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FR2987287B1 - Procede de fabrication d'une piece metallique a symetrie de revolution, notamment pour turboreacteur d'aeronef - Google Patents

Procede de fabrication d'une piece metallique a symetrie de revolution, notamment pour turboreacteur d'aeronef

Info

Publication number
FR2987287B1
FR2987287B1 FR1200577A FR1200577A FR2987287B1 FR 2987287 B1 FR2987287 B1 FR 2987287B1 FR 1200577 A FR1200577 A FR 1200577A FR 1200577 A FR1200577 A FR 1200577A FR 2987287 B1 FR2987287 B1 FR 2987287B1
Authority
FR
France
Prior art keywords
manufacturing
metallic part
aircraft airborne
revolution symmetry
symmetry metallic
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
FR1200577A
Other languages
English (en)
Other versions
FR2987287A1 (fr
Inventor
Philippe Bienvenu
Pierre Marcel Dupuis
Helene Malot
Franciso Caneque
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 Nacelles SAS
Original Assignee
Aircelle 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 Aircelle SA filed Critical Aircelle SA
Priority to FR1200577A priority Critical patent/FR2987287B1/fr
Publication of FR2987287A1 publication Critical patent/FR2987287A1/fr
Application granted granted Critical
Publication of FR2987287B1 publication Critical patent/FR2987287B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
    • B21D22/14—Spinning
    • B21D22/16—Spinning over shaping mandrels or formers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
    • B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
    • B21D26/033—Deforming tubular bodies
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D53/00—Making other particular articles
    • B21D53/92—Making other particular articles other parts for aircraft
    • 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
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/008—Rocket engine parts, e.g. nozzles, combustion chambers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
FR1200577A 2012-02-28 2012-02-28 Procede de fabrication d'une piece metallique a symetrie de revolution, notamment pour turboreacteur d'aeronef Active FR2987287B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1200577A FR2987287B1 (fr) 2012-02-28 2012-02-28 Procede de fabrication d'une piece metallique a symetrie de revolution, notamment pour turboreacteur d'aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1200577A FR2987287B1 (fr) 2012-02-28 2012-02-28 Procede de fabrication d'une piece metallique a symetrie de revolution, notamment pour turboreacteur d'aeronef

Publications (2)

Publication Number Publication Date
FR2987287A1 FR2987287A1 (fr) 2013-08-30
FR2987287B1 true FR2987287B1 (fr) 2014-11-28

Family

ID=45930817

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1200577A Active FR2987287B1 (fr) 2012-02-28 2012-02-28 Procede de fabrication d'une piece metallique a symetrie de revolution, notamment pour turboreacteur d'aeronef

Country Status (1)

Country Link
FR (1) FR2987287B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
PL240055B1 (pl) * 2019-03-27 2022-02-14 Inst Obrobki Plastycznej Sposób wytwarzania elementów stożkowych z blachy i zespół do wytwarzania elementów stożkowych z blachy
FR3096907B1 (fr) * 2019-06-07 2021-06-11 Safran Aircraft Engines Procédé de realisation d’une pièce renforcée mecaniquement
FR3104050B1 (fr) * 2019-12-06 2022-07-29 Safran Nacelles Procede de fabrication d’une paroi annulaire de turbomachine d’aeronef

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10148451C2 (de) * 2001-10-01 2002-12-05 Leico Werkzeugmaschb Gmbh & Co Verfahren zur Herstellung eines Hohlkörpers und Vorform
FR2949820B1 (fr) * 2009-09-04 2011-10-14 Aircelle Sa Ensemble structurant pour une tuyere d'ejection.
JP5913792B2 (ja) * 2010-04-13 2016-04-27 一般社団法人日本航空宇宙工業会 成形方法および成形装置

Also Published As

Publication number Publication date
FR2987287A1 (fr) 2013-08-30

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