new surface treatments for titanium · 2018. 4. 14. · solidified metal in the top of figure 2....

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NEW SURFACE TREATMENTS FOR TITANIUM Robert H. Shoemaker, President Kolene Corporation Detroit, Michigan An objective for this paper is to examine and evaluate the present methods of removing surface contamination from titanium in light of future high production re- quirements. Mass construction of the F-15, F-14 and B-1 aircraft, along with other anticipated 60% to 80% titanium structures will require automated processing. The second part of this paper is concerned with the removal of the oxygen-rich alpha case resulting from elevated temperature treatment of titanium in oxidizing atmosphere. The necessity for complete cleaning prior to chemical milling is shown graphi- cally. The etched surface condition developed in improperly cleaned titanium is illustrated. Condi- tioning and treatment cycles prior to effective gauge removal are tabulated. The final phase of surface treatment discussed is the most recent development. A liquid nitriding bath imparts a 0.001" (0.025 mm) to 0.002 (0.051 mm) wear resistant surface on titanium alloys. Treatment time is two hours and effectively overcomes the gall and wear problems characteristic of titanium. Photomicrographs, hardness traverse curves and profilometer wear patterns substantiate the advantages claimed for the nitriding process. 2501

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Page 1: NEW SURFACE TREATMENTS FOR TITANIUM · 2018. 4. 14. · solidified metal in the top of Figure 2. Forged tur bine blades and extruded shapes require the same pro cessing because of

NEW SURFACE TREATMENTS

FOR TITANIUM

Robert H. Shoemaker, President

Kolene Corporation Detroit, Michigan

An objective for this paper is to examine and evaluate the present methods of removing surface contamination from titanium in light of future high production re­quirements. Mass construction of the F-15, F-14 and B-1 aircraft, along with other anticipated 60% to 80% titanium structures will require automated processing. The second part of this paper is concerned with the removal of the oxygen-rich alpha case resulting from elevated temperature treatment of titanium in oxidizing atmosphere. The necessity for complete cleaning prior to chemical milling is shown graphi­cally. The etched surface condition developed in improperly cleaned titanium is illustrated. Condi­tioning and treatment cycles prior to effective gauge removal are tabulated. The final phase of surface treatment discussed is the most recent development. A liquid nitriding bath imparts a 0.001" (0.025 mm) to 0.002 (0.051 mm) wear resistant surface on titanium alloys. Treatment time is two hours and effectively overcomes the gall and wear problems characteristic of titanium. Photomicrographs, hardness traverse curves and profilometer wear patterns substantiate the advantages claimed for the nitriding process.

2501

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2502 R. H. SHOEMAKER

Titanium Cleaning

Perfecting titanium heat treatment hot forming techni­ques to produce complex structures required for F-14, F-15 and B-1 aircraft has generated many unforeseen problems. A primary and intricate one is the cleaning and removal of elevated temperature oxides, protective coatings and lubricant residues at intermediate steps.

Each of the contaminants shown in Table I can occur on the surface of finished products. Titanium scales a­lone in alloys such as Ti 6Al-6V-2Sn are sufficient to test any cleaning process. Glassy silicate residues, while furnishing barrier films, also tend to enhance the cleaning problems. Incorporation of MoS2 and C, two chemically resistant materials capable of bonding to metal under pressure, have also increased cleaning demands.

Hot Formed Titanium Scales

Standard procedure for hot forming titanium involves precoating with a silicate type protective coating. These coatings are uniform and continuous up to 1500°F. (816°C) Beyond this temperature spherodizing and voids can occur. Glass type coatings are subject to brittle fracture under moving load conditions.

The graphite molybdenum disulfide lubricants are gener­ally applied over the heat resistant coatings. They are more porous than the silicate type but do give some high temperature protection. Under temperature and load, binders are carbonized but the graphite and molyb­denum pigments follow the forming operation.

Effective cleaning can be accomplished rapidly by solu­tion of the oxide and silicate, with suspension of the MoS2 and C pigments.

