EP2373469A1 - Procédé de fabrication d'une pièce de forme par tissage 3d et pièce de forme ainsi obtenue. - Google Patents

Procédé de fabrication d'une pièce de forme par tissage 3d et pièce de forme ainsi obtenue.

Info

Publication number
EP2373469A1
EP2373469A1 EP09805775A EP09805775A EP2373469A1 EP 2373469 A1 EP2373469 A1 EP 2373469A1 EP 09805775 A EP09805775 A EP 09805775A EP 09805775 A EP09805775 A EP 09805775A EP 2373469 A1 EP2373469 A1 EP 2373469A1
Authority
EP
European Patent Office
Prior art keywords
preform
weaving
cavity
loosening
piece
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.)
Withdrawn
Application number
EP09805775A
Other languages
German (de)
English (en)
French (fr)
Inventor
David Marsal
Xavier Millier
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 Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of EP2373469A1 publication Critical patent/EP2373469A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • B29C70/865Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00Making preforms
    • B29B11/14Making preforms characterised by structure or composition
    • B29B11/16Making preforms characterised by structure or composition comprising fillers or reinforcement
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/44Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/48Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
    • B29C33/50Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible
    • B29C33/505Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible cores or mandrels, e.g. inflatable
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/24Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D11/00Double or multi-ply fabrics not otherwise provided for
    • D03D11/02Fabrics formed with pockets, tubes, loops, folds, tucks or flaps
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D25/00Woven fabrics not otherwise provided for
    • D03D25/005Three-dimensional woven fabrics
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D3/00Woven fabrics characterised by their shape
    • D03D3/02Tubular fabrics
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/30Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3067Ships
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2505/00Industrial
    • D10B2505/02Reinforcing materials; Prepregs
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/13Hollow or container type article [e.g., tube, vase, etc.]
    • Y10T428/1352Polymer or resin containing [i.e., natural or synthetic]

