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특허 상세정보

Co-cured composite structures and method of making them

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B32B-001/08   
미국특허분류(USC) 428/362; 428/035.7; 428/036.1; 428/036.9; 428/188; 052/793.1
출원번호 US-0797286 (2001-03-01)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Goodwin Procter LLP
인용정보 피인용 횟수 : 53  인용 특허 : 12
초록

A composite structure has composite skin layers and at least two elongated stiffener/spacer composite members interposed between the skin layers. The stiffener/spacer composite members are arranged generally longitudinally of the skin layers in spaced-apart relation laterally. Each of the skin layers is formed by assembling a layer of an uncured resin-impregnated fiber material on a forming surface of a jig. Each stiffener/spacer composite member is formed of an uncured resin-impregnated fiber material that is laid up over an elongated hollow mandrel of ...

대표
청구항

1. A composite structure comprising first and second composite skin layers, each of a resin-impregnated fiber material, at least two elongated stiffener/spacer composite members, each of a resin-impregnated fiber material and interposed between the skin layers, each stiffener/spacer composite member being arranged generally longitudinally of the skin layers and the stiffener/spacer composite members being spaced apart laterally, each stiffener/spacer composite member having side walls extending between and united with the skin layers by base w...

이 특허에 인용된 특허 (12)

  1. Whitener Philip C. (Seattle WA). Composite structural skin spar joint and method of making. USP1983074395450.
  2. Pykiet Kenneth L. (Owasso OK). Composite structural truss element. USP1995115469686.
  3. Williams Sam B. (Bloomfield Hills MI). Composite wing and manufacturing process thereof. USP1994075332178.
  4. Wong Raymond S. (San Ramon CA). Expandable films and molded products therefrom. USP1993085234757.
  5. Wang Yen-Seine (San Ramon CA) Lee Frank (Danville CA) Kuo Ching-Chi (Danville CA) Baron Ken (San Ramon CA). Foam filled honeycomb and methods for their production. USP1994085338594.
  6. Gross Bernd (Grossniedesheim DEX) Weber Heinz (Gruenstadt DEX). Laminates with stable attachment areas. USP1992085135799.
  7. Newton Jefferson F. (Seattle WA) Martin Thomas D. (Bellevue WA) Westre Willard N. (Bellevue WA) Carbery David J. (Vashon Island WA) Ikegami Roy (Seattle WA). Lightweight honeycomb panel structure. USP1995085445861.
  8. Umemoto Yoshitaka (Shizuoka JPX) Tanaka Takayuki (Shizuoka JPX) Furukawa Yasuo (Shizuoka JPX). Low fuming phenolic resin prepreg and process for producing the same. USP1994025284702.
  9. Doerer Richard P. (Grosse Pointe MI) Bihun Edward J. (Huron OH). Panel and method of making the same. USP1992025089328.
  10. Waid Robert D.. Removable adhesive of polyepoxide, curing agent and microspheres. USP2001096288170.
  11. Brambach Johan A. (Leimuiden NLX). Sandwich material provided with a local reinforcement. USP1993025186999.
  12. Ware Maximilian (Minneapolis MN). Thermal expansion resin transfer molding. USP1991105061418.

