US2834101A - Method of brazing titanium - Google Patents
Method of brazing titanium Download PDFInfo
- Publication number
- US2834101A US2834101A US490143A US49014355A US2834101A US 2834101 A US2834101 A US 2834101A US 490143 A US490143 A US 490143A US 49014355 A US49014355 A US 49014355A US 2834101 A US2834101 A US 2834101A
- Authority
- US
- United States
- Prior art keywords
- titanium
- bath
- plating
- brazing
- parts
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/001—Interlayers, transition pieces for metallurgical bonding of workpieces
- B23K35/005—Interlayers, transition pieces for metallurgical bonding of workpieces at least one of the workpieces being of a refractory metal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
Definitions
- This invention relates to titanium and is particularly directed to a method and means for brazing parts of titanium.
- titanium is used in a broad sense so as to include titanium alloys as well as titanium itself.
- An object of the present invention comprises the provision of a novel and simple method of preventing oxidation of titanium parts while brazing said parts in air at a temperature of at least 1300 F.
- a further object of the invention comprises the provision of a novel and simple method of brazing titanium parts by first plating the surfaces of said parts to be brazed together with a thin layer of iron, or cobalt.
- a still further object of the invention comprises the provision of a novel meth d of plating titanium parts with a protective adherent metal layer prior to bonding said parts together by brazing so that during the brazing operation said layer prevents oxidation of the surfaces being brazed together.
- said parts prior to brazing titanium parts together, for example with a silver base alloy, said parts are electroplated with a thin layer of iron or cobalt.
- this oxide film removing bath (activating bath) is such as to be compatible with the subsequently-used plating bath in that the constituents of the activating bath if introduced in the plating bath produce no undesirable reactions therein.
- the part to be plated and then brazed can be transferred directly from the activating bath to the plating bath without first completely rinsing or otherwise cleaning the part after its removal from the activating bath and before its immersion in the plating bath.
- This pro cedure minimizes the possibility of the part re-oxidizing after it is removed from the activating bath and before it is immersed in the plating bath.
- the part is first degreased and then cleaned in a conventional pickling bath, for example by immersing for five minutes in a solution comprising 20% nitric acid (HNO;,), 2% hydrofluoric acid (HF) and 78% water. After removal from the pickle bath the part is rinsed with cold water. Any oxide film remaining on the part is then removed (by conversion to a chloride film) by immersing Z,83 i,i0i Patented May 13, 1958 "ice
- the plating bath preferably contains fifty ounces of ferrous chloride (Fecl and twenty-five ounces of calcium chloride (CaCl per gallon of water.
- the pH value of the bath is preferably kept within the range of 0.6 to 1.0 by the addition of HCl to the bath.
- the bath is heated to maintain its temperature within the range of -2l0 F.
- said part Before immersing at least the surface of the titanium part to be plated and then brazed in the plating bath, said part is connected to one side of an electric circuit so that when immersed it forms the cathode or negative electrode in the bath and the other side of said circuit is connected to a second electrode or anode in the bath, said second electrode preferably being iron. At least said titanium part surface is then immersed in said plating bath and iron is then electroplated on said immersed titanium part surface. A current density of sixty amperes per square foot has been found satisfactory. Because the electric circuit is connected to the titanium part before it is immersed in the bath no non-electrolytic deposit, which generally has poor adherence, can form on the part.
- an adherent iron coating is plated on said part, said coating having a thickness range which may extend from 0.0001 to 0.001 inch and preferably is limited to 0.0004 to 0.0006 inch.
- the iron plated titanium part is washed, dried and covered with a suitable slushing oil to prevent rusting.
- the calcium chloride in the plating bath is inert, its function simply being to provide more chloride ions. If the pH value of the plating bath gets too high the iron plate becomes brittle. There is no lower limit to the usable range of pH values for the plating bath.