Definitions

  • the invention relates to a method of manufacturing a piece of shape by three-dimensional weaving, (called 3D weaving) of very strong weft threads and warp threads, for example made of carbon fibers, in order to obtain a preform then impregnated with thermosetting resin. It relates more particularly to an improvement to create cavities in said piece of form.
  • thermosetting resin For the manufacture of shaped parts with high mechanical strength, especially with respect to impact, it is known to use carbon fibers coated with thermosetting resin.
  • any part can be formed by cutting woven webs of pre-impregnated carbon fiber threads, stacking them to obtain a blank of the desired workpiece and fusing them under heat and pressure.
  • the document EP 1 77763 describes a more efficient method for manufacturing a shaped part, in this case a turbomachine blade, by 3D weaving of weft yarns and warp yarns. This process makes it possible to obtain parts of exceptional strength, in particular very good impact resistance, without risk of delamination.
  • the invention aims an improvement of this type of process for the manufacture of a piece of any shape as it is necessary to lighten and / or provide a passage.
  • the invention therefore relates to a method of manufacturing a shaped piece, consisting in producing a 3 D woven preform, by weaving weft son through a bundle of warp son arranged in different layers and impregnating this preform with a hardenable resin, characterized in that it consists, during weaving # practicing partial debonding between two warp son plies and expanding said preform by creating a desired shape cavity through said loosening and then impregnating said preform, thus shaped, by said resin.
  • Untying is a peculiarity of weaving which consists in not passing through a certain plane of the bundle of warp threads (more exactly a part of this plane) by any weft thread.
  • an advantageous loosening in the context of the invention is obtained by ensuring that, at least from a certain stage of weaving, each weft yarn is woven normally on the sides of the preform being formed. but without ever crossing a central flat area defined between two layers of warp son.
  • the operation of creating said cavity is performed by introducing an inflatable piece in the preform at the location of said looseness and by filling this inflatable piece with a fluid to give it the shape and dimensions of the desired cavity. After impregnation, the fluid and possibly the inflatable piece are extracted from the cavity thus created.
  • the invention also relates to any shaped part obtained by 3D weaving of a preform and by impregnation of this preform by means of a curable resin, characterized in that it comprises a cavity defined by expansion of said preform made possible by a loosening during 3D weaving.
  • the form piece may constitute a rudder or a boat drift.
  • the invention will be better understood and other advantages thereof will appear more clearly in the light of the description which follows. a method of manufacturing a workpiece conforming to its principle, given solely by way of example and with reference to the accompanying drawings, in which:
  • FIG. 1 is a diagrammatic view illustrating the 3D weaving of a preform, for the manufacture of a piece of shape such as a rudder or a boat fin;
  • FIG. 3 schematically illustrates the shaped preform by developing a cavity filled with a rigid material of lower density
  • FIG. 5 is a variant of FIG. 2 schematically illustrating another woven preform; and - Figure 6 schematically illustrates the shaping of the preform of Figure 5.
  • Figure 1 illustrates the weaving of a preform 11 to be converted into a boat rudder.
  • a jacquard loom is used on which a bundle 12 of warp yarns or strands having a number of layers of several hundred threads each is arranged.
  • the mechanism is such that one can act on each of these son transversely to the warp son plies as shown, to insert the weft son 14.
  • a number of warp son are not woven, which allows to define the contour and the desired thickness, continuously variable, said preform.
  • the warp and weft threads are cut at the limit of the woven mass in order to extract the preform 11. This is shown in FIG. 2, as it comes from 3D weaving and before any According to an important characteristic, the weaving is accompanied by a partial loosening 19 between two layers of warp threads and within a planar zone defined by the contour 16, in FIG.
  • this loosening is a particularity of weaving which has the consequence of creating a pocket 18, here open at one end of the woven mass, which can be expanded during a subsequent shaping operation, before impregnation with thermosetting resin.
  • the preform 11 of the future rudder is then shaped by introducing into this pocket 18, a block of low density material 20 having substantially the shape and dimensions of the desired cavity. This operation has the effect of giving the preform a form closer to that of the desired rudder. This is the situation illustrated in Figure 3.
  • the step illustrated in Figure 4 is a conventional step of impregnating the preform with thermosetting resin.
  • the preform formed by the introduction of the block of low density material 20 is transported in a mold 22 forming an oven, for the injection of the thermosetting resin.
  • the rudder is completed by machining and by adding a maneuvering shaft attached to one of its ends. It should be noted that this tree can also be essentially obtained by weaving at one end of the preform. It is also possible to report such an element to one end of the preform, before or after impregnation.
  • Figures 5 and 6 illustrate a variant for the manufacture of a hollow-shaped part forming part of any structure.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Woven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
EP09805775A 2008-12-23 2009-12-22 Procédé de fabrication d'une pièce de forme par tissage 3d et pièce de forme ainsi obtenue. Withdrawn EP2373469A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0858996A FR2940173B1 (fr) 2008-12-23 2008-12-23 Procede de fabrication d'une piece de forme par tissage 3d et piece de forme ainsi obtenue.
PCT/FR2009/052654 WO2010072967A1 (fr) 2008-12-23 2009-12-22 Procédé de fabrication d'une pièce de forme par tissage 3d et pièce de forme ainsi obtenue.

Publications (1)

Publication Number Publication Date
EP2373469A1 true EP2373469A1 (fr) 2011-10-12

Family

ID=40897434

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09805775A Withdrawn EP2373469A1 (fr) 2008-12-23 2009-12-22 Procédé de fabrication d'une pièce de forme par tissage 3d et pièce de forme ainsi obtenue.

Country Status (9)

