US2431691A - Method and apparatus for consolidating refractory metal powder to dense coherent form - Google Patents

Method and apparatus for consolidating refractory metal powder to dense coherent form Download PDF

Info

Publication number
US2431691A
US2431691A US526153A US52615344A US2431691A US 2431691 A US2431691 A US 2431691A US 526153 A US526153 A US 526153A US 52615344 A US52615344 A US 52615344A US 2431691 A US2431691 A US 2431691A
Authority
US
United States
Prior art keywords
powder
molybdenum
metal
consolidating
tungsten
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
US526153A
Inventor
William J Newman
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.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Priority to US526153A priority Critical patent/US2431691A/en
Application granted granted Critical
Publication of US2431691A publication Critical patent/US2431691A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F7/00Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
    • B22F7/02Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers
    • B22F7/04Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers with one or more layers not made from powder, e.g. made from solid metal
    • 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
    • C22C1/045Alloys based on refractory metals

Definitions

  • This invention relates to the consolidation of metal powder, and more particularly, to an improvement in the method of and apparatus for consolidating metal in a convenient and economical manner.
  • the principal object of my invention is an improvement in powder metallurgy, and more particularly in connection with the manufacture of refractory metals such as molybdenum and tungsten in coherent form.
  • Another object of my invention is to prevent sticking to the supporting means during the sintering operation, of refractory metal powder after having been pressed into shape.
  • a further object of my invention is to provide a support for pressed ingots of refractory metal powder, such as molybdenum and tungsten, during the sintering operation, whereby sticking and the formation of cracks during such sintering Vtreatment is obviated.
  • refractory metal powder such as molybdenum and tungsten
  • a still further object of my invention is the provision of a corrugated support of refractory metal for use during sintering to hold pressed metal powder of corresponding character for uniform treatment by the ambient atmosphere in the sintering furnace and to avoid sticking to the supporting slab or boat.
  • Fig. 1 is an axial sectional view of a furnace containing pressed ingots or slugs of refractory metal powder, during the process of sintering in accordance with my invention.
  • Fig. 2 is a fragmentary perspective approximately full size view of an ingot, a supporting corrugated metal plate, and an underlying slab or boat, without the furnace shown in Fig. 1.
  • Fig. 3 is a view corresponding to Fig. l, but showing only the supporting slab or boat, the corrugated underlying supporting strip, and the employment of such a strip on top of the lower ingot in order to allow for double or multiple decking of such ingots.
  • I thereby provide for the manufacture of metal of uniform strength and density, avoid the local welding or fusion 0f the ingot to the support, and at the same time make it possible to double or multiple deck the ingots.
  • refractory metal such as molybdenum and tungsten are desirably manufactured in dense coherent form by pressing in molds and then either sintering to final density or firing at a temperature not high enough to cause actual sintering to the finished condition then forming to shape, as by machining, andafterwards sintering to final density, the sintering temperature being about 1600* C., if molybdenum is the metal. It is the final sintering of such material that I am particularly concerned with and especially when said material is molybdenum, although the same principle applies to other similar materials such as tungsten.
  • a furnace a middle or intermediate hot zone any suitable heating means, such as resistance wire I3 around a heating tube I4 and the whole enclosed in suitable insulating means such as alumina or magnesia I5 held in an outer casing Z0.
  • suitable heating means such as resistance wire I3 around a heating tube I4 and the whole enclosed in suitable insulating means such as alumina or magnesia I5 held in an outer casing Z0.
  • a relatively cold tunnel (not shown) the length of which is suii'icient for effecting the desired cooling of the treated material and may be shortened by surrounding, at least a part thereof, with a water cooling jacket (not shown).
  • the furnace is provided with a pusher element I6 as well as means for introducing and exhaust- Ycorrugated preferably resilient strip I8 of molybdenum, if the ingotsbeing treated in said furnace are molybdenum as is assumed in the embodiment illustrated.
  • a similar strip formed of tungsten may be used for supporting molybdenum or tungsten ingots.
  • the upper portions of the corrugations of which are desirably coated with a lm of refractory inert finely-divided or cation.
