FR2683764B1 - Procede de fabrication d'une aube de turbomachine realisee en materiau composite. - Google Patents

Procede de fabrication d'une aube de turbomachine realisee en materiau composite.

Info

Publication number
FR2683764B1
FR2683764B1 FR9114067A FR9114067A FR2683764B1 FR 2683764 B1 FR2683764 B1 FR 2683764B1 FR 9114067 A FR9114067 A FR 9114067A FR 9114067 A FR9114067 A FR 9114067A FR 2683764 B1 FR2683764 B1 FR 2683764B1
Authority
FR
France
Prior art keywords
manufacturing
composite material
blade made
turbomachine blade
turbomachine
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.)
Expired - Lifetime
Application number
FR9114067A
Other languages
English (en)
Other versions
FR2683764A1 (fr
Inventor
Robert Imbault Jean-Francois
Claudine Planquet
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
Priority to FR9114067A priority Critical patent/FR2683764B1/fr
Publication of FR2683764A1 publication Critical patent/FR2683764A1/fr
Application granted granted Critical
Publication of FR2683764B1 publication Critical patent/FR2683764B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0025—Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68—Shaping 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
    • B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR9114067A 1991-11-15 1991-11-15 Procede de fabrication d'une aube de turbomachine realisee en materiau composite. Expired - Lifetime FR2683764B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9114067A FR2683764B1 (fr) 1991-11-15 1991-11-15 Procede de fabrication d'une aube de turbomachine realisee en materiau composite.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9114067A FR2683764B1 (fr) 1991-11-15 1991-11-15 Procede de fabrication d'une aube de turbomachine realisee en materiau composite.

Publications (2)

Publication Number Publication Date
FR2683764A1 FR2683764A1 (fr) 1993-05-21
FR2683764B1 true FR2683764B1 (fr) 1995-03-24

Family

ID=9418955

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9114067A Expired - Lifetime FR2683764B1 (fr) 1991-11-15 1991-11-15 Procede de fabrication d'une aube de turbomachine realisee en materiau composite.

Country Status (1)

Country Link
FR (1) FR2683764B1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2740378B1 (fr) * 1995-10-30 1998-01-02 Eurocopter France Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere, et pale a pas variable pouvant etre obtenue par un tel procede
FR2740379B1 (fr) * 1995-10-30 1998-01-02 Eurocopter France Procede de fabrication d'une pale en materiau composite pour rotor d'helicoptere, et pale pouvant etre obtenue par un tel procede
FR2740380B1 (fr) * 1995-10-30 1998-01-02 Eurocopter France Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere
GB0908707D0 (en) 2009-05-21 2009-07-01 Rolls Royce Plc Reinforced composite aerofoil blade
US8556579B2 (en) 2009-05-21 2013-10-15 Rolls-Royce Plc Composite aerofoil blade with wear-resistant tip
FR2970943B1 (fr) 2011-01-31 2014-02-28 Eurocopter France Pale et procede de fabrication de ladite pale
FR2985927B1 (fr) * 2012-01-25 2014-12-26 Snecma Outillage de fabrication d'une pale d'helice, comprenant un patin de serrage
FR2985940B1 (fr) * 2012-01-25 2014-10-24 Snecma Procede de fabrication d'une pale d'helice en materiau composite
CN104105581B (zh) 2012-01-25 2016-08-17 斯奈克玛 由复合材料制造螺旋桨叶片的方法
FR2985928B1 (fr) * 2012-01-25 2014-03-07 Snecma Outillage de fabrication d'une pale d'helice, comprenant un dispositif ecarteur

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL257765A (fr) * 1960-11-09 1900-01-01
FR1433773A (fr) * 1964-04-30 1966-04-01 Thomson Houston Comp Francaise Perfectionnements aux procédés de fabrication d'objets en plastique multicellulaire
DD100058A1 (de) * 1972-10-12 1980-10-01 Schaufeln für Axialventilatoren und Verfahren zur Herstellung dieser Schaufeln
DE3840191A1 (de) * 1987-12-03 1989-06-15 Barmag Barmer Maschf Verfahren zum verstaerken eines endlichen werkstuecks

Also Published As

Publication number Publication date
FR2683764A1 (fr) 1993-05-21

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CD Change of name or company name
TP Transmission of property
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