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Composite material-stiffened panel and manufacturing method thereof 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B32B-003/06
출원번호 US-0717514 (2003-11-21)
우선권정보 JP-2000-390312(2000-12-22)
발명자 / 주소
  • Toi,Yasuhiro
  • Noda,Masahiro
  • Harada,Atsushi
  • Tanaka,Shigeki
출원인 / 주소
  • Fuji Jukogyo Kabushiki Kaisha
대리인 / 주소
    Smith, Gambrell &
인용정보 피인용 횟수 : 73  인용 특허 : 6

초록

A composite material-stiffened panel has a skin obtained by molding a fiber-reinforced resin composite material into a flat skin, stiffeners arranged in rows on one surface of the skin, and a fiber-reinforced resin-composite material stitched on the skin covering the stiffeners. The composite materi

대표청구항

What is claimed is: 1. A composite material-stiffened panel, comprising: a skin of fiber-reinforced resin composite material; stiffeners with flange portions arranged in rows on one surface of said skin; and a fiber-reinforced resin-composite material covering that covers at least some of said stif

이 특허에 인용된 특허 (6)

  1. Hamm Robert A. (Bellevue WA), Advanced composite.
  2. Willden Kurtis S. (Kent WA) Goodno Kenneth N. (Federal Way WA), Caul and method for bonding and curing intricate composite structures.
  3. Palmer Raymond J. ; Palmer Michael B. ; Weege Thomas, Immersion process for impregnation of resin into preforms.
  4. Tunis ; III George C. ; Winckler Steven J., Large composite core structures formed by vacuum assisted resin transfer molding.
  5. Le Comte Adolf (101 Harbor La. West New Rochelle NY 10805), Method for manufacturing a large-sized object of fiber reinforced synthetic resin.
  6. Palmer Raymond J., Stitch-reinforced sandwich panel and method of making same.

이 특허를 인용한 특허 (73)