  • the powder is to avoid the possibility of sticking during the sintering operation. It may be sprinkled on dry or made into an aqueciably restricted by said powder. derstood that although I have shown an elongated ingot rectangular previously referred to, especially noticed in treating long heavy ingots, ⁇ are avoided by using my invention.
  • the corrugations 1n the supporting'strip are desirably tributes the weight of the ingot, asby necessary flexure or partial attening, so that substantially Vequal portions of the weight are supported along the VcrestV of each corrugation 2
  • the supporting corrugated strip I8 may also be considered as an anti-friction device under the ingot, allowing free sliding of the same therealong during the shrinking operation, thereby not only avoiding any severe pressure and consequent welding or sticking but allowing for slight changes in the lines of support as the ingot tendencies during sintering treatments.
  • a supporting slabV Ila which may correspond with the slab 'Il of the preceding embodiment shown, said slab being used in a furnace as in said preceding embodiment.
  • a corrugated strip of molybdenum or the like I8 corre- AA satisfactory used in sintering 11/ width and 1" embodiment of the apparatus slugs of molybdenum 24" long, thick, is a plate of molybdenum and width with that of the base of the slug to be treated, in this case about 24" long and 11/2 wide, and with eorrugations Tg deep or somewhat more, spaced a distance of s or somewhat
  • I have provided an improvement in connection with the manufacture of refractory metal, and particularly molybdenum, whereby the tendency to stick during the final sintering operation.
  • the method of consolidating molybdenum powder to dense coherent form comprising pressing said powder to a shape about 24;" long, 11/2l Wide, and 1Y thick, placing said pressed shape on a transversely corrugated resilient plate of molybdenum, and heating for a relatively long period of time said pressed shape in a hydrogenbearing reducing atmosphere, saturated between about 20 C. and 40 C. with water vapor, to a temperature, not higher than about '70% of that of fusion as measured in degrees C., at which a reversible reaction between such materials occurs.
  • the method of consolidating molybdenum powder to dense coherent form comprising pressingY said powder to a shape not lighter than one about 12 long, /r" wide and 3A" thick, placing said pressed shape on a transversely corrugated resilient plate of molybdenum, and heating in a hydrogen-bearing reducing atmosphere saturated at a temperature between about 20 C. and 40 C. with water vapor to a temperature of between about 50% and 70% of that of fusion as measured in degrees C., for a relatively long period of time.
  • the method of consolidating molybdenum powder to form dense coherent metal comprising pressing said powder to an elongated Shape heavy per longitudinal inch, placing the pressed shape on a transversely corrugated resilient plate of molybdenum, and heating in an atmosphere of hydrogen saturated at about 30 C. with water vapor to a temperature of about 1600 C. for about two hours.
  • the method of consolidating a metal powder selected from the group consisting of molybdenum and tungsten to form dense coherent metal comprising pressing the selected powder to an elongated body of heavy weight per running inch, placing the body on a transversely corrugated resilient plate formed of the same metal to support it at a plurality of spaced positions from end to end and allow for circulation of the treating atmosphere thereunder, and heating said pressed body in a hydrogen-bearing reducing atmosphere containing a large enough proportion of water vapor to provide for a reversible oxidation-reduction reaction, to a temperature not higher than about '70% of that of fusion as measured in degrees C. but sufliciently high to cause the reaction to occur rapidly, for a relatively long period of time until a strong coherent article is produced.
  • the method of consolidating a metal powder selected from the group consisting oi molybdenum and tungsten to form dense coherent metal comprising pressing the selected powder to an elongated shape heavy per longitudinal inch, placing the pressed shape on a transversely corrugated resilient plate of the same metal, and heating said pressed shape in a hydrogen-bearing reducing atmosphere perature not higher than 40 C. but high enough to provide for a reversible oxidation-reduction reaction, with water vapor, to a temperature not higher than about 70% of that of fusion as measured in degrees C., for a relatively long period of time until a strong coherent article is produced.
  • the method of consolidating a metal powder selected from the group consisting of molybdenum and tungsten to form dense coherent metal comprising pressing the selected powder to an elongated shape at least as large as l2 X 3A" X 3/4", placing the pressed shape on a transversely corrugated resilient plate of the same metal, and heating said pressed shape in a hydrogen-bearing reducing atmosphere containing water vapor, to a temperature between about 50% and r70% of that of fusion as measured saturated, at a temin degrees C.. for a relatively long period of time.
