FR3003668B1 - Procede de conception d'une preforme commune pour la realisation de preformes d'aubes directrices de sortie de turbomachine en materiau composite a profils geometriques differents - Google Patents
Procede de conception d'une preforme commune pour la realisation de preformes d'aubes directrices de sortie de turbomachine en materiau composite a profils geometriques differents Download PDFInfo
- Publication number
- FR3003668B1 FR3003668B1 FR1352638A FR1352638A FR3003668B1 FR 3003668 B1 FR3003668 B1 FR 3003668B1 FR 1352638 A FR1352638 A FR 1352638A FR 1352638 A FR1352638 A FR 1352638A FR 3003668 B1 FR3003668 B1 FR 3003668B1
- Authority
- FR
- France
- Prior art keywords
- preforms
- guide vane
- geometric profiles
- designing
- composite material
- 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
Links
- 239000002131 composite material Substances 0.000 title abstract 2
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/17—Mechanical parametric or variational design
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B11/00—Making preforms
- B29B11/14—Making preforms characterised by structure or composition
- B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
-
- 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
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/10—Processes of additive manufacturing
- B29C64/106—Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/005—Selecting particular materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/20—Design optimisation, verification or simulation
-
- 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
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous 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
-
- 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)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Theoretical Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Geometry (AREA)
- General Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Evolutionary Computation (AREA)
- Computer Hardware Design (AREA)
- Manufacturing & Machinery (AREA)
- Optics & Photonics (AREA)
- Computational Mathematics (AREA)
- Mathematical Analysis (AREA)
- Mathematical Optimization (AREA)
- Pure & Applied Mathematics (AREA)
- Moulding By Coating Moulds (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1352638A FR3003668B1 (fr) | 2013-03-25 | 2013-03-25 | Procede de conception d'une preforme commune pour la realisation de preformes d'aubes directrices de sortie de turbomachine en materiau composite a profils geometriques differents |
PCT/FR2014/050670 WO2014154981A1 (fr) | 2013-03-25 | 2014-03-21 | Procede de conception d'une preforme commune pour la realisation de preformes d'aubes directrices de sortie de turbomachine en materiau composite a profils geometriques differents. |
US14/863,871 US10019549B2 (en) | 2013-03-25 | 2015-09-24 | Method of designing a common preform for providing preforms for turbine engine outlet guide vanes of different geometrical profiles and made out of composite material |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1352638A FR3003668B1 (fr) | 2013-03-25 | 2013-03-25 | Procede de conception d'une preforme commune pour la realisation de preformes d'aubes directrices de sortie de turbomachine en materiau composite a profils geometriques differents |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3003668A1 FR3003668A1 (fr) | 2014-09-26 |
FR3003668B1 true FR3003668B1 (fr) | 2020-10-30 |
Family
ID=48979886
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1352638A Active FR3003668B1 (fr) | 2013-03-25 | 2013-03-25 | Procede de conception d'une preforme commune pour la realisation de preformes d'aubes directrices de sortie de turbomachine en materiau composite a profils geometriques differents |
Country Status (3)
Country | Link |
---|---|
US (1) | US10019549B2 (fr) |
FR (1) | FR3003668B1 (fr) |
WO (1) | WO2014154981A1 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201513321D0 (en) | 2015-07-29 | 2015-09-09 | Rolls Royce Plc | Methods of estimating a precursor shape for a part to be manufactured |
FR3071765B1 (fr) | 2017-10-03 | 2020-11-20 | Safran Ceram | Realisation en materiau composite d'une structure a lobes de melangeur de flux |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6843565B2 (en) * | 2002-08-02 | 2005-01-18 | General Electric Company | Laser projection system to facilitate layup of complex composite shapes |
FR2861143B1 (fr) * | 2003-10-20 | 2006-01-20 | Snecma Moteurs | Aube de turbomachine, notamment aube de soufflante et son procede de fabrication |
FR2933634B1 (fr) * | 2008-07-10 | 2010-08-27 | Snecma | Aube redresseur de soufflante en composite 3d |
EP2472063B1 (fr) * | 2010-12-30 | 2015-02-11 | Techspace Aero S.A. | Aube en matériau composite |
US20130052004A1 (en) * | 2011-08-25 | 2013-02-28 | Nicholas D. Stilin | Structural composite fan exit guide vane for a turbomachine |
WO2013088040A2 (fr) | 2011-12-14 | 2013-06-20 | Snecma | Structure fibreuse tissee en une seule piece par tissage 3d et application a la fabrication de piece en materiau composite |
-
2013
- 2013-03-25 FR FR1352638A patent/FR3003668B1/fr active Active
-
2014
- 2014-03-21 WO PCT/FR2014/050670 patent/WO2014154981A1/fr active Application Filing
-
2015
- 2015-09-24 US US14/863,871 patent/US10019549B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US10019549B2 (en) | 2018-07-10 |
FR3003668A1 (fr) | 2014-09-26 |
US20160012178A1 (en) | 2016-01-14 |
WO2014154981A1 (fr) | 2014-10-02 |
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Legal Events
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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CD | Change of name or company name |
Owner name: SNECMA, FR Effective date: 20170713 Owner name: SAFRAN, FR Effective date: 20170713 |
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Year of fee payment: 6 |
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Year of fee payment: 8 |
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Year of fee payment: 10 |
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Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |