GB723842A - Process for the manufacture of composite metal-ceramic material - Google Patents

Process for the manufacture of composite metal-ceramic material

Info

Publication number
GB723842A
GB723842A GB28143/52A GB2814352A GB723842A GB 723842 A GB723842 A GB 723842A GB 28143/52 A GB28143/52 A GB 28143/52A GB 2814352 A GB2814352 A GB 2814352A GB 723842 A GB723842 A GB 723842A
Authority
GB
United Kingdom
Prior art keywords
support
metal
ceramic
constituents
projected
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
GB28143/52A
Inventor
Roger Jacques Wellard
Yves Pierre Le Sech
Raymond Joseph Anto Perfettini
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of GB723842A publication Critical patent/GB723842A/en
Expired legal-status Critical Current

Links

Classifications

    • 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

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Laminated Bodies (AREA)
  • Powder Metallurgy (AREA)

Abstract

<PICT:0723842/III/1> <PICT:0723842/III/2> A process for manufacturing refractory and mechanically strong composite material of the type having metallic and ceramic constituents other than siliceous substances in close adhesive relationship for gas turbine blades or other heat engine elements comprises heating separately said constituents to a temperature at which they are in a softened condition and simultaneously and separately spraying said constituents on to a support whereby said metallic and ceramic constituents closely mix on the surface of said support. Apparatus for carrying out the invention comprises an oxyacetylene blow pipe 1 into which metal is fed in the form of a filament 4 so that the jet issuing from the nozzle 5 of the gun carries grains of molten metal which are projected on to a support 6 heated by a furnace 11. Another similar gun 7 is fed with a powdered ceramic constituent from a hopper 9 and this also is projected on to the support 6. On cooling, the composite material is separated from the support. The guns may be operated simultaneously to deposit a mixture of metal and ceramic grains on the support or they may be operated alternately to form fused laminated layers of metal and ceramic on the support. The metal projected from the gun 1 may be steel or an alloy containing nickel, chromium, cobalt. The ceramic constituent is a mixture containing a high proportion of refractory grains, e.g. an oxide, a carbide, a boride, a nitride or a mixture of these substances and a binder which may comprise vitrifying agents e.g. agents having a base of borax or of lithium oxide. In a modification a number of fixed guns are used to deposit metal and ceramic constituents alternately on a travelling or reciprocating support resting on rollers 12. The support may be a mould of metal or refractory material from which the composite material is withdrawn. In a further modification of the invention in order to increase the porosity of the material, one of the constituents is partially replaced by a third constituent which may be an organic or organo-metallic material or a mineral salt which is volatile or soluble or decomposable by heat, e.g. plastic materials.
GB28143/52A 1951-12-08 1952-11-07 Process for the manufacture of composite metal-ceramic material Expired GB723842A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR723842X 1951-12-08

Publications (1)

Publication Number Publication Date
GB723842A true GB723842A (en) 1955-02-09

Family

ID=9106417

Family Applications (1)

Application Number Title Priority Date Filing Date
GB28143/52A Expired GB723842A (en) 1951-12-08 1952-11-07 Process for the manufacture of composite metal-ceramic material

Country Status (1)

Country Link
GB (1) GB723842A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3020182A (en) * 1958-09-26 1962-02-06 Gen Electric Ceramic-to-metal seal and method of making the same
GB2239264A (en) * 1989-12-19 1991-06-26 Mtu Muenchen Gmbh Method for depositing wear-resistant dispersion coatings
GB2239462A (en) * 1989-12-26 1991-07-03 Gen Electric Microlaminated structure formed using two plasma guns
US5340615A (en) * 1993-06-01 1994-08-23 Browning James A Method to produce non-stressed flame spray coating and bodies

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3020182A (en) * 1958-09-26 1962-02-06 Gen Electric Ceramic-to-metal seal and method of making the same
GB2239264A (en) * 1989-12-19 1991-06-26 Mtu Muenchen Gmbh Method for depositing wear-resistant dispersion coatings
GB2239264B (en) * 1989-12-19 1993-10-06 Mtu Muenchen Gmbh Method for depositing wear-resistant dispersion coatings
GB2239462A (en) * 1989-12-26 1991-07-03 Gen Electric Microlaminated structure formed using two plasma guns
US5340615A (en) * 1993-06-01 1994-08-23 Browning James A Method to produce non-stressed flame spray coating and bodies

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