CA1104004A - Method and apparatus for plasma flame-spraying coating material onto a substrate - Google Patents
Method and apparatus for plasma flame-spraying coating material onto a substrateInfo
- Publication number
- CA1104004A CA1104004A CA302,053A CA302053A CA1104004A CA 1104004 A CA1104004 A CA 1104004A CA 302053 A CA302053 A CA 302053A CA 1104004 A CA1104004 A CA 1104004A
- Authority
- CA
- Canada
- Prior art keywords
- plasma
- flame
- shroud
- coating material
- forming
- 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
Links
- 238000000576 coating method Methods 0.000 title claims abstract description 51
- 239000011248 coating agent Substances 0.000 title claims abstract description 47
- 239000000463 material Substances 0.000 title claims abstract description 46
- 239000000758 substrate Substances 0.000 title claims abstract description 35
- 238000000034 method Methods 0.000 title claims abstract description 32
- 238000010285 flame spraying Methods 0.000 title claims abstract description 25
- 239000007921 spray Substances 0.000 claims description 44
- 239000007789 gas Substances 0.000 claims description 36
- 230000008569 process Effects 0.000 claims description 25
- 239000000203 mixture Substances 0.000 claims description 20
- 238000002485 combustion reaction Methods 0.000 claims description 13
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 claims description 12
- 239000000843 powder Substances 0.000 claims description 7
- 238000005507 spraying Methods 0.000 claims description 7
- 239000001294 propane Substances 0.000 claims description 6
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 5
- 239000000567 combustion gas Substances 0.000 claims description 5
- 239000000498 cooling water Substances 0.000 claims description 5
- 239000001257 hydrogen Substances 0.000 claims description 5
- 229910052739 hydrogen Inorganic materials 0.000 claims description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 5
- 238000001816 cooling Methods 0.000 claims description 4
- 230000000694 effects Effects 0.000 claims description 4
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 claims description 3
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 claims description 3
- VBUBYMVULIMEHR-UHFFFAOYSA-N propa-1,2-diene;prop-1-yne Chemical compound CC#C.C=C=C VBUBYMVULIMEHR-UHFFFAOYSA-N 0.000 claims description 3
- 239000012530 fluid Substances 0.000 claims description 2
- 239000012255 powdered metal Substances 0.000 claims description 2
- 229910010293 ceramic material Inorganic materials 0.000 claims 1
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 12
- 238000012360 testing method Methods 0.000 description 7
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- 229910052786 argon Inorganic materials 0.000 description 6
- 238000009434 installation Methods 0.000 description 6
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 5
- 239000001301 oxygen Substances 0.000 description 5
- 229910052760 oxygen Inorganic materials 0.000 description 5
- 239000012254 powdered material Substances 0.000 description 4
- 239000000919 ceramic Substances 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- 239000002245 particle Substances 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 239000012159 carrier gas Substances 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 238000011109 contamination Methods 0.000 description 2
- 230000008021 deposition Effects 0.000 description 2
- -1 for example Substances 0.000 description 2
- 239000001307 helium Substances 0.000 description 2
- 229910052734 helium Inorganic materials 0.000 description 2
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 230000001603 reducing effect Effects 0.000 description 2
- 239000002002 slurry Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- JRPBQTZRNDNNOP-UHFFFAOYSA-N barium titanate Chemical compound [Ba+2].[Ba+2].[O-][Ti]([O-])([O-])[O-] JRPBQTZRNDNNOP-UHFFFAOYSA-N 0.000 description 1
- 229910002113 barium titanate Inorganic materials 0.000 description 1
- 239000011230 binding agent Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010891 electric arc Methods 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000010721 machine oil Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000007750 plasma spraying Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
- H05H1/00—Generating plasma; Handling plasma
- H05H1/24—Generating plasma
- H05H1/26—Plasma torches
- H05H1/32—Plasma torches using an arc
- H05H1/42—Plasma torches using an arc with provisions for introducing materials into the plasma, e.g. powder, liquid
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05B—SPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
- B05B7/00—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas
- B05B7/16—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas incorporating means for heating or cooling the material to be sprayed
- B05B7/22—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas incorporating means for heating or cooling the material to be sprayed electrically, magnetically or electromagnetically, e.g. by arc
- B05B7/222—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas incorporating means for heating or cooling the material to be sprayed electrically, magnetically or electromagnetically, e.g. by arc using an arc
- B05B7/226—Spraying apparatus for discharge of liquids or other fluent materials from two or more sources, e.g. of liquid and air, of powder and gas incorporating means for heating or cooling the material to be sprayed electrically, magnetically or electromagnetically, e.g. by arc using an arc the material being originally a particulate material
-
- 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
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
- C23C4/134—Plasma spraying
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
- H05H1/00—Generating plasma; Handling plasma
- H05H1/24—Generating plasma
- H05H1/26—Plasma torches
- H05H1/28—Cooling arrangements
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
- H05H1/00—Generating plasma; Handling plasma
- H05H1/24—Generating plasma
- H05H1/26—Plasma torches
- H05H1/32—Plasma torches using an arc
- H05H1/34—Details, e.g. electrodes, nozzles
- H05H1/341—Arrangements for providing coaxial protecting fluids
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
- H05H1/00—Generating plasma; Handling plasma
- H05H1/24—Generating plasma
- H05H1/26—Plasma torches
- H05H1/32—Plasma torches using an arc
- H05H1/34—Details, e.g. electrodes, nozzles
- H05H1/3478—Geometrical details
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
- H05H1/00—Generating plasma; Handling plasma
- H05H1/24—Generating plasma
- H05H1/26—Plasma torches
- H05H1/32—Plasma torches using an arc
- H05H1/34—Details, e.g. electrodes, nozzles
- H05H1/3457—Nozzle protection devices
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Spectroscopy & Molecular Physics (AREA)
- Chemical & Material Sciences (AREA)
- Metallurgy (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Organic Chemistry (AREA)
- Electromagnetism (AREA)
- Geometry (AREA)
- Nozzles (AREA)
- Coating By Spraying Or Casting (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Plasma Technology (AREA)
Abstract
ABSTRACT OF THE DISCLOSURE Method and apparatus for plasma flame-spraying coating material onto a substrate by means of passing a plasma-forming gas through a nozzle electrode, passing an arc-forming current between said nozzle electrode and a rear electrode to form a plasma effluent, introducing coating material into the plasma effluent, passing the plasma effluent axially through a wall shroud extending from the exit of said nozzle electrode and forming a flame shroud for the plasma effluent at least within the wall shroud.
Description
\
BACKGROUND OF THE INVENTION
This i~vention relates to the application of coatings onto substrates by plasma spray techniques, and more particularly, to method and apparatus for shielding the effluent from plasma spray gun assemblies from contamination by the surrounding en-vironment.
Plasma spray gun assemblies are known which use an electric arc to excite a gas, thereby producing a thermal plasma of very ~ !
high temperature. Spray or powdered materials are introduced into the thermal plasma, melted and projected onto a substrate or base to form coatings. Such powdered materials may include ~etals, metal alloys, ceramics such as metal oxides, and carbides or the like, for example.
Heretofore, difficulties were experienced due to contamin-ation of the effluent from the nozzle of the spray gun, such as air entrapment, for example, that resulted in significant oxida-tion of the coating materials. The spraying conditions, part-icularly heat and velocity, were often adjusted to a compromise to heat the powder just enough to melt it. Attempts have been made to overcome this problem, but they have been only moderately successful. One such attempt involved completely enclosing the apparatus in a chamber, but this was expensive and also very cumbersome. In other installations, efforts were made to use a gas shroud to solve -the problem. For example, the Jackson U.S.
Patent 3~470r347 shows the use of a coaxial annular stream of un-heated gas. However, this required a relatively large flow of gas, such as argon, which is expensive. In addition, there was a tendancy with such prior art devices to build up a coating on the shrouding device. Other related patents in this art include Anderson et al, U.S. Patent 2,951,143; Yoshiaki Arata et al, Patent 3,082,314; and Unger et al, U.S. Patent 3,313,909, for example.
!~
!4 SUMP~RY OF THE INVENTION
The basic and genexal object of the present invention is the provision of a new and improved method and apparatus, which overcomes or at least mitigates some of the problems of the prior art.
A more specific object is the provision of method and appar-atus which provides improvements in one or more of the following aspects: higher deposition efficiency; reduced oxygen content in the effluent for metallic materials; reduced unmel-ted particle ~;
inclusions; increased feed rates; and improved quality of the coating.
~To the accomplishment of the foregoing objectives, and addi--~;tional objectives and advantages, which will become apparent as this description proceeds, the invention contemplates, in one form thereof, the provision of a new and improved plasma spray gun assembly for coating substrates which includes, in combination, a nozzle electrode having a nozzle passage therethrough, a rear electrode, and means for passing plasma-forming gas through the nozzle electrode. In addition, the assembly includes means for passing an arc-forming current between the electrodes to form a plasma effluent, and means for introducing coating material into the plasma effluent. Further, the assembly according to the invention, includes a wall shroud for the plasma effluent extend-ing from the exit of the nozzle electrode, and means for forming a flame shroud for the plasma effluent within the wall shroud and in some instances extending beyond the wall shroud.
In one preferred form of the invention, the flame shroud is directed at an angle of between about 160 and about 180 with respect to ~he axis of the plasma efrluent, and more preferably, the flame shroud is directed at an angle of about 180 with re-spect to the axis of the plasma effluent.
~ f~
~4~
According to an aspect of the invention, the wall shroud is cylindrical and means are provided for water cooling this shroud.
In one form of the invention, ~he means for forming a flame shroud for the plasma e-ffluent at least within the wall shroud comprises burner means disposed adjacent the outlet of the wall shroud. According to an aspect of the invention, the gas in the burner means is a combustible mixture such as, for example, air or oxygen mixed with propane, ace-tylene, APACHI gas as manufact-ured by Air Products Inc., MAPP gas as manufactured by Dow Chemical Company, or hydrogen. Preferably, high molecular weight gases are employed. It is desirable in some installations to preheat this gas. Also, in some installations, a combustible liquid is used.
In another form of the invention, an annular manifold is mounted adjacent the outer end of the wall shroud, which has jet orifice means for providing an annular curtain effect around the plasma flame as it leaves the wall shroud and passes towards the target substrate.
~; The invention, in another form thereof, is directed to a .: ~
process for plasma flame-spraying coating material onto a sub-,~
strate, which includes the steps of: passing a plasma-forming gas through a nozzle electrode, and passing an arc-forming cur-rent between the nozzle electrode and a rear electrode to form a plasma effluent. The process further includes the steps of in-troducing coating material into the plasma effluent, passing the plasma effluent through a wall shroud extending from the exit of the nozzle ele~trode, and forming a flame shroud for the plasma effluent within the wall shroud. It will be appreciated that the coating material may be in any form suitable for plasma spraying such as, for example, a solid wire ox rod. However, powder is pre-ferable. The powder may be free flowing or in a binder such as a plastic bonded wixe or the like, for example. The spray material , ~ 1 r ,~ .
introduced into the plasma effluent may be introduced at any - convenient location, including one upstream of the arc. However, it is generally introduced at a point downstream of the arc, and preferably, adjacent the nozzle e~it on the downstream side there-of. Further, several poin-ts of introduction may be utilized, simultaneously.
According to the invention, the flame shroud is preferably directed at an angle of about 180 with respect to the axis of the plasma effluent. ~s another aspect of the invention, the process includes the step of forming an annular fluid curtain around the plasma effluent as it leaves the plasma spxay gun assembly.
There has thus been outlined rather broadly the more impor-tant features of the invention in order that the detailed des-cription thereof that follows may be better understood, and in order that the present contribution to the art may be better , ., ,~ appreciated. There are, of course, additional features of the invention which will be described more fully hereinafter. Those skilled in the art will appreciate that the conception on which this disclosure is based may readily be utilized as the basis for the design of other methods and apparatus for carrying out the several purposes of the invention. It is important, therefore, that this disclosure be regarded as including such equivalent me~hods and apparatus as do not depart from the spirit and scope of the invention.
Several embodiments of the invention have been chosen for purposes of illustration and description, and are shown in the accompanying drawings, forming a part of the specification.
BRIEF DESCRIPTION OF T~E DRAWINGS
.
Fig. 1 is a medial sectional view of a plasma flame spray gun assembly constructed in accordance with the concepts of the present inventiGn;
~ -S-Fig. 2 is a sectional view taken along the line indicated ~t 2-2 in Fig. l;
Fig. 3 is a fragmentary, medial sectional view showing the outlet portion of the plasma flame spray gun according to another embodiment of the invention; ~ ~:
Fig. 4 is a table showing comparative test results of a plasma fl~ne spray gun according to the invention with respect to conventional guns; and Figs. 5 to 9 are schematic drawings each showing a wall .~ 10 shroud and flame shroud arrangement according to other embodiments of the invention. .
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
In the embodiment of the invention illustra-ted in Figs. 1 and 2, a plasma spray gun assembly, indicated generally at 10, for coating a substrate 11, includes a nozzle electrode 12 having a nozzle bore or passage 14 therethrough, and a rear electrode 16 . mounted on an electrode holder 18. Electrical cable connections 20 and 22 serve to connect the electrodes to a suitable electrical ::
~; sourceO A plasma-forming gas such as nitrogen, argon, helium, : 20 hydrogen or the like, for example, is passed from a suitable pressure source through a connector 24 into the space 14 around the tip of the electrode 16, through an annular passage formed by the electrode tip and the tapered portion of the nozzle. The current is caused to flow from the connector 20 through the electrode holder 18 to the electrode 16 and from the tip of the electrode 16 in the form of an arc to the nozzle 12 and then to connector 22, to thereby form a very hot plasma flame which ex-tends out through the exit 26 of the nozzle electrode 12. One or more secondary gases can be mixed with the primary gas, if desired.
~ 6-- r ~1040(~4 Heat fusible powdered coating material, such as powdered metal, or ceramics or the like, for example, is entrained in a carrier gas, which, for example, may be a gas such as nitrogen, helium, argon, or e~en air, received from a suitable source through a connection 28 provided for the purpose. In the embodi~
ment illustrated, the powdered material is injected into the plas-.
ma flame adjacent the nozzle exit 26, as by means of the nozzle 30. As a result, in operation, the plasma effluent or flame~ ~
with the powdered material carried therewith passes in the dir- ;
ection indicated by arrow 32 at a very high velocity, the axis thereof being indicated at 33.
, According -to the invention, an annularly-shaped wall shroud, indicated at 34, is mounted on the nozzle 12 adjacent the nozzle ~;` exit 36 to form a shroud chamber 37. In the embodiment illus-trated, the wall shroud 34 is cylindrical, having an inner step portion 38 and an outer step portion 40.