  • the method of consolidating a metal powder selected from the group consisting of molybdenum and tungsten to form dense coherent metal comprising pressing the selected powder to an elongated shape at least as large as 12" X 3A" X 3/21, placing the pressed shape on a transversely corrugated resilient plate of the same metal, and heating said pressed shape in a hydrogen-bearing reducing atmosphere saturated at a temperature between about 20 C. and 40 C. with water vapor, to a temperature between about 50% and 70% of that of fusion as measured in degrees C., :for a relatively long period of time.
  • the method of consolidating molybdenum powder to dense coherent form comprising pressing said powder to an elongated shape at least as heavy as one about 12 X 3A X 3A", placing said pressed shape on a transversely corrugated resilient plate of metal selected from the group consisting of molybdenum and tungsten, land heating said pressed shape in a hydrogen-bearing reducing atmosphere saturated at a temperature between about 20 C. and 40 C. with water vapor, to a temperature between about 50% and 70% of that of fusion as measured in degrees C., for a relatively long period of time.
  • the method of consolidating tungsten powder to dense coherent form comprising pressing said powder to an elongated shape at least as heavy as one about 24" X 11/2" X 1", placing said pressed shape on a transversely corrugated resilient plate of tungsten, and heating said pressed shape in a hydrogen-bearing reducing atmosphere saturated between about 20 C. and 40 C. with water vapor, for a relatively long period of time to a temperature not higher than about 70% of that of fusion as measured in degrees C., at which a reversible reactance between such materials takes place rapidly.
  • the method of consolidating tungsten powder to dense coherent form comprising pressing said powder to a shape having a length of about 24, a width of about 11/2", and a thickness of about 1", placing said pressed shape on a transversely corrugated resilient plate of tungsten, and heating in a hydrogen-bearing reducing atmosphere saturated at a temperature between about 20 C. and 40 C. with water vapor to a temperature of between about 50% and '70% of that of fusion as measured in degrees C., for a relatively long period of time.
  • the method of consolidating tungsten powder to form dense coherent metal comprising pressing said powder to an elongated shape of heavy weight per running inch, placing the pressed shape on a transversely corrugated resilient plate of tungsten, and heating in an atmosphere of hydrogen saturated between about 20 C. and 40 C. with water vapor, to a temperature between about 1600 C. and 2000 C. for a relatively long period of time.
  • the method of consolidating a metal powder selected from the group consisting of molybdenum and tungsten to form dense coherent metal comprising pressing the selected powder to consolidate it into an elongated ingot heavy per longitudinal inch, placing said ingot on a transversely corrugated resilient plate of the same metal, placing a similar resilient plate of metal on top of said ingot, forming another ingot in the same manner, placing said second ingot on top of the ingot-supported resilient plate of metal, and heating said ingots in a hydrogenybearing reducing atmosphere saturated at a temperature between about 20 C. and 40 C. with water vapor to a temperature between about 50% and 70% of that of fusion as measured in degrees C. for a relatively long period of time.
  • the method of consolidating a metal powder selected from the group consistingof molybdenum and tungsten to form dense coherent metal comprising pressing the selected powder to an elongated shape heavy per longitudinal inch, applying a lm of inert refractory powder y50% and 70% of that of fusion as measured in degrees C. for a relatively long period of time.
  • apparatus for consolidating to dense coherent form -a refractory metal powder selected from the group consisting of molybdenum and tungsten comprising a furnace with heating means, a tube of refractory material adapted to stand a desired high temperature obtained by Iactivation of said heating means, insulating means around said tube and heating means,
  • the tube maybe raised in temperature sufficiently to heat enclosed selected metal pow'- der to a sintering. temperature, and means for introducing a hydrogen-bearing reducing atmos- Vphere into said tube, the combination therewith of a transversely corrugated resilient plate of the metal selected for consolidation disposed in said tube, in order to support an elongated pressed shape, heavy per longitudinal inch, of the selected metal powder, at a plurality of uniformly-spaced positions along its length, to prevent sticking and crack formation, and allow for uniform sintering and treatment of said shape in the hydrogen-bearing atmosphere.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Powder Metallurgy (AREA)

