US3894867A - Incendiary alloys existing as a dispersion of incendiary particles in a non-incendiary atmospheric attack-resistant matrix - Google Patents

Incendiary alloys existing as a dispersion of incendiary particles in a non-incendiary atmospheric attack-resistant matrix Download PDF

Info

Publication number
US3894867A
US3894867A US431830A US43183074A US3894867A US 3894867 A US3894867 A US 3894867A US 431830 A US431830 A US 431830A US 43183074 A US43183074 A US 43183074A US 3894867 A US3894867 A US 3894867A
Authority
US
United States
Prior art keywords
incendiary
dispersion
particles
matrix
mischmetal
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
US431830A
Inventor
Steven G Fishman
C Robert Crowe
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.)
US Department of Navy
Original Assignee
US Department of Navy
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 US Department of Navy filed Critical US Department of Navy
Priority to US431830A priority Critical patent/US3894867A/en
Application granted granted Critical
Publication of US3894867A publication Critical patent/US3894867A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C28/00Alloys based on a metal not provided for in groups C22C5/00 - C22C27/00
    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06CDETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
    • C06C15/00Pyrophoric compositions; Flints
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C11/00Alloys based on lead
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C13/00Alloys based on tin
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C18/00Alloys based on zinc
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C20/00Alloys based on cadmium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper

Definitions

  • ABSTRACT A class of alloys comprising a dispersion of pyrophoric particles in a non-incendiary, atmospheric-attackresistant matrix.
  • the pyrophoric particles are one of the rare earth metals or a mixture of these such as Mischmetal and the matrix material is one of the more common metallic elements having good corrosion resistance properties.
  • the dispersion of the pyrophoric particles in the matrix may be accomplished either by solidification from the melt or precipitation and growth from solid solution.
  • Mischmetal which has excellent incendiary properties, has been proposed and used in the past as an incendiary material for projectile liners; but in unalloyed form possesses certain drawbacks.
  • the principle disadvantage of unalloyed Mischmetal is that it is susceptible to relatively rapid corrosion or oxidation when exposed to the atmosphere. Unalloyed Mischmetal also possesses relatively little mechanical strength and is somewhat brittle which poses problems in manufacture and handling.
  • alloys comprising a dispersion of pyrophoric particles in a non-incendiary, atmospheric-attack-resistant matrix make excellent incendiary materials. This dispersion is accomplished by solidification from the melt, or precipitation and growth from the solid solution which yields a finer dispersion.
  • the amount of pyrophoric phase present can be altered by selecting the desired composition from within the ranges given below:
  • alloys possess good mechanical strength, are substantially free from corrosion problems and are characterized by spontaneous ignition upon explosive or impact fragmentation.
  • the alloys of the present invention may be prepared by melting in' a proper crucible the appropriate percentages of the selected materials under vacuum'or in' an inert atmosphere to a tem- I perature above the liquidus temperature for the materials involved. The melt is then agitated to insure homogeneity. The melt is allowed to slowly cool through the 2-phase region (liquid-solid) if the pyrophoric particles are to be grown from the melt. The melt is quickly solidified and held for several hours at a temperature just below the solidus temperature if precipitation of the pyrophoric particles from the solid phase is desired. The precipitation technique will generally yield finer dispersions if this should be desired. The rate of cooling and hold times can be varied to vary particle size, distribution, etc. Of course, varying the composition will affect the volume of the pyrophoric particles present.
  • EXAMPLE 1 wt. percent Aluminum, balance Mischmetal was melted in a Quartz crucible in vacuuo at about 800C and agitated to insure homogeneity. The melt was then slow cooled (approximately 100C per hour) to a temperature of approximately 680C, within the two-phase region, and then removed from the furnace and air quenched. A portion of the solidified melt was then machined into a /2-inch cube and explosively projected against a witness structure which was essentially a hollow metal cube approximately one foot on a side. Impact of the cube with a side of the cube caused the cube to disintegrate and rapidly expose large fresh surface areas of the Mischmetal to atmosphere. The spontaneous ignition of the Mischmetal generated a gas pressure of 70 psi within the cube, as measured by a Bikini gage, demonstrated that the particular alloy was indeed an incendiary.
  • Example 2 The procedure of Example 1 was repeated using wt. percent Lead, balance Mischmetal. The melt was heated to about 1 C, agitated, and then slow cooled to a temperature of approximately 350C, within the two-phase region. The melt was then removed from the furnace and air quenched. Microscopic examination of the melt revealed a fine dispersion of Mischmetal crystals distributed throughout a Lead matrix and thus another alloy which possesses incendiary properties upon fragmentation.
  • EXAMPLE 3 A mixture of 50 wt. percent Iron, balance Mischmetal was melted in an arc melting furnace and then removed and air quenched. The melt was reheated to approximately 600C to cause precipitation of Mischmetal particles from the solid phase. Microscopic examination of the melt revealed a very fine dispersion of Mischmetal crystals distributed evenly in an Iron matrix and thus was still another alloy which upon rapid fragmentation would spontaneously ignite.
  • An incendiary alloy consisting essentially of a dispersion of pyrophoric particles in a non-incendiary ma trix wherein the matrix material is selected from the group consisting of:

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)

Abstract

A class of alloys comprising a dispersion of pyrophoric particles in a non-incendiary, atmospheric-attack-resistant matrix. The pyrophoric particles are one of the rare earth metals or a mixture of these such as Mischmetal and the matrix material is one of the more common metallic elements having good corrosion resistance properties. The dispersion of the pyrophoric particles in the matrix may be accomplished either by solidification from the melt or precipitation and growth from solid solution.

Description

United States Patent Fishman et al.
INCENDIARY ALLOYS EXISTING AS A DISPERSION OF INCENDIARY PARTICLES IN A NON-INCENDIARY ATMOSPHERIC ATTACK-RESISTANT MATRIX Inventors: Steven G. Fishman, F redericksburg, Va.; C. Robert Crowe, La Plata, Md.
Assignee: The United States of Anierica as represented by the Secretary of the Navy, Washington, DC.
Filed: Jan. 9, 1974 Appl. N0.: 431,830
US. Cl. 75/134 N; 75/122; 75/123 E; 75/134 M; 75/134 S; 75/138; 75/152;
75/153; 75/166 R; 75/168 .1; 75/170; 75/175 R; 75/178 R Int. C1. ..C22C 9/00;C22C 11/00;C22C 13/00; C22C 18/00; C22C 19/00; C22C 21/00;
C22C 22/00; C22C 28/00 Field of Search 149/17, 134 N; 75/152, 75/153, 168 J, 134 M, 170, 166 R, 175 R,
178 R,138, 122,134 S, 123 E, .5 R
[56] References Cited UNITED STATES PATENTS 2,389,198 11/1945 Kent 75/152 3,203,790 8/1965 Bungardt 75/152 3,236,633 2/1966 Bungardt 75/152 X 3,539,334 11/1970 Goeddel 75/152 3,653,995 Sclleck 75/.5 R
Primary Examiner'L. Dewayne Rutledge Assistant ExaminerArthur J. Steiner [57] ABSTRACT A class of alloys comprising a dispersion of pyrophoric particles in a non-incendiary, atmospheric-attackresistant matrix. The pyrophoric particles are one of the rare earth metals or a mixture of these such as Mischmetal and the matrix material is one of the more common metallic elements having good corrosion resistance properties. The dispersion of the pyrophoric particles in the matrix may be accomplished either by solidification from the melt or precipitation and growth from solid solution.
2 Claims, N0 Drawings INCENDIARY ALLOYS EXISTING AS A DISPERSION OF INCENDIARY PARTICLES IN A NON-INCENDIARY ATMOSPHERIC ATTACK-RESISTANT MATRIX BACKGROUND OF THE INVENTION This invention relates to incendiary alloys and more particularly to incendiary alloys having good corrosion resistance and adequate mechanical strength.
Mischmetal, which has excellent incendiary properties, has been proposed and used in the past as an incendiary material for projectile liners; but in unalloyed form possesses certain drawbacks. The principle disadvantage of unalloyed Mischmetal is that it is susceptible to relatively rapid corrosion or oxidation when exposed to the atmosphere. Unalloyed Mischmetal also possesses relatively little mechanical strength and is somewhat brittle which poses problems in manufacture and handling.
Various techniques have been utilized in an attempt to overcome the aforementioned drawbacks. Coatings have been provided on Mischmetal incendiaries in an attempt to preclude atmospheric attack and small amounts (e.g. 4 wt percent) of Aluminum have been alloyed with Mischmetal to produce intermetallics in an attempt to cope with these problems. However, these techniques have had very limited success.
SUMMARY OF THE INVENTION Applicants have discovered that alloys comprising a dispersion of pyrophoric particles in a non-incendiary, atmospheric-attack-resistant matrix make excellent incendiary materials. This dispersion is accomplished by solidification from the melt, or precipitation and growth from the solid solution which yields a finer dispersion. The amount of pyrophoric phase present can be altered by selecting the desired composition from within the ranges given below:
Matrix Pyrophoric Cu 74-99 wt.% Sn 72-88 wt.% Balance Lanthanum, Mg 75-99 wt.% Zn 82-99 wt.% Cerium, Praseodymium, Mn 50-99 wt.% Al 60-90 wt.% Neodymium, Promethium Ni 68-99 wt.% Si 47-99 wt.% or Mischmetal Pb 82-99 wt.% Fe 35-99 wt.%
These alloys possess good mechanical strength, are substantially free from corrosion problems and are characterized by spontaneous ignition upon explosive or impact fragmentation.