Still referring to Fig. 1, a gas burner, indicated generally at 42, is mounted at the outer end of the wall shroud 34, which includes an annular plenum chamber 44 feeding a plurality of jet orifices 46 that are directed at an angle of between about 160 and about 180 wi-th respect to the axis 33 of the plasma effluent or flame. Preferably, the jet orifices are directed at an angle of about 180 with respect to the axis 33 of the plasma flame to form an annularly-shaped combustion flame shroud within the chamber 37, adjacent the wall shroud, as indicated by arrows 48. Alter-nativelyl the jet orifices may be in the form of a continuous narrow annular slit-like opening. The combustion gases for the flame shroud are fed to the plenum chamber 44 through a control device 50, a combustion gas inlet 52 and tubes 54 within the wall shroud 34. The function of the control device will be explained ,:
- more fully hereinafter.
~.
~: . ;
Due to the high temperatures involved wikh pl~sma spray guns of this nature, water cooling is provided. The electrical cable connections 20 and 22 are constructed so as to receive water cooled electric cables through which cooling water is fore~d.
This cooling water flows through the connection 22 and around the nozzle 12, and then outwardly through one side and then inwardly . through the other side of a water jacket 56 to cool the wall - ~ shroud 34. The cooling water thereaf-ter is directed through a passage 58 to cool the electrode 16 before passing out of the system through the connection 20.
It will be appreciated that the flame shroud, as indicated by arrow 48, within the wall shroud 34 is directed to~ards the exit flow of the arc plasma flame, as indicated by the arrow 32.
The conbination of these two flows, together with the high temp- ~
erature of the flame gases satisfies the arc plasma jet's charact- ;
eristic aspiration of the surrGunding atmosphere without the plasma jet being either quenched by a cold gas stream or entrain-ing air, whi~h otherwise has a propensity to produce an uncontrolled oxidizing reaction with the material being sprayed. Any suitable combustion mixture may be employed. ~owever, it has been found desirable to utilize a high molecular weight gas in order to pro-vide substantial expansion eharacteristics and a relatively large quantity of combustion products. Presently preferred combustion mixtures include air or oxygen mixed with acetylene, propane, APACHI gas as manufactured by Air Produets Inc., MAPP gas as manufactured by Dow Chemical Company, or hydrogen. The control device serves to eontrol the characteristics of the gas supplied to the plenum chamber 44. It is desirable in some installations to preheat the combustion mixture. Moreover, depending on the particular material being sprayed, the combustion gases may be adjusted to provide either oxidizing, neutral or reducing atmosphere both within the chamber 37 and beyond the exit thereo~. This ,~ .
enables the chemical composition of the spray coating to be con-trolled such as, for example, con-trolling the carbon content of carbides, iron or the like and, also, compounds such as barium titanate may be sprayed without the usual reduction of oxygen content. In general, the spraying of metals requires a reducing atmosphere, whereas when spraying ceramics, it is desirable to provide an excess of oxygen.
In order to more fully illustrate the nature of the inven-tion, Fig. 4 presents a table indicating the comparative test results, spraying the same material, of a conventional plasma spray gun assembly without shrouding and a plasma spray gun assembly constructed according to the invention, which includes an annularly-shaped wall shroud and an annularly-shaped flame shroud within and adjacent the wall shroud, directed at an angle of about 180 w~th respect -to the axis of the plasma flame.
The wear resistance specified in the table of Fig. 4 was deter-mined according to the test procedure set forth in Addendum -Table I. The test results show a clear superiority of the spray gun assembly of the present invention.
The following example describes the typical operation of the plasma spray ~un assembly.
Example 1 . .
A plasma spray gun assembly similar to that shown in Figs. 1 and 2 was used. ~he bore diameter Dl of the nozzle electrode 12 was 0.25 inches. The inside diame-ter D2 of the wall shroud 34 was 1.50 inches and the inside diameter D3 of the gas burner 42 was 1.15 inches. The distance Ll between the end of the nozzle 12 and the inner end of the gas buxner 42 was 1.70 inches and the distance L2 between the end of the nozzle electrode 12 and the substrate or work piece 11 was 2.75 inches~ The diameter of the nozzle 30 for the powdered coating material was 0.060 inches.
Thirty-six jet orifices 46 having a diameter of 0.023 inches were r ~
employed on a 1.38 inch diameter circle. The plasma gases uti-lized were argon, at a pressure of 100 p.s.i.y. and a flow rate of 90 soc~f~h~ and hydrogen at a pressure of 60 p.sOi.g. at a flow rate of 7 s.c.f.h. The arc current was 700 amperes at 48 volts. The shroud gases employed were air at a pressure of 50 p.s.i.g. at a flow rate of 400 s.c.f.h. mixed with propane at a ;:
pressure of 50 p.s.i.g. at a flow rate of 90 s.c.f.h. The powdered coating material was a coba]t base alloy having a particle size of from about 10 to about 40 microns and a flow .
rate of 6 pounds per hour~ The carrier gas was argon with a flow rate of 7 s.c~f.h. The coatings obtained were substantially superior to those normally obtained with conventional spray guns.
`-~In certain installations, an annular manifold 59, Fig. 3, ~ ;
is mounted on the outer end of the gas burner 42. Cooling water `~
or an inert gas such as, for example, nitrogen or argon is supplied to this manifold through an inlet 61, and annular jPt -~orifice outlet means 60 are provided on the side of the manifold ;:
towards the substrate 11 to provide an annular curtain effect around the plasma flame, as indicated by arrow 62. Not only does the jet spray serve to shield the spray stream, it also allows the spray cone to be controlled and furthermore serves to provide some cooling of the substrate. Similarly, the same manifold may be used with propane to provide a secondary flame shroud around the spray stream and thereby further reduce the oxide content of the coating. In certain installations it is desirable to utilize carbon dioxide for this purpose.
While the embodiment of Figs. 1 and 2 is the presently preferred embodiment, other desirable embodiments of the invention are illustrated in Figs. 5 to 9. Fig~ 5 shows in schematic form ;~
an annular wall shroud 64 with plasma flame or effluent 66 pas-sing longitudinally therethrough along an axis indicated at 68.
',' ' . .
-- . . . - : .;: :: , . .
In this embodiment, an annular flame shroud 70 is directed parallel to the direction of flow of the plasma effluent.
In the embodiment of Fig. 6, the plasma ef~luent 66 passes longitudinally along its axis 68 through an annular wall shroud 72, and an annular flame shroud 74 is directed at an angle having a component extending parallel to the direction of flow of the plasma effluent.
; Referring next to the embodiment of Fig. 7, the plasma `
effluent 66 passes longitudinally along its axis 68 through an ;~ 10 annularly-shaped wall shroud 76, and a portion of the gas for .~:
forming the flame shroud is introduced, as indicated at 78, at an angle of about 180 with respect to the axis 68 of the plasma effluent or flame, and a second portion of the gas for forming the flame shroud is introduced, as indicated at 80, at an angle having a component extending parallel to the direction of flow of the plasma effluent.
In the embodiment of Fig. 8, the plasma effluent 66 ;~
passes longitudinally along its axis 68 through an annular wall shroud 82, and an annular flame shroud 84 IS directed at an an~le having a component extending in a direction opposite to the direction of flow of said plasma effluent.
