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특허 상세정보

Method for making parts in composite material with thermoplastic matrix

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B29C-065/40    B29C-070/32    B29C-051/02    B29C-053/04   
미국특허분류(USC) 264/102; 264/160; 264/248; 264/250; 264/255; 264/257; 264/258; 264/310; 264/324; 264/339; 264/510; 264/511; 264/512; 156/189; 156/297
출원번호 US-0462748 (2000-05-03)
우선권정보 FR-0009265 (1997-07-22)
국제출원번호 PCT/FR98/01584 (1998-07-20)
국제공개번호 WO99/04952 (1999-02-04)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Thelen Reid & Priest LLP
인용정보 피인용 횟수 : 78  인용 특허 : 9
초록

A process is proposed for the fabrication of parts with large dimensions formed of a skin (10) and stiffeners (12, 16) such as aircraft fuselage segments made of a composite material with a thermoplastic matrix. After stiffeners have been made separately by lay-up, consolidation and shaping, these stiffeners are placed on a tooling (23) and the skin (10) is simultaneously fabricated and assembled to the stiffeners (12, 16) by diffusion welding. More precisely, the skin (10) is laid up and continuously consolidated by the lay-up head (36) such that the re...

대표
청구항

1. Fabrication process for parts from a composite material comprising a skin and stiffeners, the process comprising: separately fabricating stiffeners by lay-up, consolidation and shaping, starting from a strip of long fibers impregnated with thermoplastic resin; placing the stiffeners on a tooling with a shape complementary to the shape of the part to be fabricated; simultaneously fabricating and assembling the skin with the stiffeners by lay-up and continuous consolidation of strips of long fibers impregnated with thermoplastic resin, directly on ...