OBJECTS OF THE INVENTION 2 DESCRIPTION OF THE PREFERRED.-
EMBODIMENTS The alloys of the present invention,'as set forth in the summary, may be prepared by melting in' a proper crucible the appropriate percentages of the selected materials under vacuum'or in' an inert atmosphere to a tem- I perature above the liquidus temperature for the materials involved. The melt is then agitated to insure homogeneity. The melt is allowed to slowly cool through the 2-phase region (liquid-solid) if the pyrophoric particles are to be grown from the melt. The melt is quickly solidified and held for several hours at a temperature just below the solidus temperature if precipitation of the pyrophoric particles from the solid phase is desired. The precipitation technique will generally yield finer dispersions if this should be desired. The rate of cooling and hold times can be varied to vary particle size, distribution, etc. Of course, varying the composition will affect the volume of the pyrophoric particles present.
The following examples are illustrative of the invention:
EXAMPLE 1 wt. percent Aluminum, balance Mischmetal was melted in a Quartz crucible in vacuuo at about 800C and agitated to insure homogeneity. The melt was then slow cooled (approximately 100C per hour) to a temperature of approximately 680C, within the two-phase region, and then removed from the furnace and air quenched. A portion of the solidified melt was then machined into a /2-inch cube and explosively projected against a witness structure which was essentially a hollow metal cube approximately one foot on a side. Impact of the cube with a side of the cube caused the cube to disintegrate and rapidly expose large fresh surface areas of the Mischmetal to atmosphere. The spontaneous ignition of the Mischmetal generated a gas pressure of 70 psi within the cube, as measured by a Bikini gage, demonstrated that the particular alloy was indeed an incendiary.
The remainder of the solidified melt was machined into a liner for a 40mm projectile and the projectile was then detonated within an arena surrounded by a plurality of gasoline containers. Ignition of the gasoline again demonstrated the incendiary properties of the alloy since earlier tests had shown that projectile fragments alone would not ignite the gasoline.
EXAMPLE 2 The procedure of Example 1 was repeated using wt. percent Lead, balance Mischmetal. The melt was heated to about 1 C, agitated, and then slow cooled to a temperature of approximately 350C, within the two-phase region. The melt was then removed from the furnace and air quenched. Microscopic examination of the melt revealed a fine dispersion of Mischmetal crystals distributed throughout a Lead matrix and thus another alloy which possesses incendiary properties upon fragmentation.
EXAMPLE 3 A mixture of 50 wt. percent Iron, balance Mischmetal was melted in an arc melting furnace and then removed and air quenched. The melt was reheated to approximately 600C to cause precipitation of Mischmetal particles from the solid phase. Microscopic examination of the melt revealed a very fine dispersion of Mischmetal crystals distributed evenly in an Iron matrix and thus was still another alloy which upon rapid fragmentation would spontaneously ignite.
Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
What is claimed is:
1. An incendiary alloy consisting essentially of a dispersion of pyrophoric particles in a non-incendiary ma trix wherein the matrix material is selected from the group consisting of:
Sn 72-88 wt.% Zn 32-99 Wtv% Al -90 wt.% Si 47-99 wt.%

Claims (2)

1. AN INCENDIARY ALLOY CONSISTING ESSENTIALLY OF A DISPERSION OF PYROPHORIC PARTICLES IN A NON-INCENDIARY MATRIX WHEREIN THE MATRIX MATERIAL IS SELECTED FROM THE GROUP CONSISTING OF:
2. An incendiary alloy as defined in claim 1 wherein the pyrophoric material is Mischmetal.
US431830A 1974-01-09 1974-01-09 Incendiary alloys existing as a dispersion of incendiary particles in a non-incendiary atmospheric attack-resistant matrix Expired - Lifetime US3894867A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US431830A US3894867A (en) 1974-01-09 1974-01-09 Incendiary alloys existing as a dispersion of incendiary particles in a non-incendiary atmospheric attack-resistant matrix

