Nothing Special   »   [go: up one dir, main page]

FR3113255B1 - Protection contre l’oxydation ou la corrosion d’une pièce creuse en superalliage - Google Patents

Protection contre l’oxydation ou la corrosion d’une pièce creuse en superalliage Download PDF

Info

Publication number
FR3113255B1
FR3113255B1 FR2008334A FR2008334A FR3113255B1 FR 3113255 B1 FR3113255 B1 FR 3113255B1 FR 2008334 A FR2008334 A FR 2008334A FR 2008334 A FR2008334 A FR 2008334A FR 3113255 B1 FR3113255 B1 FR 3113255B1
Authority
FR
France
Prior art keywords
corrosion
against oxidation
protection against
superalloy part
hollow
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.)
Active
Application number
FR2008334A
Other languages
English (en)
Other versions
FR3113255A1 (fr
Inventor
Jérémy Rame
Amar Saboundji
Mirna Bechelany
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.)
Safran SA
Original Assignee
Safran SA
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 Safran SA filed Critical Safran SA
Priority to FR2008334A priority Critical patent/FR3113255B1/fr
Publication of FR3113255A1 publication Critical patent/FR3113255A1/fr
Application granted granted Critical
Publication of FR3113255B1 publication Critical patent/FR3113255B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/10Cores; Manufacture or installation of cores
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C23/00Tools; Devices not mentioned before for moulding
    • B22C23/02Devices for coating moulds or cores
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/12Treating moulds or cores, e.g. drying, hardening
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/22Moulds for peculiarly-shaped castings
    • B22C9/24Moulds for peculiarly-shaped castings for hollow articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/08Casting in, on, or around objects which form part of the product for building-up linings or coverings, e.g. of anti-frictional metal
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D27/00Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
    • B22D27/18Measures for using chemical processes for influencing the surface composition of castings, e.g. for increasing resistance to acid attack
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

Est concerné un procédé de protection, pour protéger d’une oxydation et/ou d’une corrosion au moins une zone interne creuse (13, 14) d’une pièce (2) de turbomachine en un superalliage, ladite au moins une zone interne creuse ayant été formée, par l’intermédiaire d’au moins un noyau en matériau céramique limité par une surface extérieure (26) qui l’entoure, caractérisé en ce qu’avant d’apporter le superalliage autour du noyau en matériau céramique, on revêt ladite surface extérieure avec un matériau comprenant au moins :- une couche nanométrique d’hafnium (Hf), et/ou- une couche micronique de platine (Pt), ou - un mélange au moins d’hafnium et de platine. Figure à publier avec l’abrégé : figure 4
FR2008334A 2020-08-06 2020-08-06 Protection contre l’oxydation ou la corrosion d’une pièce creuse en superalliage Active FR3113255B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2008334A FR3113255B1 (fr) 2020-08-06 2020-08-06 Protection contre l’oxydation ou la corrosion d’une pièce creuse en superalliage

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2008334A FR3113255B1 (fr) 2020-08-06 2020-08-06 Protection contre l’oxydation ou la corrosion d’une pièce creuse en superalliage
FR2008334 2020-08-06

Publications (2)

Publication Number Publication Date
FR3113255A1 FR3113255A1 (fr) 2022-02-11
FR3113255B1 true FR3113255B1 (fr) 2022-10-07

Family

ID=74183214

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2008334A Active FR3113255B1 (fr) 2020-08-06 2020-08-06 Protection contre l’oxydation ou la corrosion d’une pièce creuse en superalliage

Country Status (1)

Country Link
FR (1) FR3113255B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116121523A (zh) * 2023-02-20 2023-05-16 西安诺博尔稀贵金属材料股份有限公司 一种薄壁管热处理用垂直热处理组件及应用方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4190450A (en) 1976-11-17 1980-02-26 Howmet Turbine Components Corporation Ceramic cores for manufacturing hollow metal castings
FR2626794B1 (fr) 1988-02-10 1993-07-02 Snecma Pate thermoplastique pour la preparation de noyaux de fonderie et procede de preparation desdits noyaux
KR100354411B1 (ko) * 1994-10-14 2002-11-18 지멘스 악티엔게젤샤프트 부식,산화및과도한열응력으로부터부품을보호하기위한보호층및그제조방법
FR2785836B1 (fr) 1998-11-12 2000-12-15 Snecma Procede de fabrication de noyaux ceramiques minces pour fonderie
US7055574B2 (en) * 2004-07-27 2006-06-06 Honeywell International Inc. Method of producing metal article having internal passage coated with a ceramic coating
FR2889088B1 (fr) 2005-07-29 2008-08-22 Snecma Noyau pour aubes de turbomachine
US20100330295A1 (en) * 2009-06-30 2010-12-30 General Electric Company Method for providing ductile environmental coating having fatigue and corrosion resistance
EP2329901A1 (fr) * 2009-12-03 2011-06-08 Siemens Aktiengesellschaft Moule en fonte doté de noyaux de fonderie internes stabilisés, procédé de fonte et pièce moulée
US9975173B2 (en) * 2013-06-03 2018-05-22 United Technologies Corporation Castings and manufacture methods
US10556269B1 (en) * 2017-03-29 2020-02-11 United Technologies Corporation Apparatus for and method of making multi-walled passages in components

Also Published As

Publication number Publication date
FR3113255A1 (fr) 2022-02-11

Similar Documents

Publication Publication Date Title
FR3113255B1 (fr) Protection contre l’oxydation ou la corrosion d’une pièce creuse en superalliage
US6171711B1 (en) Apertured article preconditioned for recoating
CN1629450A (zh) 具有成形后缘基座的翼型
FR3113254B1 (fr) Protection contre l’oxydation ou la corrosion d’une pièce creuse en superalliage
FR2711181A1 (fr) Procédés et dispositifs aptes à réduire les contraintes sur les pointes des pales de turbine ou de compresseur, ainsi que les moteurs ou compresseurs utilisant de tels procédés et dispositifs.
US10024161B2 (en) Turbine blade tip repair
BR102015032102A2 (pt) componente de motor e métodos de produção de um componente de motor e de reparo de um componente de motor
EP2956564B1 (fr) Procede de fabrication d'une piece d'aeronef comportant un substrat et une piece comportant un substrat recouvert d'une couche de revetement
FR3079847B1 (fr) Procede de fabrication d'un element aubage metallique d'une turbomachine d'aeronef
RU2643682C1 (ru) Устройство для определения адгезионной прочности многослойного керамического теплозащитного покрытия
FR2970666A1 (fr) Procede de perforation d'au moins une paroi d'une chambre de combustion
FR3096400B1 (fr) Aube de turbomachine à bord d’attaque métallique intégré et procédé pour l’obtenir
EP3687727B1 (fr) Dispositif porte-electrode(s) pour usinage par electroerosion, et procede d'obtention
EP2082823A2 (fr) Canal de refroidissement ménagé dans une paroi
US20160169013A1 (en) Gas Turbine Engine Component with Abrasive Surface Formed by Electrical Discharge Machining
FR3096690B1 (fr) Procédé de protection contre la corrosion
JP2006220072A (ja) 燃料噴射弁
FR3080385B1 (fr) Procede de fabrication d'un element aubage metallique pour une turbomachine d'aeronef
FR3108145B1 (fr) Aube creuse de turbomachine
US20160169039A1 (en) Slots for turbomachine structures
JP5883644B2 (ja) コネクティングロッドの製造方法
BR102015020400A2 (pt) anel de pistão
Gallimore et al. Geometric Study of Anodes for use with Low-power, Uncooled Plasma Torches Part A: The Effects of Geometry on Erosion and Stability
FR2979664A1 (fr) Paroi stator de turbomachine recouverte d'un revetement abradable a faible rugosite aerodynamique
JP2023124634A (ja) ラジアントチューブ

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20220211

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5