Description

Dec. 2, 1947. w. J. NEWMAN 2,431,691
METHOD AND APPARATUS Fon coNsomDATING REFRAcToRY METAL POWDER To DENsE coHERENT FORM Filed March 13, 1944 +NvENToR WJ: /VEWMy/Vy BY ,umm
ATTORNEY Patented Dec. 2, 1947 UNITED STATES METHOD AND APPAR DATING REFRACTORY COHERENT FORM Application March 13, 1944, Seri 14 Claims.
TO DENSE William J. Newman,
to Westinghouse This invention relates to the consolidation of metal powder, and more particularly, to an improvement in the method of and apparatus for consolidating metal in a convenient and economical manner.
The principal object of my invention, generally considered, is an improvement in powder metallurgy, and more particularly in connection with the manufacture of refractory metals such as molybdenum and tungsten in coherent form.
Another object of my invention is to prevent sticking to the supporting means during the sintering operation, of refractory metal powder after having been pressed into shape.
A further object of my invention is to provide a support for pressed ingots of refractory metal powder, such as molybdenum and tungsten, during the sintering operation, whereby sticking and the formation of cracks during such sintering Vtreatment is obviated.
A still further object of my invention is the provision of a corrugated support of refractory metal for use during sintering to hold pressed metal powder of corresponding character for uniform treatment by the ambient atmosphere in the sintering furnace and to avoid sticking to the supporting slab or boat.
Other objects and advantages of the invention will become apparent as the description proceeds.
Referring to the scale drawing:
Fig. 1 is an axial sectional view of a furnace containing pressed ingots or slugs of refractory metal powder, during the process of sintering in accordance with my invention.
Fig. 2 is a fragmentary perspective approximately full size view of an ingot, a supporting corrugated metal plate, and an underlying slab or boat, without the furnace shown in Fig. 1.
Fig. 3 is a view corresponding to Fig. l, but showing only the supporting slab or boat, the corrugated underlying supporting strip, and the employment of such a strip on top of the lower ingot in order to allow for double or multiple decking of such ingots.
In the final heat treatment of refractory metal bars, and particularly molybdenum in a moist hydrogen-bearing reducing atmosphere, or one preferably saturated at between about 20 C. and 40 C. with water vapor, at approximately 1600 C., or between about 50% and '70% of its temperature of melting as measured in degrees C., described and claimed as a reversible reaction treatment in the Hall et al. application Serial No. 943, and the Hall et al. 1,392, filed November 23,
486,812, filed May 13, 1
application, Serial No. 51
ATUS FOR CONSOLI- METAL POWDER rporation of Pennsylvania al No. 526,153
(Cl. i5-22) 1943, both cases now replaced by the I-Iall et al. continuation-in-part application, Ser. No. 579,080, filed February 21, 1945, it is found desirable to use relatively long ingots, for example those of the order of 20" to 30" in length, cr such lengths as can be conveniently pressed in molds available. If, then, these ingots are large in cross section, the weight per running inch is high and where slabs or boats of refractory metal, such as tungsten or molybdenum, are used to carry these through a horizontal furnace, the pressed ingot, especially on acco of being rough, has a tendency to weld onto the slab or boat, such welding resulting from the same reaction and at the same temperature that brings about the sintering of the bar.
As this occurs before the shrinkage of the bar is ended, such shrinkage being of the order of 15% to 17%, there is a tendency of the bar to pull apart, developing transverse cracks at intervals.
I propose to avoid the foregoing difficulty by using directly under the bar of molybdenum or tungsten a preferably transversely corrugated, desirably resilient strip of thin molybdenum, tungsten, or other similar refractory metal, thereby not only supporting the latter at a plurality of closely-spaced positions along its length, and because of the resiliency of the strip avoiding concentration or substantial variation of pressure at the support positions, but at the same time holding the ingot above the iioor of the furnace and allowing for free circulation of the ambient treating atmosphere, such as wet hydrogen, around the ingot. I thereby provide for the manufacture of metal of uniform strength and density, avoid the local welding or fusion 0f the ingot to the support, and at the same time make it possible to double or multiple deck the ingots.
In accordance with the Hall et al. applications, 40 previously referred to, refractory metal such as molybdenum and tungsten are desirably manufactured in dense coherent form by pressing in molds and then either sintering to final density or firing at a temperature not high enough to cause actual sintering to the finished condition then forming to shape, as by machining, andafterwards sintering to final density, the sintering temperature being about 1600* C., if molybdenum is the metal. It is the final sintering of such material that I am particularly concerned with and especially when said material is molybdenum, although the same principle applies to other similar materials such as tungsten.
Referring to the drawing in detail, and first 55 considering the embodiment of my invention illustrated in Figs. 1 and 2, there is shown a furnace a middle or intermediate hot zone any suitable heating means, such as resistance wire I3 around a heating tube I4 and the whole enclosed in suitable insulating means such as alumina or magnesia I5 held in an outer casing Z0. At the front end (not shown) there is a relatively cool vestibule portion. At the rear or exit end there is a relatively cold tunnel (not shown) the length of which is suii'icient for effecting the desired cooling of the treated material and may be shortened by surrounding, at least a part thereof, with a water cooling jacket (not shown).