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US431830A US3894867A (en) 1974-01-09 1974-01-09 Incendiary alloys existing as a dispersion of incendiary particles in a non-incendiary atmospheric attack-resistant matrix

Publications (1)

Publication Number Publication Date
US3894867A true US3894867A (en) 1975-07-15

Family

ID=23713622

Family Applications (1)

Application Number Title Priority Date Filing Date
US431830A Expired - Lifetime US3894867A (en) 1974-01-09 1974-01-09 Incendiary alloys existing as a dispersion of incendiary particles in a non-incendiary atmospheric attack-resistant matrix

Country Status (1)

Country Link
US (1) US3894867A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4121924A (en) * 1976-09-16 1978-10-24 The International Nickel Company, Inc. Alloy for rare earth treatment of molten metals and method
US5096507A (en) * 1989-10-12 1992-03-17 Buck Werke Gmbh & Co. Method of applying a cerium misch metal coating to the surface of a splinter-active component of an incendiary splinter projectile
US5098487A (en) * 1990-11-28 1992-03-24 Olin Corporation Copper alloys for shaped charge liners
FR2867469A1 (en) * 2004-03-15 2005-09-16 Alliant Techsystems Inc Reactive composition, useful in military and industrial explosives, comprises a metallic material defining a continuous phase and having an energetic material, which comprises oxidant and/or explosive of class 1.1
US20070272112A1 (en) * 2000-02-23 2007-11-29 Alliant Techsystems Inc. Reactive material compositions, shot shells including reactive materials, and a method of producing same
US20080035007A1 (en) * 2005-10-04 2008-02-14 Nielson Daniel B Reactive material enhanced projectiles and related methods
US20080229963A1 (en) * 2004-03-15 2008-09-25 Alliant Techsystems Inc. Reactive material enhanced munition compositions and projectiles containing same
CN102899529A (en) * 2012-08-13 2013-01-30 梁建烈 Pyrophoric alloy and production method
CN102978503A (en) * 2012-12-17 2013-03-20 李宏伟 Inflammable sparking alloy and preparation method thereof
CN102978504A (en) * 2012-12-17 2013-03-20 李宏伟 Inflammable alloy and preparation method thereof
USRE45899E1 (en) 2000-02-23 2016-02-23 Orbital Atk, Inc. Low temperature, extrudable, high density reactive materials

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2389198A (en) * 1942-07-24 1945-11-20 Kent Henry Flint alloy
US3203790A (en) * 1955-11-22 1965-08-31 Ronson Corp Extruded flints and process for making same
US3236633A (en) * 1955-11-30 1966-02-22 Goldschmidt Ag Th Extruded flints and process for making same
US3539334A (en) * 1968-08-13 1970-11-10 Gulf General Atomic Inc Method for producing pyrophoric metal alloy powders
US3653995A (en) * 1969-03-26 1972-04-04 Gulf Oil Corp Incendiary composition

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2389198A (en) * 1942-07-24 1945-11-20 Kent Henry Flint alloy
US3203790A (en) * 1955-11-22 1965-08-31 Ronson Corp Extruded flints and process for making same
US3236633A (en) * 1955-11-30 1966-02-22 Goldschmidt Ag Th Extruded flints and process for making same
US3539334A (en) * 1968-08-13 1970-11-10 Gulf General Atomic Inc Method for producing pyrophoric metal alloy powders
US3653995A (en) * 1969-03-26 1972-04-04 Gulf Oil Corp Incendiary composition