Fig. 9 shows an embodiment of the invention wherein the plasma effluent 66 passes longitudinally along the axis 58 ;
through an annular wall shroud 86. A portion of the gas for forming the flame shroud is introduced, as indicated at 88, at an angle of about 180 with respect to the axis 68 of the plasma ~, effluent and a second portion of the gas for forming said flame ,. ~ .
~-~ shroud is introduced, as indicated at 90, at an angle having a component extending in a direction opposite to the direction of ' flow of the plasma effluent.
, ,"~ .
,~' .~ ' ., .: ., . . . ,, .. . .... ~ .
Thus, it will be appreciated that the gas for forming the flame shroud may be introduced at one or more inlets and each inlet may be disposed at any angle from about zero to about 180, and may even be normal to the direction of flow :
of the plasma effluent. ' It will thus be seen that the present invention does indeed provide a new and improved plasma spray gun assembly which is superior to conventional spray guns with respect to ;~
deposition efficiency, reduced oxide contents, reduced un-melted particle inclusions, as well as other operative characteristics. ,~
~aving thus described the invention with particular reference to the preferred forms thereof, it will be obvious .
to those skilled in the art to which the invention pertains, after understanding the invention that various changes and modifications may be.made therein without departing from the ~
spirit and scope of the invention, as defined by the claims ~ .
appended hereto.
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. ` .
1 ADDENDUM _ rrABLE I
The powders were sprayed under conditions to produce coatings which were tested for abrasion or wear resistance, as follows:
~13 Measure the thickness of the test buttons (including 7 coating) in four places, using a Supermicrometer, and record the 8 readin~s. ~Locate the four points for a suhsequent measurement by placing marks or numbers on the periphery of the ~utton.)
BACKGROUND OF THE INVENTION
This i~vention relates to the application of coatings onto substrates by plasma spray techniques, and more particularly, to method and apparatus for shielding the effluent from plasma spray gun assemblies from contamination by the surrounding en-vironment.
Plasma spray gun assemblies are known which use an electric arc to excite a gas, thereby producing a thermal plasma of very ~ !
high temperature. Spray or powdered materials are introduced into the thermal plasma, melted and projected onto a substrate or base to form coatings. Such powdered materials may include ~etals, metal alloys, ceramics such as metal oxides, and carbides or the like, for example.
Heretofore, difficulties were experienced due to contamin-ation of the effluent from the nozzle of the spray gun, such as air entrapment, for example, that resulted in significant oxida-tion of the coating materials. The spraying conditions, part-icularly heat and velocity, were often adjusted to a compromise to heat the powder just enough to melt it. Attempts have been made to overcome this problem, but they have been only moderately successful. One such attempt involved completely enclosing the apparatus in a chamber, but this was expensive and also very cumbersome. In other installations, efforts were made to use a gas shroud to solve -the problem. For example, the Jackson U.S.
Patent 3~470r347 shows the use of a coaxial annular stream of un-heated gas. However, this required a relatively large flow of gas, such as argon, which is expensive. In addition, there was a tendancy with such prior art devices to build up a coating on the shrouding device. Other related patents in this art include Anderson et al, U.S. Patent 2,951,143; Yoshiaki Arata et al, Patent 3,082,314; and Unger et al, U.S. Patent 3,313,909, for example.
!~
!4 SUMP~RY OF THE INVENTION
The basic and genexal object of the present invention is the provision of a new and improved method and apparatus, which overcomes or at least mitigates some of the problems of the prior art.
A more specific object is the provision of method and appar-atus which provides improvements in one or more of the following aspects: higher deposition efficiency; reduced oxygen content in the effluent for metallic materials; reduced unmel-ted particle ~;
inclusions; increased feed rates; and improved quality of the coating.
~To the accomplishment of the foregoing objectives, and addi--~;tional objectives and advantages, which will become apparent as this description proceeds, the invention contemplates, in one form thereof, the provision of a new and improved plasma spray gun assembly for coating substrates which includes, in combination, a nozzle electrode having a nozzle passage therethrough, a rear electrode, and means for passing plasma-forming gas through the nozzle electrode. In addition, the assembly includes means for passing an arc-forming current between the electrodes to form a plasma effluent, and means for introducing coating material into the plasma effluent. Further, the assembly according to the invention, includes a wall shroud for the plasma effluent extend-ing from the exit of the nozzle electrode, and means for forming a flame shroud for the plasma effluent within the wall shroud and in some instances extending beyond the wall shroud.
In one preferred form of the invention, the flame shroud is directed at an angle of between about 160 and about 180 with respect to ~he axis of the plasma efrluent, and more preferably, the flame shroud is directed at an angle of about 180 with re-spect to the axis of the plasma effluent.
~ f~
~4~
According to an aspect of the invention, the wall shroud is cylindrical and means are provided for water cooling this shroud.
In one form of the invention, ~he means for forming a flame shroud for the plasma e-ffluent at least within the wall shroud comprises burner means disposed adjacent the outlet of the wall shroud. According to an aspect of the invention, the gas in the burner means is a combustible mixture such as, for example, air or oxygen mixed with propane, ace-tylene, APACHI gas as manufact-ured by Air Products Inc., MAPP gas as manufactured by Dow Chemical Company, or hydrogen. Preferably, high molecular weight gases are employed. It is desirable in some installations to preheat this gas. Also, in some installations, a combustible liquid is used.
In another form of the invention, an annular manifold is mounted adjacent the outer end of the wall shroud, which has jet orifice means for providing an annular curtain effect around the plasma flame as it leaves the wall shroud and passes towards the target substrate.
~; The invention, in another form thereof, is directed to a .: ~
process for plasma flame-spraying coating material onto a sub-,~
strate, which includes the steps of: passing a plasma-forming gas through a nozzle electrode, and passing an arc-forming cur-rent between the nozzle electrode and a rear electrode to form a plasma effluent. The process further includes the steps of in-troducing coating material into the plasma effluent, passing the plasma effluent through a wall shroud extending from the exit of the nozzle ele~trode, and forming a flame shroud for the plasma effluent within the wall shroud. It will be appreciated that the coating material may be in any form suitable for plasma spraying such as, for example, a solid wire ox rod. However, powder is pre-ferable. The powder may be free flowing or in a binder such as a plastic bonded wixe or the like, for example. The spray material , ~ 1 r ,~ .
introduced into the plasma effluent may be introduced at any - convenient location, including one upstream of the arc. However, it is generally introduced at a point downstream of the arc, and preferably, adjacent the nozzle e~it on the downstream side there-of. Further, several poin-ts of introduction may be utilized, simultaneously.
According to the invention, the flame shroud is preferably directed at an angle of about 180 with respect to the axis of the plasma effluent. ~s another aspect of the invention, the process includes the step of forming an annular fluid curtain around the plasma effluent as it leaves the plasma spxay gun assembly.
There has thus been outlined rather broadly the more impor-tant features of the invention in order that the detailed des-cription thereof that follows may be better understood, and in order that the present contribution to the art may be better , ., ,~ appreciated. There are, of course, additional features of the invention which will be described more fully hereinafter. Those skilled in the art will appreciate that the conception on which this disclosure is based may readily be utilized as the basis for the design of other methods and apparatus for carrying out the several purposes of the invention. It is important, therefore, that this disclosure be regarded as including such equivalent me~hods and apparatus as do not depart from the spirit and scope of the invention.
Several embodiments of the invention have been chosen for purposes of illustration and description, and are shown in the accompanying drawings, forming a part of the specification.
BRIEF DESCRIPTION OF T~E DRAWINGS
.