- the HCl on the titanium part after its removal from the HCl (activating) bath can be carried over directly into the plating bath whereby there is no need for completely cleaning the titanium part, for example by rinsing, to remove all the I-ICl before the part is immersed in the plating bath. This minimizes any danger of an oxide film reforming on the titanium part as the part is being transferred from the HCl (activating bath) to the plating bath.
- the parts to be bonded together After at least the surfaces of the titanium parts to be bonded together have been plated with iron, as described, said parts are brazed together in air, for example with a silver base alloy at a temperature of about 1300 F. Because the parts have been plated with iron the silver brazing procedure can be and is quite conventional.
- the iron plate on the titanium part must be thick enough to prevent contamination or oxidation of the titanium by the air during the brazing operation but not so thick that the strength of the resulting brazed joint depends on the strength of the iron plate.
- a thickness of iron plate or coating of 0.0004 to 0.0006 inch has been found highly satisfactory for this purpose.
- a coating of iron is suitable for this purpose because it does not melt at the brazing temperature, because its for t is pu no en ete ab y on in Instead of plating the titanium parts to be brazed with iron they may be plated with cobalt. For this purpose the titanium part to be plated is first degreased and cleaned.
- the part is then immereed in an act iyati ng a h t re a y ox de urfi m- ,A aitah e 1 th v A b yo sf a hydrofluoric acid solution .of whi 38% by weight is hydrofluoric acid with the bil hll water, 9-1079 by o m o a sh ir ic a i s ut on conta n n b weight sulfuric acid with the balance water, and 90%).1
- the part is immersed in this bath at room temperature for a period of 15 minutes.
- the titanium part is removed frpm the actiya ting o r deoxidizing bath and immersed in the eobalt plating bath without any intervening washing or rinsing of the part.
- the cobalt plating bath preferably contains 504 grams per liter oficobalt sulfate (C050 45 grams per liter of boric acid (H 30 and 14 grams per liter of sodium fluoride e I d i io h r lu d is a ded o dj t the pn ,of the bath to a range of 1.0-3.0.
- the titanium part Before immersion in the plating bath, the titanium part is connected to one side of an electric circuit so that when immersed it forms the cathode or negative electrode inthe bath and the other side of the electric circuit is connected to a second electrode or anode in the bath, said second electrode preferably being made of eobalt.
- At least the surface of the titanium part to be plated is ir mme sed in t e plat n t nd oba t is en electroplated on said immersed titanium surface.
- the bath is agitated and kept at a temperature of 140l0 F.
- a relatively high current de y o abo t 80 amp rs P r s u re f et is used i iir ly t r a short period f t me a t en a lo er cur n density for rfemair der of the plating period. After the plating operation the part is rinsed and dried.
- a hi h i it al den o e p t n cu rent is u 9 hat a hp ste o tin coba s q i k pla ed over the titanium part.
- the thick: ness range of the cobalt plate is limited to 0.0002 to 0.0995 i Phr 995 l8 i n h s an e ein h gh y f P Q 9 r s sh 'spnteminati n or ox dat on of' he t n u Par s wt rrsth sslasaqsn r e as 9f th in Platin t 16 h 'hi w shed 9;
- the titanium parts to be bonded together are thus plated with cobalt, said parts are brazed together in air, for example with a silver base alloy at a temperature of a ou 1300" F- in a ord nc with conventional z ng i hsl oba pla an platns pr eedhre ha c rta n a an a er ro n th t a tivat ng b t attacks the ti zrrr im i a l s x e t the asti at sand pl.
- t n ba s function at lower temperatures and the cohalt plhte has superior corrosion resistance.
- the iron plate can more readily be cleaned by ordinary fluxes.
Description
United States Patent'O METHOD or BRAZING TITANIUM Willard M. Boam, Fairlawn, N. 3., Isidore Friedman, Brooklyn, Henry Paige, New York, and Leo Souzis, Brooklyn, N. Y., and Kurt Strater, Paterson, N. L, assignors to Curtiss-Wright Corporation, a corporation of Delaware No Drawing. Application February 23, 1955 Serial No. 490,143
1 Claim. (Cl. 29-488) This invention relates to titanium and is particularly directed to a method and means for brazing parts of titanium. As used herein the word titanium is used in a broad sense so as to include titanium alloys as well as titanium itself.