이 특허를 인용한 특허 피인용횟수: 53

  1. Porte, Alain; Fargues, Matthieu; Marro, Martial. Aircraft nacelle comprising a reinforced connection between an air intake and a powerplant. USP2017029567905.
  2. Wen, Ed; Ehrmantraut, Adam Scott; Snider, II, James McDaniel; Parks, Robert. Apparatus and method for an aircraft conductor sandwich assembly embedded to an aircraft structure. USP2015018937254.
  3. Stephens, Jeffrey Scott; Bye, Steven Douglas; Day, Dan. Apparatus for co-curing composite skins and stiffeners in an autoclave. USP2017089738039.
  4. Kirkpatrick, Bowden. Apparatus for forming flanges on components. USP2014018622731.
  5. Kirkpatrick, Bowden; Vermilyea, Mark Ernest; Lamm, Derrick Wayne; Bramell, Melissa Ann Marie; Callahan, David Louis; Seabrease, Jason Michael. Apparatus for manufacturing a flanged composite component and methods of manufacturing the same. USP2016029248587.
  6. Kamimura, Shinya; Ikeda, Koki; Hokazono, Kiyoshi. Battery mounting structure for vehicle. USP2017019533631.
  7. Fong, Tony; Axford, Timothy. Braided composite spar. USP20180710023292.
  8. Fong, Tony; Axford, Timothy. Braided composite spar. USP20180710011345.
  9. Fong, Tony; Axford, Timothy. Braided composite spar. USP2018029896186.
  10. Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H.. Composite barrel sections for aircraft fuselages and other structures. USP2013028382037.
  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. USP2012048157212.
  12. 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.
  13. Robins, Brian G.; Rotter, Daniel M.; Washburn, Todd J.; George, Panagiotis E.. Composite mandrel for autoclave curing applications. USP2016059327467.
  14. 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.
  15. 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.
  16. Bremmer, Jonathan; Sauer, Jeffrey G.; Fabian, Edward Joseph; Denavit, Paul H.; Toni, Darryl Mark; Hovan, III, William E.. Composite structure and core positioning ply. USP2017019539769.
  17. Drever, Michael. Composite structure manufacturing method and apparatus. USP2015099138942.
  18. Victorazzo, Danilo Seixas. Composite tubular-reinforced integrated structural panels with mutually intersecting stiffeners and fabrication processes. USP2016039284035.
  19. Bech, Anton; Hahn, Frank A. Hoelgaard. Connection between composites with non-compatible properties and method for preparation. USP2013048409396.
  20. Noble, Robert; Hunt, John F.; Newburn, Timothy L.; Gu, Hongmei. Engineered molded fiberboard panels and methods of making and using the same. USP2015018936699.
  21. Zorzetto, Daniel; Lataillade, Jean-Christophe. Floor made out of composite material and process for manufacturing such a floor. USP2014088814091.
  22. Boone, Richard; de Putter, Benjamin. Formation of complex composite structures using laminate templates. USP20180610005267.
  23. Hanson, Russell B.. Iso-grid composite component. USP2015099126374.
  24. Hanson, Russell B.. Iso-grid composite component. USP2017109789570.
  25. McCarville, Douglas A.; Guzman, Juan C.. Joining curved composite sandwich panels. USP2017039586379.
  26. McCarville, Douglas A.; Guzman, Juan C.. Joining curved composite sandwich panels. USP2014088815038.
  27. Robins, Brian G.; Willden, Kurtis; Hunter, Ethan W.; McManus, Nika. Mandrel for autoclave curing applications. USP2016019238335.
  28. Miller, Zev; Rubinstein, Daniel Itzchak; Yurovitch, Yaniv; Rosenfeld, Harry; Ben Yaacov, Jacob; Leibovich, Herman; Ghilai, Gila. Manufacture of integrated structures formed of composite materials. USP2018029889613.
  29. Goehlich, Robert Alexander; Sander, Malte. Method and device for joining adherends, as well as component. USP2014068741090.
  30. Stephens, Jeffrey Scott; Bye, Steven Douglas; Day, Dan. Method for co-curing composite skins and stiffeners in an autoclave. USP2016059333713.
  31. McCarville, Douglas A.; Guzman, Juan C.; Hand, Michael Leslie. Method for joining sandwich truss core panels and composite structures produced therefrom. USP2014098834667.
  32. McCarville, Douglas A.; Guzman, Juan C.; Hand, Michael L.; Robinson, Michael J.. Method for making composite truss panel having a fluted core. USP2011087998299.
  33. Ashton, Larry J.; Allman, Michael G.; White, Troy L.; Ta'ala, Benko S.. Method for manufacturing a reinforced panel of composite material. USP2014038668858.
  34. Bech, Anton. Method for preparing pre-form materials. USP2014078778106.
  35. Childress, James J.; Perron, Dan. Method of fabricating a tank having integral restraining elements. USP2016029266619.
  36. De Vita, Vincenzo; Inserra Imparato, Sabato; Lanfranco, Giovanni; Miani, Nicola; Sagnella, Giovanni; Riccio, Massimo. Method of manufacturing an integral profile monolithic wing structure. USP2015038980152.
  37. Anderson,Donald A.; Johnson,Brice A.; Spoon,Stephen S.. Method of transferring large uncured composite laminates. USP2007067228611.
  38. 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.
  39. Hand, Michael L.; Guzman, Juan C.; McCarville, Douglas A.; Eichinger, Jeffrey D.; Chong, Keith. Methods of internally insulating a fluted core sandwich structure. USP2017099770864.
  40. Wen, Ed; Cottrell, Dan; Ehrmantraut, Adam; Blehar, Mark; Kordonowy, David. Multi-functional composite structures. USP20190110167550.
  41. Tsotsis, Thomas K.. Nanotube-enhanced interlayers for composite structures. USP2014028657990.
  42. Witte, Philipp; Stawski, Stanley Warren; Kleshchev, Fedor A.; Zarfos, Joshua William; Naidu, Parth R.. One-piece composite bifurcated winglet. USP2017089738375.
  43. Victorazzo, Danilo Seixas. Processes to fabricate composite tubular-reinforced panels integrating skin and stringers and the panels thereby fabricated. USP2016039278748.
  44. Pacary, Jean-Luc; Francisco, Paulo. Reinforced composite sandwich panel. USP2013078474573.
  45. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2017089738371.
  46. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2011118061035.
  47. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2014108869403.
  48. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2014118882040.
  49. Toledano, Ilan. System and method for inspecting structures formed of composite materials during the fabrication thereof. USP2015038983171.
  50. Coxon, Brad Andrew; Rotter, Daniel M.; Robins, Brian G.; Chan, Wallace C. H.; Dopker, Bernhard; Kirchmeier, Stephen Keith. Systems, tools, and methods for forming composite tubular stringers and stiffened composite structures having composite tubular stringers. USP2014128906179.
  51. Ishida, Ryuichi; Oki, Ryosuke; Tamada, Teruo. Vehicle interior panel and producing method thereof. USP2013018349245.
  52. Ashton, Larry J.; Allman, Michael G.; White, Troy L.; Stark, Danny L.. Wing with sectioned tubular members. USP2010117828246.
  53. Fong, Tony; Axford, Timothy; Chaussee, Julien. Winglet. USP20180710029779.