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[미국특허] Reinforced composite structure and method of fabrication thereof 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B32B-003/12
출원번호 US-0870684 (1978-01-19)
발명자 / 주소
  • Lackman Leslie M. (Tarzana CA) Hill John A. (Lawndale CA)
출원인 / 주소
  • Rockwell International Corporation (Los Angeles CA 02)
인용정보 피인용 횟수 : 83  인용 특허 : 8

초록

A composite structure has two composite panels which are bonded together at a joint. The joint is reinforced by composite thread being sewn in a series of stitches through the panels. Sewing the panels while they are in a staged condition allows the structure to be co-cured as assembled.

대표청구항

A reinforced cured composite structure comprising: a first composite panel, said first panel having a plurality of fiber composite plies, said plies being adhesively bonded together; a second composite panel, said second panel having a plurality of fiber composite plies, said plies being adhesively

이 특허에 인용된 특허 (8) 인용/피인용 타임라인 분석

  1. Rhodes Marvin D. (Yorktown VA) Mikulas ; Jr. Martin M. (Williamsburg VA), Composite sandwich lattice structure.
  2. Loyd ; Morris S., Composite structural joint and method of fabrication thereof.
  3. Wallin Erik Wilhelm (Gamleby SW), Heat welded joints between webs of reinforced plastic foil.
  4. Draper Homer L. (Bartlesville OK) Gray Lew T. (Bartlesville OK), Liner for reservoir of layered liquids.
  5. Holmes Richard N. (Laguna Beach CA), Lock core panel.
  6. Allen John D. (5005 Zahm Rd. Belding MI 48809), Method of fabricating a tank by joining wall sections with fiber reinforced joiner panels.
  7. Marquis Paul (Tassin-La-Demi-Lune FR), Ply of parallel filaments.
  8. Jutte, Ralph B.; Lehman, Roger L., Sink-free panels.

