US3247297A - Process for the preparation of metallic materials by compression of a magnesium or magnesium alloy powder - Google Patents

Process for the preparation of metallic materials by compression of a magnesium or magnesium alloy powder Download PDF

Info

Publication number
US3247297A
US3247297A US165035A US16503562A US3247297A US 3247297 A US3247297 A US 3247297A US 165035 A US165035 A US 165035A US 16503562 A US16503562 A US 16503562A US 3247297 A US3247297 A US 3247297A
Authority
US
United States
Prior art keywords
magnesium
powder
compression
fluorine
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
US165035A
Inventor
Salesse Marc
Herenguel Jean
Caillat Roger
Boghen Jacques
Darras Raymond
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.)
Commissariat a lEnergie Atomique et aux Energies Alternatives CEA
Original Assignee
Commissariat a lEnergie Atomique CEA
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 Commissariat a lEnergie Atomique CEA filed Critical Commissariat a lEnergie Atomique CEA
Application granted granted Critical
Publication of US3247297A publication Critical patent/US3247297A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C8/00Solid 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
    • C23C8/06Solid 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
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0408Light metal alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C32/00Non-ferrous alloys containing at least 5% by weight but less than 50% by weight of oxides, carbides, borides, nitrides, silicides or other metal compounds, e.g. oxynitrides, sulfides, whether added as such or formed in situ
    • GPHYSICS
    • G21NUCLEAR PHYSICS; NUCLEAR ENGINEERING
    • G21CNUCLEAR REACTORS
    • G21C3/00Reactor fuel elements and their assemblies; Selection of substances for use as reactor fuel elements
    • G21C3/02Fuel elements
    • G21C3/04Constructional details
    • G21C3/06Casings; Jackets
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00Energy generation of nuclear origin
    • Y02E30/30Nuclear fission reactors
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/29Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2982Particulate matter [e.g., sphere, flake, etc.]