이 특허를 인용한 특허 피인용횟수: 78

  1. Mores, Sebastian; Barnerssoi, Johann; Probst, Stefan; Schneeberger, Marco; Jutt, Hartmut. Aircraft framework structure with integral ventilation air duct. USP2018019873512.
  2. Noebel, Torsten. Aircraft fuselage reinforcement system. USP2016019227717.
  3. Haack, Cord. Aircraft fuselage structure and method for its production. USP2014028651421.
  4. Schroeer, Thorsten; Roming, Thorsten. Aircraft fuselage structure and method for its production. USP2014048695922.
  5. Haack, Cord. Aircraft fuselage structure and method for producing it. USP2013098534605.
  6. Porte, Alain; Fargues, Matthieu; Marro, Martial. Aircraft nacelle comprising a reinforced connection between an air intake and a powerplant. USP2017029567905.
  7. Stephens, Jeffrey Scott; Bye, Steven Douglas; Day, Dan. Apparatus for co-curing composite skins and stiffeners in an autoclave. USP2017089738039.
  8. Boone, Richard; De Putter, Benjamin. Assembly using skeleton structure. USP2017059649820.
  9. Boone, Richard; De Putter, Benjamin. Assembly using skeleton structure. USP2015069051062.
  10. Collins, Alexandra; Collins, Mark. Commercial aircraft passenger cabin seat and partition. USP201207D663256.
  11. Lee, Shin S.; Viisoreanu, Adrian; Koch, William J.. Composite aircraft structures with hat stiffeners. USP2011017871040.
  12. Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H.. Composite barrel sections for aircraft fuselages and other structures. USP2013028382037.
  13. Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H.. Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections. USP2009057527222.
  14. Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H.. Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections. USP2012048157212.
  15. Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H.. Composite barrel sections for aircraft fuselages and other structures, and methods for systems for manufacturing such barrel sections. USP2012058182628.
  16. Velicki, Alexander; Thrash, Patrick J.. Composite fabric with rigid member structure. USP2011108042767.
  17. Robins, Brian G.; Rotter, Daniel M.; Washburn, Todd J.; George, Panagiotis E.. Composite mandrel for autoclave curing applications. USP2016059327467.
  18. Chapman, Michael R.; Watson, Robert M.; Anderson, Donald A.; Piehl, Marc J.; Sweetin, Joseph L.; Grose, Douglas L.. Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections. USP2012058168023.
  19. Chapman, Michael R.; Watson, Robert M.; Anderson, Donald A.; Piehl, Marc J.; Sweetin, Joseph L.; Grose, Douglas L.. Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections. USP2013048418740.
  20. Chapman,Michael R.; Watson,Robert M.; Anderson,Donald A.; Piehl,Marc J.; Sweetin,Joseph L.; Grose,Douglas L.. Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections. USP2009037503368.
  21. Lloyd, James. Composite structure. USP2012108283018.
  22. Weidmann, Bjorn; Rudqvist, Claes; Krogager, Max; Petersson, Mikael. Curved beam of fiber composite material. USP2012048151529.
  23. Kehrl, David J.; Johnson, Kent E.; McCarville, Douglas A.. Curved composite frames and method of making the same. USP2015089096305.
  24. Kehrl, David J.; Johnson, Kent E.; McCarville, Douglas A.. Curved composite frames and method of making the same. USP2013018349105.
  25. Barlag, Carsten; Steiger, Christian; Deschauer, Niels. Device and method for manufacturing a fiber-reinforced composite fuselage shell for an aircraft. USP2014128911585.
  26. Jessrang, Mathias. Device for producing a fiber-reinforced thermoplastic composite component. USP20180710029426.
  27. Hugon, Michael; Pelard, Alexandre; Soubelet, Dominique. Double-sided stiffened composite panel and method for producing such a panel. USP2015119193433.
  28. Tacke, Stefan; Roming, Thorsten. Fiber composite component for absorbing energy. USP2015079079653.
  29. Boone, Richard; de Putter, Benjamin. Formation of complex composite structures using laminate templates. USP20180610005267.
  30. Robins, Brian G.; Willden, Kurtis; Hunter, Ethan W.; McManus, Nika. Mandrel for autoclave curing applications. USP2016019238335.
  31. Yip, Thomas A.; Decoux, Steve P.. Manufacturing process using bladderless mold line conformal hat stringer. USP2011108043554.
  32. Jessrang, Mathias. Method and a device for the manufacture of a fibre-reinforced thermoplastic composite module. USP2015099126376.
  33. Maille, Laurence; Mouton, Luc. Method and apparatus for manufacturing a helicopter rotor fairing, and a fairing obtained thereby. USP2010037676923.
  34. Guzman, Juan Carlos; McCarville, Douglas Alan; Sweetin, Joseph L.; Messinger, Ross. Method and apparatus for producing contoured composite structures and structures produced thereby. USP2016039278484.
  35. Duqueine, Gilles; Aubry, Jerome. Method and device for moulding a curved part made from composite material and corresponding part. USP2014038663526.
  36. Stephens, Jeffrey Scott; Bye, Steven Douglas; Day, Dan. Method for co-curing composite skins and stiffeners in an autoclave. USP2016059333713.
  37. Burgos Gallego, Raúl; Villarrubia Cortés, José. Method for designing a composite material part with a curved surface. USP2014068751197.
  38. Weidmann, Björn; Rudqvist, Claes; Krogager, Max; Petersson, Mikael. Method for fabricating a curved beam from composite material. USP2010037670525.
  39. Cacciaguerra, Bruno. Method for fabricating an aircraft fuselage in composite material. USP2012078220154.
  40. Kurtz, Didier; Chotard, Florian. Method for finished-rib compacting a thermoplastic composite part with continuous fibers. USP2014058721830.
  41. Ingram, Jr., William H.; Dull, Kenneth M.; Biornstad, Robert. Method for minimizing fiber distortion during fabrication of one-piece composite barrel section. USP2014048691037.
  42. Blot, Philippe; Colmargo, Jerome; Soula, Denis; Guillemaut, Julien; Le Hetet, Thomas; Guittard, Dominique. Method for producing a central wing box. USP2015089114582.
  43. McCarville, Douglas A.; Stickler, Patrick B.; Guzman, Juan C.; Noel, Jennifer S.; Sweetin, Joseph L.. Method for producing contoured composite structures and structures produced thereby. USP2015079090028.
  44. McCarville, Douglas A.; Sweetin, Joseph L.; Guzman, Juan C.. Method for producing contoured composite structures and structures produced thereby. USP2015018932423.
  45. Simpson,Craig B.; Allman,Mike G.; Tuttle,Steven T.; Ashton,Larry J.. Method of assembling a single piece co-cured structure. USP2007057216832.
  46. Kurtz, Didier; Vaudour, Julie. Method of forming a composite thermoplastic material with continuous fiber reinforcement by stamping. USP20180710016931.
  47. Goodworth, Alan R.; Anthony, James A.; Forster, William V.. Method of forming panels using an in-situ tape placement process and panels formed therefrom. USP2011108043458.
  48. Brown, Todd A.; Friddell, Stephen Douglas; Harris, Christopher G.; Modin, Andrew E.. Method of manufacturing curved composite structural elements. USP2017049630390.
  49. Brown, Todd A.; Friddell, Stephen Douglas; Harris, Christopher G.; Modin, Andrew E.. Method of manufacturing curved composite structural elements. USP2014018632653.
  50. Frankel, Kenneth A.. Methods for forming fiber reinforced composite parts having one or more selectively positioned core, structural insert, or veneer pieces integrally associated therewith. USP2009127638084.
  51. Chapman, Michael R.; Watson, Robert M.; Anderson, Donald A.; Piehl, Marc J.; Sweetin, Joseph L.; Grose, Douglas L.. Methods for manufacturing composite sections for aircraft fuselages and other structures. USP2012118303758.
  52. Johnson, Kent E.; Ulvin, Mark A.. Methods of manufacturing structural panels. USP2010057716835.
  53. Sarh, Branko. Multi-ring system for fuselage barrel formation. USP2012058173055.
  54. Sarh,Branko. Multi-ring system for fuselage barrel formation. USP2008087410352.
  55. Johnson,Brice A.; Spoon,Stephen S.; Darras,Randal S.. Multiple head automated composite laminating machine for the fabrication of large barrel section components. USP2007107282107.
  56. Tsotsis, Thomas K.. Nanotube-enhanced interlayers for composite structures. USP2014028657990.
  57. Tsotsis, Thomas K.. Nanotube-enhanced interlayers for composite structures. USP2013038388795.
  58. Anderson,Alan H.; Bowman,Kathlene K.; Teufel,Paul D.. One-piece closed-shape structure and method of forming same. USP2008107431239.
  59. Pham, Doan D.; Tollan, Mark W.. One-piece inner shell for full barrel composite fuselage. USP2012018091603.
  60. Pham, Doan D.; Tollan, Mark W.. One-piece inner shell for full barrel composite fuselage. USP2013098524025.
  61. Pham,Doan D.; Tollan,Mark W.. One-piece inner shell for full barrel composite fuselage. USP2008127459048.
  62. Bock, Thomas-Mathias. Partition for a commercial aircraft passenger cabin. USP201008D621329.
  63. Bock, Thomas-Mathias. Partition for a commercial aircraft passenger cabin. USP201008D621330.
  64. Bock, Thomas-Mathias. Partition for a commercial aircraft passenger cabin. USP201008D621331.
  65. Lieven, Patrick; Delahaye, Romain. Self-stiffened skin for aircraft fuselage including stringers with a closed section and associated manufacturing method. USP2016099446834.
  66. Bock, Thomas-Mathias. Set of partitions for a commercial aircraft passenger cabin. USP201005D615919.
  67. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2017089738371.
  68. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2011118061035.
  69. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2014108869403.
  70. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2014118882040.
  71. Stulc,Jeffrey F.; Chan,Wallace C.; Clapp,Brian C.; Rolfes,Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2008027325771.
  72. Marcoe, Jeffery L.. Stabilizer torque box assembly and method. USP2017119808996.
  73. Fischer, Christian; Rion, Julien. Stiffened thin-walled fibre composite products and method of making same. USP20180910071528.
  74. Horstman, Hugh L.. Storage vessel for compressed fluids. USP2018059981461.
  75. Grantham,Kent; Harrison,Thomas D.; Kay,Robert M.; Kuss,Michael R.; Turnmire,William W.; Venskus,Mark K.; Whitcomb,Tory R.; Christie, legal representative,Rose; Christie, deceased,Peter S.. Structural panels for use in aircraft fuselages and other structures. USP2007017159822.
  76. Johnson, Kent E.; Ulvin, Mark A.. Structural panels for use in aircraft fuselages and other structures. USP2013078496206.
  77. Johnson,Kent; Ulvin,Mark A.. Structural panels for use in aircraft fuselages and other structures. USP2006117134629.
  78. Martinez Cerezo, Alberto Ramon; Arevalo Rodriguez, Elena; Galiana Blanco, Jorge Juan; Jordan Carnicero, Francisco Javier. Tubular components for aeronautical fuselages and processes and jigs for its manufacturing. USP2009107597772.