Approaches to Titanium Cleaning

There are several choices available to clean hot formed titanium surfaces. Selection is based on the require­ments placed on the finished parts. Mechanical finish­ing, such as shot blasting, is the most rapid when con­trasted with chemical cleaning. The limitations on this process are shown in Table II.

To assume from examining this table that mechanical treatments have little place in a titanium cleaning operation would be a fallacy. Many of these factors

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NEW SURFACE TREATMENTS FOR TITANIUM 2503

increase directly with the energy of cleaning and are negligible where mechanical precede chemical methods.

Various combinations of oxidizing compounds, chelates and caustic are available in water solutions for com­plexing and removing titanium scales. The chief dis­advantages are their inability to dissolve all types of soils and the rather slow speed of reaction. Heat and pressure formed glass and carbon residues are quite re­sistant to the action of these compounds resulting in the retention of minute scale areas on the finished surface. These chemical solutions are adequate for treating certain titanium scales if sufficient process­ing time is available. Manual finishing may be re­quired in the inspection area. Chelated compounds can also be used in secondary cleaning operations to re­place acid baths.

Molten salt baths are ideally suited for meeting the requirements for high volume cleaning systems. At the elevated temperatures employed, reactions are almost instantaneous. Characteristics of molten salt b~ths that qualify them as complete metal cleaners are shown in Table III.

Molten cleaning salt temperatures may vary between a low of 400°F. (204°C) and a high of 850°F. (454°C). The former is preferable for fabricated structures and thin sheets as shown in Figure 1. Low temperature salts are also used in the mill cleaning operations shown in Table IV.

Heavy torch cut titanium sections require an 850°F. (454°C) molten salt to remove the combined oxide and solidified metal in the top of Figure 2. Forged tur­bine blades and extruded shapes require the same pro­cessing because of the ceramic-metal complexes devel­oped.

Salt Bath Reactions

Molten salt reactions with the soils in Table I are identical with those expected from a standard chemical approach. The metal rich oxides are reacted to form the more soluble gas rich compounds or neutralization products as shown:

(1) 2MO + 2AO +2NaN03 = M203 + A203 + 2NaN02

(2) M203 + 2NaOH = Na2M204 + H20

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2504 R. H. SHOEMAKER

Table I Nature of Contaminants on Hot Worked Surfaces

Type

1. Titanium & alloy oxides

2. Organic

3. Sintered ceramic

4. Chemical complexes

Formula Source

MO Hot work and heat treat scales

C Free graphite lubricants and binders

Si02 Protective coatings

Special pigmented lubricants

Table II Limitations on Mechanical Cleaning Systems

1. Inability to effectively clean internal sections and shielded areas.

2. Deformation of formed parts.

3. Compressive stresses developed at surface.

4. Surface contamination with corrosive material.

Table III Characteristics of Molten Salt Baths

1. Excellent solvency or fusion properties with metal oxides, glass and carbonaceous residues.

2. Wetting and penetration of discontinuities at metal-oxide interface.

3. Strong oxidizing potential to convert metal rich oxides to more soluble gas rich compounds.

4. Expansion differential promoting separation between oxide and base metal in direct proportion to salt base temperature.

5. Minimum salt-metal reaction after oxide complexing and removal.

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NEW SURFACE TREATMENTS FOR TITANIUM 2505

Figure 1 Titanium Sheet Descaling in 400°F. (204°C) Molten Salt Bath.

Figure 2 Torch Cut Titanium Sections.

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2506 R. H. SHOEMAKER

Graphite and carbonaceous lubricant residues can be chemically oxidized to destruction or assimilated and removed as sludge.

(3) c + 2NaN03 + 2NaOH = Na2C03 + 2NaN02 + H20

(4) NaN03 + 0.502 = NaN03

Ceramic residues are attacked by the alkaline base to yield water soluble silicates.

Pigmented lubricant residues may, if inert to the molten salt, be removed as sludge. Reactive compounds are chemically attacked as shown:

(6) MoS2 + 6NaOH + 9NaN03 = Na2Mo04 + 2Na2S04 + 9NaN02 + 3H20

Titanium Pickling

The pickling operations following molten salt condi­tioning can be better evaluated by considering the com­plete cleaning cycle involving a 400°F. (204°C) molten salt as shown in Table V.

