CS197698B1 - Double course protective coat of heat stressed components - Google Patents

Double course protective coat of heat stressed components Download PDF

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Publication number
CS197698B1
CS197698B1 CS777659A CS765977A CS197698B1 CS 197698 B1 CS197698 B1 CS 197698B1 CS 777659 A CS777659 A CS 777659A CS 765977 A CS765977 A CS 765977A CS 197698 B1 CS197698 B1 CS 197698B1
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CS
Czechoslovakia
Prior art keywords
layer
weight
nickel
calcium oxide
percent
Prior art date
Application number
CS777659A
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Czech (cs)
Inventor
Vaclav Pilous
Jan Vaclav
Evzen Kubes
Eduard Golias
Milan Hryciow
Angel Angelov
Jiri Kaspar
Original Assignee
Vaclav Pilous
Jan Vaclav
Evzen Kubes
Eduard Golias
Milan Hryciow
Angel Angelov
Jiri Kaspar
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.)
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Publication date
Application filed by Vaclav Pilous, Jan Vaclav, Evzen Kubes, Eduard Golias, Milan Hryciow, Angel Angelov, Jiri Kaspar filed Critical Vaclav Pilous
Priority to CS777659A priority Critical patent/CS197698B1/en
Priority to DE19782850288 priority patent/DE2850288A1/en
Priority to GB7845489A priority patent/GB2009622B/en
Priority to SE7812003A priority patent/SE7812003L/en
Priority to FR7833009A priority patent/FR2409323A3/en
Priority to IN1264/CAL/78A priority patent/IN150434B/en
Publication of CS197698B1 publication Critical patent/CS197698B1/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F22—STEAM GENERATION
    • F22B—METHODS OF STEAM GENERATION; STEAM BOILERS
    • F22B37/00—Component parts or details of steam boilers
    • F22B37/02—Component parts or details of steam boilers applicable to more than one kind or type of steam boiler
    • F22B37/04—Component parts or details of steam boilers applicable to more than one kind or type of steam boiler and characterised by material, e.g. use of special steel alloy
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/341—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one carbide layer
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
    • C23C28/3455—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
    • C23C4/11—Oxides

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Inorganic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Laminated Bodies (AREA)

Abstract

A protective coating for heat stressed parts, particularly firing chambers of steam boilers, comprises a first, base, layer and a second, upper, layer. The base layer comprises nickel and 10 to 30% by weight of chromium and the upper layer comprises zirconium dioxide and up to 20%, more particularly up to 10%, by weight of calcium oxide.

Description

Vynález řeší ochranné povlaky pro použití při ochraně tepelně namáhaných součástí, zejména spalovacích komor parních kotlů plazmovým nebo žárovým nástřikem.The invention solves protective coatings for use in the protection of thermally stressed components, in particular combustion chambers of steam boilers by plasma or heat spraying.

Pro zajištění ochrany stěn spalovacích komor parních kotlů proti korozi jsou na kotlové trubky navařovány trny z nerezavějící oceli, na kterých je keramický omaz. Uvedený způsob ochrany je velice pracný a předpokládá obnovu keramického omazu v pravidelných cyklech.In order to protect the walls of the combustion chambers of the steam boilers against corrosion, stainless steel mandrels are welded onto the boiler tubes on which the ceramic coating is applied. Said method of protection is very laborious and assumes the renewal of ceramic smearing in regular cycles.

Jedním ze známých způsobů ochrany ocelových součástí je podle čs. patentu Č. ' 130001 žárový nástřik vrstvy niklu v tloušťce 50 až 200 μια,' na kterou se musí nejpozději do 5 minut · nanést žárovým stříkáním· · vrstva hliníku ve stejné nebo větší · tloušťce, než · je · tloušťka niklo. vé · · vrstvy. Tento ·ochranný povlak · je· použitelný do teploty 1200 °C na vzduchu · a · v atmosféře obsahující sloučeniny síry.One of the known methods of protection of steel parts is according to MS. No. 130001, a thermal spray of a nickel layer of 50 to 200 μια, to which an aluminum layer of equal or greater than the nickel thickness must be applied by spraying at the latest within 5 minutes. layer. This protective coating can be used up to 1200 ° C in air and in an atmosphere containing sulfur compounds.