The furnace is provided with a pusher element I6 as well as means for introducing and exhaust- Ycorrugated preferably resilient strip I8 of molybdenum, if the ingotsbeing treated in said furnace are molybdenum as is assumed in the embodiment illustrated. A similar strip formed of tungsten may be used for supporting molybdenum or tungsten ingots. Y
On the corrugated strip I 8, the upper portions of the corrugations of which are desirably coated with a lm of refractory inert finely-divided or cation. The powder is to avoid the possibility of sticking during the sintering operation. It may be sprinkled on dry or made into an aqueciably restricted by said powder. derstood that although I have shown an elongated ingot rectangular previously referred to, especially noticed in treating long heavy ingots,` are avoided by using my invention.
It will, however, be understood that the corrugations 1n the supporting'strip are desirably tributes the weight of the ingot, asby necessary flexure or partial attening, so that substantially Vequal portions of the weight are supported along the VcrestV of each corrugation 2|, rather than having concentrated points of pressure.
It will be seen that by virtue of the transverse corrugations, free lcirculation of the wet hydrogen or other treating atmosphere under the ingot,
' 22, is permitted, thereoccurs during the sintering operation.
The supporting corrugated strip I8 may also be considered as an anti-friction device under the ingot, allowing free sliding of the same therealong during the shrinking operation, thereby not only avoiding any severe pressure and consequent welding or sticking but allowing for slight changes in the lines of support as the ingot tendencies during sintering treatments.
Referring now to the embodiment of my in- Vention illustrated in Fig. 3, there is shown a supporting slabV Ila, which may correspond with the slab 'Il of the preceding embodiment shown, said slab being used in a furnace as in said preceding embodiment. On the slab I'la is a corrugated strip of molybdenum or the like I8, corre- AA satisfactory used in sintering 11/ width and 1" embodiment of the apparatus slugs of molybdenum 24" long, thick, is a plate of molybdenum and width with that of the base of the slug to be treated, in this case about 24" long and 11/2 wide, and with eorrugations Tg deep or somewhat more, spaced a distance of s or somewhat Of course it will be under- From the foregoing it will be seen that I have provided an improvement in connection with the manufacture of refractory metal, and particularly molybdenum, whereby the tendency to stick during the final sintering operation.
Although preferred embodiments of my inand scope of the appended claims.
I claim:
1. The method of consolidating molybdenum powder to dense coherent form, comprising pressing said powder to a shape about 24;" long, 11/2l Wide, and 1Y thick, placing said pressed shape on a transversely corrugated resilient plate of molybdenum, and heating for a relatively long period of time said pressed shape in a hydrogenbearing reducing atmosphere, saturated between about 20 C. and 40 C. with water vapor, to a temperature, not higher than about '70% of that of fusion as measured in degrees C., at which a reversible reaction between such materials occurs.
2. The method of consolidating molybdenum powder to dense coherent form, comprising pressingY said powder to a shape not lighter than one about 12 long, /r" wide and 3A" thick, placing said pressed shape on a transversely corrugated resilient plate of molybdenum, and heating in a hydrogen-bearing reducing atmosphere saturated at a temperature between about 20 C. and 40 C. with water vapor to a temperature of between about 50% and 70% of that of fusion as measured in degrees C., for a relatively long period of time.
3. The method of consolidating molybdenum powder to form dense coherent metal, comprising pressing said powder to an elongated Shape heavy per longitudinal inch, placing the pressed shape on a transversely corrugated resilient plate of molybdenum, and heating in an atmosphere of hydrogen saturated at about 30 C. with water vapor to a temperature of about 1600 C. for about two hours.
4. The method of consolidating a metal powder selected from the group consisting of molybdenum and tungsten to form dense coherent metal, comprising pressing the selected powder to an elongated body of heavy weight per running inch, placing the body on a transversely corrugated resilient plate formed of the same metal to support it at a plurality of spaced positions from end to end and allow for circulation of the treating atmosphere thereunder, and heating said pressed body in a hydrogen-bearing reducing atmosphere containing a large enough proportion of water vapor to provide for a reversible oxidation-reduction reaction, to a temperature not higher than about '70% of that of fusion as measured in degrees C. but sufliciently high to cause the reaction to occur rapidly, for a relatively long period of time until a strong coherent article is produced.
5. The method of consolidating a metal powder selected from the group consisting oi molybdenum and tungsten to form dense coherent metal, comprising pressing the selected powder to an elongated shape heavy per longitudinal inch, placing the pressed shape on a transversely corrugated resilient plate of the same metal, and heating said pressed shape in a hydrogen-bearing reducing atmosphere perature not higher than 40 C. but high enough to provide for a reversible oxidation-reduction reaction, with water vapor, to a temperature not higher than about 70% of that of fusion as measured in degrees C., for a relatively long period of time until a strong coherent article is produced.