  1. Márquez López, Ignacio José; Cuenca Rincón, José; Chamorro Alonso, Francisco Javier; Nogueroles Viñes, Pedro, Aircraft frames.
  2. Fernandez, Fernando Ferreira; Takanashi, Sadao; Fortes, Lucio Camargo; Cruz, Marcio; do Prado, Marcelo Galvão; Eça Ferreira, Clovis Augusto; Aguiar, José Donizette, Aircraft fuselage structural components and methods of making same.
  3. Savian, Scott; Long, Eric; De Botton, Jordan, Aircraft interior panel with acoustic materials.
  4. Savian, Scott; Long, Eric; De Botton, Jordan, Aircraft interior panel with acoustic materials.
  5. Bouchet,Eric; Mahieu,Benjamin; Juillen,Lionel; Vinches,Frederic, Aircraft partition designed to separate a cargo part from a cockpit or from a passenger compartment.
  6. Stephens, Jeffrey Scott; Bye, Steven Douglas; Day, Dan, Apparatus for co-curing composite skins and stiffeners in an autoclave.
  7. Anderson, Donald A.; Cao, Tuan Quang; Leggett, Michael L.; Kyriakides, Anne E., Automated placement of vibration damping materials.
  8. Anderson, Donald A.; Parsons, Anne E.; Cao, Tuan Q.; Leggett, Michael L., Automated placement of vibration damping materials.
  9. Kismarton, Max U.; Andrews, Francis E.; Koch, William J., Compliant stiffener for aircraft fuselage.
  10. Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H., Composite barrel sections for aircraft fuselages and other structures.
  11. 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.
  12. 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.
  13. 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.
  14. Velicki, Alexander; Thrash, Patrick J., Composite fabric with rigid member structure.
  15. Montgomery, Joshua M.; Liguore, Salvatore L.; Cao, Tuan Q., Composite laminate having a damping interlayer and method of making the same.
  16. Kismarton, Max U., Composite laminate including beta-reinforcing fibers.
  17. Robins, Brian G.; Rotter, Daniel M.; Washburn, Todd J.; George, Panagiotis E., Composite mandrel for autoclave curing applications.
  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.
  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.
  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.
  21. Holemans, Peter; Stauffer, Matthew, Composite stiffener with integral conductive element.
  22. Kismarton, Max U., Composite stiffeners for aerospace vehicles.
  23. Pook, David A.; Lockett, Peter J.; Glynn, Andrew, Composite structures having integrated stiffeners and method of making the same.
  24. Pook, David A.; Lockett, Peter J.; Glynn, Andrew, Composite structures having integrated stiffeners with smooth runouts and method of making the same.
  25. Pook, David A.; Lockett, Peter J.; Glynn, Andrew K., Composite structures having integrated stiffeners with smooth runouts and method of making the same.
  26. Mänz, Christian, Cover for an aircraft structure.
  27. Mäkelä, Juha; Halme, Juha; Halme, Lauri; Hoffrén, Mikko, Curved element, wing, control surface and stabilizer for aircraft.
  28. Guzman, Juan C.; McCarville, Douglas A.; Rotter, Daniel M.; VanWest, Barry P., Foam stiffened hollow composite stringer.
  29. Lutz, Andreas, Frame and method for producing such a frame.
  30. Grauerholz, Thomas, Hull structure.
  31. Lobato, Fabiano; Ferreira, Clóvis Augusto Eça; Aguiar, José Donizette; Fortes, Lucio Camargo; Takanashi, Sadao, Hybrid aircraft fuselage structural components and methods of making same.
  32. Arévalo Rodríguez, Elena; Muñoz Royo, Pedro Luis, Integrated aircraft structure in composite material.
  33. Vichniakov, Alexei, Lightweight structural panel.
  34. Vichniakov, Alexei, Lightweight structural panel.
  35. Vichniakov, Alexei, Lightweight structural panel.
  36. Schmidt, Hans-Juergen; Vichniakov, Alexei, Lightweight structure especially for an aircraft and method for making such a structure.
  37. Robins, Brian G.; Willden, Kurtis; Hunter, Ethan W.; McManus, Nika, Mandrel for autoclave curing applications.
  38. Huddleston, Nicholas Lee; Ballester, Jaime, Mandrel forming for discrete wing skin stiffeners.
  39. Lewis, Dennis Michael; Geren, William Preston; Bommer, Jason P., Method and apparatus for wireless aircraft communications and power system using fuselage stringers.
  40. Fahley, Stephen L.; Geren, William Preston; Bommer, Jason P., Method and apparatus for wireless sensing with power harvesting of a wireless signal.
  41. Stephens, Jeffrey Scott; Bye, Steven Douglas; Day, Dan, Method for co-curing composite skins and stiffeners in an autoclave.
  42. Roming, Thorsten; Schroeer, Thorsten; Kirstein, Hauke; Gensch, Hinnik; Tacke, Stefan, Method for coupling stiffening profile elements and structural component.
  43. Arnold, Ralph; Eisenbeiss, Fred, Method for producing a component comprising at least one hollow profile.
  44. Goering, Jonathan, Method for weaving substrates with integral sidewalls.
  45. Senibi, Simon D.; Van West, Barry P.; Guzman, Juan Carlos; McCarville, Douglas A.; Rotter, Daniel M., Method of forming a reinforced foam-filled composite stringer.
  46. Senibi, Simon D.; Van West, Barry P.; Guzman, Juan Carlos; McCarville, Douglas A.; Rotter, Daniel M., Method of forming a reinforced foam-filled composite stringer.
  47. Lockett, Peter J.; Pook, David; Glynn, Andrew K., Method of manufacturing resin infused composite parts using a perforated caul sheet.
  48. 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.
  49. Johnson, Kent E.; Ulvin, Mark A., Methods of manufacturing structural panels.
  50. McCarville, Douglas A.; Guzman, Juan C.; Rotter, Daniel M., Multi-functional aircraft structures.
  51. Dorsy, Sean C., Multi-tiered, expandable panel structures and methods of manufacturing the same.
  52. Tsotsis, Thomas K., Nanotube-enhanced interlayers for composite structures.
  53. Tsotsis, Thomas K., Nanotube-enhanced interlayers for composite structures.
  54. Victorazzo, Danilo Seixas, Processes to fabricate composite tubular-reinforced panels integrating skin and stringers and the panels thereby fabricated.
  55. Noebel, Torsten; Paulukuhn, Arne, Profile comprising at least one hollow profile section.
  56. Ashton, Larry J.; Allman, Michael G.; White, Troy L.; Simpson, Craig B.; Ta'ala, Benko S., Reinforced composite panel.
  57. Lockett, Peter J.; Pook, David; Glynn, Andrew K., Resin infusion of composite parts using a perforated caul sheet.
  58. Lockett, Peter J.; Pook, David; Glynn, Andrew K., Resin infusion of composite parts using a perforated caul sheet.
  59. Guzman, Juan C.; McCarville, Douglas A.; Rotter, Daniel M.; Robins, Brian G., Shaped composite stringers and methods of making.
  60. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  61. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  62. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  63. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  64. Stulc,Jeffrey F.; Chan,Wallace C.; Clapp,Brian C.; Rolfes,Neal G., Splice joints for composite aircraft fuselages and other structures.
  65. Mialhe, Christophe; Delahaye, Romain; Rodrigo, Philipe, Stiffener for an aircraft fuselage, method for manufacturing same, and aircraft fuselage equipped with such a stiffener.
  66. Ochoa, Carlos M., Stiffeners for utility trailer structural panels.
  67. Childs, Thomas, Stringer for an aircraft wing and a method of reinforcing thereof.
  68. Johnson, Kent E.; Ulvin, Mark A., Structural panels for use in aircraft fuselages and other structures.
  69. Verweyen, Hendrik, Structuring construction for an aircraft fuselage.
  70. Liguore, Salvatore L.; Montgomery, Joshua M., Systems and methods for reducing noise in aircraft fuselages and other structures.
  71. Liguore, Salvatore L.; Montgomery, Joshua M., Systems and methods for reducing noise in aircraft fuselages and other structures.
  72. Liguore, Salvatore L.; Montgomery, Joshua M., Systems and methods for reducing noise in aircraft fuselages and other structures.
  73. Froeschner, Neal A.; Piszar, Jim S., Trimming composite skin stiffener ends.
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