Pro ochranu kotlových trubek je třeba uvažovat s povlaky, které jsou namáhány vyššími teplotami, než je teplota tavení strusky, která stéká po stěnách spalovacích komor. A ochranné povlaky musí plnit především úlohu tepelné clony · a tím snížit tepelné namáhání základního materiálu. Při výrobě ochranných povlaku, je však třeba použít · takovou technologii, · která dovolí nástřik základní · a · ·krycí vrstvy s · větším časovým odstupem než u známých způsobů.In order to protect the boiler pipes, it is necessary to consider coatings subjected to higher temperatures than the melting temperature of the slag which flows down the walls of the combustion chambers. And the protective coatings must primarily fulfill the function of a heat curtain and thus reduce the thermal stress of the base material. However, in the manufacture of protective coatings, it is necessary to use a technology which allows the base coat to be sprayed and the coating layer to be sprayed over a longer time interval than in the known methods.

Nevýhody · stávající ochrany stěn · spalovacíchDisadvantages · existing wall protection · combustion

V7 6 9 8 komor řeší dvouvrstvý ochranný povlak podle vynálezu, · který obsahuje v první vrstvě 70 až 90 hmotnostních procent niklu a 10 až 30 hmotnostních procent chrómu, v podstatě tím, že druhá vrstva obsahuje stopy až 10 hmotnostních procent kysličníku · vápenatého a · zbytek kysličníku zirkoničitého.The V7 6 9 8 chambers provide a two-layer protective coating according to the invention, which contains 70 to 90 weight percent nickel and 10 to 30 weight percent chromium in the first layer, essentially in that the second layer contains traces of up to 10 weight percent calcium oxide; the rest of the zirconia.

Použitím ochranných · plazmových a žárových nástřiků na tepelně namáhaný materiál, zejména spalovaných komor dojde· k· vytvoření vyhovující korozní ochrany na · povrchu základního materiálu, přičemž účinná korozní ochrana plazmovým nebo žárovým ' · nástřikem má v rozsahu pracovních teplot ve srovnání · , s · keramickým omazem několikanásobně · ..větší životnost. Použitím uvedené ochrany · materiálu spalovacích ko* mor parních kotlů dojde”k podstatnému snížení pracnosti při výrobě kotlů, úspoře materiálu trnů, úspoře keramického omazu a odstraní se odstavování parních kotlů z důvodu opravy omazu. Odstraněním výpadků kotlů dojde ke zvýšení výkonu energetických bloků. · Snížením tepelné setrvačnosti spalovacích komor je možné dosáhnout · rychlejšího najíždění kotlů na plný výkon.The use of protective plasma and heat spray coatings on thermally stressed material, in particular combustion chambers, results in the formation of satisfactory corrosion protection on the surface of the base material, while effective corrosion protection with plasma or heat spray coatings over a range of operating temperatures ceramic grease several times longer life. The use of the above-mentioned protection of the combustion chamber material of the steam boilers will significantly reduce the work required in the manufacture of boilers, saving the material of mandrels, saving ceramic smearing and eliminating the shutdown of steam boilers due to the repair of smearing. The elimination of boiler failures will increase the output of the power units. · By reducing the thermal inertia of combustion chambers, it is possible to achieve faster start-up of boilers at full output.

Použitím dvouvrstvého ochranného povlaku dojde.· · v důsledku setrvání na pracovní teplotě k tepelně aktivovaným dějům, které · mají za následek zvýšení přilnavosti · podkladové vrstvy k základnímu materiálu. Výsledky · dlouhodobých zkoušek · prokázaly odolnost · dvouvrstvého ochranného povlaku . k cyklickému tepelnému . namáhám, ' zachovám celistvosti a požadovanou žáruvzdornost v atmosféře, 'obsahující sloučeniny síry za teplot převyšujících na povrchu ochranného povlaku 1500 °C.The use of a double-layered protective coating results in thermally activated processes resulting in an increase in the adhesion of the undercoat to the base material due to staying at the working temperature. The results of · long-term tests · showed resistance · double-layer protective coating. to cyclic heat. I try to maintain the integrity and the desired heat resistance in the atmosphere containing sulfur compounds at temperatures in excess of 1500 ° C on the surface of the protective coating.

Vynález je blíže objasněn na uvedených příkladech provedení.The invention is illustrated by the following examples.