6. The method of consolidating a metal powder selected from the group consisting of molybdenum and tungsten to form dense coherent metal, comprising pressing the selected powder to an elongated shape at least as large as l2 X 3A" X 3/4", placing the pressed shape on a transversely corrugated resilient plate of the same metal, and heating said pressed shape in a hydrogen-bearing reducing atmosphere containing water vapor, to a temperature between about 50% and r70% of that of fusion as measured saturated, at a temin degrees C.. for a relatively long period of time.
7. The method of consolidating a metal powder selected from the group consisting of molybdenum and tungsten to form dense coherent metal, comprising pressing the selected powder to an elongated shape at least as large as 12" X 3A" X 3/21, placing the pressed shape on a transversely corrugated resilient plate of the same metal, and heating said pressed shape in a hydrogen-bearing reducing atmosphere saturated at a temperature between about 20 C. and 40 C. with water vapor, to a temperature between about 50% and 70% of that of fusion as measured in degrees C., :for a relatively long period of time.
8. The method of consolidating molybdenum powder to dense coherent form, comprising pressing said powder to an elongated shape at least as heavy as one about 12 X 3A X 3A", placing said pressed shape on a transversely corrugated resilient plate of metal selected from the group consisting of molybdenum and tungsten, land heating said pressed shape in a hydrogen-bearing reducing atmosphere saturated at a temperature between about 20 C. and 40 C. with water vapor, to a temperature between about 50% and 70% of that of fusion as measured in degrees C., for a relatively long period of time.
9. The method of consolidating tungsten powder to dense coherent form, comprising pressing said powder to an elongated shape at least as heavy as one about 24" X 11/2" X 1", placing said pressed shape on a transversely corrugated resilient plate of tungsten, and heating said pressed shape in a hydrogen-bearing reducing atmosphere saturated between about 20 C. and 40 C. with water vapor, for a relatively long period of time to a temperature not higher than about 70% of that of fusion as measured in degrees C., at which a reversible reactance between such materials takes place rapidly.
10. The method of consolidating tungsten powder to dense coherent form, comprising pressing said powder to a shape having a length of about 24, a width of about 11/2", and a thickness of about 1", placing said pressed shape on a transversely corrugated resilient plate of tungsten, and heating in a hydrogen-bearing reducing atmosphere saturated at a temperature between about 20 C. and 40 C. with water vapor to a temperature of between about 50% and '70% of that of fusion as measured in degrees C., for a relatively long period of time.
11. The method of consolidating tungsten powder to form dense coherent metal comprising pressing said powder to an elongated shape of heavy weight per running inch, placing the pressed shape on a transversely corrugated resilient plate of tungsten, and heating in an atmosphere of hydrogen saturated between about 20 C. and 40 C. with water vapor, to a temperature between about 1600 C. and 2000 C. for a relatively long period of time.
12. The method of consolidating a metal powder selected from the group consisting of molybdenum and tungsten to form dense coherent metal, comprising pressing the selected powder to consolidate it into an elongated ingot heavy per longitudinal inch, placing said ingot on a transversely corrugated resilient plate of the same metal, placing a similar resilient plate of metal on top of said ingot, forming another ingot in the same manner, placing said second ingot on top of the ingot-supported resilient plate of metal, and heating said ingots in a hydrogenybearing reducing atmosphere saturated at a temperature between about 20 C. and 40 C. with water vapor to a temperature between about 50% and 70% of that of fusion as measured in degrees C. for a relatively long period of time.
13. The method of consolidating a metal powder selected from the group consistingof molybdenum and tungsten to form dense coherent metal, comprising pressing the selected powder to an elongated shape heavy per longitudinal inch, applying a lm of inert refractory powder y50% and 70% of that of fusion as measured in degrees C. for a relatively long period of time.
14. In apparatus for consolidating to dense coherent form -a refractory metal powder selected from the group consisting of molybdenum and tungsten, comprising a furnace with heating means, a tube of refractory material adapted to stand a desired high temperature obtained by Iactivation of said heating means, insulating means around said tube and heating means,
whereby the tube maybe raised in temperature sufficiently to heat enclosed selected metal pow'- der to a sintering. temperature, and means for introducing a hydrogen-bearing reducing atmos- Vphere into said tube, the combination therewith of a transversely corrugated resilient plate of the metal selected for consolidation disposed in said tube, in order to support an elongated pressed shape, heavy per longitudinal inch, of the selected metal powder, at a plurality of uniformly-spaced positions along its length, to prevent sticking and crack formation, and allow for uniform sintering and treatment of said shape in the hydrogen-bearing atmosphere.
- WILLIAM J. NEWMAN.
REFERENCES CITED- `The following references are of record in the ile of this patent:
` UNITED STATES PATENTS Oct.. 27, v1942
US526153A 1944-03-13 1944-03-13 Method and apparatus for consolidating refractory metal powder to dense coherent form Expired - Lifetime US2431691A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US526153A US2431691A (en) 1944-03-13 1944-03-13 Method and apparatus for consolidating refractory metal powder to dense coherent form