Fig. 1 is a medial sectional view of a plasma flame spray gun assembly constructed in accordance with the concepts of the present inventiGn;
~ -S-Fig. 2 is a sectional view taken along the line indicated ~t 2-2 in Fig. l;
Fig. 3 is a fragmentary, medial sectional view showing the outlet portion of the plasma flame spray gun according to another embodiment of the invention; ~ ~:
Fig. 4 is a table showing comparative test results of a plasma fl~ne spray gun according to the invention with respect to conventional guns; and Figs. 5 to 9 are schematic drawings each showing a wall .~ 10 shroud and flame shroud arrangement according to other embodiments of the invention. .
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
In the embodiment of the invention illustra-ted in Figs. 1 and 2, a plasma spray gun assembly, indicated generally at 10, for coating a substrate 11, includes a nozzle electrode 12 having a nozzle bore or passage 14 therethrough, and a rear electrode 16 . mounted on an electrode holder 18. Electrical cable connections 20 and 22 serve to connect the electrodes to a suitable electrical ::
~; sourceO A plasma-forming gas such as nitrogen, argon, helium, : 20 hydrogen or the like, for example, is passed from a suitable pressure source through a connector 24 into the space 14 around the tip of the electrode 16, through an annular passage formed by the electrode tip and the tapered portion of the nozzle. The current is caused to flow from the connector 20 through the electrode holder 18 to the electrode 16 and from the tip of the electrode 16 in the form of an arc to the nozzle 12 and then to connector 22, to thereby form a very hot plasma flame which ex-tends out through the exit 26 of the nozzle electrode 12. One or more secondary gases can be mixed with the primary gas, if desired.
~ 6-- r ~1040(~4 Heat fusible powdered coating material, such as powdered metal, or ceramics or the like, for example, is entrained in a carrier gas, which, for example, may be a gas such as nitrogen, helium, argon, or e~en air, received from a suitable source through a connection 28 provided for the purpose. In the embodi~
ment illustrated, the powdered material is injected into the plas-.
ma flame adjacent the nozzle exit 26, as by means of the nozzle 30. As a result, in operation, the plasma effluent or flame~ ~
with the powdered material carried therewith passes in the dir- ;
ection indicated by arrow 32 at a very high velocity, the axis thereof being indicated at 33.
, According -to the invention, an annularly-shaped wall shroud, indicated at 34, is mounted on the nozzle 12 adjacent the nozzle ~;` exit 36 to form a shroud chamber 37. In the embodiment illus-trated, the wall shroud 34 is cylindrical, having an inner step portion 38 and an outer step portion 40.
Still referring to Fig. 1, a gas burner, indicated generally at 42, is mounted at the outer end of the wall shroud 34, which includes an annular plenum chamber 44 feeding a plurality of jet orifices 46 that are directed at an angle of between about 160 and about 180 wi-th respect to the axis 33 of the plasma effluent or flame. Preferably, the jet orifices are directed at an angle of about 180 with respect to the axis 33 of the plasma flame to form an annularly-shaped combustion flame shroud within the chamber 37, adjacent the wall shroud, as indicated by arrows 48. Alter-nativelyl the jet orifices may be in the form of a continuous narrow annular slit-like opening. The combustion gases for the flame shroud are fed to the plenum chamber 44 through a control device 50, a combustion gas inlet 52 and tubes 54 within the wall shroud 34. The function of the control device will be explained ,:
- more fully hereinafter.
~.
~: . ;
Due to the high temperatures involved wikh pl~sma spray guns of this nature, water cooling is provided. The electrical cable connections 20 and 22 are constructed so as to receive water cooled electric cables through which cooling water is fore~d.
This cooling water flows through the connection 22 and around the nozzle 12, and then outwardly through one side and then inwardly . through the other side of a water jacket 56 to cool the wall - ~ shroud 34. The cooling water thereaf-ter is directed through a passage 58 to cool the electrode 16 before passing out of the system through the connection 20.
It will be appreciated that the flame shroud, as indicated by arrow 48, within the wall shroud 34 is directed to~ards the exit flow of the arc plasma flame, as indicated by the arrow 32.
The conbination of these two flows, together with the high temp- ~
erature of the flame gases satisfies the arc plasma jet's charact- ;
eristic aspiration of the surrGunding atmosphere without the plasma jet being either quenched by a cold gas stream or entrain-ing air, whi~h otherwise has a propensity to produce an uncontrolled oxidizing reaction with the material being sprayed. Any suitable combustion mixture may be employed. ~owever, it has been found desirable to utilize a high molecular weight gas in order to pro-vide substantial expansion eharacteristics and a relatively large quantity of combustion products. Presently preferred combustion mixtures include air or oxygen mixed with acetylene, propane, APACHI gas as manufactured by Air Produets Inc., MAPP gas as manufactured by Dow Chemical Company, or hydrogen. The control device serves to eontrol the characteristics of the gas supplied to the plenum chamber 44. It is desirable in some installations to preheat the combustion mixture. Moreover, depending on the particular material being sprayed, the combustion gases may be adjusted to provide either oxidizing, neutral or reducing atmosphere both within the chamber 37 and beyond the exit thereo~. This ,~ .
enables the chemical composition of the spray coating to be con-trolled such as, for example, con-trolling the carbon content of carbides, iron or the like and, also, compounds such as barium titanate may be sprayed without the usual reduction of oxygen content. In general, the spraying of metals requires a reducing atmosphere, whereas when spraying ceramics, it is desirable to provide an excess of oxygen.
In order to more fully illustrate the nature of the inven-tion, Fig. 4 presents a table indicating the comparative test results, spraying the same material, of a conventional plasma spray gun assembly without shrouding and a plasma spray gun assembly constructed according to the invention, which includes an annularly-shaped wall shroud and an annularly-shaped flame shroud within and adjacent the wall shroud, directed at an angle of about 180 w~th respect -to the axis of the plasma flame.
The wear resistance specified in the table of Fig. 4 was deter-mined according to the test procedure set forth in Addendum -Table I. The test results show a clear superiority of the spray gun assembly of the present invention.
The following example describes the typical operation of the plasma spray ~un assembly.
Example 1 . .
A plasma spray gun assembly similar to that shown in Figs. 1 and 2 was used. ~he bore diameter Dl of the nozzle electrode 12 was 0.25 inches. The inside diame-ter D2 of the wall shroud 34 was 1.50 inches and the inside diameter D3 of the gas burner 42 was 1.15 inches. The distance Ll between the end of the nozzle 12 and the inner end of the gas buxner 42 was 1.70 inches and the distance L2 between the end of the nozzle electrode 12 and the substrate or work piece 11 was 2.75 inches~ The diameter of the nozzle 30 for the powdered coating material was 0.060 inches.
Thirty-six jet orifices 46 having a diameter of 0.023 inches were r ~
employed on a 1.38 inch diameter circle. The plasma gases uti-lized were argon, at a pressure of 100 p.s.i.y. and a flow rate of 90 soc~f~h~ and hydrogen at a pressure of 60 p.sOi.g. at a flow rate of 7 s.c.f.h. The arc current was 700 amperes at 48 volts. The shroud gases employed were air at a pressure of 50 p.s.i.g. at a flow rate of 400 s.c.f.h. mixed with propane at a ;:
pressure of 50 p.s.i.g. at a flow rate of 90 s.c.f.h. The powdered coating material was a coba]t base alloy having a particle size of from about 10 to about 40 microns and a flow .
rate of 6 pounds per hour~ The carrier gas was argon with a flow rate of 7 s.c~f.h. The coatings obtained were substantially superior to those normally obtained with conventional spray guns.
