US3850712A - Method of etching a titanium or titanium alloy part - Google Patents

Method of etching a titanium or titanium alloy part Download PDF

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Publication number
US3850712A
US3850712A US00261815A US26181572A US3850712A US 3850712 A US3850712 A US 3850712A US 00261815 A US00261815 A US 00261815A US 26181572 A US26181572 A US 26181572A US 3850712 A US3850712 A US 3850712A
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US
United States
Prior art keywords
titanium
mixture
etching
titanium alloy
minutes
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
Application number
US00261815A
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English (en)
Inventor
T Broughton
B Forman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
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Rolls Royce PLC
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Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of US3850712A publication Critical patent/US3850712A/en
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Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23GCLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
    • C23G1/00Cleaning or pickling metallic material with solutions or molten salts
    • C23G1/02Cleaning or pickling metallic material with solutions or molten salts with acid solutions
    • C23G1/10Other heavy metals
    • C23G1/106Other heavy metals refractory metals

Definitions

  • ABSTRACT relates to a method of etching a titanium or titanium alloy part in which the part is immersed in a mixture comprising nitric acid, hydro fluorosilicic acid and water.
  • the present invention provides a method of etching which is relatively slow and which produces a matt surface condition on which the grain etched surface is less pronounced and which is suitable for both binocular and subsequent penetrant inspection.
  • a method of etching a titanium or titanium alloy part comprises immersing the part in a mixture comprising nitric acid, hydrofluorosilicic acid and water.
  • the necessary time of immersion of the part in the mixture will vary in accordance with the amount of metal to be removed, the temperature of the mixture and various other factors, but we have found that for a metal removal of approximately a tenth of a thousandth of an inch, at a mixture temperature of about 20C, an immersion time of from 4 to 20 minutes may be used.
  • the invention also comprises a mixture suitable for etching titanium or alloys thereof and comprising nitric acid, hydrofluorosilicic acid, and water.
  • the mixture comprises between I60 and I80 grams per litre of nitric acid, between'8 and 12 grams per litre of the hydrofluorosilicic acid, the remainder comprising water.
  • the titanium or alloy part has been heated it may be necessary to pre-condition the oxide film so as to avoid uneven etchirigfTypically this would use an alkaline permanganate solution which would comprise 50-100 grams per litre of potassium permanganate, l-l25 grams per litre of sodium hydroxide and 100-125 grams per litre of sodium carbonate, the remainder comprising water. Alternatively a proprietary solution could be used.
  • the invention is particularly useful when applied to parts such as compressor drums of gas turbine engines.
  • a solution was made up comprising 170 grams per litre of nitric acid and grams per litre of hydro fluorosilicic acid, the remainder comprising water.
  • a tank was filled with the solution at a temperature of approximately C and the compressor drum of a gas turbine engine was immersed inthe solution.
  • the drum comprised a titanium alloy known as lMl 684 which is basically titanium with the addition of 6 percent Al, Zr 5 percent, W 1 percent.
  • the drum was left in the solution for some 20 minutes and was then removed and washed out with water.
  • the drum was then inspected through binocular microscopes and using a penetrant technique to determine the location of any flaws such as cracks or the like.
  • the time of immersion of similar titanium parts in the etchant mixture could sometimes be reduced to 4 minutes for a metal removal of about a tenth of a thoube reduced still further if the temperature of the etch- 'ant mixture, which is normally room temperature, is increased above room temperature or if the ambient temperature happens to be high.
  • the times of immersion not to be altered to a large extent within the range of l6-22C mixture temperature, and within this range we find that an immersion time between 4 and 20 minutes will produce metal removal of about a tenth of a thousandth of an inch, which is normally an optimum amount to minimise metal removal while producing the necessary surface finish to allow surface inspection.
  • drums were etched and inspected after they had been run on a gas turbine engine and were therefore coated with oxides.
  • a method of etching a titanium or titanium alloy part comprising contacting the part with a mixture consistingessentially of nitric acid, hydrofluorosilicic acid and water, and continuing contact with said mixture until a matt surface is produced on said part adapted for improvedvisualdetection of flaws therein.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • ing And Chemical Polishing (AREA)
  • Cleaning And De-Greasing Of Metallic Materials By Chemical Methods (AREA)
US00261815A 1971-06-17 1972-06-12 Method of etching a titanium or titanium alloy part Expired - Lifetime US3850712A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2836771 1971-06-17