Country Link
US (1) US20110318513A1 (ru)
EP (1) EP2373469A1 (ru)
JP (1) JP2012513322A (ru)
CN (1) CN102264518A (ru)
BR (1) BRPI0923626A2 (ru)
CA (1) CA2748006A1 (ru)
FR (1) FR2940173B1 (ru)
RU (1) RU2513202C2 (ru)
WO (1) WO2010072967A1 (ru)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9315927B2 (en) 2010-07-12 2016-04-19 Snecma Method for producing a solid part
FR2974752B1 (fr) * 2011-05-06 2013-04-19 Snecma Procede de moulage par injection d'une piece en materiau composite
WO2013088037A2 (fr) * 2011-12-14 2013-06-20 Snecma Metier a tisser avec contexture en chaine optimisee
FR2985940B1 (fr) * 2012-01-25 2014-10-24 Snecma Procede de fabrication d'une pale d'helice en materiau composite
BR112014018031B1 (pt) 2012-01-25 2020-12-01 Safran processo e ferramenta para a fabricação de uma pá de hélice
FR3012064B1 (fr) * 2013-10-23 2016-07-29 Snecma Preforme fibreuse pour aube creuse de turbomachine
FR3032145B1 (fr) * 2015-01-29 2017-02-10 Snecma Procede de fabrication d'une pale d'helice
FR3032648B1 (fr) * 2015-02-16 2017-03-03 Herakles Procede de fabrication d'une aube de turbomachine en materiau composite
US10392731B2 (en) 2015-03-29 2019-08-27 unspun, Inc. Systems and methods for creating three-dimensional woven textile products
WO2017165178A1 (en) * 2016-03-24 2017-09-28 Honda Motor Co., Ltd. Fabric processing method and component
CN106037119A (zh) * 2016-07-25 2016-10-26 信泰(福建)科技有限公司 一体鞋面制造方法及一体编织鞋面
FR3100741B1 (fr) * 2019-09-13 2021-09-10 Safran Dispositif de fabrication d’une piece creuse
FR3107299B1 (fr) 2020-02-14 2022-03-11 Safran Aircraft Engines Aube en matériau composite pour stator de turbomachine comprenant un noyau creux en plastique non poreux
FR3109115B1 (fr) 2020-04-10 2024-04-05 Safran Aircraft Engines Procede de fabrication d’une preforme pour une piece en materiau composite de turbomachine et piece correspondante
CN112680867B (zh) * 2020-12-11 2022-05-10 江苏恒力化纤股份有限公司 一种安全气囊及其制备方法
GB2620928A (en) * 2022-07-25 2024-01-31 Rolls Royce Plc Woven structure and method of manufacture
GB2620927A (en) * 2022-07-25 2024-01-31 Rolls Royce Plc Woven structure and method of manufacture

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3102559A (en) * 1959-12-24 1963-09-03 Raymond Dev Ind Inc Woven honeycomb cellular fabrics
US3965942A (en) * 1972-09-20 1976-06-29 Hitco Multi-ply woven article having stiffening elements between double plies
EP0607168B1 (en) * 1991-09-12 1997-11-26 Finnclever Oy A method for manufacturing a laminating reinforced fibre structure and a corresponding reinforced fibre structure
US20070175577A1 (en) * 2005-01-26 2007-08-02 Dagher Habib J Composite construction members and method of making

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3779789A (en) * 1971-04-20 1973-12-18 Celanese Corp Production of pervious low density carbon fiber reinforced composite articles
KR930006866B1 (ko) 1984-09-07 1993-07-24 쏘니 가부시기가이샤 텔레비젼신호의 움직임검출회로
JPS61220830A (ja) * 1985-03-27 1986-10-01 Sumitomo Electric Ind Ltd 繊維強化プラスチツクス製パイプの製造方法
JPS63115578A (ja) * 1986-10-31 1988-05-20 ヤマハ発動機株式会社 ボ−ド
JPH0814054B2 (ja) * 1989-02-16 1996-02-14 株式会社豊田自動織機製作所 三次元織物及びその製造方法
US5156786A (en) * 1990-07-02 1992-10-20 Hudson Products Corporation Method for manufacuring fan blades
US5346774A (en) * 1992-02-27 1994-09-13 Techniweave, Inc. Fiber-reinforced composite structures, and methods of making same
JPH06134878A (ja) * 1992-10-29 1994-05-17 Teijin Ltd 複合成形品の製造方法
FR2699498B1 (fr) * 1992-12-23 1995-03-10 Eurocopter France Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication.
JPH0781664A (ja) * 1993-09-17 1995-03-28 Takashi Hayashizaki ヨット様の水上遊戯具
JPH10151692A (ja) * 1996-11-21 1998-06-09 Toray Ind Inc 繊維強化プラスチック製品
JP2006150614A (ja) * 2004-11-25 2006-06-15 Toho Tenax Co Ltd Frp製中空部材の樹脂トランスファー成形法
FR2907707B1 (fr) * 2006-10-26 2009-01-30 Snecma Sa Procede de fabrication d'une aube temoin en materiau composite
JP2008159457A (ja) * 2006-12-25 2008-07-10 Momo Alliance Co Ltd 照明装置