The chemistry of molten salt conditioning which pro­duces potassium titanates, KxTiyOz, on the surface per­mits the major pickling action to take place in the sulfuric acid. Surface damage can thus be prevented with good inspection practice prior to nitric-hydro­fluoric pickling, since the sulfuric acid is much less reactive with titanium as shown in Figure 3. Unaffected oxide remaining can be recycled through the salt and removed before the final pickle.

Hot 35% sulfuric acid has been determined to have the maximum effect on conditioned oxides. The concentra­tion of nitric and hydrofluoric acid is not as import­ant as the 10 to 1 ratio. The excess nitric acid pre­vents the generation and absorption of free hydrogen, Equation 7, by the oxidation reaction in Equation 8.

(7) 2Ti + 6HF = 2TiF3 + 3H2

(8) 3Ti + 4HN03 + 12HF = 3TiF4 + 4NO + 8H20

Experimental work is continuing to effect the complete removal of titanium scales without the use of acids. Molten salt conditioning followed by treatment in

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NEW SURFACE TREATMENTS FOR TITANIUM 2507

chelated alkaline solutions continues to show promise.

Surf ace Removal

In addition to high reaction rates, salt baths are at­tractive because of the chemically clean surfaces ob­tainable. In titanium processing this condition pre­vents scrap losses resulting from subsequent acid treatments to remove contaminated surface. Even 0.002" (0.051 mm) alpha case removal in strong acid can develop poor surfaces, Figure 4, when pre-cleaning is incomplete.

The acid solutions, Table VI, used to effect removal of the oxygen contaminated layer are generally mixtures of hydrofluoric, nitric and acetic acids with wetting agents and inhibitors. These solutions do tend to level and remove imperfections from clean surfaces by selec­tive attack on hills and valleys. However, even in­hibited solutions will differentiate between scale and base metal creating a reverse effect as shown in Fig­ure 4, emphasizing the necessity for chemically clean surfaces.

Experimental investigations continue in the area of electrolytic low acid etching. The advantages expected are more uniformity since metal removal is a function of current density. It is relatively independent of acid concentration. Also the high hydrogen levels ex­perienced with strong acid solutions under certain conditions are lacking in the electrolytic processes.

Surface Treatments for Drawing

More recently the surface from molten oxidizing salt baths has been used in the production forming of titan­ium. The ~se of salt baths for this purpose originated during the early experiments with beta III fastener stock. It was found that the potassium titanate formed on the surface of the metal during processing provided an excellent base for drawing lubricants. The compound not only served the purpose of lubricant retention but actually furnished the pigmentation needed to prevent metal to metal contact. For maximum uniformity the annealed wire was cleaned in molten salt, and acid etched for alpha case removal. The cleaned wire was then recycled through the salt bath, water rinsed and redrawn, or shipped to the fastener manufacturer with the coating intact.

The titanium surface resulting from molten oxidizing salt treatment is shown in Figure 5. McDonnell Douglas

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2508 R. H. SHOEMAKER

.006" 1--------;1--------1------~~

• 005" t--------1-------+------+-1 Ti 6Al-4V

.004"

.002"

NO .GAUGE LOSS .001" ~--,,C---..+--AFTER 160 MINUTES AT 140F

IN 10% H2S04 , 1% CuS04

MINUTES 60 120 180

Figure 3 Comparison of Nitric-Hydrofluoric and Sulfuric Acid Pickles with Respect to Titanium Gauge Loss.

Figure 4 Acid Etch Pattern Resulting from Improperly Cleaned Surfaces.