Definitions

  • the present invention relates to a process for the preparation of metallic materials by compression of a magnesium or magnesium alloy powder.
  • the invention also relates to powders and materials obtained by this process.
  • Known processes for improving the mechanical resistance of magnesium generally consist in utilising alloys or, preferably, in making magnesium materials from powders which undergo oxidation before, during and/or after compaction of the powder.
  • Oxidation of magnesium particles is a very difficult operation, however, particularly with those fine powders which confer a high mechanical resistance on the material. This also applies to the fine parts of mixtures of powders of a range of particle sizes. With such fine powders, oxidation produces quite thick oxide films, if it does not cause, through uncontrollable elevation of the temperature, substantially complete oxidation which involves the risk of extending to the entire mass.
  • the products obtained have the following disadvantages:
  • the present invention has the object of providing an improved process for the preparation of magnesium-base materials which avoids these disadvantages and permits such materials to be obtained from magnesium or magnesium alloy powders.
  • the materials produced have excellent mechanical properties, both in the cold and hot, and also have excellent resistance to corrosion at elevated temperatures in oxidising and humid atmospheres.
  • a process for the preparation of a magnesium-base material comprises compressing a magnesium-containing powder before, during and/or after subjecting it to an atmosphere containing fluorine or a fluorine compound at a temperature in the range of 0 to 600 C. so as to produce a compact material containing 0.1 to 15% by weight of combined fluorine.
  • the substance or substances which can be used, in carrying out the process, to incorporate the fluorine into the ultimate product, which is referred to for brevity as fluorina-tion,” can include gaseous fluorine, hydrogen fluoride, hydrofluoric acid or any other fluorinated substance capable of readily evolving fluorine, and can if desired be diluted with an inert gas, such as argon.
  • the particle size range of the initial powder can be from 1 to 2000 microns.
  • the process can be applied to powders having particles of any shape, such as spheres or dendrites, and also to powders having particles of very irregular shapes and sizes.
  • the temperature at which fluorination is carried out preferably lies between the ambient temperature and 600 C.
  • the duration of the fluorination step depends upon the composition of the gaseous phase used and also upon the temperature, and is generally from 2 to 5 hours.
  • the fluorination step can be effected in various ways.
  • a first preferred embodiment consists in introducing the powder to be fluorinated, before it is compacted into a receptacle made of suitable material, such as nickel or stainless steel, and placing the receptacle inside a sealed and fixed horizontal furance, made of a suitable material such as copper.
  • the apparatus is then purged with an inert gas, for example argon, and then gaseous fluorine or a fluorine compound, diluted with an inert gas if desired, is introduced.
  • an inert gas for example argon
  • gaseous fluorine or a fluorine compound diluted with an inert gas if desired, is introduced.
  • the introduction of the gas and, if desired, the temperature of heating are so controlled that the temperature lies between the ambient temperature and 600 C.
  • Another embodiment in which fluorination is also eflected before compaction, consists in using a rotary furnace containing balls.
  • the powder is continuously eroded as it is fluorinated.
  • the balls can be of an appropriate material, such as steel covered with magnesium.
  • This process allows very fine particles to be obtained and lower temperatures to be used, for a given ombined fluorine content, as compared with the first embodiment. Also, the subsequent compaction of the treated powder more readily yields a material having good mechanical properties.
  • the fluorination treatment can also be eflected upon a compressed material obtained from the powder while subjecting the material to plastic deformation, for example rolling or drawing.
  • a fluorination agent can also be reacted with a more or less compact mass formed previously by compression of the powder.
  • the mass can be produced by compression in the cold or at an elevated temperature. Either a non-fluorinated compacted powder or one previously compressed can be treated in the process.
  • a thin coating of magnesium fluoride is obtained on the metal particles, having a thickness of about one hundredth of a micron.
  • the combined fluorine content of the metal should be controlled so as to have a value from 0.1 to 15% by weight in the final product.
  • the fluorine content which allows given mechanical properties to be obtained is a function of the particle size of the powder.
  • the combined fluorine content preferably lies between 0.5 and 2%, if good ductiltiy with flow resistance are to be obtained.
  • Mg-MgO material 100-200 Specific surface (mi/g.) 0. 25 0.25 0. 25 0. 50
  • compression is effected in the cold with a compressive force of 4 to 60 metric tons/mm
  • One or more compressions in the hot are then eiiected, depending upon the particle size range of the powder used, at temperatures below 600C. If the powders have particle sizes below 100 microns, two or three successive compressions at increasing temperatures are of advantages, since if compression at the maximum temperature were effected immediately after cold compression, oxidation would occur or even ignition of the magnesium powder.
  • the compressed materials so obtained can then be subjected to plastic deformation by the standard techby heating in air.
  • the right-hand column of the table shows the results obtained for a material prepared by the above compaction treatment, starting with a non- ;fiuorinated composite Mg-MgO material, having a particle size range of 100-200 microns.
  • the material obtained was taken up to 450C. by heating in air. It may be mentioned in this connection that, if a very fine Mg-MgO powder is used, having a particle size range of 10 to 65
  • the table shows the improvement in mechanical properties which can be obtained by using the process of the invent-ion.
  • the rupture load, elasticity and rupture elongation values, both cold and hot, are clearly better than the corresponding values of known magnesium-base materials, such as magnesium alloys or composite materials of the Mg-MgO type.
  • the fluorinated and compacted materials of the invention are of great interest because of their remarkable resistance to corrosion in air. They can be heated to 500 C. in air saturated with water vapour Without appreciably corroding, the increase in weight being less than 1 mg./ cm. after exposure for 800 hours, whereas with ordinary magnesium-base materials a very large degradation occurs in air at 400 C. and, from 350 C., oxidation is very substantial and can have serious effects.
  • the ignition temperature in humid air of the novel material is 640 C. and is about 40 to 50 C. higher than that of pure magnesium and undergoes much less violent combustion.
  • a process for the preparation of an improved metall'ic material formed from the compression of a member selected from the group consisting of a magnesium powder and a magnesium alloy powder comprising the steps of subjecting particles of said powder having a size range of from 1 to 2,000 microns to a gaseous atmosphere consisting essentially of a fluorine containing gas at a temperature from 0 C. to 600 C. until a material containing 0.1 to 15% by weight of combined fluorine as a thin film of magnesium fluoride on the particles is produced and compressing said particles of powder.
  • a magnesium-base material comprising a powder, the particles of which comprise substantially magnesium