In brazing parts of titanium it is necessary that steps be taken to prevent oxidation of the titanium at the surfaces being brazed together. This can be accomplished by brazing in an inert atmosphere. In general however such a procedure is not commercially feasible for large scale production. Titanium parts to be brazed can also be coated with special fluxes to prevent oxidation during the brazing operation. However, fluxes for brazing titanium in air have not been entirely satisfactory.
An object of the present invention comprises the provision of a novel and simple method of preventing oxidation of titanium parts while brazing said parts in air at a temperature of at least 1300 F. A further object of the invention comprises the provision of a novel and simple method of brazing titanium parts by first plating the surfaces of said parts to be brazed together with a thin layer of iron, or cobalt. A still further object of the invention comprises the provision of a novel meth d of plating titanium parts with a protective adherent metal layer prior to bonding said parts together by brazing so that during the brazing operation said layer prevents oxidation of the surfaces being brazed together.
In accordance with the present invention, prior to brazing titanium parts together, for example with a silver base alloy, said parts are electroplated with a thin layer of iron or cobalt.
In order to obtain an adherent electroplated deposit of iron or cobalt on titanium it is first necessary that the surface to be plated be free of any oxide film. This is accomplished by immersing at least the surface of the titanium part, to be plated and then brazed, in a bath for removing any oxide from said surface. In accordance with the present invention this oxide film removing bath (activating bath) is such as to be compatible with the subsequently-used plating bath in that the constituents of the activating bath if introduced in the plating bath produce no undesirable reactions therein. Accordingly, the part to be plated and then brazed can be transferred directly from the activating bath to the plating bath without first completely rinsing or otherwise cleaning the part after its removal from the activating bath and before its immersion in the plating bath. This pro cedure minimizes the possibility of the part re-oxidizing after it is removed from the activating bath and before it is immersed in the plating bath.
In preparing the titanium part for iron plating the part is first degreased and then cleaned in a conventional pickling bath, for example by immersing for five minutes in a solution comprising 20% nitric acid (HNO;,), 2% hydrofluoric acid (HF) and 78% water. After removal from the pickle bath the part is rinsed with cold water. Any oxide film remaining on the part is then removed (by conversion to a chloride film) by immersing Z,83 i,i0i Patented May 13, 1958 "ice The plating bath preferably contains fifty ounces of ferrous chloride (Fecl and twenty-five ounces of calcium chloride (CaCl per gallon of water. The pH value of the bath is preferably kept within the range of 0.6 to 1.0 by the addition of HCl to the bath. The bath is heated to maintain its temperature within the range of -2l0 F.
Before immersing at least the surface of the titanium part to be plated and then brazed in the plating bath, said part is connected to one side of an electric circuit so that when immersed it forms the cathode or negative electrode in the bath and the other side of said circuit is connected to a second electrode or anode in the bath, said second electrode preferably being iron. At least said titanium part surface is then immersed in said plating bath and iron is then electroplated on said immersed titanium part surface. A current density of sixty amperes per square foot has been found satisfactory. Because the electric circuit is connected to the titanium part before it is immersed in the bath no non-electrolytic deposit, which generally has poor adherence, can form on the part.
For the purpose of subsequently brazing the titanium part an adherent iron coating is plated on said part, said coating having a thickness range which may extend from 0.0001 to 0.001 inch and preferably is limited to 0.0004 to 0.0006 inch.
After iron plating, the iron plated titanium part is washed, dried and covered with a suitable slushing oil to prevent rusting. r
The calcium chloride in the plating bath is inert, its function simply being to provide more chloride ions. If the pH value of the plating bath gets too high the iron plate becomes brittle. There is no lower limit to the usable range of pH values for the plating bath.