`-~In certain installations, an annular manifold 59, Fig. 3, ~ ;
is mounted on the outer end of the gas burner 42. Cooling water `~
or an inert gas such as, for example, nitrogen or argon is supplied to this manifold through an inlet 61, and annular jPt -~orifice outlet means 60 are provided on the side of the manifold ;:
towards the substrate 11 to provide an annular curtain effect around the plasma flame, as indicated by arrow 62. Not only does the jet spray serve to shield the spray stream, it also allows the spray cone to be controlled and furthermore serves to provide some cooling of the substrate. Similarly, the same manifold may be used with propane to provide a secondary flame shroud around the spray stream and thereby further reduce the oxide content of the coating. In certain installations it is desirable to utilize carbon dioxide for this purpose.
While the embodiment of Figs. 1 and 2 is the presently preferred embodiment, other desirable embodiments of the invention are illustrated in Figs. 5 to 9. Fig~ 5 shows in schematic form ;~
an annular wall shroud 64 with plasma flame or effluent 66 pas-sing longitudinally therethrough along an axis indicated at 68.
',' ' . .
-- . . . - : .;: :: , . .
In this embodiment, an annular flame shroud 70 is directed parallel to the direction of flow of the plasma effluent.
In the embodiment of Fig. 6, the plasma ef~luent 66 passes longitudinally along its axis 68 through an annular wall shroud 72, and an annular flame shroud 74 is directed at an angle having a component extending parallel to the direction of flow of the plasma effluent.
; Referring next to the embodiment of Fig. 7, the plasma `
effluent 66 passes longitudinally along its axis 68 through an ;~ 10 annularly-shaped wall shroud 76, and a portion of the gas for .~:
forming the flame shroud is introduced, as indicated at 78, at an angle of about 180 with respect to the axis 68 of the plasma effluent or flame, and a second portion of the gas for forming the flame shroud is introduced, as indicated at 80, at an angle having a component extending parallel to the direction of flow of the plasma effluent.
In the embodiment of Fig. 8, the plasma effluent 66 ;~
passes longitudinally along its axis 68 through an annular wall shroud 82, and an annular flame shroud 84 IS directed at an an~le having a component extending in a direction opposite to the direction of flow of said plasma effluent.
Fig. 9 shows an embodiment of the invention wherein the plasma effluent 66 passes longitudinally along the axis 58 ;
through an annular wall shroud 86. A portion of the gas for forming the flame shroud is introduced, as indicated at 88, at an angle of about 180 with respect to the axis 68 of the plasma ~, effluent and a second portion of the gas for forming said flame ,. ~ .
~-~ shroud is introduced, as indicated at 90, at an angle having a component extending in a direction opposite to the direction of ' flow of the plasma effluent.
, ,"~ .
,~' .~ ' ., .: ., . . . ,, .. . .... ~ .
Thus, it will be appreciated that the gas for forming the flame shroud may be introduced at one or more inlets and each inlet may be disposed at any angle from about zero to about 180, and may even be normal to the direction of flow :
of the plasma effluent. ' It will thus be seen that the present invention does indeed provide a new and improved plasma spray gun assembly which is superior to conventional spray guns with respect to ;~
deposition efficiency, reduced oxide contents, reduced un-melted particle inclusions, as well as other operative characteristics. ,~
~aving thus described the invention with particular reference to the preferred forms thereof, it will be obvious .
to those skilled in the art to which the invention pertains, after understanding the invention that various changes and modifications may be.made therein without departing from the ~
spirit and scope of the invention, as defined by the claims ~ .
appended hereto.
`;5;1 l ME 2363 ~
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1 ADDENDUM _ rrABLE I
The powders were sprayed under conditions to produce coatings which were tested for abrasion or wear resistance, as follows:
~13 Measure the thickness of the test buttons (including 7 coating) in four places, using a Supermicrometer, and record the 8 readin~s. ~Locate the four points for a suhsequent measurement by placing marks or numbers on the periphery of the ~utton.)
2) ~eîgh each button accurately, using an analytical 11 balance, and record the weight.
12 3) Insert a drive assembly in a drill press spindle.
13 4~ Place a platform scale on the drill press table.
14 Pull the drill press arm (handle) down to a horizontal position ;15 and lock~it in place.
~ ~ ~ i) Raise the drill prsss table until the drive assembly indicates a 11.2~ kg load on the sca]e platform. -18 6~ Unlock the drill press spindle. Hang a weight on the lg press arm, located so as to indicate a 11.25 kg reading on the scale~ Mark ~he point on the arm where this reading is obtained.
21 ~ ~ ~ 7) R~moYe the scale.
228) Raise the spindle and replace the aligning pin with a 253.18 cm~ blanX pin.
249) Place two test huttons on a wear track. Lower the 2~spindle until drive pins enter the drive holes in the buttons.
26Lock in place, with no load on the buttons.
æ7~o3 Start;the drill press. Pour into pan a thoroughly 28mi~xed slurry of alumina abrasive powder (Metco 101) - 270 mesh 2g ~ + 15 micro~s in a slurry of 25 grams of abrasive in 200 cc of light machine oil. ReIease the lock on the spindle so that the 11.25 kg load is applied to the test buttons. Record the starting 32 time.
_13_ q~-2363 .
1~) Allow the test to run 20 minutes.
1 12) Remove the buttons and wash them in solvent. Weight .
2 and measure the thickness and record the readings ~or comparison S l wit he original re~dinqs.
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12 3) Insert a drive assembly in a drill press spindle.
13 4~ Place a platform scale on the drill press table.
14 Pull the drill press arm (handle) down to a horizontal position ;15 and lock~it in place.
~ ~ ~ i) Raise the drill prsss table until the drive assembly indicates a 11.2~ kg load on the sca]e platform. -18 6~ Unlock the drill press spindle. Hang a weight on the lg press arm, located so as to indicate a 11.25 kg reading on the scale~ Mark ~he point on the arm where this reading is obtained.
21 ~ ~ ~ 7) R~moYe the scale.
228) Raise the spindle and replace the aligning pin with a 253.18 cm~ blanX pin.
249) Place two test huttons on a wear track. Lower the 2~spindle until drive pins enter the drive holes in the buttons.
26Lock in place, with no load on the buttons.
æ7~o3 Start;the drill press. Pour into pan a thoroughly 28mi~xed slurry of alumina abrasive powder (Metco 101) - 270 mesh 2g ~ + 15 micro~s in a slurry of 25 grams of abrasive in 200 cc of light machine oil. ReIease the lock on the spindle so that the 11.25 kg load is applied to the test buttons. Record the starting 32 time.
_13_ q~-2363 .
1~) Allow the test to run 20 minutes.
1 12) Remove the buttons and wash them in solvent. Weight .
2 and measure the thickness and record the readings ~or comparison S l wit he original re~dinqs.