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Plasma & Fusion (AREA)
  • General Engineering & Computer Science (AREA)
  • High Energy & Nuclear Physics (AREA)
  • Powder Metallurgy (AREA)

Description

United States Patent 3 247 297 raocnss roa THE PfiErARA'rIoN "or METALLIC MATERIALS BY COMPRESSIQN OF A MAGNE- SIUM 0R MAGNESIUM ALLOY POWDER Marc Salesse, Gif sur Yvette, Jean Herenguel, Versailles,
Roger Caillat, Sevres, Jacques Boghen, Argenteuil, and
Raymond Darras, Versailles, France, assignors to Commissariat a lEnergie Atomique, Paris, France N0 Drawing. Filed .Ian. 8, 1962, Ser. No. 165,035
Claims priority, application France, Mar. 3, 1961, 854,486 7 Claims. (Cl. 264-82) The present invention relates to a process for the preparation of metallic materials by compression of a magnesium or magnesium alloy powder.
The invention also relates to powders and materials obtained by this process.
It is well known that the fields of use of metallic materials depend essentially upon their mechanical properties and their resistance to oxidation Within a given temperature range. In the case of magnesium and its alloys, a degradation of the mechanical properties of materials made from such metal occurs from about 350- 400 C. On the other hand, oxidation in air becomes very appreciable and rapidly accelerates when the temperature rises above 350-400 C., for example, the metal is completely unusable in dry or humid oxidising atmospheres or in a non-oxidising but humid medium.
Known processes for improving the mechanical resistance of magnesium generally consist in utilising alloys or, preferably, in making magnesium materials from powders which undergo oxidation before, during and/or after compaction of the powder.
Oxidation of magnesium particles is a very difficult operation, however, particularly with those fine powders which confer a high mechanical resistance on the material. This also applies to the fine parts of mixtures of powders of a range of particle sizes. With such fine powders, oxidation produces quite thick oxide films, if it does not cause, through uncontrollable elevation of the temperature, substantially complete oxidation which involves the risk of extending to the entire mass. The products obtained have the following disadvantages:
(a) Insufliciently high rupture load, due to the impossibility of using sufliciently fine powders;
'(b) Low rupture elongations in traction, both in the cold and hot, due to excessive general or local oxidation;
(0) Irregular and dispersed properties when the heating of the powders has not been suflicient before compaction;
(d) No improvement in the oxidation resistance.
The present invention has the object of providing an improved process for the preparation of magnesium-base materials which avoids these disadvantages and permits such materials to be obtained from magnesium or magnesium alloy powders. The materials produced have excellent mechanical properties, both in the cold and hot, and also have excellent resistance to corrosion at elevated temperatures in oxidising and humid atmospheres.
According to the invention, a process for the preparation of a magnesium-base material comprises compressing a magnesium-containing powder before, during and/or after subjecting it to an atmosphere containing fluorine or a fluorine compound at a temperature in the range of 0 to 600 C. so as to produce a compact material containing 0.1 to 15% by weight of combined fluorine.
The substance or substances which can be used, in carrying out the process, to incorporate the fluorine into the ultimate product, which is referred to for brevity as fluorina-tion," can include gaseous fluorine, hydrogen fluoride, hydrofluoric acid or any other fluorinated substance capable of readily evolving fluorine, and can if desired be diluted with an inert gas, such as argon.
The particle size range of the initial powder can be from 1 to 2000 microns. The process can be applied to powders having particles of any shape, such as spheres or dendrites, and also to powders having particles of very irregular shapes and sizes.
The temperature at which fluorination is carried out preferably lies between the ambient temperature and 600 C.
The duration of the fluorination step depends upon the composition of the gaseous phase used and also upon the temperature, and is generally from 2 to 5 hours.
The fluorination step can be effected in various ways.