이 특허를 인용한 특허 (83) 인용/피인용 타임라인 분석

  1. Johnson,David W., 3D fiber elements with high moment of inertia characteristics in composite sandwich laminates.
  2. Hamm Robert A. (Bellevue WA), Advanced composite.
  3. Johnson,David W.; Garrett,Scott A.; Hooks,James M.; Moyers,Stephen G., Apparatus for inserting z-axis reinforcing fibers into a composite laminate.
  4. Brown, Stephen T.; Kismarton, Max U., Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures.
  5. Brown, Stephen T.; Kismarton, Max U., Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures.
  6. Bruno Joseph W. (Shirley NY) Cacho-Negrete Carlos (Massapequa NY), Blow off panel for controlling hydrodynamic ram.
  7. Zalewski, Bart F.; Dial, William B., Bonded and stitched composite structure.
  8. Bergmann, Blaise F., Composite assembly with integrated composite joints.
  9. Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H., Composite barrel sections for aircraft fuselages and other structures.
  10. 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.
  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 for systems for manufacturing such barrel sections.
  13. Velicki, Alexander; Thrash, Patrick J., Composite fabric with rigid member structure.
  14. Velicki, Alexander; Thrash, Patrick J., Composite fabric with rigid member structure.
  15. Adams Thomas R. (Huntington Beach CA) Wittman Gary R. (Costa Mesa CA), Composite fastener.
  16. Thomas, Charles William, Composite filler.
  17. Uskert, Richard Christopher, Composite gas turbine engine component.
  18. Johnson, David W.; Garrett, Scott A.; Moyers, Stephen G., Composite laminate structure.
  19. Johnson, David W.; Garrett, Scott A.; Moyers, Stephen G.; Hook, James M., Composite laminate structure.
  20. Johnson, David W.; Garrett, Scott A.; Moyers, Stephen G.; Hook, James M., Composite laminate structure.
  21. Johnson,David W; Garrett,Scott A.; Moyers,Stephen G., Composite laminate structure.
  22. Therrien Keith E. (Wausau WI), Composite material structure with integrated insulating blanket and method of manufacture.
  23. Johnson, David W., Composite sandwich panel and method of making same.
  24. 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.
  25. 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.
  26. 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.
  27. Deobald, Lyle R.; Rinn, Aaron N.; Shan, Ying; Ramnath, Madhavadas; Vetter, Derek P.; Griess, Kenneth H.; Graves, Michael J., Composite structures having reduced area radius fillers and methods of forming the same.
  28. Hertzberg Paul E. (San Diego CA), Composites made of fiber reinforced resin elements joined by adhesive.
  29. Tacke, Stefan; Lengsfeld, Hauke; Reye, Volker, Connecting arrangement for joining two stiffening elements having different cross-sectional profiles for an aircraft or spacecraft, and shell component.
  30. Goering, Jonathan; McClain, Michael, Corner fitting preforms and method of making thereof.
  31. Whitener Philip C. (Seattle WA) Olason Ray (Seattle WA), Double-lobe fuselage composite airplane.
  32. Daws David Eric, Dowel adhesive method for repair of ceramic matrix composites.
  33. Bradley, Jeremy Peter; Sutton, David Alistair; West, Colin John; Withers, Andrew, Edge seal for fibre-reinforced composite structure.
  34. Goering, Jonathan; Ouellette, Kenneth, Fiber architecture for Pi-preforms.
  35. Burgess Keith E., Fiber-reinforced composite materials structures and methods of making same.
  36. Brenner,Berndt; Winderlich,Bernd; Standfuβ,Jens; Schumacher,J��rg; Brenneis,Hartmut; Zink,Walter, Lightweight structural component in particular for aircraft and method for its production.
  37. Gants, Wilbur L.; Kline, William T.; Sneddon, Jonathan T., Machine for forming composite material into fillets.
  38. Koji Shiraishi JP; Makoto Nasu JP, Method for forming fiber-reinforced composite member.
  39. Bech, Anton, Method for preparing pre-form materials.
  40. Henze Siegfried,DEX ; Schnaus Martin,DEX, Method for producing a seam reinforcement.
  41. Halcomb Ronald G. (Tulsa OK), Method for producing integrally stiffened fiber reinforced plastic panels.
  42. Goering, Jonathan, Method for weaving substrates with integral sidewalls.
  43. Marrache Albert A. (Smyrna GA) Snipes ; Jr. Frank C. (Marietta GA), Method of and apparatus for blind tufting composite laminated joints.
  44. Johnson, David W.; Hook, James M.; Garrett, Scott A.; Moyers, Steven G., Method of clinching the top and bottom ends of Z-axis fibers into the respective top and bottom surfaces of a composite laminate.
  45. Johnson, David W.; Garrett, Scott A.; Hook, James H.; Moyers, Stephen G., Method of inserting Z-axis reinforcing fibers into a composite laminate.
  46. Johnson, David W.; Garrett, Scott A; Hook, James M.; Moyers, Steven G., Method of inserting z-axis reinforcing fibers into a composite laminate.
  47. Johnson,David W.; Garrett,Scott A.; Hook,James M.; Moyers,Stephen G., Method of inserting z-axis reinforcing fibers into a composite laminate.
  48. Hertzberg Paul E. (San Diego CA), Method of making delamination resistant composites.
  49. Andreas Kielies DE; Rolf Beck DE; Guenter Doehle DE, Method of manufacturing a profile member of a hybrid composite material.
  50. 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.
  51. Johnson, Kent E.; Ulvin, Mark A., Methods of manufacturing structural panels.
  52. Velicki, Alexander; Thrash, Patrick Joseph; Burgess, Roger Alan; Standish, Cole, Molding process and apparatus for producing unified composite structures.
  53. Tsotsis, Thomas K., Nanotube-enhanced interlayers for composite structures.
  54. Tsotsis, Thomas K., Nanotube-enhanced interlayers for composite structures.
  55. Ouellette, Kenneth; Goering, Jonathan; Gilbertson, Brock, Pi-preform with variable width clevis.
  56. Gilbertson, Brock; Goering, Jonathan, Pi-shaped preform with bias fibers.
  57. Born Eberhard (Cologne DEX), Post forming semi-finished product for the manufacture of moulded parts resistant to bending.
  58. Bech, Anton, Pre-form and method of preparing a pre-form.
  59. Garate Fel, Enrique; Redondo Vara, Enrique; Sanchez Gomez, Jose; Ruiseco Salgado, Rafael; Serrano Velaz, César, Process of manufacturing composite structures with embedded precured tools.
  60. Goering, Jonathan, Quasi-isotropic three-dimensional preform and method of making thereof.
  61. Poertner, Joshua; Hall, Michael, Reinforced composite rim.
  62. Steele,Robin S.; Stenger,Jennifer L., Reinforced composite structure.
  63. McKinney Maurice E. (Bellevue WA), Reinforced honeycomb core sandwich panels and method for making same.
  64. Deobald, Lyle R.; Morris, John D.; Lee, Karl B.; Marcoe, Jeffery L.; Iden, Mark C.; Harris, Christopher G., Reinforced stiffeners and method for making the same.
  65. Deobald, Lyle R.; Morris, John D.; Lee, Karl B.; Marcoe, Jeffery L.; Iden, Mark C.; Harris, Christopher G., Reinforced stiffeners and method for making the same.
  66. Goering, Jonathan; McClain, Michael, Reinforcement for darted Pi preforms.
  67. Palmer Raymond J. ; Sarh Branko, Reinforcing member for composite workpieces and associated methods.
  68. Fournie,Ludovic; Herve,Claude; Fort,Fr��d��ric, Self-stiffened panels of preimpregnated composite and manufacturing process for components of such panels.
  69. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  70. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  71. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  72. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  73. Stulc,Jeffrey F.; Chan,Wallace C.; Clapp,Brian C.; Rolfes,Neal G., Splice joints for composite aircraft fuselages and other structures.
  74. Palmer Raymond J., Stitch-reinforced sandwich panel and method of making same.
  75. Vichniakov, Alexei, Structural element, method for manufacturing a structural element and use of a structural element for an aircraft hull.
  76. Christ-Janer Victor F. (4 Forest St. New Canaan CT 06840), Structural member suitable for use as a joist, beam, girder or the like.
  77. Johnson, Kent E.; Ulvin, Mark A., Structural panels for use in aircraft fuselages and other structures.
  78. Walker, Jared T.; Barnes, John E., System, method, and apparatus for structural lug formed from a combination of metal and composite laminate materials.
  79. Goering, Jonathan, Three-dimensional woven integrally stiffened panel.
  80. McCarville Douglas A. ; Howitt ; Jr. John S. ; Younie Mark L., Titanium radius filler for use in composite interfaces.
  81. Tucker, Michael; Sanderson, Timothy, Wing structure.
  82. Goering, Jonathan, Woven preform with integral off axis stiffeners.
  83. Burgess Keith E., Yarn insertion mechanism.

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