With this de-oxidizing and plating procedure the HCl on the titanium part after its removal from the HCl (activating) bath can be carried over directly into the plating bath whereby there is no need for completely cleaning the titanium part, for example by rinsing, to remove all the I-ICl before the part is immersed in the plating bath. This minimizes any danger of an oxide film reforming on the titanium part as the part is being transferred from the HCl (activating bath) to the plating bath.
After at least the surfaces of the titanium parts to be bonded together have been plated with iron, as described, said parts are brazed together in air, for example with a silver base alloy at a temperature of about 1300 F. Because the parts have been plated with iron the silver brazing procedure can be and is quite conventional.
The iron plate on the titanium part must be thick enough to prevent contamination or oxidation of the titanium by the air during the brazing operation but not so thick that the strength of the resulting brazed joint depends on the strength of the iron plate. A thickness of iron plate or coating of 0.0004 to 0.0006 inch has been found highly satisfactory for this purpose.
A coating of iron is suitable for this purpose because it does not melt at the brazing temperature, because its for t is pu no en ete ab y on in Instead of plating the titanium parts to be brazed with iron they may be plated with cobalt. For this purpose the titanium part to be plated is first degreased and cleaned. The part is then immereed in an act iyati ng a h t re a y ox de urfi m- ,A aitah e 1 th v A b yo sf a hydrofluoric acid solution .of whi 38% by weight is hydrofluoric acid with the bil hll water, 9-1079 by o m o a sh ir ic a i s ut on conta n n b weight sulfuric acid with the balance water, and 90%).1
percent water. The part is immersed in this bath at room temperature for a period of 15 minutes.
The titanium part is removed frpm the actiya ting o r deoxidizing bath and immersed in the eobalt plating bath without any intervening washing or rinsing of the part. The cobalt plating bath preferably contains 504 grams per liter oficobalt sulfate (C050 45 grams per liter of boric acid (H 30 and 14 grams per liter of sodium fluoride e I d i io h r lu d is a ded o dj t the pn ,of the bath to a range of 1.0-3.0.
Before immersion in the plating bath, the titanium part is connected to one side of an electric circuit so that when immersed it forms the cathode or negative electrode inthe bath and the other side of the electric circuit is connected to a second electrode or anode in the bath, said second electrode preferably being made of eobalt. At least the surface of the titanium part to be plated is ir mme sed in t e plat n t nd oba t is en electroplated on said immersed titanium surface. During the plating operation the bath is agitated and kept at a temperature of 140l0 F. A relatively high current de y o abo t 80 amp rs P r s u re f et is used i iir ly t r a short period f t me a t en a lo er cur n density for rfemair der of the plating period. After the plating operation the part is rinsed and dried.
A hi h i it al den o e p t n cu rent is u 9 hat a hp ste o tin coba s q i k pla ed over the titanium part. The lower final current density s. u e? so that th sphah l t i 9 m r vnit m' th f o he Pur ose o r s a ept h az ne'thf ,ti- 41 8 P rt itl 9b l P1a F m h ve a hick tens of 0.0001 to 0.001 inch. Preferably, however, the thick: ness range of the cobalt plate is limited to 0.0002 to 0.0995 i Phr 995 l8 i n h s an e ein h gh y f P Q 9 r s sh 'spnteminati n or ox dat on of' he t n u Par s wt rrsth sslasaqsn r e as 9f th in Platin t 16 h 'hi w shed 9;
- sh iqu 4 activating bath and prior to its immersion in the plating bath since all the constituents of the activating bath are also present in the palting bath.
After the titanium parts to be bonded together are thus plated with cobalt, said parts are brazed together in air, for example with a silver base alloy at a temperature of a ou 1300" F- in a ord nc with conventional z ng i hsl oba pla an platns pr eedhre ha c rta n a an a er ro n th t a tivat ng b t attacks the ti zrrr im i a l s x e t the asti at sand pl. t n ba s function at lower temperatures and the cohalt plhte has superior corrosion resistance. On the other hand the iron plate can more readily be cleaned by ordinary fluxes.