A first preferred embodiment consists in introducing the powder to be fluorinated, before it is compacted into a receptacle made of suitable material, such as nickel or stainless steel, and placing the receptacle inside a sealed and fixed horizontal furance, made of a suitable material such as copper.
The apparatus is then purged with an inert gas, for example argon, and then gaseous fluorine or a fluorine compound, diluted with an inert gas if desired, is introduced. The introduction of the gas and, if desired, the temperature of heating are so controlled that the temperature lies between the ambient temperature and 600 C.
Another embodiment, in which fluorination is also eflected before compaction, consists in using a rotary furnace containing balls. In this case, the powder is continuously eroded as it is fluorinated. The balls can be of an appropriate material, such as steel covered with magnesium.
This process allows very fine particles to be obtained and lower temperatures to be used, for a given ombined fluorine content, as compared with the first embodiment. Also, the subsequent compaction of the treated powder more readily yields a material having good mechanical properties.
The fluorination treatment can also be eflected upon a compressed material obtained from the powder while subjecting the material to plastic deformation, for example rolling or drawing.
A fluorination agent can also be reacted with a more or less compact mass formed previously by compression of the powder. The mass can be produced by compression in the cold or at an elevated temperature. Either a non-fluorinated compacted powder or one previously compressed can be treated in the process.
Irrespective of the procedure adopted, a thin coating of magnesium fluoride is obtained on the metal particles, having a thickness of about one hundredth of a micron. The combined fluorine content of the metal should be controlled so as to have a value from 0.1 to 15% by weight in the final product. For a given sample of powder, the fluorine content which allows given mechanical properties to be obtained is a function of the particle size of the powder. With fine powders, having a particle size below 60 microns, the combined fluorine content preferably lies between 0.5 and 2%, if good ductiltiy with flow resistance are to be obtained.
In general, as the particle size of the powder increases the value of the rupture load decreases, while the rupture elongation value increases. For a powder of given particle size, increase in the fluorine content has the eflect of very slightly increasing the rupture load value and greatly decreasing the rupture elongation value. Use of the process of the invention consequently allows predetermined mechanical properties to be obtained, by varying the particle size of the powder or the fluorine content or both.
Compaction of the fluorinated powders is preferably carried out in several stages:
Table Particle size range of magnesium 10-65 10-65 10-65 5-40 Composite powder (microns). Mg-MgO material, 100-200 Specific surface (mi/g.) 0. 25 0.25 0. 25 0. 50
Typo of treatment Hydrogen Gaseous Gaseous Gaseous No fiuorinatluoride, 1 fluorine, 2 fluorine, 2 fluorine, 2 tion hr. at 290 hrs. at 330 hrs. at 475 hrs. at 475 treatment 0. C. O. C.
Fluorine content as percent by weight of product obtained 0.88 2 6 12 Thickness of fluorine on each grain (mircons) 0.02 0.05 0. 14 0. 14
Average mechanical properties at 20 C.
R, kgJmm. 33. 7 32. 3 34. 8 35 28 E, kg./mm. 31. 4 30. 6 33.1 34. 21 A percent (elongation) [V678 4. 5 3. 6 2. 01 1. 4 3 A (Brinell hardness) 57. 5 53. 4 59 69 47 Average mechanical properties at; 450 C.
R, k.g/mm. 1.65 2.03 2.6 2. 8 1. 2 K, kg./mm. 1. 4 1. 75 2. 2 2. 5 1 A percent (elongation)/; 67S 13. 5 13. 9 10. 5 4. 3 4
Firstly, compression is effected in the cold with a compressive force of 4 to 60 metric tons/mm With low compressions, it is advantageous first to place the powder within an auxiliary container of magnesium.
One or more compressions in the hot are then eiiected, depending upon the particle size range of the powder used, at temperatures below 600C. If the powders have particle sizes below 100 microns, two or three successive compressions at increasing temperatures are of advantages, since if compression at the maximum temperature were effected immediately after cold compression, oxidation would occur or even ignition of the magnesium powder.
The compressed materials so obtained can then be subjected to plastic deformation by the standard techby heating in air.
All the powder samples were subjected, after fluorination to a compaction treatment effected in a drawing mill having a drawing die ratio, S/s, of 49, with a compressive force of 40 metric tons/mm. The four following stages were employed.