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US526153A US2431691A (en) 1944-03-13 1944-03-13 Method and apparatus for consolidating refractory metal powder to dense coherent form

Publications (1)

Publication Number Publication Date
US2431691A true US2431691A (en) 1947-12-02

Family

ID=24096134

Family Applications (1)

Application Number Title Priority Date Filing Date
US526153A Expired - Lifetime US2431691A (en) 1944-03-13 1944-03-13 Method and apparatus for consolidating refractory metal powder to dense coherent form

Country Status (1)

Country Link
US (1) US2431691A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2886433A (en) * 1951-01-04 1959-05-12 Blainey Alan Production of sheet from particulate material
US3454396A (en) * 1964-07-09 1969-07-08 Minnesota Mining & Mfg Fuel elements
JPS51108966A (en) * 1975-03-19 1976-09-27 Yoshiaki Sakai Karaaringu paama
JPS53118231A (en) * 1977-03-25 1978-10-16 Fujitsu Ltd Sintered tray for use in producing sintered al-cu alloy
JPS54103708A (en) * 1978-02-02 1979-08-15 Toshiba Corp Method of sintering molybdenum
JPS54103707A (en) * 1978-02-02 1979-08-15 Toshiba Corp Method of sintering molybdenum
EP0326861A1 (en) * 1988-01-30 1989-08-09 H.C. Starck GmbH & Co. KG Composite agglomerated metal powder, process for manufacturing it an its use

