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GB1449978A - Refractory metal-containing bodies - Google Patents

Refractory metal-containing bodies

Info

Publication number
GB1449978A
GB1449978A GB4315174A GB4315174A GB1449978A GB 1449978 A GB1449978 A GB 1449978A GB 4315174 A GB4315174 A GB 4315174A GB 4315174 A GB4315174 A GB 4315174A GB 1449978 A GB1449978 A GB 1449978A
Authority
GB
United Kingdom
Prior art keywords
particles
matrix
refractory metal
skeleton
matrix alloy
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
Application number
GB4315174A
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.)
Duracell Inc USA
Original Assignee
PR Mallory and Co Inc
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 PR Mallory and Co Inc filed Critical PR Mallory and Co Inc
Publication of GB1449978A publication Critical patent/GB1449978A/en
Expired legal-status Critical Current

Links

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
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24After-treatment of workpieces or articles
    • B22F3/26Impregnating
    • 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
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12014All metal or with adjacent metals having metal particles
    • Y10T428/1216Continuous interengaged phases of plural metals, or oriented fiber containing
    • Y10T428/12174Mo or W containing

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Powder Metallurgy (AREA)

Abstract

1449978 Refractory metal containing bodies PR MALLORY & CO Inc 4 Oct 1974 [23 Oct 1973] 43151/74 Heading C7D A body comprising a major amount by weight of particles of Ta, Mo or W or a refractory compound thereof (e.g. a carbide) in a minor amount by weight of a metal matrix comprising Ta, Mo or W and one or more of Ni, Fe, Co, Cu, Cr the average particle size of the particles being substantially the same as their average particle size prior to the formation of the body. The body may be prepared by forming a porous shaped skeleton of the refractory metal particles (e.g. by pressing at 10 t.s.i. and sintering at 1460‹C in hydrogen for 4 hours) and adding the matrix alloy in an amount in excess of that required to fill the voids in the porous skeleton and heating the skeleton and matrix alloy in a hydrogen atmosphere to 1,000-1100‹C for one hour at 1,000-1100‹C followed by ¢ hour at 1450-1480‹C, cooling and machining off the excess matrix alloy from the body. The Examples include the use of W and Mo particles and matrix alloys of composition:- 40% Mo 20% Fe 40% Ni; 40% W 20% Fe 40% Ni; 28.5% Mo, 28.5% Cu 28.5% Ni 14.5% Fe; 40% Mo 40% Co 20% Fe. The product may be used in aircraft counterbalances, radiation shielding, gyroscopic inertia members and die casting dies.
GB4315174A 1973-10-23 1974-10-04 Refractory metal-containing bodies Expired GB1449978A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US408606A US3929424A (en) 1973-10-23 1973-10-23 Infiltration of refractory metal base materials

Publications (1)

Publication Number Publication Date
GB1449978A true GB1449978A (en) 1976-09-15

Family

ID=23616968

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4315174A Expired GB1449978A (en) 1973-10-23 1974-10-04 Refractory metal-containing bodies

Country Status (4)

Country Link
US (1) US3929424A (en)
JP (1) JPS5083210A (en)
DE (1) DE2450361A1 (en)
GB (1) GB1449978A (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS598015B2 (en) * 1978-05-31 1984-02-22 三菱電機株式会社 Vacuum shield contact
JPS5578429A (en) * 1978-12-06 1980-06-13 Mitsubishi Electric Corp Contact material for vacuum breaker
JPS55152141A (en) * 1979-05-14 1980-11-27 Agency Of Ind Science & Technol Hybrid metal material and preparation thereof
US4364530A (en) * 1980-09-08 1982-12-21 The United States Of America As Represented By The Secretary Of The Navy Propulsion/control modular booster
DE3249505C2 (en) * 1982-06-10 1987-01-29 Ford-Werke AG, 5000 Köln Process for the manufacture of wear-resistant iron-based parts
US4605599A (en) * 1985-12-06 1986-08-12 Teledyne Industries, Incorporated High density tungsten alloy sheet
US4801330A (en) * 1987-05-12 1989-01-31 Rensselaer Polytechnic Institute High strength, high hardness tungsten heavy alloys with molybdenum additions and method
US4846885A (en) * 1987-11-27 1989-07-11 Haynes International, Inc. High molybdenum nickel-base alloy
US5008071A (en) * 1988-01-04 1991-04-16 Gte Products Corporation Method for producing improved tungsten nickel iron alloys
JP2950436B2 (en) * 1990-03-15 1999-09-20 株式会社東芝 Manufacturing method of composite material
KR100186931B1 (en) * 1996-04-30 1999-04-01 배문한 Method for producing tungsten polymerized gold
US6451385B1 (en) 1999-05-04 2002-09-17 Purdue Research Foundation pressure infiltration for production of composites
US8486541B2 (en) * 2006-06-20 2013-07-16 Aerojet-General Corporation Co-sintered multi-system tungsten alloy composite
JP6467535B1 (en) * 2018-02-13 2019-02-13 福田金属箔粉工業株式会社 Cu-based powder for infiltration

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3338687A (en) * 1965-06-16 1967-08-29 Gen Telephone & Elect Infiltrated composite refractory material
US3384464A (en) * 1966-02-16 1968-05-21 Mallory & Co Inc P R Tungsten structures
US3368879A (en) * 1966-02-16 1968-02-13 Mallory & Co Inc P R Tungsten structures
US3353933A (en) * 1966-03-11 1967-11-21 Mallory & Co Inc P R Tungsten powder bodies infiltrated with copper-titanium alloys
US3440043A (en) * 1966-03-11 1969-04-22 Mallory & Co Inc P R Method of producing tungsten powder bodies infiltrated with copper titanium alloys
US3340022A (en) * 1966-04-21 1967-09-05 Mallory & Co Inc P R Tungsten powder bodies infiltrated with copper-zirconium alloy
US3305324A (en) * 1966-05-26 1967-02-21 Mallory & Co Inc P R Tungsten powder bodies infiltrated with copper-titanium-bismuth or copper-titanium-tin
US3407048A (en) * 1968-01-22 1968-10-22 Mallory & Co Inc P R Molybdenum composite materials and method of making the same
US3505065A (en) * 1968-08-12 1970-04-07 Talon Inc Method of making sintered and infiltrated refractory metal electrical contacts

Also Published As

Publication number Publication date
DE2450361A1 (en) 1975-04-24
US3929424A (en) 1975-12-30
JPS5083210A (en) 1975-07-05

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee