ZA200808371B - Process for the repair and restoration of dynamically stressed components comprising aluminium alloys for aircraft applications - Google Patents

Process for the repair and restoration of dynamically stressed components comprising aluminium alloys for aircraft applications

Info

Publication number
ZA200808371B
ZA200808371B ZA200808371A ZA200808371A ZA200808371B ZA 200808371 B ZA200808371 B ZA 200808371B ZA 200808371 A ZA200808371 A ZA 200808371A ZA 200808371 A ZA200808371 A ZA 200808371A ZA 200808371 B ZA200808371 B ZA 200808371B
Authority
ZA
South Africa
Prior art keywords
restoration
repair
aluminium alloys
aircraft applications
stressed components
Prior art date
Application number
ZA200808371A
Other languages
English (en)
Inventor
Stoltenhoff Thornsten
Zimmermann Folker
Goerris Klaus
Burger Hans
Original Assignee
Praxair Technology Inc
Roeder Praez Gmbh
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 Praxair Technology Inc, Roeder Praez Gmbh filed Critical Praxair Technology Inc
Publication of ZA200808371B publication Critical patent/ZA200808371B/xx

Links

Classifications

    • 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
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00—Coating starting from inorganic powder
    • C23C24/02—Coating starting from inorganic powder by application of pressure only
    • C23C24/04—Impact or kinetic deposition of particles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00—Restoring or reconditioning objects
    • 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
    • F01D5/005—Repairing methods or devices
    • 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
    • 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
    • F01D5/288—Protective coatings for blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97—Rocket nozzles
    • F02K9/974—Nozzle- linings; Ablative coatings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/01—Aircraft parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/30—Manufacture with deposition of material
    • F05D2230/31—Layer deposition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/90—Coating; Surface treatment
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/15—Rare earth metals, i.e. Sc, Y, lanthanides
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/611—Coating

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Combustion & Propulsion (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Powder Metallurgy (AREA)
ZA200808371A 2006-03-02 2008-10-01 Process for the repair and restoration of dynamically stressed components comprising aluminium alloys for aircraft applications ZA200808371B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP06004229A EP1829988A1 (de) 2006-03-02 2006-03-02 Verfahren zur Reparatur und wiederherstellung von dynamisch beanspruchten Komponenten aus Aluminiumlegierungen für luftfahrtechnische Anwendungen

Publications (1)

Publication Number Publication Date
ZA200808371B true ZA200808371B (en) 2009-11-25

Family

ID=36677049

Family Applications (1)

Application Number Title Priority Date Filing Date
ZA200808371A ZA200808371B (en) 2006-03-02 2008-10-01 Process for the repair and restoration of dynamically stressed components comprising aluminium alloys for aircraft applications

Country Status (13)

Country Link
US (1) US20090148622A1 (xx)
EP (1) EP1829988A1 (xx)
JP (1) JP2009528939A (xx)
KR (1) KR20090007306A (xx)
AU (1) AU2007220704A1 (xx)
BR (1) BRPI0708484A2 (xx)
CA (1) CA2643717A1 (xx)
MX (1) MX2008011226A (xx)
NO (1) NO20084003L (xx)
RU (1) RU2008139101A (xx)
SG (1) SG170059A1 (xx)
WO (1) WO2007098885A1 (xx)
ZA (1) ZA200808371B (xx)