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NEW SURFACE TREATMENTS FOR TITANIUM

Table IV Origin of Titanium Scales Cleaned in 400°F. (204°C) Salt Bath

Operation

Stress relieving or aging

Annealing or creep flattening

Solution treating

Hot working

Temperature Range

900°F - 1300°F. (482°C - 704°C)

1200°F - 1650°F (649°C - 899°C)

1400°F - 1B00°F (760°C - 982°C)

800°F - 2100°F (427°C - 1149°C

Table V Typical 400°F. (204°C) Molten Salt Descaling Cycle

Cycle

Condition in Molten Salt

Rinse

Acid Pickle

Rinse

Acid Pickle

Rinse

Time

3-5 minutes

1 minute

3 minutes

1 minute

1 minute

1 minute

Temperature

400°F - 425°F (204°C - 218°C)

Cold Water

35% H2S04 at 150°F (65°C)

Cold Water

10 parts HN03 + 1 part HF at 120°F (49°C)

Hot Water

Table VI Chemical Solution for Alpha Case Removal

20%

74%

6%

0.4 oz/100 gallons

Water

Nitric Acid

Hydrofluoric Acid

Wetting Agent (FC95 by 3M)

2509

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2510 R. H. SHOEMAKER

is presently processing titanium sheet in this fashion to form curved sections of aircraft ductwork. The cleaned titanium is treated in molten salt, water rinsed and coated with Everlube T-50 prior to forming.

Production Systems for Titanium Processing

All of the surface treatments described can be suitably programmed for large scale production processing. Re­ferring to Table V, the time cycles involved in molten salt descaling are sufficiently short to allow auto­mated work handling systems. Figure 6 illustrates the cycling for high volume turbine blade cleaning. Work baskets travel from station to station by the Meca-matic hoist system. Dwell time in salt baths, acid and chemi­cal treatment tanks is controlled by operator input. Systems such as this are a basic requirement where large numbers of titanium sections must be processed. The efficiency of the overall operation is still dependent upon the performance of each individual treatment.

High volume titanium cleaning for the F-14 aircraft is being done in the equipment shown in Figure 7. This salt pot is a part of a modern cleaning line at the Grumman Aircraft Engineering Corporation. Although the system is not automated, thorough chemical cleaning is obtained through the efficient use of molten salt con­ditioning. Required acid tanks and rinses complete the line which conditions very large titanium sections. Continual control of all process chemicals is part of the quality assurance program.

Surface Hardening by Salt Bath Treatment

Molten salt baths are also under consideration for their ability to affect titanium surfaces through conversion, plating, and diffusion processes. The intent of these treatments is to enhance the wear properties of titan­ium surfaces while retaining their excellent corrosion and strength characteristics.

The recently developed Tiduran process produces a true diffusion effect to a depth of 0.002" (0.051 mm), Fig­ure 8. Optimum treating time is two hours at 1480°F. (804°C) in a cyanide based molten salt.

The photomicrograph shown in Figure 8 indicates that some type of controlled alpha case structure is being formed. The surface does, however, lack the extreme brittleness, non-uniformity and cracking tendency of an oxygen stabilized surface. Also the chemistry of the

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NEW SURFACE TREATMENTS FOR TITANIUM 2511

Figure 5 Potassium Titanate Surface Prepared for Lubricant Application.

. ,,,,----p--_ -B-- Monorail

( Automatic hoist Load/Unload

I

I ~ Salt bath ~~:er Sulfuric \ .-. -. ------::_~:=fD JCJl

'---- -ir~~ : ~-:b bd

--BBBEJ& . Hot Cold Nitric-HF Nitric-HF Nitric \

n., - I

Cold

) ,__,/

[nWJ]--= ~:!ffilll!!illi~ MOLTEN SALT AUTOMATIC DESCALING SYSTEM

Figure 6 Flow Sheet of Automated Salt Bath Cleaning System.

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2512

Figure 7

Figure 8

R. H. SHOEMAKER

Salt Bath Equipment for Processing Large Titanium Sections for F-14 Aircraft.

--~..-.• ..... -- ,,.•.: Tl DURAN· ·.TREATED

·Ti 6Al·4V

500x

Diffusion Effect From Two Hour Tiduran Treatment.

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NEW SURFACE TREATMENTS FOR TITANIUM 2513

salt decomposition involving CN- and CNo- would suggest the presence of other alpha stabilizing interstitials such as carbon and nitrogen. This structure has been substantiated by chemical analysis as shown in Figure 9. It is interesting to note that the percentage of dis­solved nitrogen is about equal to that present in ni­trided ferrous materials.