' (a) Compression in the cold;
(b) Compression at 350C.; (0) Compression at 450C.;
(d) Compression at 500C.
By way of comparison, the right-hand column of the table shows the results obtained for a material prepared by the above compaction treatment, starting with a non- ;fiuorinated composite Mg-MgO material, having a particle size range of 100-200 microns. The material obtained was taken up to 450C. by heating in air. It may be mentioned in this connection that, if a very fine Mg-MgO powder is used, having a particle size range of 10 to 65 The table shows the improvement in mechanical properties which can be obtained by using the process of the invent-ion. The rupture load, elasticity and rupture elongation values, both cold and hot, are clearly better than the corresponding values of known magnesium-base materials, such as magnesium alloys or composite materials of the Mg-MgO type.
Apart from the mechanical properties described above, the fluorinated and compacted materials of the invention are of great interest because of their remarkable resistance to corrosion in air. They can be heated to 500 C. in air saturated with water vapour Without appreciably corroding, the increase in weight being less than 1 mg./ cm. after exposure for 800 hours, whereas with ordinary magnesium-base materials a very large degradation occurs in air at 400 C. and, from 350 C., oxidation is very substantial and can have serious effects.
The ignition temperature in humid air of the novel material is 640 C. and is about 40 to 50 C. higher than that of pure magnesium and undergoes much less violent combustion.
The process of the invention thus yields a novel material which is of particular interest in use in view of the following advantages:
(a) Mechanical properties in the cold and, particularly, in the hot, which are greatly superior to those of ordinary magnesium-base materials;
(b) Possibility of obtaining very varied mechanical properties as required, by varying either or both of the particle size range and the shape of the particles of the initial powder or the combined fluorine content, particularly by varying the temperature and/or duration of the treatment and the composition of the gaseous phase used;
(c) Resistance to oxidation by air, even humid, which is greatly improved at elevated temperatures, permitting use of magnesium up to a temperature of about 500 C., whereas operation was previously limited to below about Such characteristics have never previously been obtained and make the new material particularly suitable for use as a cladding material for fuel elements in nuclear reactors operating at high temperatures.
What is claimed is:
1. A process for the preparation of an improved metall'ic material formed from the compression of a member selected from the group consisting of a magnesium powder and a magnesium alloy powder comprising the steps of subjecting particles of said powder having a size range of from 1 to 2,000 microns to a gaseous atmosphere consisting essentially of a fluorine containing gas at a temperature from 0 C. to 600 C. until a material containing 0.1 to 15% by weight of combined fluorine as a thin film of magnesium fluoride on the particles is produced and compressing said particles of powder.
2. A process according to claim 1, in which the atmosphere contains the fluorination agent and an inert gas.
3. A process according to claim 1, in which the fluorination agent is fluorine.
4. A process according to claim 1, in which the fluorination agent is hydrogen fluoride.
5. A process according to claim 1, in which the powder is first subjected to the action of the fluorination atmosphere for a time sufficient to attain the desired degree of fluorination of the metal-containing powder and is then compressed.
6. A process according to claim 1, in which heating is effected for a period of 2 to 5 hours.
7. A magnesium-base material comprising a powder, the particles of which comprise substantially magnesium,
have a size range from 1 to 2,000 microns and are covered with a thin coating of magnesium fluoride, the combined fluorine content of the coated metal particles being between 0.1 to 15% by weight.
References Cited by the Examiner OTHER REFERENCES Metals Handbook, volume 1, American Society for Metals, Metals Park, Ohio, 1961. TA 472 A3, pages 1095-1111.
LEON D. ROSDOL, Primary Examiner.
RAY K. WINDHAM, CARL D. QUARFORTH,
Examiners.
A. I. MUCCINO, R. L. GOLDBERG, R. L. GRUD- ZIECKI, Assistant Examiners.