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US8597724B2 (en) * 2007-07-06 2013-12-03 United Technologies Corporation Corrosion protective coating through cold spray
DE102008057162A1 (de) * 2008-11-13 2010-05-20 Mtu Aero Engines Gmbh Verfahren zur Reparatur des Bauteils einer Gasturbine
DE102008058142A1 (de) * 2008-11-20 2010-05-27 Mtu Aero Engines Gmbh Verfahren zum Herstellen und/oder Reparieren eines Rotors einer Strömungsmaschine und Rotor hierzu
DE102008058141A1 (de) * 2008-11-20 2010-05-27 Mtu Aero Engines Gmbh Verfahren zum Herstellen einer Schaufel für einen Rotor einer Strömungsmaschine
US20100155251A1 (en) * 2008-12-23 2010-06-24 United Technologies Corporation Hard anodize of cold spray aluminum layer
US8486249B2 (en) * 2009-01-29 2013-07-16 Honeywell International Inc. Cold spray and anodization repair process for restoring worn aluminum parts
ITTO20110257A1 (it) * 2011-03-24 2012-09-25 Avio Spa Metodo per la riparazione di un componente in lega di alluminio
DE102011081998A1 (de) 2011-09-01 2013-03-07 Siemens Aktiengesellschaft Verfahren zum Reparieren einer Schadstelle in einem Gussteil und Verfahren zum Erzeugen eines geeigneten Reparaturmaterials
US9335296B2 (en) 2012-10-10 2016-05-10 Westinghouse Electric Company Llc Systems and methods for steam generator tube analysis for detection of tube degradation
AU2013375273B2 (en) * 2013-01-28 2017-08-31 Raytheon Technologies Corporation Structured material alloy component fabrication
US9337002B2 (en) 2013-03-12 2016-05-10 Lam Research Corporation Corrosion resistant aluminum coating on plasma chamber components
US9599210B2 (en) 2013-11-06 2017-03-21 Sikorsky Aircraft Corporation Damage mitigation for gearbox
US10077499B2 (en) 2013-11-06 2018-09-18 Sikorsky Aircraft Corporation Corrosion mitigation for gearbox
CN104741864B (zh) * 2013-12-31 2017-09-22 中国航空工业集团公司沈阳飞机设计研究所 一种结构损伤快速修理方法
EP3245007B1 (en) * 2015-01-16 2020-12-16 Sikorsky Aircraft Corporation Cold spray method to repair or in certain cases strengthen metals
DE102015203234B4 (de) * 2015-02-24 2018-04-26 MTU Aero Engines AG Verfahren zur Herstellung eines Bauteils, nämlich einens Gehäuses einer Gasturbine und das entsprechende Bauteil
US9765424B2 (en) * 2015-02-25 2017-09-19 Engineering And Software System Solutions, Inc. Method of refurbishing high value articles
US20170114466A1 (en) * 2015-10-21 2017-04-27 General Electric Company Article, turbine component and airfoil treatment methods
DE102018127774A1 (de) * 2018-11-07 2020-05-07 Bayerische Motoren Werke Aktiengesellschaft Bauteil sowie Verfahren zum Herstellen eines Bauteils
US11935662B2 (en) 2019-07-02 2024-03-19 Westinghouse Electric Company Llc Elongate SiC fuel elements
WO2021055284A1 (en) 2019-09-19 2021-03-25 Westinghouse Electric Company Llc Apparatus for performing in-situ adhesion test of cold spray deposits and method of employing
CN111850546B (zh) * 2020-06-28 2021-11-02 华中科技大学 一种激光熔覆修复镍铝青铜零件的方法及其产品
CN112522695B (zh) * 2020-10-06 2023-02-28 湖北超卓航空科技股份有限公司 一种冷喷涂修复疲劳裂纹的方法
CN115369397A (zh) * 2022-08-18 2022-11-22 湖北超卓航空科技股份有限公司 航空铝合金零件腐蚀故障修复方法、复合涂层及用途

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Also Published As

Publication number Publication date
JP2009528939A (ja) 2009-08-13
RU2008139101A (ru) 2010-04-20
NO20084003L (no) 2008-11-07
WO2007098885A1 (de) 2007-09-07
SG170059A1 (en) 2011-04-29
EP1829988A1 (de) 2007-09-05
AU2007220704A1 (en) 2007-09-07
CA2643717A1 (en) 2007-09-07
BRPI0708484A2 (pt) 2011-05-31
US20090148622A1 (en) 2009-06-11
KR20090007306A (ko) 2009-01-16
MX2008011226A (es) 2009-02-10

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