FR3103557B1 - Dispositif de maintien en compaction d’une texture fibreuse pour la caractérisation de matériaux composites - Google Patents

Dispositif de maintien en compaction d’une texture fibreuse pour la caractérisation de matériaux composites Download PDF

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Publication number
FR3103557B1
FR3103557B1 FR1913079A FR1913079A FR3103557B1 FR 3103557 B1 FR3103557 B1 FR 3103557B1 FR 1913079 A FR1913079 A FR 1913079A FR 1913079 A FR1913079 A FR 1913079A FR 3103557 B1 FR3103557 B1 FR 3103557B1
Authority
FR
France
Prior art keywords
compaction
fibrous texture
composite materials
maintaining
characterization
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
FR1913079A
Other languages
English (en)
Other versions
FR3103557A1 (fr
Inventor
Yanneck Wielhorski
Adrien Francis Paixao
Julien Schneider
Teddy Fixy
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
Safran Aircraft Engines 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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1913079A priority Critical patent/FR3103557B1/fr
Publication of FR3103557A1 publication Critical patent/FR3103557A1/fr
Application granted granted Critical
Publication of FR3103557B1 publication Critical patent/FR3103557B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • B29C70/04Shaping 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
    • 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
    • B29C33/20Opening, closing or clamping
    • B29C33/22Opening, closing or clamping by rectilinear movement
    • 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
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • 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
    • B29L2031/08Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2223/00Investigating materials by wave or particle radiation
    • G01N2223/40Imaging
    • G01N2223/419Imaging computed tomograph
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2223/00Investigating materials by wave or particle radiation
    • G01N2223/60Specific applications or type of materials
    • G01N2223/615Specific applications or type of materials composite materials, multilayer laminates
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2223/00Investigating materials by wave or particle radiation
    • G01N2223/60Specific applications or type of materials
    • G01N2223/63Specific applications or type of materials turbine blades

Abstract

Dispositif de maintien en compaction d’une texture fibreuse pour la caractérisation de matériaux composites Un dispositif de maintien (100) d’un effort de compaction sur une texture fibreuse comprend des premier et deuxième éléments de compaction (110, 120) en regard l’un de l’autre. Les premier et deuxième éléments de compaction sont mobiles l’un par rapport à l’autre de manière à définir entre eux un logement à hauteur variable pour une texture fibreuse (10). Le dispositif de maintien comprend en outre des organes de serrage (150, 152, 153, 154, 156, 157) aptes à maintenir les premier et deuxième éléments de compaction (110, 120) à une distance déterminée (Dc) l’un de l’autre correspondant à un effort de compaction déterminé (PC) sur la texture fibreuse. Chacun des premier et deuxième éléments de compaction présente un taux de transmittance des rayons supérieur ou égal à 20%. Figure pour l’abrégé : Fig. 2.
FR1913079A 2019-11-22 2019-11-22 Dispositif de maintien en compaction d’une texture fibreuse pour la caractérisation de matériaux composites Active FR3103557B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1913079A FR3103557B1 (fr) 2019-11-22 2019-11-22 Dispositif de maintien en compaction d’une texture fibreuse pour la caractérisation de matériaux composites

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1913079A FR3103557B1 (fr) 2019-11-22 2019-11-22 Dispositif de maintien en compaction d’une texture fibreuse pour la caractérisation de matériaux composites
FR1913079 2019-11-22

Publications (2)

Publication Number Publication Date
FR3103557A1 FR3103557A1 (fr) 2021-05-28
FR3103557B1 true FR3103557B1 (fr) 2022-11-11

Family

ID=69811069

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1913079A Active FR3103557B1 (fr) 2019-11-22 2019-11-22 Dispositif de maintien en compaction d’une texture fibreuse pour la caractérisation de matériaux composites

Country Status (1)

Country Link
FR (1) FR3103557B1 (fr)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2939129B1 (fr) 2008-11-28 2014-08-22 Snecma Propulsion Solide Aube de turbomachine en materiau composite et procede pour sa fabrication.
FR2990025B1 (fr) * 2012-04-25 2019-06-21 Safran Aircraft Engines Dispositif d'essai pour la visualisation par tomographie des chemins preferentiels d'ecoulement de resine dans une preforme fibreuse
FR3010523B1 (fr) 2013-09-06 2015-09-25 Safran Procede de caracterisation d'une piece en materiau composite
FR3034339B1 (fr) * 2015-04-01 2017-11-24 Herakles Procede de controle de la repartition des fils d'une texture fibreuse

Also Published As

Publication number Publication date
FR3103557A1 (fr) 2021-05-28

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