FR3013252B1 - HYBRID MANUFACTURING METHOD OF A RECTIFIER BLADE FOR AERONAUTICAL GAS TURBINE ENGINE - Google Patents

HYBRID MANUFACTURING METHOD OF A RECTIFIER BLADE FOR AERONAUTICAL GAS TURBINE ENGINE

Info

Publication number
FR3013252B1
FR3013252B1 FR1361390A FR1361390A FR3013252B1 FR 3013252 B1 FR3013252 B1 FR 3013252B1 FR 1361390 A FR1361390 A FR 1361390A FR 1361390 A FR1361390 A FR 1361390A FR 3013252 B1 FR3013252 B1 FR 3013252B1
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
hybrid manufacturing
rectifier blade
aeronautical gas
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
FR1361390A
Other languages
French (fr)
Other versions
FR3013252A1 (en
Inventor
Sebastien Pautard
Mathieu Renaud
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 SA
Original Assignee
Safran 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 Safran SA filed Critical Safran SA
Priority to FR1361390A priority Critical patent/FR3013252B1/en
Priority to PCT/FR2014/052850 priority patent/WO2015075347A1/en
Publication of FR3013252A1 publication Critical patent/FR3013252A1/en
Application granted granted Critical
Publication of FR3013252B1 publication Critical patent/FR3013252B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46—Shaping 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
    • B29C70/467—Shaping 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 during mould closing
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46—Shaping 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
    • B29C70/48—Shaping 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
    • 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
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • 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
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)
FR1361390A 2013-11-20 2013-11-20 HYBRID MANUFACTURING METHOD OF A RECTIFIER BLADE FOR AERONAUTICAL GAS TURBINE ENGINE Active FR3013252B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1361390A FR3013252B1 (en) 2013-11-20 2013-11-20 HYBRID MANUFACTURING METHOD OF A RECTIFIER BLADE FOR AERONAUTICAL GAS TURBINE ENGINE
PCT/FR2014/052850 WO2015075347A1 (en) 2013-11-20 2014-11-07 Method for hybrid manufacturing of a straightener vane for an aircraft gas-turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1361390A FR3013252B1 (en) 2013-11-20 2013-11-20 HYBRID MANUFACTURING METHOD OF A RECTIFIER BLADE FOR AERONAUTICAL GAS TURBINE ENGINE

Publications (2)

Publication Number Publication Date
FR3013252A1 FR3013252A1 (en) 2015-05-22
FR3013252B1 true FR3013252B1 (en) 2015-12-18

Family

ID=49917154

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1361390A Active FR3013252B1 (en) 2013-11-20 2013-11-20 HYBRID MANUFACTURING METHOD OF A RECTIFIER BLADE FOR AERONAUTICAL GAS TURBINE ENGINE

Country Status (2)

Country Link
FR (1) FR3013252B1 (en)
WO (1) WO2015075347A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3100741B1 (en) * 2019-09-13 2021-09-10 Safran HOLLOW PART MANUFACTURING DEVICE
US11352891B2 (en) 2020-10-19 2022-06-07 Pratt & Whitney Canada Corp. Method for manufacturing a composite guide vane having a metallic leading edge

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992020503A1 (en) * 1991-05-24 1992-11-26 Dow-United Technologies Composite Products, Inc. Braided complex composite parts and methods of forming same
IT1397058B1 (en) * 2009-11-23 2012-12-28 Nuovo Pignone Spa CENTRIFUGAL IMPELLER MOLD, MOLD INSERTS AND METHOD TO BUILD A CENTRIFUGAL IMPELLER
FR2953225B1 (en) * 2009-11-30 2012-03-02 Snecma COMPONENT COMPRISING REINFORCING YARNS IN THE FORM OF CHAIN YARNS AND THREE-DIMENSIONED WOVEN FABRIC YARNS.

Also Published As

Publication number Publication date
WO2015075347A1 (en) 2015-05-28
FR3013252A1 (en) 2015-05-22

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