IL37743A - Method for fabricating corrosion resistant gas turbine engine components - Google Patents

Method for fabricating corrosion resistant gas turbine engine components

Info

Publication number
IL37743A
IL37743A IL37743A IL3774371A IL37743A IL 37743 A IL37743 A IL 37743A IL 37743 A IL37743 A IL 37743A IL 3774371 A IL3774371 A IL 3774371A IL 37743 A IL37743 A IL 37743A
Authority
IL
Israel
Prior art keywords
gas turbine
turbine engine
corrosion resistant
engine components
resistant gas
Prior art date
Application number
IL37743A
Other languages
English (en)
Other versions
IL37743A0 (en
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 IL37743A0 publication Critical patent/IL37743A0/xx
Publication of IL37743A publication Critical patent/IL37743A/xx

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
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/22—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded
    • B23K20/233—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded without ferrous layer
    • B23K20/2333—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded without ferrous layer one layer being aluminium, magnesium or beryllium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
    • C22C49/02—Alloys containing metallic or non-metallic fibres or filaments characterised by the matrix material
    • C22C49/04—Light metals
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S29/00—Metal working
    • Y10S29/045—Titanium
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49337—Composite blade
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49801—Shaping fiber or fibered material

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Laminated Bodies (AREA)
IL37743A 1970-10-20 1971-09-17 Method for fabricating corrosion resistant gas turbine engine components IL37743A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US8225270A 1970-10-20 1970-10-20

Publications (2)

Publication Number Publication Date
IL37743A0 IL37743A0 (en) 1971-11-29
IL37743A true IL37743A (en) 1974-05-16

Family

ID=22170021

Family Applications (1)

Application Number Title Priority Date Filing Date
IL37743A IL37743A (en) 1970-10-20 1971-09-17 Method for fabricating corrosion resistant gas turbine engine components

Country Status (9)

Country Link
US (1) US3699623A (nl)
JP (1) JPS5434087B1 (nl)
AU (1) AU460007B2 (nl)
CA (1) CA949266A (nl)
DE (1) DE2149634A1 (nl)
FR (1) FR2111243A5 (nl)
GB (1) GB1339652A (nl)
IL (1) IL37743A (nl)
NL (1) NL167620C (nl)