The hardness traverse curves shown in Figure 10 verify the selection of a two hour treatment time. The 55 Re surface hardness obtained is a substantial improvement over untreated titanium. Following the two hour tra­verse to a point of parallelism with the abscissa, a measurable diffusion zone of 0.002" (0.051 mm) is in­dicated.

The expected improvement in wear resistance resulting from this hardness increase has been verified by ex­tensive laboratory and field testing. Figure 11 was developed from a laboratory tribometer test performed in the metallurgical laboratory of an aircraft eng'ine manufacturer. The area included between the horizontal base line and the profilometer trace is a direct ni~a­surement of the amount of wear developed during the test.

Any improvement in wear and gall resistance at the ex­pense of fatigue properties is not tolerable in a ma­terial which claims as its largest consumer an aircraft engine manufacturer. Consequently close scrutiny on all types of fatigue testing equipment has been made of Tiduran treated titanium test parts. Initial investi­gations of the structures indicated some loss in fati­gue strength resulting from the stress relieving ef­fect of the 1480°F. (804°C) treatment. Glass beading following heat treatment restored the original machin~ ing stress pattern and produced acceptable high cycle fatigue values as shown in Figure 12. Substantial im­provements in these results have been obtained more recently by long time (10 hours) over-aging at l060°F. (571°C) 'and glass beading following Tiduran treatment.

Many commercial applications of salt bath nitriding of titanium are still pending in this country. Aircraft engine manufacturers are continuing to examine the ef­fect of Tiduran treatment plus dry-film lubricants on the fretting fatigue properties of turbine blades. Wear testing of Tiduran treated titanium ball valves in naval submarines has shown promise. Titanium valves for the chemical industry, Figure 13, and the automotive industry, Figure 14, are also excellent Tiduran prospects.

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2514 R. H. SHOEMAKER

4.-------..,....---,,------------...,.4 Ti 6Al-4V,Tiduran-treated

~(SCALE AT RIGHT)

3 I f---=>--""""d--_ ___::::,,,,._-+=-b.L---+~---1.1 3

~ ~ ~ ~

.DOI"

.025mm DISTANCE FROM SURFACE

.002" .003" .004" .Imm

Figure 9 Elemental Distribution of O, C and N in Tiduran Diffusion Zone.

ROCKWELL 'C'

40r----:--;'1':~::1'-.....;:::::::~:::;;;;:::::jt=:::=:::i-

.001" DISTANCE FROM SURFACE

.002" .003"

Figure 10 Tiduran Hardness Patterns.

367 PLATE TREATED------------'1-------,.....-

~LBS

u UNTREATED

36 CYLINDER TREATEDt--.::::=======~::::::::::==-

CYLINDER +PLATEt--~--=======--18=!;,~~~ TREATED WEAR OF TEST CYLINDERS (IO-' ln2 )

Figure 11 Ti 6Al-4V Wear Tests.

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NEW SURFACE TREATMENTS FOR TITANIUM

Ti 8Al-1Mo-1V

70F k=2

MACHINED+ TIDURAN STRESS RELIEVED

93 ksi

TIDURAN + GLASS BEAD BLAST

Figure 12 High Cycle (107) Fatigue Strength.

2515

Figure 13 Tiduran Treated Titanium Valve for the Chemical Industry.

Figure 14 Tiduran Treated Automotive Valve.

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2516 R. H.SHOEMAKER

Summary

Surface treatments for titanium metal will always pre­sent challenges. Some of the most difficult can be found in ordinary cleaning operations. This is primar­ily due to the extreme activity of the metal under pro­cessing conditions.

Molten salt baths have the capability of producing chemi­cally clean surfaces. Acid etching and alpha case re­moval operations are quite dependent on these results. Salt bath oxides also furnish excellent intermediate bases for drawing and forming operations.

The finished titanium surface properties can be improved by salt bath treatment. A molten salt nitriding process is available to produce wear resistant surfaces on ti­tanium. Fatigue properties can be enhanced by glass beading following the Tiduran treatment. Future appli­cations for this process and all surface treatments of titanium should increase as the metal's non-aerospace applications become more diversified.