Claims (1)

1. A PROCESS FOR THE PREPARATION OF AN IMPROVED METALLIC MATERIAL FORMED FROM THE COMPRESSION OF A MEMBER SELECTED FROM THE GROUP CONSISTING OF A MAGNESIUM POWDER AND A MAGNESIUM ALLOY POWDER COMPRISING THE STEPS OF SUBJECTING PARTICLES OF SAID POWDER HAVING A SIZE RANGE OF FROM 1 TO 2,000 MICRONS TO A GASEOUS ATMOSPHERE CONSISTING ESSENTIALLY OF A FLUORINE CONATINING GAS AT A TEMPERATURE FROM 0* C. TO 600*C. UNTIL A MATERIAL CONTAINING 0.1 TO 15% BY WEIGHT OF COMBINED FLUORINE AS A THIN FILM OF MAGNESIUM FLUORIDE ON THE PARTICLES IS PRODUCED AND COMPRESSING SAID PARTICLES OF POWDER.
US165035A 1961-03-03 1962-01-08 Process for the preparation of metallic materials by compression of a magnesium or magnesium alloy powder Expired - Lifetime US3247297A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR854486A FR1292322A (en) 1961-03-03 1961-03-03 Process for the preparation of masses based on fluorinated and compressed magnesium powder

Publications (1)

Publication Number Publication Date
US3247297A true US3247297A (en) 1966-04-19

Family

ID=8750057

Family Applications (1)

Application Number Title Priority Date Filing Date
US165035A Expired - Lifetime US3247297A (en) 1961-03-03 1962-01-08 Process for the preparation of metallic materials by compression of a magnesium or magnesium alloy powder

Country Status (9)

Country Link
US (1) US3247297A (en)
BE (1) BE612189A (en)
CH (1) CH410437A (en)
DK (1) DK110025C (en)
ES (1) ES273932A1 (en)
FR (1) FR1292322A (en)
GB (1) GB963605A (en)
LU (1) LU41034A1 (en)
SE (1) SE209881C1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4185136A (en) * 1976-08-03 1980-01-22 Eutectic Corporation Coated electrodes
US4482607A (en) * 1982-09-23 1984-11-13 Amax Inc. Method for coating magnesium granules with fluoride-containing flux
US4659373A (en) * 1983-11-09 1987-04-21 Studiengesellschaft Kohle Mbh Process for preparing finely divided highly reactive magnesium and use thereof
US4731203A (en) * 1983-11-09 1988-03-15 Studiengesellschaft Kohle Mbh Process for using finely divided highly reactive magnesium
DE102018128206A1 (en) * 2018-11-12 2020-05-14 Innovent E.V. Process for producing a magnesium fluoride layer on a magnesium alloy and components produced therewith

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2549086B1 (en) * 1983-06-21 1987-02-20 Pechiney Electro Metallurg PROCESS FOR DRY PASSIVATION OF MAGNESIUM IN DIVIDED CONDITIONS
CN114833335B (en) * 2022-04-20 2023-08-11 西安近代化学研究所 Coated magnesium powder with combustion micro-explosion effect, preparation method and application thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2288995A (en) * 1940-04-13 1942-07-07 Dow Chemical Co Surface treatment of magnesium and its alloys
US2380202A (en) * 1942-08-31 1945-07-10 Aluminum Co Of America Method of thermal treatment
US2885316A (en) * 1958-07-21 1959-05-05 Aluminum Co Of America Method for degassing aluminum articles by means of a vaporous fluoride

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2288995A (en) * 1940-04-13 1942-07-07 Dow Chemical Co Surface treatment of magnesium and its alloys
US2380202A (en) * 1942-08-31 1945-07-10 Aluminum Co Of America Method of thermal treatment
US2885316A (en) * 1958-07-21 1959-05-05 Aluminum Co Of America Method for degassing aluminum articles by means of a vaporous fluoride

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4185136A (en) * 1976-08-03 1980-01-22 Eutectic Corporation Coated electrodes
US4482607A (en) * 1982-09-23 1984-11-13 Amax Inc. Method for coating magnesium granules with fluoride-containing flux
US4659373A (en) * 1983-11-09 1987-04-21 Studiengesellschaft Kohle Mbh Process for preparing finely divided highly reactive magnesium and use thereof
US4731203A (en) * 1983-11-09 1988-03-15 Studiengesellschaft Kohle Mbh Process for using finely divided highly reactive magnesium
DE102018128206A1 (en) * 2018-11-12 2020-05-14 Innovent E.V. Process for producing a magnesium fluoride layer on a magnesium alloy and components produced therewith
DE102018128206B4 (en) 2018-11-12 2024-09-19 Innovent E.V. Process for producing a magnesium fluoride layer on a magnesium alloy and components produced thereby

Also Published As

Publication number Publication date
DK110025C (en) 1968-08-26
LU41034A1 (en) 1962-03-02
CH410437A (en) 1966-03-31
ES273932A1 (en) 1962-03-16
BE612189A (en) 1962-05-02
GB963605A (en) 1964-07-15
FR1292322A (en) 1962-05-04
SE209881C1 (en) 1966-12-20

Similar Documents

Publication Publication Date Title
US3775823A (en) Dispersion-strengthened zirconium products
US3872022A (en) Sintering uranium oxide in the reaction products of hydrogen-carbon dioxide mixtures
US3247297A (en) Process for the preparation of metallic materials by compression of a magnesium or magnesium alloy powder
KR101868185B1 (en) Uranium-and molybdenum-based alloy powder that can be used for the production of nuclear fuel and targets intended for the production of radioisotopes
US2884688A (en) Sintered ni-al-zr compositions
US3046090A (en) Production of uranium monocarbide
US3275564A (en) Process of fabrication of sintered compounds based on uranium and plutonium
US3150975A (en) Method of making intermetallic compound-composition bodies
US3216824A (en) Preparation of materials of composite structure
US3147543A (en) Dispersion hardened metal product
US3213032A (en) Process for sintering uranium nitride with a sintering aid depressant
US2952535A (en) Sintering metal oxides
US2934482A (en) Nuclear reactor fuel element and method of manufacture
US3619894A (en) Process for the production of a composite material al-mg-al2o3-mgo
US3766082A (en) Sintering of compacts of un,(u,pu)n, and pun
US3172196A (en) Sintered intermetallic compoundcomposition bodies
US3231344A (en) Sintered intermetallic bodies composed of aluminum and niobium or tantalum
US3135697A (en) Method of hydriding
US3228748A (en) Process for the preparation of a uranium compound in powder form
Chakraborty et al. Factors affecting the swelling during degassing of compacts containing uranium-aluminum intermetallics dispersed in aluminum
Vaughan et al. Experiments on the preparation of UO2− x and UO
US3145182A (en) Method for improving hydrolysis resistance of uranium carbide containing composition
US3431104A (en) Zirconium base alloy
US3168371A (en) Process for producing high density urania fuel elements
US3394000A (en) Process for obtaining al-al2o3 structures for nuclear applications