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3827118A (en) * 1970-11-27 1974-08-06 Garrett Corp Airfoil and method of forming the same
US4011295A (en) * 1974-10-07 1977-03-08 The Garrett Corporation Ceramic rotor for gas turbine engine
US3904101A (en) * 1974-10-10 1975-09-09 Gen Electric Method of bonding a sheet cladding to a concave-convex substrate
US3928901A (en) * 1974-10-10 1975-12-30 Gen Electric Forming a cladding sheet to a convex/concave substrate
US3981616A (en) * 1974-10-22 1976-09-21 The United States Of America As Represented By The Secretary Of The Air Force Hollow composite compressor blade
US4010884A (en) * 1974-11-20 1977-03-08 United Technologies Corporation Method of fabricating a filament-reinforced composite article
DE2550858C3 (de) * 1975-11-12 1978-09-28 8000 Muenchen Verfahren zur Herstellung und/oder Wärmebehandlung von metallischen Form-
US4000956A (en) * 1975-12-22 1977-01-04 General Electric Company Impact resistant blade
US4108572A (en) * 1976-12-23 1978-08-22 United Technologies Corporation Composite rotor blade
US4111606A (en) * 1976-12-27 1978-09-05 United Technologies Corporation Composite rotor blade
DE2819076C2 (de) * 1978-04-29 1982-02-25 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zum Herstellen eines metallischen Mehschicht-Verbundwerkstoffes
DE3151413A1 (de) * 1981-12-24 1983-07-14 MTU Motoren- und Turbinen-Union München GmbH, 8000 München "schaufel einer stroemungsmaschine, insbesondere gasturbine"
DE3419674A1 (de) * 1983-05-26 1984-11-29 Rolls-Royce Ltd., London Verfahren zum aufbringen eines ueberzugs auf ein bauteil
GB2141359B (en) * 1983-05-26 1986-10-15 Rolls Royce Improvements in or relating to the application of coatings to articles
JPS6029431A (ja) * 1983-07-28 1985-02-14 Toyota Motor Corp 合金の製造方法
JPS61114848A (ja) * 1984-11-12 1986-06-02 工業技術院長 金属基複合材料の製造法
US4929322A (en) * 1985-09-30 1990-05-29 Union Carbide Corporation Apparatus and process for arc vapor depositing a coating in an evacuated chamber
US4839245A (en) * 1985-09-30 1989-06-13 Union Carbide Corporation Zirconium nitride coated article and method for making same
FR2589485B1 (fr) * 1985-11-05 1991-12-13 Nippon Telegraph & Telephone Magnesium ou alliage du magnesium traite en surface et procede pour le traitement de surface du magnesium ou d'un alliage de magnesium
US4919594A (en) * 1987-05-15 1990-04-24 Allied-Signal Inc. Composite member, unitary rotor member including same, and method of making
US5080558A (en) * 1990-06-07 1992-01-14 Westinghouse Electric Corp. Control stage nozzle vane for use in partial arc operation
US5137426A (en) * 1990-08-06 1992-08-11 General Electric Company Blade shroud deformable protective coating
US5149251A (en) * 1990-11-15 1992-09-22 Auto Air Composites, Inc. Metal/composite spinner cone
US5141400A (en) * 1991-01-25 1992-08-25 General Electric Company Wide chord fan blade
SE511439C2 (sv) 1997-06-16 1999-09-27 Amal Ab Förfarande för åstadkommande av en böjstyv, långsträckt kropp samt en anordning vid en böjstyv, långsträckt kropp
US6190133B1 (en) 1998-08-14 2001-02-20 Allison Engine Company High stiffness airoil and method of manufacture
DE19959598A1 (de) 1999-12-10 2001-06-13 Rolls Royce Deutschland Verfahren zum Herstellen einer Schaufel einer Strömungsmaschine
GB2391270B (en) * 2002-07-26 2006-03-08 Rolls Royce Plc Turbomachine blade
US8623446B2 (en) 2006-02-25 2014-01-07 Metascape Llc Ultraviolet activated antimicrobial surfaces
US20080102292A1 (en) * 2006-11-01 2008-05-01 United Technologies Corporation Surface treatment for a thin titanium foil
US7828526B2 (en) * 2007-04-11 2010-11-09 General Electric Company Metallic blade having a composite inlay
US8241003B2 (en) * 2008-01-23 2012-08-14 United Technologies Corp. Systems and methods involving localized stiffening of blades
DE102008019296A1 (de) * 2008-04-16 2009-10-22 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Herstellung eines Feuerschutzes für aus Titan bestehende Bauteilkörper einer Fluggasturbine und Bauteilkörper aus Titan für eine Fluggasturbine
US8794925B2 (en) 2010-08-24 2014-08-05 United Technologies Corporation Root region of a blade for a gas turbine engine
DE102010062357B4 (de) 2010-12-02 2013-08-14 Innovent E.V. Vorrichtung und Verfahren zur Herstellung eines mit zumindest einer Korrosionsschutzschicht beschichteten magnesiumhaltigen Substrats
US9970303B2 (en) 2014-05-13 2018-05-15 Entrotech, Inc. Erosion protection sleeve
DE102015223404B4 (de) * 2015-11-26 2019-01-31 Airbus Defence and Space GmbH Zugprobe, Verfahren zum Herstellen einer Zugprobe, Vorrichtung zur Durchführung eines Zugversuchs und Verfahren zur Durchführung eines Zugversuchs
CN108453362A (zh) * 2018-03-07 2018-08-28 哈尔滨工业大学（威海） 一种铝合金表面活化辅助直接扩散焊方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2982017A (en) * 1953-05-22 1961-05-02 Union Carbide Corp Method of protecting magnesium with a coating of titanium
US3041040A (en) * 1955-12-23 1962-06-26 Gen Electric Metal clad blade
GB831786A (en) * 1956-05-28 1960-03-30 Gen Electric Method of coating molybdenum and its alloys for protection against oxidation at elevated temperatures
US3098723A (en) * 1960-01-18 1963-07-23 Rand Corp Novel structural composite material
US3165829A (en) * 1962-01-29 1965-01-19 Titanium Metals Corp Method of cladding aluminum with titanium
US3460920A (en) * 1966-10-10 1969-08-12 Whittaker Corp Filament reinforced metal composites for gas turbine blades
US3572971A (en) * 1969-09-29 1971-03-30 Gen Electric Lightweight turbo-machinery blading
US3600103A (en) * 1969-10-06 1971-08-17 United Aircraft Corp Composite blade

Also Published As

Publication number Publication date
JPS5434087B1 (nl) 1979-10-24
NL7114268A (nl) 1972-04-24
US3699623A (en) 1972-10-24
NL167620B (nl) 1981-08-17
FR2111243A5 (nl) 1972-06-02
GB1339652A (en) 1973-12-05
CA949266A (en) 1974-06-18
AU3478671A (en) 1973-05-03
NL167620C (nl) 1982-01-18
IL37743A0 (en) 1971-11-29
DE2149634A1 (de) 1972-04-27
AU460007B2 (en) 1975-04-10

Similar Documents

Publication Publication Date Title
IL37743A (en) Method for fabricating corrosion resistant gas turbine engine components
CA939522A (en) Gas turbine engine
IL37773A (en) Wall structure for a gas turbine engine
CA938796A (en) Gas turbine engine
IL33996A (en) Combustion chamber for a gas turbine engine
AU4998572A (en) Gas turbine engine blades
AU447212B2 (en) Gas turbine engines
AU6681474A (en) Gas turbine engine combustion equipment
CA933369A (en) Gas turbine engine
AU463411B2 (en) Flame-tube fora combustionchamber ofa gas turbine engine
CA985918A (en) Gas turbine engine combustion equipment
SE414071B (sv) Kontinuerligt arbetande brensleinsprutningsanordning for fordonsgasturbiner
BE774297A (nl) Werkwijze ter bereiding van een asvrije motoroliecomposite vooraardgasmotoren
AU5010069A (en) Gas turbine engines
CH526039A (de) Verbrennungskammer für Gasturbinen
CA834433A (en) Gas turbine engines
AU4402272A (en) Gas turbine engine
GB1363956A (en) Fuel controls for turbine engines
CA843080A (en) Combustion apparatus for gas turbine engines
CA836231A (en) Combustion apparatus for gas turbine engines
CA852452A (en) Gas turbine engine
CA851426A (en) Gas turbine engines
CA835631A (en) Gas turbine engines
AU5053672A (en) Gas turbine engine
CA847038A (en) Starting system for gas turbine engines