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4121924A (en) * 1976-09-16 1978-10-24 The International Nickel Company, Inc. Alloy for rare earth treatment of molten metals and method
US5096507A (en) * 1989-10-12 1992-03-17 Buck Werke Gmbh & Co. Method of applying a cerium misch metal coating to the surface of a splinter-active component of an incendiary splinter projectile
US5098487A (en) * 1990-11-28 1992-03-24 Olin Corporation Copper alloys for shaped charge liners
US7977420B2 (en) 2000-02-23 2011-07-12 Alliant Techsystems Inc. Reactive material compositions, shot shells including reactive materials, and a method of producing same
US9103641B2 (en) 2000-02-23 2015-08-11 Orbital Atk, Inc. Reactive material enhanced projectiles and related methods
US20070272112A1 (en) * 2000-02-23 2007-11-29 Alliant Techsystems Inc. Reactive material compositions, shot shells including reactive materials, and a method of producing same
USRE45899E1 (en) 2000-02-23 2016-02-23 Orbital Atk, Inc. Low temperature, extrudable, high density reactive materials
US9982981B2 (en) 2000-02-23 2018-05-29 Orbital Atk, Inc. Articles of ordnance including reactive material enhanced projectiles, and related methods
US20080229963A1 (en) * 2004-03-15 2008-09-25 Alliant Techsystems Inc. Reactive material enhanced munition compositions and projectiles containing same
US8075715B2 (en) 2004-03-15 2011-12-13 Alliant Techsystems Inc. Reactive compositions including metal
US20100276042A1 (en) * 2004-03-15 2010-11-04 Alliant Techsystems Inc. Reactive compositions including metal
US8361258B2 (en) 2004-03-15 2013-01-29 Alliant Techsystems Inc. Reactive compositions including metal
US8568541B2 (en) 2004-03-15 2013-10-29 Alliant Techsystems Inc. Reactive material compositions and projectiles containing same
FR2867469A1 (en) * 2004-03-15 2005-09-16 Alliant Techsystems Inc Reactive composition, useful in military and industrial explosives, comprises a metallic material defining a continuous phase and having an energetic material, which comprises oxidant and/or explosive of class 1.1
US20080035007A1 (en) * 2005-10-04 2008-02-14 Nielson Daniel B Reactive material enhanced projectiles and related methods
US8122833B2 (en) 2005-10-04 2012-02-28 Alliant Techsystems Inc. Reactive material enhanced projectiles and related methods
CN102899529A (en) * 2012-08-13 2013-01-30 梁建烈 Pyrophoric alloy and production method
CN102978504A (en) * 2012-12-17 2013-03-20 李宏伟 Inflammable alloy and preparation method thereof
CN102978504B (en) * 2012-12-17 2014-07-23 李宏伟 Inflammable alloy and preparation method thereof
CN102978503B (en) * 2012-12-17 2014-08-13 李宏伟 Inflammable sparking alloy and preparation method thereof
CN102978503A (en) * 2012-12-17 2013-03-20 李宏伟 Inflammable sparking alloy and preparation method thereof

Similar Documents

Publication Publication Date Title
EP0219628B1 (en) Rapidly solidified high strength, corrosion resistant magnesium base metal alloys
Das et al. High performance aerospace alloys via rapid solidification processing
US4938809A (en) Superplastic forming consolidated rapidly solidified, magnestum base metal alloy powder
EP0230123A1 (en) Formation of intermetallic and intermetallic-type precursor alloys for subsequent mechanical alloying applications
US3894867A (en) Incendiary alloys existing as a dispersion of incendiary particles in a non-incendiary atmospheric attack-resistant matrix
US4668282A (en) Formation of intermetallic and intermetallic-type precursor alloys for subsequent mechanical alloying applications
US4676829A (en) Cold worked tri-nickel aluminide alloy compositions
US4799955A (en) Soft composite metal powder and method to produce same
AU623872B2 (en) Third element additions to aluminum-titanium master alloys
US5078806A (en) Method for superplastic forming of rapidly solidified magnesium base metal alloys
JPH0625791A (en) High-strength magnesium alloy
US5603780A (en) Light weight, high strength beryllium-aluminum alloy
US3622234A (en) Hot corrosion resistant superalloys
US5071474A (en) Method for forging rapidly solidified magnesium base metal alloy billet
US5346562A (en) Method of production of iron aluminide materials
US4787943A (en) Dispersion strengthened aluminum-base alloy
US5417778A (en) Ductile, light weight, high strength beryllium-aluminum cast composite alloy
US4857109A (en) Rapidly solidified high strength, corrosion resistant magnesium base metal alloys
US4853035A (en) Rapidly solidified high strength, corrosion resistant magnesium base metal alloys
McCormick et al. The design and properties of new, Pb-free solder alloys
CN116723904A (en) Powder material with high thermal conductivity
US3539334A (en) Method for producing pyrophoric metal alloy powders
US3544394A (en) Aluminum-copper-magnesium-zinc powder metallurgy alloys
JPH062057A (en) Al base composite material
JPH06279894A (en) Copper alloy excellent in strength and electrical conductivity