While we have described our invention in detal in its present preferred embodiment, it be obvious to those skilled in the art, after understanding our invention, that ari u e a o fi on may h made here without departing from the spirit .or scope thereof. We ai n he ppend d claim t s e .allsuh mod fi ations- We claim as our invention:
The method of bonding together two parts in which at least one of said parts is of titanium; said method comprising the steps of immersing at least the surface of said one pa t to e nded to t e othe part in a ba h of boili hy o c cid o at l as humm r; while still wet with said hydrochloric acid, connecting said part to the negative side of an electric circuit; after making I said electric circuit connection and while still wet with said hydrochloric acid, immersing at least said surface of the'part in a ferrous chloride bath; while immersed in a d att r b t e plat a a r of iron ha in a thickness of 0.0004 to 0.0006 inch on at least said surface; and th n br n a p t tog her a a t mp ra u e of a leas 30 F- References it n t the of hi pa ent UN TED STAT15 PAIENLS
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US490143A US2834101A (en) | 1955-02-23 | 1955-02-23 | Method of brazing titanium |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US490143A US2834101A (en) | 1955-02-23 | 1955-02-23 | Method of brazing titanium |
Publications (1)
Publication Number | Publication Date |
---|---|
US2834101A true US2834101A (en) | 1958-05-13 |
Family
ID=23946792
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US490143A Expired - Lifetime US2834101A (en) | 1955-02-23 | 1955-02-23 | Method of brazing titanium |
Country Status (1)
Country | Link |
---|---|
US (1) | US2834101A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2987453A (en) * | 1959-04-14 | 1961-06-06 | Harshaw Chem Corp | Method of electrodepositing chromium |
US3006827A (en) * | 1959-01-06 | 1961-10-31 | United Aircraft Corp | Method of pickling titanium and compositions used therein |
US3073269A (en) * | 1957-12-24 | 1963-01-15 | Gen Electric | Metallic brazing mixture |
US3148038A (en) * | 1958-05-27 | 1964-09-08 | Westinghouse Electric Corp | Bonding of metal members |
US3188720A (en) * | 1965-06-15 | Method of sealing and joining and articles made thereby | ||
US3282809A (en) * | 1962-11-07 | 1966-11-01 | Clevite Corp | Iron coating for refractory metal |
US3412000A (en) * | 1965-04-14 | 1968-11-19 | M & T Chemicals Inc | Cathodic protection of titanium surfaces |
US5354623A (en) * | 1991-05-21 | 1994-10-11 | Cook Incorporated | Joint, a laminate, and a method of preparing a nickel-titanium alloy member surface for bonding to another layer of metal |
US6149051A (en) * | 1997-08-07 | 2000-11-21 | Alliedsignal Inc. | Braze titanium |
US20050156014A1 (en) * | 2002-08-09 | 2005-07-21 | Korea Institute Of Science And Technology | Clad sheets for corrosion resistance and fabricating method thereof |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB446439A (en) * | 1933-11-23 | 1936-04-30 | Percy Albert Ernest Armstrong | Improvements in and relating to the manufacture of composite metal bodies |
US2123384A (en) * | 1936-04-07 | 1938-07-12 | American Brass Co | Copper base alloy article for brazing and method of preparing it |
US2145651A (en) * | 1935-03-11 | 1939-01-31 | Edward T O Brien | Composite article and method of making the same |
GB592733A (en) * | 1945-05-30 | 1947-09-26 | Standard Telephones Cables Ltd | Improvements in or relating to methods of soldering metal details |
US2713196A (en) * | 1953-03-17 | 1955-07-19 | Chicago Bridge & Iron Co | Method for cladding and product resulting therefrom |
US2770033A (en) * | 1951-06-14 | 1956-11-13 | Machlett Lab Inc | Method of soldering a thin beryllium member to a metal part |