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Claims (42)
1. A plasma spray gun assembly for coating substrates comprising, in combination;
a nozzle electrode having a nozzle passage therethrough;
a rear electrode;
means for passing plasma-forming gas through the nozzle electrode;
means for passing an arc-forming current between said electrodes to form a plasma effluent;
means for introducing spray coating material into the plasma effluent;
a wall shroud for said plasma effluent extending from the exit of the nozzle electrode; and means for forming a flame shroud for said plasma effluent at least within the wall shroud.
a nozzle electrode having a nozzle passage therethrough;
a rear electrode;
means for passing plasma-forming gas through the nozzle electrode;
means for passing an arc-forming current between said electrodes to form a plasma effluent;
means for introducing spray coating material into the plasma effluent;
a wall shroud for said plasma effluent extending from the exit of the nozzle electrode; and means for forming a flame shroud for said plasma effluent at least within the wall shroud.
2. A plasma spray gun assembly according to claim 1 wherein said spray coating material is in the form of a powder.
3. A plasma spray gun assembly according to claim 1 wherein said means for forming a flame shroud for said plasma effluent at least within the wall shroud comprises means for directing said flame shroud at an angle of between about 160°
to about 180° with respect to the axis of the plasma effluent.
to about 180° with respect to the axis of the plasma effluent.
4. A plasma spray gun assembly according to claim 1 wherein said means for forming a flame shroud for said plasma effluent at least within the wall shroud comprises means for directing said flame shroud at an angle of about 180° with respect to the axis of the plasma effluent.
5. A plasma spray gun assembly according to claim 4 wherein said means for forming a flame shroud for said plasma effluent at least within the wall shroud comprises burner means disposed adjacent the outlet of the wall shroud.
6. A plasma spray gun assembly according to claim 5 wherein said burner means includes an annular plenum chamber having jet orifice means directed at an angle of about 180° with respect to the axis of the plasma effluent.
7. A plasma spray gun assembly according to claim 6 wherein said burner means further includes combustion gas inlet means that pass longitudinally through said wall shroud.
8. A plasma spray gun assembly according to claim 1 further comprising means for water cooling said wall shroud.
9. A plasma spray gun assembly according to claim 1 wherein said wall shroud is of cylindrical configuration.
10. A plasma spray gun assembly according to claim 2 wherein said means for introducing powdered coating material into the plasma effluent is disposed adjacent the exit of the electrode nozzle.
11. A plasma spray gun assembly according to claim 1 wherein said means for forming a flame shroud for said plasma effluent within the wall shroud includes means for burning a high molec-ular weight combustion mixture.
12. A plasma spray gun assembly according to claim 11 wherein the high molecular weight combustion mixture includes propane.
13. A plasma spray gun assembly according to claim 1 further comprising means for forming an annular curtain effect around the plasma effluent as it leaves the wall shroud and passes towards the substrate.
14. A plasma spray gun assembly according to claim 13 wherein said means for forming an annular curtain effect includes an annular manifold and orifice means mounted adjacent the outer end of said wall shroud.
15. A plasma spray gun assembly according to claim 1 wherein said means for forming a flame shroud for said plasma effluent at least within the wall shroud comprises means for directing said flame shroud at an angle having a component extending parallel to the direction of flow of said plasma effluent.
16. A plasma spray gun assembly according to claim 1 wherein said means for forming a flame shroud for said plasma effluent at least within the wall shroud comprises means for directing said flame shroud at an angle having a component extending in a direction opposite to the direction of flow of said plasma effluent.
17. A plasma spray gun assembly according to claim 6 further comprising second jet orifice means directed at an angle of from about zero degrees to about 180 degrees with respect to the axis of the plasma effluent.
18. A plasma spray gun assembly according to claim 6 further comprising second jet orifice means directed at an angle having a component extending parallel to the direction of flow of said plasma effluent.
19. A plasma spray gun assembly according to claim 6 further comprising second jet orifice means directed at an angle having a component extending in a direction opposite to the direction of flow of said plasma effluent.
20. A plasma spray gun assembly according to claim 1 wherein said wall shroud has a radially-inwardly directed lip portion disposed towards the exit end thereof.
21. A process for plasma flame-spraying coating material onto a substrate, which comprises the steps of:
passing a plasma-forming gas through a nozzle electrode;
passing an arc-forming current between said nozzle electrode and a rear electrode to form a plasma effluent;
introducing coating material into the plasma effluent;
passing the plasma effluent longitudinally through a wall shroud extending from the exit of said nozzle electrode; and forming a flame shroud for said plasma effluent at least within the wall shroud.
passing a plasma-forming gas through a nozzle electrode;
passing an arc-forming current between said nozzle electrode and a rear electrode to form a plasma effluent;
introducing coating material into the plasma effluent;
passing the plasma effluent longitudinally through a wall shroud extending from the exit of said nozzle electrode; and forming a flame shroud for said plasma effluent at least within the wall shroud.
22. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein said coating material is in a powder form.
23. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein said flame shroud is directed at an angle of between about 160° to about 180°
with respect to the axis of the plasma effluent.
with respect to the axis of the plasma effluent.
24. A process for plasma flame-spraying coating material onto a substrate according to claim 23 wherein said flame shroud is directed at an angle of about 180° with respect to the axis of the plasma flame.
25. A process for plasma flame-spraying coating material onto a substrate according to claim 21 further comprising the step of passing cooling water through said wall shroud.
26. A process for plasma flame-spraying coating material onto a substrate according to claim 21 further comprising the step of preheating combustion gas for the flame shroud.
27. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein said coating material is introduced into the plasma effluent adjacent the exit of the electrode nozzle.
28. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein a mixture for forming said flame shroud is a high molecular weight combustion mixture.
29. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein a combustion mixture for forming said flame shroud includes propane.
30. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein a combustion mixture for forming said flame shroud includes acetylene.
31. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein a combustion mixture for forming said flame shroud includes MAPP gas.
32. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein a combustion mixture for forming said flame shroud includes APACHI gas.
33. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein a combustion mixture for forming said flame shroud includes hydrogen.
34. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein said coating material is a fusible powdered metal.
35. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein said coating material is a ceramic material.
36. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein said coating material is a carbide.
37. A process for plasma flame-spraying coating material onto a substrate according to claim 21 further comprising the step of forming a fluid annular curtain around the plasma effluent as it leaves the wall shroud passing towards said substrate.
38. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein said flame shroud is directed at an angle having a component extending parallel to the direction of flow of said plasma effluent.
39. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein said flame shroud is directed at an angle having a component extending in a direction opposite to the direction of flow of said plasma effluent.
40. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein a portion of the mixture for forming said flame shroud is introduced at an angle of about 180° with respect to the axis of the plasma effluent and a second portion of the mixture for forming said flame shroud is introduced at an angle of from about zero degrees to about 180° with respect to the axis of the plasma effluent.
41. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein a portion of the mixture for forming said flame shroud is introduced at an angle of about 180° with respect to the axis of the plasma effluent and a second portion of the mixture for forming said flame shroud is introduced at an angle having a component extending parallel to the direction of flow of said plasma effluent.