Příklad 1Example 1

Příkladem použití ochrany tepelně namáhaných materiálů spalovacích komor parních kotlů je plazmový nástřik trubek povrchově zdrsněných tryskáním 0 76 mm, tloušťky stěny 5 mm, parního kotle. Podkladová vrstva v tloušťce 0,1 mm je tvořená nástřikem, který obsahujeAn example of the use of the protection of thermally stressed materials of the combustion chambers of steam boilers is the plasma spraying of tubes with surface blasting of 76 mm, wall thickness of 5 mm, of the steam boiler. The backing layer at a thickness of 0.1 mm is formed by a spray which it contains

Claims (1)

P R E D M É TSUBJECT Dvouvrstvý ochranný povlak tepelně namáhaných součástí .obsahující v první vrstvě 70 až 90 hmotnostních procent niklu . a 10 až .30 hmotnostních .procent chrómu, vyznačený tím, že dru kromě niklu 18,30 hmotnostních procent chromu. Krycí vrstva v tloušťce 0,48 až ' 0,62 mm obsahuje kromě kysličníku zirkoničitého 4,80 hmotnostních procent kysličníku vápenatého.Two-layer protective coating of thermally stressed components containing 70 to 90 weight percent nickel in the first layer. and 10 to 30 percent by weight of chromium, characterized in that the other than nickel is 18.30 percent by weight of chromium. The covering layer 0.48 to 0.62 mm thick contains 4.80 weight percent calcium oxide in addition to zirconia. Příklad 2Example 2 Obdobným příkladem je plazmový nástřik dopravníkových válečků průběžné žíhací pece. Na trubky povrchově zdrsněné tryskáním byla nastříkána podkladová vrstva v tloušťce 0,09 až 0,12 mm obsahující kromě niklu 14,2 hmotnostních procent . chr-omu. Krycí vrstva Obsahovala kromě kysličníku zirkoničitého. 4,20 hmotnostních procent kysličníku vápenatého a dosahovala tloušťky 0,53 až 0,71 mm.A similar example is the plasma spraying of conveyor rollers of a continuous annealing furnace. Blast-coated pipes were sprayed with a backing layer of 0.09 to 0.12 mm thickness containing 14.2 weight percent in addition to nickel. chr-omu. Cover layer Contained in addition to zirconia. 4.20% by weight of calcium oxide and reached a thickness of 0.53-0.71 mm. VYNÁLEZU há vrstva obsahuje stopy až 10 hmotnostních procent kysličníku vápenatého a zbytek kysličníku zirkoničitého.OF THE INVENTION The layer comprises traces of up to 10% by weight of calcium oxide and the remainder of zirconia.
CS777659A 1977-11-22 1977-11-22 Double course protective coat of heat stressed components CS197698B1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
CS777659A CS197698B1 (en) 1977-11-22 1977-11-22 Double course protective coat of heat stressed components
DE19782850288 DE2850288A1 (en) 1977-11-22 1978-11-20 TWO-LAYER PROTECTIVE COVER PRODUCED BY A PLASMA OR HEAT SPRAY APPLICATION FOR THERMAL EXPOSED PARTS
GB7845489A GB2009622B (en) 1977-11-22 1978-11-21 Protective coating for heat stressed parts
SE7812003A SE7812003L (en) 1977-11-22 1978-11-21 PROTECTIVE TWO-LAYER COATING FOR HEAT PACKING PARTS SUPPLIED WITH A PLASMA-MADE RADIATION OR A HIGH-TEMPERATURE RADIATION
FR7833009A FR2409323A3 (en) 1977-11-22 1978-11-22 TWO-LAYER PROTECTIVE COATING FOR HEAT-SUBJECTED PARTS, PRODUCED BY SPRAYING PLASMA OR HOT MATERIALS
IN1264/CAL/78A IN150434B (en) 1977-11-22 1978-11-22

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CS777659A CS197698B1 (en) 1977-11-22 1977-11-22 Double course protective coat of heat stressed components

Publications (1)

Publication Number Publication Date
CS197698B1 true CS197698B1 (en) 1980-05-30

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CS777659A CS197698B1 (en) 1977-11-22 1977-11-22 Double course protective coat of heat stressed components

Country Status (6)

Country Link
CS (1) CS197698B1 (en)
DE (1) DE2850288A1 (en)
FR (1) FR2409323A3 (en)
GB (1) GB2009622B (en)
IN (1) IN150434B (en)
SE (1) SE7812003L (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3242543C2 (en) * 1982-11-18 1985-09-19 Glyco-Metall-Werke Daelen & Loos Gmbh, 6200 Wiesbaden Layer material with a functional layer made of a metallic suspension alloy applied to a metallic carrier layer and a method for its production
DE3724995A1 (en) * 1987-02-26 1988-09-08 Radex Heraklith Process for manufacturing a composite body and the composite body itself
DE19721080C1 (en) * 1997-05-20 1998-10-01 Siemens Ag Corrosion protective coating especially of nuclear plant component

Also Published As

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GB2009622B (en) 1982-04-07
GB2009622A (en) 1979-06-20
DE2850288A1 (en) 1979-05-23
IN150434B (en) 1982-10-09
SE7812003L (en) 1979-05-23
FR2409323A3 (en) 1979-06-15
FR2409323B3 (en) 1980-12-05

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