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US534207A (en) * 1895-02-12 Manufacture of carbon filaments
US1536438A (en) * 1923-08-15 1925-05-05 Koehnline Irvin John Annealing box
US1731255A (en) * 1929-10-15 Alloy and its manufacture
US1768719A (en) * 1927-10-12 1930-07-01 American Brake Shoe & Foundry Annealing pot
US1808314A (en) * 1929-05-24 1931-06-02 Otis Steel Company Annealing box
US2300048A (en) * 1940-03-27 1942-10-27 Gen Motors Corp Method of making porous material

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US534207A (en) * 1895-02-12 Manufacture of carbon filaments
US1731255A (en) * 1929-10-15 Alloy and its manufacture
US1536438A (en) * 1923-08-15 1925-05-05 Koehnline Irvin John Annealing box
US1768719A (en) * 1927-10-12 1930-07-01 American Brake Shoe & Foundry Annealing pot
US1808314A (en) * 1929-05-24 1931-06-02 Otis Steel Company Annealing box
US2300048A (en) * 1940-03-27 1942-10-27 Gen Motors Corp Method of making porous material

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2886433A (en) * 1951-01-04 1959-05-12 Blainey Alan Production of sheet from particulate material
US3454396A (en) * 1964-07-09 1969-07-08 Minnesota Mining & Mfg Fuel elements
JPS51108966A (en) * 1975-03-19 1976-09-27 Yoshiaki Sakai Karaaringu paama
JPS53118231A (en) * 1977-03-25 1978-10-16 Fujitsu Ltd Sintered tray for use in producing sintered al-cu alloy
JPS5758402B2 (en) * 1977-03-25 1982-12-09 Fujitsu Ltd
JPS54103708A (en) * 1978-02-02 1979-08-15 Toshiba Corp Method of sintering molybdenum
JPS54103707A (en) * 1978-02-02 1979-08-15 Toshiba Corp Method of sintering molybdenum
JPS5613762B2 (en) * 1978-02-02 1981-03-31
JPS578162B2 (en) * 1978-02-02 1982-02-15
EP0326861A1 (en) * 1988-01-30 1989-08-09 H.C. Starck GmbH & Co. KG Composite agglomerated metal powder, process for manufacturing it an its use
US4915733A (en) * 1988-01-30 1990-04-10 Hermann C. Starck Berlin Gmbh & Co. Kg Agglomerated metal composite powders

Similar Documents

Publication Publication Date Title
US2431691A (en) Method and apparatus for consolidating refractory metal powder to dense coherent form
US2735170A (en) Method-of producing a multilayer strep
US3193888A (en) Continuous casting apparatus including endless steel belt with red iron oxide coating
US2267342A (en) Method of making composite strip
US2128943A (en) Formation of encased structures by direct casting
US2128942A (en) Direct casting apparatus
US3816572A (en) Ceramic articles
US4915158A (en) Belt composition for improving performance and flatness of thin revolving endless flexible casting belts in continuous metal casting machines
US2433903A (en) Method of making clad metal bodies
US4211271A (en) Continuous casting mold geometry improvement
US3519062A (en) Apparatus for producing strip metal by continuous casting
US3234052A (en) Beryllium sheet and method of producing same
US7059384B2 (en) Apparatus and method for metal strip casting
US2686118A (en) Method of making metal products directly from ores
US2323666A (en) Method of making composite metal slabs
US3549410A (en) Process of rebuilding steel structures
US3083407A (en) Powder cladding
US2056673A (en) Method of and apparatus for making composite ingots
US2772454A (en) Apparatus for casting
SU867568A1 (en) Method of producing bimetallic tubes
US2840685A (en) Method of electrowelding and products made thereby
US905558A (en) Process of and apparatus for making compound metal objects.
DE1127033B (en) Lining for water-cooled shaft ovens
JPS59209460A (en) Casting device and method in low-density atmosphere
JPS60149717A (en) Manufacture of hot extruded material using cast billet as blank