42. A process for plasma flame-spraying coating material onto a substrate according to claim 21 wherein a portion of the mixture for forming said flame shroud is introduced at an angle of about 180° with respect to the axis of the plasma effluent and a second portion of the mixture for forming said flame shroud is introduced at an angle having a component ex-tending in a direction opposite to the direction of flow of said plasma effluent.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/791,479 US4121083A (en) | 1977-04-27 | 1977-04-27 | Method and apparatus for plasma flame-spraying coating material onto a substrate |
US791,479 | 2006-04-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1104004A true CA1104004A (en) | 1981-06-30 |
Family
ID=25153863
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA302,053A Expired CA1104004A (en) | 1977-04-27 | 1978-04-26 | Method and apparatus for plasma flame-spraying coating material onto a substrate |
Country Status (7)
Country | Link |
---|---|
US (1) | US4121083A (en) |
JP (1) | JPS53137036A (en) |
CA (1) | CA1104004A (en) |
DE (1) | DE2818304A1 (en) |
FR (1) | FR2389297A1 (en) |
GB (1) | GB1597559A (en) |
IT (1) | IT1102190B (en) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4341941A (en) * | 1979-03-01 | 1982-07-27 | Rikagaku Kenkyusho | Method of operating a plasma generating apparatus |
US4357387A (en) * | 1981-08-20 | 1982-11-02 | Subtex, Inc. | Flame resistant insulating fabric compositions prepared by plasma spraying |
SE8306107D0 (en) * | 1983-11-07 | 1983-11-07 | Skf Steel Eng Ab | TETNINGSANORDNING |
FR2555392B1 (en) * | 1983-11-17 | 1986-08-22 | Air Liquide | PROCESS FOR HEAT TREATMENT, ESPECIALLY CUTTING, WITH A PLASMA JET |
USRE32908E (en) * | 1984-09-27 | 1989-04-18 | Regents Of The University Of Minnesota | Method of utilizing a plasma column |
US4725447A (en) * | 1984-09-27 | 1988-02-16 | Regents Of The University Of Minnesota | Method of utilizing a plasma column |
US4818837A (en) * | 1984-09-27 | 1989-04-04 | Regents Of The University Of Minnesota | Multiple arc plasma device with continuous gas jet |
JPS62500290A (en) * | 1984-09-27 | 1987-02-05 | リ−ジエンツ オブ ザ ユニバ−シイテイ オブ ミネソタ | Multi-arc plasma device producing continuous gas jets |
US4634611A (en) * | 1985-05-31 | 1987-01-06 | Cabot Corporation | Flame spray method and apparatus |
US4806384A (en) * | 1987-05-29 | 1989-02-21 | The United States Of America As Represented By The United States Department Of Energy | Process for forming exoergic structures with the use of a plasma |
US4933241A (en) * | 1987-05-29 | 1990-06-12 | United States Department Of Energy | Processes for forming exoergic structures with the use of a plasma and for producing dense refractory bodies of arbitrary shape therefrom |
US5244727A (en) * | 1988-10-11 | 1993-09-14 | Nichias Corporation | Refractories for use in firing ceramics |
US4964568A (en) * | 1989-01-17 | 1990-10-23 | The Perkin-Elmer Corporation | Shrouded thermal spray gun and method |
US5135166A (en) * | 1991-05-08 | 1992-08-04 | Plasma-Technik Ag | High-velocity thermal spray apparatus |
US5384164A (en) * | 1992-12-09 | 1995-01-24 | Browning; James A. | Flame sprayed coatings of material from solid wire or rods |
US5662266A (en) * | 1995-01-04 | 1997-09-02 | Zurecki; Zbigniew | Process and apparatus for shrouding a turbulent gas jet |
US5707694A (en) * | 1996-05-31 | 1998-01-13 | Caterpillar Inc. | Process for reducing oxygen content in thermally sprayed metal coatings |
US7045172B2 (en) * | 2003-07-31 | 2006-05-16 | Praxair S.T. Technology, Inc. | Method of shielding effluents in spray devices |
US8367963B2 (en) * | 2004-10-29 | 2013-02-05 | United Technologies Corporation | Method and apparatus for microplasma spray coating a portion of a turbine vane in a gas turbine engine |
US7763823B2 (en) * | 2004-10-29 | 2010-07-27 | United Technologies Corporation | Method and apparatus for microplasma spray coating a portion of a compressor blade in a gas turbine engine |
US8367967B2 (en) | 2004-10-29 | 2013-02-05 | United Technologies Corporation | Method and apparatus for repairing thermal barrier coatings |
US20060091117A1 (en) * | 2004-11-04 | 2006-05-04 | United Technologies Corporation | Plasma spray apparatus |
US20060168808A1 (en) * | 2005-02-03 | 2006-08-03 | United Technologies Corporation | Plasma ARC weld repair of IN100 material |
US8931429B2 (en) | 2008-05-05 | 2015-01-13 | United Technologies Corporation | Impingement part cooling |
US9997325B2 (en) | 2008-07-17 | 2018-06-12 | Verity Instruments, Inc. | Electron beam exciter for use in chemical analysis in processing systems |
DE102008050184B4 (en) * | 2008-10-01 | 2011-04-21 | Technische Universität Chemnitz | Method and apparatus for high velocity flame spraying |
US20110121107A1 (en) * | 2009-11-24 | 2011-05-26 | Frederic Gerard Auguste Siffer | Plasma polymerization nozzle |
KR101996433B1 (en) * | 2012-11-13 | 2019-07-05 | 삼성디스플레이 주식회사 | Thin film forming apparatus and the thin film forming method using the same |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE345653C (en) * | 1919-11-25 | 1922-03-27 | Nicolaus Meurer | Device for executing cover layers made of enamel, glass, quartz, hard metal and the like, which are produced by means of spraying onto heat-resistant workpieces and are connected to the latter by welding. like |
US2922869A (en) * | 1958-07-07 | 1960-01-26 | Plasmadyne Corp | Plasma stream apparatus and methods |
US3082314A (en) * | 1959-04-20 | 1963-03-19 | Shin Meiwa Kogyo Kabushiki Kai | Plasma arc torch |
US3312566A (en) * | 1962-08-01 | 1967-04-04 | Giannini Scient Corp | Rod-feed torch apparatus and method |
US3373306A (en) * | 1964-10-27 | 1968-03-12 | Northern Natural Gas Co | Method and apparatus for the control of ionization in a distributed electrical discharge |
US3313908A (en) * | 1966-08-18 | 1967-04-11 | Giannini Scient Corp | Electrical plasma-torch apparatus and method for applying coatings onto substrates |
US3470347A (en) * | 1968-01-16 | 1969-09-30 | Union Carbide Corp | Method for shielding a gas effluent |
US3958097A (en) * | 1974-05-30 | 1976-05-18 | Metco, Inc. | Plasma flame-spraying process employing supersonic gaseous streams |
JPS5349197A (en) * | 1976-10-15 | 1978-05-04 | Hinode Sengiyou Kk | Creping method of polyester fabric |
-
1977
- 1977-04-27 US US05/791,479 patent/US4121083A/en not_active Expired - Lifetime
-
1978
- 1978-04-24 JP JP4919878A patent/JPS53137036A/en active Granted
- 1978-04-25 FR FR7812220A patent/FR2389297A1/en active Granted
- 1978-04-26 IT IT49090/78A patent/IT1102190B/en active
- 1978-04-26 DE DE19782818304 patent/DE2818304A1/en active Granted
- 1978-04-26 CA CA302,053A patent/CA1104004A/en not_active Expired
- 1978-04-26 GB GB16555/78A patent/GB1597559A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE2818304C2 (en) | 1987-12-10 |
DE2818304A1 (en) | 1978-11-16 |
US4121083A (en) | 1978-10-17 |
IT1102190B (en) | 1985-10-07 |
FR2389297A1 (en) | 1978-11-24 |
GB1597559A (en) | 1981-09-09 |
IT7849090A0 (en) | 1978-04-26 |
FR2389297B1 (en) | 1983-11-18 |
JPS53137036A (en) | 1978-11-30 |
JPS6242666B2 (en) | 1987-09-09 |
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