-
1955
- 1955-02-23 US US490143A patent/US2834101A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB446439A (en) * | 1933-11-23 | 1936-04-30 | Percy Albert Ernest Armstrong | Improvements in and relating to the manufacture of composite metal bodies |
US2145651A (en) * | 1935-03-11 | 1939-01-31 | Edward T O Brien | Composite article and method of making the same |
US2123384A (en) * | 1936-04-07 | 1938-07-12 | American Brass Co | Copper base alloy article for brazing and method of preparing it |
GB592733A (en) * | 1945-05-30 | 1947-09-26 | Standard Telephones Cables Ltd | Improvements in or relating to methods of soldering metal details |
US2770033A (en) * | 1951-06-14 | 1956-11-13 | Machlett Lab Inc | Method of soldering a thin beryllium member to a metal part |
US2713196A (en) * | 1953-03-17 | 1955-07-19 | Chicago Bridge & Iron Co | Method for cladding and product resulting therefrom |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3188720A (en) * | 1965-06-15 | Method of sealing and joining and articles made thereby | ||
US3073269A (en) * | 1957-12-24 | 1963-01-15 | Gen Electric | Metallic brazing mixture |
US3148038A (en) * | 1958-05-27 | 1964-09-08 | Westinghouse Electric Corp | Bonding of metal members |
US3006827A (en) * | 1959-01-06 | 1961-10-31 | United Aircraft Corp | Method of pickling titanium and compositions used therein |
US2987453A (en) * | 1959-04-14 | 1961-06-06 | Harshaw Chem Corp | Method of electrodepositing chromium |
US3282809A (en) * | 1962-11-07 | 1966-11-01 | Clevite Corp | Iron coating for refractory metal |
US3412000A (en) * | 1965-04-14 | 1968-11-19 | M & T Chemicals Inc | Cathodic protection of titanium surfaces |
US5354623A (en) * | 1991-05-21 | 1994-10-11 | Cook Incorporated | Joint, a laminate, and a method of preparing a nickel-titanium alloy member surface for bonding to another layer of metal |
US6149051A (en) * | 1997-08-07 | 2000-11-21 | Alliedsignal Inc. | Braze titanium |
US20050156014A1 (en) * | 2002-08-09 | 2005-07-21 | Korea Institute Of Science And Technology | Clad sheets for corrosion resistance and fabricating method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2983634A (en) | Chemical nickel plating of magnesium and its alloys | |
US4416739A (en) | Electroplating of titanium and titanium base alloys | |
US3666529A (en) | Method of conditioning aluminous surfaces for the reception of electroless nickel plating | |
US5246565A (en) | High adherence copper plating process | |
US3147547A (en) | Coating refractory metals | |
US2834101A (en) | Method of brazing titanium | |
US2829091A (en) | Method for electroplating titanium | |
US2541083A (en) | Electroplating on aluminum | |
US1971761A (en) | Protection of metals | |
US3989606A (en) | Metal plating on aluminum | |
US2457059A (en) | Method for bonding a nickel electrodeposit to a nickel surface | |
US2748066A (en) | Process of enameling steel | |
US2078868A (en) | Electroplating process | |
US2894885A (en) | Method of applying copper coatings to uranium | |
US3065154A (en) | Method of plating chromium and the like to titanium, its alloys, and the like | |
US2970090A (en) | Plating nickel on aluminum | |
US2662054A (en) | Method of electrodepositing chromium directly on aluminum | |
US2975073A (en) | Corrosion resistance of electroless nickel plate | |
US4285782A (en) | Method for providing uranium with a protective copper coating | |
US2938841A (en) | Preparation of zirconium for cold working | |
US3505181A (en) | Treatment of titanium surfaces | |
US2856333A (en) | Electroplating | |
US2801960A (en) | Gold plating process | |
US2442195A (en) | Cleaning and electroplating process | |
US2729601A (en) | Electroplating on beryllium |