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특허 상세정보

Light weight and high strength fuselage

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-001/12   
미국특허분류(USC) 244/119; 244/120
출원번호 US-0017732 (2001-10-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Alston & Bird LLP
인용정보 피인용 횟수 : 75  인용 특허 : 12
초록

A fuselage comprising a skin assembly including an outer, laminate skin bonded to an inner, aluminum doubler. The fuselage also includes a support structure comprising a plurality of longitudinal stringer members and a plurality of annular frame members that are attached to, and cooperate to support, the skin assembly. The aluminum doubler provides additional structural support for the fuselage, and in particular, for the outer laminate skin of the skin assembly. The additional structural strength added by the aluminum doubler allows the use of an improv...

대표
청구항

A fuselage comprising a skin assembly including an outer, laminate skin bonded to an inner, aluminum doubler. The fuselage also includes a support structure comprising a plurality of longitudinal stringer members and a plurality of annular frame members that are attached to, and cooperate to support, the skin assembly. The aluminum doubler provides additional structural support for the fuselage, and in particular, for the outer laminate skin of the skin assembly. The additional structural strength added by the aluminum doubler allows the use of an improv...

이 특허에 인용된 특허 (12)

  1. Willden Kurtis S. (Kent WA) Goodno Kenneth N. (Federal Way WA). Caul and method for bonding and curing intricate composite structures. USP1993095242523.
  2. Pettit Richard G.. Fiber/metal laminate splice. USP1999095951800.
  3. Hammer Robert H. (Kirkland WA). Hybrid composite structures. USP1982084344995.
  4. Gupta Gautam Sen (Bellevue WA). Intrinsically tuned structural panel. USP1976083976269.
  5. Schijve Jacobus (Pijnacker NLX) Vogelesang Laurens B. (Nieuwkoop NLX) Marissen Roelof (Cologne DEX). Laminate of aluminum sheet material and aramid fibers. USP1985024500589.
  6. Schijve Jacobus (Pijnacker NLX) Vogelesang Laurens B. (Nieuwkoop NLX) Marissen Roelof (Cologne DEX). Laminate of metal sheet material and threads bonded thereto, as well as processes for the manufacture thereof. USP1984124489123.
  7. Vogelesang Laurens B. (Nieuwkoop NLX) Meyers Leendert G. (Den Bommel NLX) van Velze Tom M. (Delft NLX). Laminate of metal sheets and continuous filaments-reinforced thermoplastic synthetic material, as well as a process for. USP1991024992323.
  8. Vogelesang Laurens B. (Nieuwkoop NLX) Roebroeks Gerardus H. J. J. (Den Bommel NLX). Metal-resin laminate reinforced with S2-glass fibres. USP1991085039571.
  9. Richard L. Raun ; Patrick R. Oyler ; Bruce D. Hopkins. Payload fairing with jettisonable mass acoustic suppression. USP2002056394394.
  10. Garesch Carl E. (New Kensington PA) Roebroeks Gerandus H. J. J. (Den Bommel NLX) Greidanus Buwe V. W. (Delft NLX) Oost Rob C. V. (Heerjansdam NLX) Gunnink Jan W. (Nieuwerkerk a/d Ijssel NLX). Spliced laminate for aircraft fuselage. USP1995075429326.
  11. Westre Willard N. ; Allen-Lilly Heather C. ; Ayers Donald J. ; Cregger Samuel E. ; Evans David W. ; Grande Donald L. ; Hoffman Daniel J. ; Rogalski Mark E. ; Rothschilds Robert J.. Titanium-polymer hybrid laminates. USP1999025866272.
  12. Tarbox Jack M. ; Baker Philip J.. Wing spar modification kit. USP2001126328260.

이 특허를 인용한 특허 피인용횟수: 75

  1. 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. USP2014098844871.
  2. Engelbart,Roger W; Hannebaum,Reed; Pollock,Tim; Orr,Sam; Putnam,Jeff; Rector,Eric. Apparatus and methods for inspecting a composite structure for inconsistencies. USP2008057372556.
  3. Engelbart, Roger W; Hannebaum, Reed; Hensley, Brian S; Pollock, Timothy T; Orr, Samuel D. Apparatus and methods for inspecting tape lamination. USP2011027889907.
  4. Engelbart,Roger W.; Hannebaum,Reed; Putnam,Jeff. Apparatus and methods for integrating encoding functions in material placement machines. USP2008107435947.
  5. Childress, James J.; Viniotis, John J.. Autonomous aircraft with disconnectable tether. USP2015069045218.
  6. Anast, Peter Z.; Horst, Perry T.. Bonded metal fuselage and method for making the same. USP2011108038099.
  7. Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H.. Composite barrel sections for aircraft fuselages and other structures. USP2013028382037.
  8. 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.
  9. 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.
  10. 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.
  11. Velicki, Alexander; Thrash, Patrick J.. Composite fabric with rigid member structure. USP2011108042767.
  12. Braun,Rudolf. Composite fuselage machine and method of automated composite lay up. USP2006077080441.
  13. Alby, Sebastien; Gauthie, Laurent; Bernadet, Philippe. Composite internal beam for reinforcing the structure of an aircraft. USP2010107810756.
  14. Nelson, Paul E.; Kramp, Jr., Robert A.; Lum, Matthew K.. Composite lamination using array of parallel material dispensing heads. USP2014028641847.
  15. Nelson, Paul E.; Kramp, Jr., Robert Alan; Lum, Matthew K.. Composite lamination using array of parallel material dispensing heads. USP2012128336596.
  16. 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.
  17. 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.
  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. USP2009037503368.
  19. Bense, Rolf. Connection arrangement, particularly for aircraft structure parts. USP2015028950707.
  20. Mänz, Christian. Cover for an aircraft structure. USP2012108276847.
  21. Kehrl, David J.; Johnson, Kent E.; McCarville, Douglas A.. Curved composite frames and method of making the same. USP2015089096305.
  22. Griess, Kenneth H.; MacKenzie, Karen D.. Elongated structures and related assemblies. USP2016129527572.
  23. Griess, Kenneth H.; MacKenzie, Karen D.. Elongated structures and related assemblies. USP2018049950779.
  24. Griess, Kenneth H.; MacKenzie, Karen D.. Elongated structures and related assemblies. USP20190210207786.
  25. Haack, Cord; Beumler, Thomas. Fire protection space for aircraft passengers provided with the aid of fuselage skin of fibre-metal laminates. USP2014128899523.
  26. Stephan, Andreas. Fuselage cell structure of an airplane for the simplified installation and attachment of fasteners for fastening conduits. USP2013048408496.
  27. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim. In-process vision detection of flaw and FOD characteristics. USP2010037688434.
  28. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim. In-process vision detection of flaw and FOD characteristics. USP2010057712502.
  29. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim. In-process vision detection of flaw and FOD characteristics. USP2013098524021.
  30. Engelbart,Roger W.; Hannebaum,Reed; Pollock,Tim. In-process vision detection of flaw and FOD characteristics. USP2008097424902.
  31. Englebart, Roger W.; Hannebaum, Reed; Pollock, Tim. In-process vision detection of flaw and FOD characteristics. USP2014078770248.
  32. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim. In-process vision detection of flaws and FOD by back field illumination. USP2009087576850.
  33. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim. In-process vision detection of flaws and FOD by back field illumination. USP2010037678214.
  34. Rajabali, Abdoel Faziel; Markestein, Max Arjan. Laminate with local reinforcement. USP2013048426007.
  35. Schmidt, Hans-Juergen; Vichniakov, Alexei. Lightweight structure especially for an aircraft and method for making such a structure. USP2010077753312.
  36. Olson,Vincent T.; Koppelmann,Richard E.; Berntsson,Peter; Pettersson,Johnny. Mandrel segment loader. USP2007107278198.
  37. Guzman, Juan Carlos; McCarville, Douglas Alan; Sweetin, Joseph L.; Messinger, Ross. Method and apparatus for producing contoured composite structures and structures produced thereby. USP2016039278484.
  38. Bechtold, Michael. Method and device for producing fiber-reinforced plastic profile parts. USP2014038663519.
  39. Thomaschewski, Oliver Sascha. Method for measuring the internal space of an aircraft. USP2013118576409.
  40. 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.
  41. Brown, Todd A.; Friddell, Stephen Douglas; Harris, Christopher G.; Modin, Andrew E.. Method of manufacturing curved composite structural elements. USP2017049630390.
  42. Engelbart, Roger W.; Hannebaum, Reed; Schrader, Steve. Methods for determining inconsistency characteristics of a composite structure. USP2012058184281.
  43. 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.
  44. Johnson, Kent E.; Ulvin, Mark A.. Methods of manufacturing structural panels. USP2010057716835.
  45. Sarh, Branko. Multi-ring system for fuselage barrel formation. USP2012058173055.
  46. Tsotsis, Thomas K.. Nanotube-enhanced interlayers for composite structures. USP2014028657990.
  47. Tsotsis, Thomas K.. Nanotube-enhanced interlayers for composite structures. USP2013038388795.
  48. Lum, Matthew K.; Wagner, David L.; Hall, Thomas D.; Jones, Darrell D.; Appleton, Joseph A.; Olson, Vincent T.; Spishak, Noel A.. One-piece barrel assembly cart. USP2009127624488.
  49. Nelson,Paul E.. Parallel configuration composite material fabricator. USP2006117137182.
  50. Nelson, Paul E.. Parallel configuration composite material fabricator and related methods. USP2013118578995.
  51. Ehinger, Ryan T.; McGlaun, Monte A.. Passive cooling of transmission using mast mounted heat pipes. USP2015038985517.
  52. Cosentino, Enzo. Reinforced panel. USP2012118302486.
  53. 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. USP2018059981444.
  54. 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. USP2013098540833.
  55. Blankinship,Bruce C.. Segmented flexible barrel lay-up mandrel. USP2007017166251.
  56. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2017089738371.
  57. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2011118061035.
  58. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2014108869403.
  59. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2014118882040.
  60. Stulc,Jeffrey F.; Chan,Wallace C.; Clapp,Brian C.; Rolfes,Neal G.. Splice joints for composite aircraft fuselages and other structures. USP2008027325771.
  61. Meyer, Cedric. Splice plate for stringers and orbital joining device. USP2010117823362.
  62. Ohrloff, Nikolaus; Beumler, Thomas; Daverschot, Derk; Plokker, Matthijs. Structural element for reinforcing a fuselage of an aircraft. USP2015038974885.
  63. Martin, Alexander; Tillich, Arthur; Pellenkoft, Frederik. Structural element, method for producing such a structural element, and aircraft having such a structural element. USP2011108042770.
  64. 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.
  65. Johnson, Kent E.; Ulvin, Mark A.. Structural panels for use in aircraft fuselages and other structures. USP2013078496206.
  66. Johnson,Kent; Ulvin,Mark A.. Structural panels for use in aircraft fuselages and other structures. USP2006117134629.
  67. Engelbart, Roger W.; Hannebaum, Reed; Rector, Eric; Haywood, Jeffrey. System and method for determining cumulative tow gap width. USP2015018934702.
  68. Walker, Jared T.; Barnes, John E.. System, method, and apparatus for structural lug formed from a combination of metal and composite laminate materials. USP2010047690164.
  69. Engelbart,Roger W; Hannebaum,Reed; Schrader,Steve; Holmes,Scott T; Walters,Craig. Systems and method for identifying foreign objects and debris (FOD) and defects during fabrication of a composite structure. USP2007067236625.
  70. Engelbart,Roger W.; Chapman,Michael R.; Johnson,Brice A.; Soucy,Kathryn A.; Hannebaum,Reed; Schrader,Steve. Systems and methods enabling automated return to and/or repair of defects with a material placement machine. USP2006057039485.
  71. Engelbart, Roger W; Hannebaum, Reed; Schrader, Steve. Systems and methods for determining inconsistency characteristics of a composite structure. USP2010087769224.
  72. Engelbart, Roger W; Hannebaum, Reed; Schrader, Steve. Systems and methods for determining inconsistency characteristics of a composite structure. USP2011077983469.
  73. Engelbart,Roger W.; Hannebaum,Reed; Schrader,Steve. Systems and methods for determining inconsistency characteristics of a composite structure. USP2007107289656.
  74. Engelbart,Roger W.; Speno,Frank Gregory. Systems and methods for using light to indicate defect locations on a composite structure. USP2007037193696.
  75. Engelbart,Roger W.; Speno,Frank G.. Systems and methods for using light to indicate inconsistency locations on a composite structure. USP2009027489392.