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3102559A (en) * 1959-12-24 1963-09-03 Raymond Dev Ind Inc Woven honeycomb cellular fabrics
US3965942A (en) * 1972-09-20 1976-06-29 Hitco Multi-ply woven article having stiffening elements between double plies
EP0607168B1 (en) * 1991-09-12 1997-11-26 Finnclever Oy A method for manufacturing a laminating reinforced fibre structure and a corresponding reinforced fibre structure
US20070175577A1 (en) * 2005-01-26 2007-08-02 Dagher Habib J Composite construction members and method of making

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO2010072967A1 *

Also Published As

Publication number Publication date
FR2940173A1 (fr) 2010-06-25
CA2748006A1 (fr) 2010-07-01
FR2940173B1 (fr) 2013-02-08
WO2010072967A1 (fr) 2010-07-01
CN102264518A (zh) 2011-11-30
US20110318513A1 (en) 2011-12-29
BRPI0923626A2 (pt) 2016-01-19
JP2012513322A (ja) 2012-06-14
RU2513202C2 (ru) 2014-04-20
RU2011130855A (ru) 2013-01-27

Similar Documents

Publication Publication Date Title
WO2010072967A1 (fr) Procédé de fabrication d'une pièce de forme par tissage 3d et pièce de forme ainsi obtenue.
EP3393764B1 (fr) Carter allégé en matériau composite et son procédé de fabrication
EP3052286B1 (fr) Ensemble de compactage et procede de fabrication d'une aube composite de turbomachine
CA2858320C (fr) Structure fibreuse tissee en une seule piece par tissage 3d et application a la fabrication de piece en materiau composite.
CA2784740C (fr) Pale d'helice d'aeronef
EP3052304B1 (fr) Procédé et ensemble de fabrication d'aube composite
CA2804098A1 (fr) Aube a longeron composite integre
FR2861143A1 (fr) Aube de turbomachine, notamment aube de soufflante et son procede de fabrication
CA3004161C (fr) Procede de fabrication d'une piece en materiau composite comprenant un corps solidaire d'une ou plusieurs plates-formes
EP4051476B1 (fr) Preforme fibreuse tissee pour realiser une piece en materiau composite, notamment une aube de turbomachine
EP4077884B1 (fr) Aube de soufflante ou d'helice pour une turbomachine d'aeronef et procédé de fabrication
EP4051477B1 (fr) Preforme fibreuse tissee pour realiser une aube de soufflante en materiau composite
WO2020021185A1 (fr) Texture fibreuse pour carter en materiau composite a resistance a l'impact amelioree
FR3045448A1 (fr) Carter allege en materiau composite et son procede de fabrication
FR3097799A1 (fr) Pièce de révolution en matériau composite ayant une résistance au délaminage améliorée
EP2828426A1 (fr) Procédé de fabrication d'une préforme monobloc pour structure composite
FR3108666A1 (fr) Texture fibreuse pour aube de turbomachine en matériau composite
FR3134338A1 (fr) Mise en forme reproductible d’une ébauche fibreuse
EP4363204A1 (fr) Mise en forme reproductible d'une ébauche fibreuse
WO2023067286A1 (fr) Procede de fabrication d'une piece en materiau composite
FR3137013A1 (fr) Procédé de fabrication d’une pièce en matériau composite destinée à être articulée avec d’autres pièces
WO2023247868A1 (fr) Renfort fibreux pour la fabrication d'une pièce composite destinée à être articulée avec d'autres pièces
EP4308792A1 (fr) Piece de turbomachine composite formee d'une ame entouree par deux preformes fibreuses tissees 3d

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20110704

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

DAX Request for extension of the european patent (deleted)
17Q First examination report despatched

Effective date: 20140507

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: SAFRAN AIRCRAFT ENGINES

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20190917