Publications (1)

Publication Number Publication Date
US3850712A true US3850712A (en) 1974-11-26

Family

ID=10274536

Family Applications (1)

Application Number Title Priority Date Filing Date
US00261815A Expired - Lifetime US3850712A (en) 1971-06-17 1972-06-12 Method of etching a titanium or titanium alloy part

Country Status (4)

Country Link
US (1) US3850712A (cs)
FR (1) FR2142079B1 (cs)
GB (1) GB1344711A (cs)
IT (1) IT960821B (cs)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4551434A (en) * 1983-03-16 1985-11-05 Mtu Motoren-Und Turbinen-Union Muenchen Gmbh Method for recognizing structural inhomogeneities in titanium alloy test samples including welded samples
EP0179013A1 (en) * 1984-10-16 1986-04-23 United Technologies Corporation Chemical milling using an inert particulate and moving vessel
US20050011863A1 (en) * 2003-07-17 2005-01-20 Peter Wayte Method for inspecting a titanium-based component
WO2005017230A1 (ja) * 2003-08-19 2005-02-24 Mitsubishi Chemical Corporation チタン含有層用エッチング液およびチタン含有層のエッチング方法
US20070283560A1 (en) * 2006-06-05 2007-12-13 United Technologies Corporation Enhanced weldability for high strength cast and wrought nickel superalloys
CN100537847C (zh) * 2005-02-24 2009-09-09 关东化学株式会社 钛、铝金属层叠膜蚀刻液组合物

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2457471A2 (fr) * 1979-05-23 1980-12-19 Pechiney Aluminium Procede continu d'elimination des incrustations essentiellement titaniferes des parois d'echangeurs thermiques
FR2431671A1 (fr) * 1978-07-19 1980-02-15 Pechiney Aluminium Procede d'elimination des incrustations essentiellement titaniferes des parois d'echangeurs thermiques
FR2961598B1 (fr) * 2010-06-21 2012-07-27 Snecma Procede de controle d'une piece en titane ou en alliage de titane en vue de la detection de defauts d'usinage

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2711364A (en) * 1953-12-31 1955-06-21 John G Beach Polishing metals and composition therefor
US2981609A (en) * 1956-11-20 1961-04-25 United Aircraft Corp Etching bath for titanium and its alloys and process of etching
US3514407A (en) * 1966-09-28 1970-05-26 Lockheed Aircraft Corp Chemical polishing of titanium and titanium alloys

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2711364A (en) * 1953-12-31 1955-06-21 John G Beach Polishing metals and composition therefor
US2981609A (en) * 1956-11-20 1961-04-25 United Aircraft Corp Etching bath for titanium and its alloys and process of etching
US3514407A (en) * 1966-09-28 1970-05-26 Lockheed Aircraft Corp Chemical polishing of titanium and titanium alloys

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4551434A (en) * 1983-03-16 1985-11-05 Mtu Motoren-Und Turbinen-Union Muenchen Gmbh Method for recognizing structural inhomogeneities in titanium alloy test samples including welded samples
EP0179013A1 (en) * 1984-10-16 1986-04-23 United Technologies Corporation Chemical milling using an inert particulate and moving vessel
US20050011863A1 (en) * 2003-07-17 2005-01-20 Peter Wayte Method for inspecting a titanium-based component
US7097783B2 (en) * 2003-07-17 2006-08-29 General Electric Company Method for inspecting a titanium-based component
WO2005017230A1 (ja) * 2003-08-19 2005-02-24 Mitsubishi Chemical Corporation チタン含有層用エッチング液およびチタン含有層のエッチング方法
CN100537847C (zh) * 2005-02-24 2009-09-09 关东化学株式会社 钛、铝金属层叠膜蚀刻液组合物
US20070283560A1 (en) * 2006-06-05 2007-12-13 United Technologies Corporation Enhanced weldability for high strength cast and wrought nickel superalloys
US7854064B2 (en) * 2006-06-05 2010-12-21 United Technologies Corporation Enhanced weldability for high strength cast and wrought nickel superalloys

Also Published As

Publication number Publication date
IT960821B (it) 1973-11-30
DE2229897B2 (de) 1975-06-12
DE2229897A1 (de) 1972-12-21
FR2142079B1 (cs) 1977-12-23
GB1344711A (en) 1974-01-23
FR2142079A1 (cs) 1973-01-26

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