[go: up one dir, main page]

GB1459032A - Inhibiting vanadium corrosion in a gas turbine engines - Google Patents

Inhibiting vanadium corrosion in a gas turbine engines

Info

Publication number
GB1459032A
GB1459032A GB2112574A GB2112574A GB1459032A GB 1459032 A GB1459032 A GB 1459032A GB 2112574 A GB2112574 A GB 2112574A GB 2112574 A GB2112574 A GB 2112574A GB 1459032 A GB1459032 A GB 1459032A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
vanadium
corrosion
vanadate
stable
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
Application number
GB2112574A
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.)
RTX Corp
Original Assignee
United Aircraft Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Publication of GB1459032A publication Critical patent/GB1459032A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/30—Preventing corrosion or unwanted deposits in gas-swept spaces
    • C—CHEMISTRY; METALLURGY
    • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G OR C10K; LIQUIFIED PETROLEUM GAS; USE OF ADDITIVES TO FUELS OR FIRES; FIRE-LIGHTERS
    • C10L1/00—Liquid carbonaceous fuels
    • C10L1/10—Liquid carbonaceous fuels containing additives
    • C—CHEMISTRY; METALLURGY
    • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G OR C10K; LIQUIFIED PETROLEUM GAS; USE OF ADDITIVES TO FUELS OR FIRES; FIRE-LIGHTERS
    • C10L1/00—Liquid carbonaceous fuels
    • C10L1/10—Liquid carbonaceous fuels containing additives
    • C10L1/14—Organic compounds
    • C10L1/18—Organic compounds containing oxygen
    • C10L1/1814—Chelates
    • 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
    • C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
    • C23F11/00—Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent
    • C23F11/08—Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent in other liquids
    • C23F11/18—Inhibiting corrosion of metallic material by applying inhibitors to the surface in danger of corrosion or adding them to the corrosive agent in other liquids using inorganic inhibitors
    • C23F11/185—Refractory metal-containing compounds
    • C—CHEMISTRY; METALLURGY
    • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G OR C10K; LIQUIFIED PETROLEUM GAS; USE OF ADDITIVES TO FUELS OR FIRES; FIRE-LIGHTERS
    • C10L1/00—Liquid carbonaceous fuels
    • C10L1/10—Liquid carbonaceous fuels containing additives
    • C10L1/12—Inorganic compounds
    • C10L1/1233—Inorganic compounds oxygen containing compounds, e.g. oxides, hydroxides, acids and salts thereof

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Organic Chemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • Emergency Medicine (AREA)
  • Inorganic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Preventing Corrosion Or Incrustation Of Metals (AREA)

Abstract

1459032 Preventing vanadium gas turbine corrosion UNITED AIRCRAFT CORP 13 May 1974 [14 May 1973] 21125/74 Heading C5G Vanadium corrosion in a gas turbine engine whose combustion products contain vanadium in a form corrosive to hot engine alloy components is inhibited by exposing the combustion products, upstream of the components, to the oxide of a metal selected from the rare earths, yttium, scandium, nobium, nickel, cobalt and iron, forming a stable vanadate of the metal having a m.p. in excess of the combustion product temperature and not forming the sulphate or any other compound (apart from the vanadate) which is stable at the engine operation temperature and whose generation or presence would prevent the additive combining with the vanadium. The metal oxide may originate from an organometallic compound, e.g. yttrium acetyl acetonate dissolved in the fuel to the gas turbine.
GB2112574A 1973-05-14 1974-05-13 Inhibiting vanadium corrosion in a gas turbine engines Expired GB1459032A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US35983473A 1973-05-14 1973-05-14

Publications (1)

Publication Number Publication Date
GB1459032A true GB1459032A (en) 1976-12-22

Family

ID=23415481

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2112574A Expired GB1459032A (en) 1973-05-14 1974-05-13 Inhibiting vanadium corrosion in a gas turbine engines

Country Status (5)

Country Link
JP (1) JPS5014911A (en)
DE (1) DE2421927A1 (en)
FR (1) FR2229861A1 (en)
GB (1) GB1459032A (en)
IT (1) IT1012237B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4749550A (en) * 1983-09-15 1988-06-07 The British Petroleum Company P.L.C. Method of inhibiting corrosion in aqueous systems
WO2004026996A1 (en) * 2002-09-17 2004-04-01 Systemseparation Sweden Ab Fuel additive composition and its preparation
EP1255879A4 (en) * 2000-02-15 2009-06-24 Univ California METHOD AND COMPOSITION FOR PREVENTING HIGH-TEMPERATURE CORROSION DUE TO ALKALI SULPHATES AND ALKALINE CHLORIDES
US10557099B2 (en) 2017-08-09 2020-02-11 General Electric Company Oil based product for treating vanadium rich oils
US10577553B2 (en) 2017-08-09 2020-03-03 General Electric Company Water based product for treating vanadium rich oils

