an aqueous solution consisting essentially of water and about 5% by weight of sodium molybdate at a temperature of about 350 F. for a period of at least 16 hours under pressure sufficient to maintain said temperature.
9. Method for protecting particles of aluminum and aluminum base alloys for propping fractured subsurface well formations against corrosion by well brines, which comprises immersing said particles in an aqueous solution consisting essentially of water and about 5% by weight of potassium molybdate at a temperature of about 350 F. for a period of at least 16 hours under pressure sulficient to maintain said temperature.
10. The method of claim 1 in which the aluminum and aluminum base alloy is in the form of sheet.
11. Method for protecting particles of aluminum and aluminum base alloys against corrosion which comprises immersing said particles in an aqueous solution consisting essentially of water and about 5% by weight of sodium molybdate at a temperature of about 350 F. and a pressure of about 275 pounds per sq. inch in presence of carbon dioxide gas for about 6 hours.
12. Generally spherical particles of aluminum and aluminum base alloys adapted for propping fractured subsurface well formation and having their surfaces treated in accordance with the method of claim 4.
13. Aluminum and aluminum base alloys having their surfaces treated in accordance with the method of claim 1.
References Cited by the Examiner UNITED STATES PATENTS 1,811,298 6/1931 Boulanger 1486.27 X 2,554,256 5/1951 Lewis et a1. 148-627 2,899,368 8/1959 Spooner 20435.1 3,173,484 3/1965 Huitt 2528.55 FOREIGN PATENTS 535,614 4/1941 Great Britain.
ALFRED L. LEAVITT, Primary Examiner.
R. S. KENDALL, Assistant Examiner.

Claims (1)

1. METHOD FOR PROTECTING THE SURFACE OF ALUMINUM AND ALUMINUM BASE ALLOYS AGAINST CORROSION WHICH COMPRISES IMMERSING SAID SURFACE IN AN AQUEOUS SOLUTION CONSISTING ESSENTIALLY OF WATER AND AT LEAST ABOUT 4% BY WEIGHT OF AN ALKALI METAL MOLYBDATE AT A TEMPERATURE BETWEEN ABOUT 325* AND ABOUT 400*F. FOR A PERIOD OF AT LEAST 2 HOURS UNDER PRESSURE SUFFICIENT TO MAINTAIN THE SOLUTION AND THE METAL SURFACE AT SAID TEMPERATURE.
US275225A 1963-04-24 1963-04-24 Molybdate coatings on aluminum and aluminum base alloys Expired - Lifetime US3272665A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US275225A US3272665A (en) 1963-04-24 1963-04-24 Molybdate coatings on aluminum and aluminum base alloys

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US275225A US3272665A (en) 1963-04-24 1963-04-24 Molybdate coatings on aluminum and aluminum base alloys

Publications (1)

Publication Number Publication Date
US3272665A true US3272665A (en) 1966-09-13

Family

ID=23051384

Family Applications (1)

Application Number Title Priority Date Filing Date
US275225A Expired - Lifetime US3272665A (en) 1963-04-24 1963-04-24 Molybdate coatings on aluminum and aluminum base alloys

Country Status (1)

Country Link
US (1) US3272665A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992005297A1 (en) * 1990-09-19 1992-04-02 Michigan Chrome And Chemical Company Corrosion resistant coated articles and process for making same
US5219617A (en) * 1989-09-19 1993-06-15 Michigan Chrome And Chemical Company Corrosion resistant coated articles and process for making same

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1811298A (en) * 1928-11-10 1931-06-23 Parker Ste Continentale Process and product for protecting aluminium, magnesium and their alloys against corrosion
GB535614A (en) * 1939-09-07 1941-04-16 British Aluminium Co Ltd Improvements in or relating to the surface treatment of aluminium and aluminium alloys
US2554256A (en) * 1948-05-15 1951-05-22 Westinghouse Electric Corp Process for treating aluminum to provide selective coloration of portions thereof
US2899368A (en) * 1959-08-11 Methods of sealing anodic aluminium
US3173484A (en) * 1958-09-02 1965-03-16 Gulf Research Development Co Fracturing process employing a heterogeneous propping agent

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2899368A (en) * 1959-08-11 Methods of sealing anodic aluminium
US1811298A (en) * 1928-11-10 1931-06-23 Parker Ste Continentale Process and product for protecting aluminium, magnesium and their alloys against corrosion
GB535614A (en) * 1939-09-07 1941-04-16 British Aluminium Co Ltd Improvements in or relating to the surface treatment of aluminium and aluminium alloys
US2554256A (en) * 1948-05-15 1951-05-22 Westinghouse Electric Corp Process for treating aluminum to provide selective coloration of portions thereof
US3173484A (en) * 1958-09-02 1965-03-16 Gulf Research Development Co Fracturing process employing a heterogeneous propping agent

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5219617A (en) * 1989-09-19 1993-06-15 Michigan Chrome And Chemical Company Corrosion resistant coated articles and process for making same
US5492766A (en) * 1989-09-19 1996-02-20 Michigan Chrome And Chemical Company Corrosion resistant coated articles and process for making same
WO1992005297A1 (en) * 1990-09-19 1992-04-02 Michigan Chrome And Chemical Company Corrosion resistant coated articles and process for making same

Similar Documents

Publication Publication Date Title
DE10163107C1 (en) Magnesium workpiece and method for forming a corrosion-protective top layer of a magnesium workpiece
Meletis et al. A review of the crystallography of stress corrosion cracking
US3003899A (en) Removal of scale deposits
US3272665A (en) Molybdate coatings on aluminum and aluminum base alloys
US2011579A (en) Intensified hydrochloric acid
Shuaib-Babata et al. Corrosion inhibition of AISI 1007 steel in hydrochloric acid using cucumis sativus (cucumber) extracts as green inhibitor
US2750271A (en) Process of making pulverulent metallic titanium
US2122535A (en) Duplex metal article
JPS6058161B2 (en) Flexible layered graphite material and its manufacturing method
US3620939A (en) Coating for magnesium and its alloys and method of applying
US1509605A (en) Process of making aluminum chloride
US2313754A (en) Method of protecting magnesium and its alloys from corrosion
US2017428A (en) Protection of metal surfaces
US2384835A (en) Production of metallic magnesium
Abiola et al. Anti-corrosive properties of Delonix regia extract on mild steel corrosion in acid fluid for industrial operations
US3129760A (en) Hot caustic treatment of earth formations
Antill et al. Deformation of magnesium and its alloys on oxidation
US3389982A (en) Method for making high strength spherical glass bodies
US2339545A (en) Method of plating polonium
US2337940A (en) Method of treating aluminum surfaces
Hodges Problems and ethics in the conservation of metal objects
Ahmad et al. Corrosion resistance of a new AL 6013-20 SiC (P) in salt spray chamber
US716977A (en) Process of purifying aluminium.
Maskell et al. Influence of Nitrogen Content on the Stress-Corrosion Susceptibility of Some Austenitic Chromium-Nickel Steels
US1927660A (en) Treating materials with hydrochloric acid gas at elevated temperatures