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2603905A1 (en) * 1986-09-12 1988-03-18 Elf France METHOD FOR PROTECTING METAL SURFACES FROM VANADOSODIC CORROSION
DE4413202C2 (en) * 1994-04-13 2000-08-17 Ver Energiewerke Ag Method and arrangement for avoiding the adherence of particles carried in a hot gas to a part of the system which is exposed to the hot gas, in particular to the blades of a gas turbine
RU2093696C1 (en) * 1996-03-19 1997-10-20 Конструкторское бюро химавтоматики Method for failure protection of power plants using hydrogen as working medium
FR2810341B1 (en) * 2000-06-19 2003-03-28 Ge Energy Products France Snc USE OF NICKEL COMPOUNDS AS VANADIC CORROSION INHIBITORS AND COMBUSTION METHOD USING SUCH NICKEL COMPOUNDS
US20130323518A1 (en) * 2012-06-05 2013-12-05 General Electric Company Coating process, coating, and coated component
RU2540521C2 (en) * 2012-07-02 2015-02-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) Method of determination of rational parameters of modes of wet cleaning of gte flow duct
FR3044684B1 (en) * 2015-12-03 2017-12-08 Ge Energy Products France Snc VANADI CORROSION INHIBITORS BASED ON YTTRIUM AND MAGNESIUM
WO2017096334A1 (en) * 2015-12-03 2017-06-08 General Electric Company Yttrium and magnesium based vanadium corrosion inhibitors

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4749550A (en) * 1983-09-15 1988-06-07 The British Petroleum Company P.L.C. Method of inhibiting corrosion in aqueous systems
EP1255879A4 (en) * 2000-02-15 2009-06-24 Univ California METHOD AND COMPOSITION FOR PREVENTING HIGH-TEMPERATURE CORROSION DUE TO ALKALI SULPHATES AND ALKALINE CHLORIDES
WO2004026996A1 (en) * 2002-09-17 2004-04-01 Systemseparation Sweden Ab Fuel additive composition and its preparation
CN100443573C (en) * 2002-09-17 2008-12-17 系统分离瑞典股份公司 Fuel additive composition and its preparation
US10557099B2 (en) 2017-08-09 2020-02-11 General Electric Company Oil based product for treating vanadium rich oils
US10577553B2 (en) 2017-08-09 2020-03-03 General Electric Company Water based product for treating vanadium rich oils

Also Published As

Publication number Publication date
IT1012237B (en) 1977-03-10
AU6847174A (en) 1975-11-06
FR2229861A1 (en) 1974-12-13
JPS5014911A (en) 1975-02-17
DE2421927A1 (en) 1974-12-05

Similar Documents

Publication Publication Date Title
GB1459032A (en) Inhibiting vanadium corrosion in a gas turbine engines
CA1014361A (en) Fuel pumping and metering system for small gas turbine engines
GB1500780A (en) Mcraly type coating alloy
GB1322405A (en) Oil systems for gas turbine engines
GB1517685A (en) Combined guide vane and mixer for a gas turbine ducted fan engine
GB816430A (en) Improvements in or relating to fuel injection systems for internal combustion engines
GB1257001A (en)
JPS5314232A (en) Fuel injection quantity calculation system for internal combustion engine
GB1533178A (en) Gas turbine engine
JPS51123413A (en) Combustion system of gas turbine
GB1322802A (en) Gas turbine engines and engine subassemblies including a temperautre control arrangement for a row of turbine blades therein
GB1077806A (en) Apparatus for counting the permissible total operating hours of heat engines
GB1328426A (en) Gas turbine engines
JPS55110748A (en) Nickel-aluminum series super heat-resistant alloy ductile at room temperature
JPS528215A (en) Fuel controlling system of gas turbine engine
HART et al. Deposition and corrosion in gas turbines; Proceedings of the Conference, London, England, December 6, 7, 1972
Supp et al. Subsonic performance potential of ramjets and ejector ramjets
GB1082232A (en) Gas turbine engine and rotary fuel injection means therefor
MARTEL et al. Aircraft turbine engine fuel corrosion inhibitors and their effects on fuel properties[Final Technical Report]
GB1039735A (en) Improvements in or relating to magnetohydrodynamic devices
GB531430A (en) Apparatus for supplying an engine from a gas-producer applicable to explosion engines employing combustible liquids
GB1036308A (en) Improvements in or relating to vessels for resisting internal fluid pressure
VAVRA Calculating procedure of sea-level static performance of two-spool afterburning bypass jet engine[Progress Report]
GB1143035A (en) High temperature alloys
JPS51126410A (en) Internal combustion engine

Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee