$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Fuselage structure using advanced technology fiber reinforced composites 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-001/06
  • B64C-001/12
출원번호 US-0878540 (1978-02-16)
발명자 / 주소
  • Frosch Robert A. Administrator of the National Aeronautics and Space Administration
  • with respect to an invention of ( Mercer Island WA) Robinson Robert K. (Mercer Island WA) Tomlinson Harry M. (Bel
인용정보 피인용 횟수 : 95  인용 특허 : 6

초록

A fuselage structure is disclosed in which the skin is comprised of layers of a matrix fiber reinforced composite, with the stringers reinforced with the same composite material. The high strength to weight ratio of the composite, particularly at elevated temperatures, and its high modulus of elasti

대표청구항

A fuselage structure comprising: a fuselage having a longitudinal axis; an external skin of alternate layers of composite material, oriented at a biased angle relative to the longitudinal axis and at approximately 90°to the biased angle; stringers, having outboard and inboard ends; frames; circumfer

이 특허에 인용된 특허 (6)

  1. Loyd ; Morris S., Composite load coupler for reinforcing composite structural joints.
  2. Olez ; Nejat A., Composite structure.
  3. Cogburn Jimmie W. (Fort Worth TX) Chitwood Billie E. (Fort Worth TX) Howeth Marvin S. (Fort Worth TX), Filament reinforced structural shapes.
  4. Slysh Paul (San Diego CA), High strength composite structure.
  5. Gupta Gautam Sen (Bellevue WA), Intrinsically tuned structural panel.
  6. Eisenmann James R. (Fort Worth TX) Kaminski Ben E. (Fort Worth TX) Waddoups ; Jr. Max E. (Fort Worth TX), Laminated structural article with constituent elements having inherent fracture arrestment capability.

이 특허를 인용한 특허 (95)

  1. Munday, Andrew Robert, Aircraft component.
  2. Sankrithi, Mithra, Aircraft frame for tailstrike angle enhancement.
  3. Marin, Yannick; Guilloteau, Damien; Luche, Emilie, Aircraft fuselage frame element integrating tabs for the fastening of stiffeners.
  4. 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.
  5. Haack, Cord, Aircraft fuselage structure and method for its production.
  6. Schroeer, Thorsten; Roming, Thorsten, Aircraft fuselage structure and method for its production.
  7. Haack, Cord, Aircraft fuselage structure and method for producing it.
  8. Gauthie, Laurent; Bernadet, Phillippe, Aircraft pressurized floor.
  9. Sarh,Branko, Airfoil box and associated method.
  10. Micale Antonio C. ; Strand David E., Airplane fuselage panel.
  11. Benson, Vernon M.; Slack, Jason K.; Rosevear, Todd A.; Harvey, James L.; Roman, Mark; Olschewski, Timothy, Apparatus and methods for forming composite stiffeners and reinforcing structures.
  12. Engelbart,Roger W; Hannebaum,Reed; Pollock,Tim; Orr,Sam; Putnam,Jeff; Rector,Eric, Apparatus and methods for inspecting a composite structure for inconsistencies.
  13. Engelbart, Roger W; Hannebaum, Reed; Hensley, Brian S; Pollock, Timothy T; Orr, Samuel D, Apparatus and methods for inspecting tape lamination.
  14. Engelbart,Roger W.; Hannebaum,Reed; Putnam,Jeff, Apparatus and methods for integrating encoding functions in material placement machines.
  15. Madsen, Christopher J.; McNabb, Eric; Schowengerdt, John; Healey, John B.; Rosevear, Todd; Fehlmann, Kevin, Automated composite annular structure forming.
  16. Madsen, Christopher J.; McNabb, Eric; Schowengerdt, John; Healey, John B.; Rosevear, Todd; Fehlmann, Kevin, Automated composite annular structure forming.
  17. Bruno Joseph W. (Shirley NY) Cacho-Negrete Carlos (Massapequa NY), Blow off panel for controlling hydrodynamic ram.
  18. Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H., Composite barrel sections for aircraft fuselages and other structures.
  19. 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.
  20. 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.
  21. 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.
  22. Velicki, Alexander; Thrash, Patrick J., Composite fabric with rigid member structure.
  23. Velicki, Alexander; Thrash, Patrick J., Composite fabric with rigid member structure.
  24. Braun,Rudolf, Composite fuselage machine and method of automated composite lay up.
  25. Kismarton, Max U., Composite laminate including beta-reinforcing fibers.
  26. Nelson, Paul E.; Kramp, Jr., Robert A.; Lum, Matthew K., Composite lamination using array of parallel material dispensing heads.
  27. Nelson, Paul E.; Kramp, Jr., Robert Alan; Lum, Matthew K., Composite lamination using array of parallel material dispensing heads.
  28. Kismarton,Max U., Composite landing gear apparatus and methods.
  29. 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.
  30. 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.
  31. 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.
  32. Kismarton, Max U., Composite skin and stringer structure and method for forming the same.
  33. Kismarton, Max U., Composite structural members and methods for forming the same.
  34. Emil M. Shtarkman, Composite structure element with built-in damping.
  35. Hanson, Steven F.; Vyas, Amitabh, Corner-consolidating inflatable apparatus and method for manufacturing composite structures.
  36. Hanson, Steven F.; Vyas, Amitabh, Corner-consolidating inflatable method for manufacturing composite structures.
  37. Mueller Dietmar,DEX, Cover-skin structure.
  38. Brofeldt,P채r, Device for bracing a shell in an aircraft fuselage.
  39. Fyfe Edward R. (Del Mar CA) Isley ; Jr. Frederick P. (Tracy CA), Fabric reinforced beam and column connections.
  40. Popp, Valentin; Beumler, Thomas, Fibre metal laminate panel.
  41. Koefinger, Christian; Metzger, Joachim; Auburger, Michael, Frame element, aircraft component assembly system and method of fitting a component in an aircraft.
  42. Kismarton, Max U., Hybrid fiberglass composite structures and methods of forming the same.
  43. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim, In-process vision detection of flaw and FOD characteristics.
  44. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim, In-process vision detection of flaw and FOD characteristics.
  45. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim, In-process vision detection of flaw and FOD characteristics.
  46. Engelbart,Roger W.; Hannebaum,Reed; Pollock,Tim, In-process vision detection of flaw and FOD characteristics.
  47. Englebart, Roger W.; Hannebaum, Reed; Pollock, Tim, In-process vision detection of flaw and FOD characteristics.
  48. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim, In-process vision detection of flaws and FOD by back field illumination.
  49. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim, In-process vision detection of flaws and FOD by back field illumination.
  50. Holdren,Richard L., Intersecting structural member and a method for joining same.
  51. Kraenzien Peter,DEX, Leading edge construction for an aerodynamic surface and method of making the same.
  52. Olson,Vincent T.; Koppelmann,Richard E.; Berntsson,Peter; Pettersson,Johnny, Mandrel segment loader.
  53. Kismarton, Max U., Method for manufacturing composite components.
  54. Stephan, Andreas, Method for producing a composite skin in the field of aeronautics and astronautics.
  55. Engelbart, Roger W.; Hannebaum, Reed; Schrader, Steve, Methods for determining inconsistency characteristics of a composite structure.
  56. Benson, Vernon M.; Slack, Jason; Rosevear, Todd A., Methods for forming composite stiffeners and reinforcing structures.
  57. 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.
  58. Johnson, Kent E.; Ulvin, Mark A., Methods of manufacturing structural panels.
  59. Gary R. Weber ; Frederick John Feiertag ; Tyre Glenn Boss ; Michael J. Reberg ; Matthew L. Anderson ; Kelly William Meloy ; Genji Mizushima JP; Takeshi Kawase ; Ronald Hitzeman ; Simon R. Wa, Monolithic structure with redundant load paths.
  60. Weber Gary R. ; Feiertag Frederick John ; Boss Tyre Glenn ; Reberg Michael J. ; Anderson Matthew L. ; Meloy Kelly William ; Mizushima Genji,JPX ; Kawase Takeshi ; Hitzeman Ronald ; Walter Simon R.,AU, Monolithic structure with redundant load paths.
  61. Sarh, Branko, Multi-ring system for fuselage barrel formation.
  62. Tsotsis, Thomas K., Nanotube-enhanced interlayers for composite structures.
  63. Tsotsis, Thomas K., Nanotube-enhanced interlayers for composite structures.
  64. 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.
  65. Scown, Stephen L., Overhead bin and monument attachment support system.
  66. Nelson,Paul E., Parallel configuration composite material fabricator.
  67. Nelson, Paul E., Parallel configuration composite material fabricator and related methods.
  68. Madsen, Christopher J.; McNabb, Eric; Healey, John B.; Rosevear, Todd, Radially extending composite structures.
  69. Tanner, Richard B.; Burford, Ian C.; Gendzwill, Thomas V.; Doty, Gregory B.; Huck, James R.; Wilson, Dean E.; Korenaga, Brian H., Rib support for wing panels.
  70. Tanner, Richard B.; Burford, Ian C.; Gendzwill, Thomas V.; Doty, Gregory B.; Huck, James R.; Wilson, Dean E.; Korenaga, Brian H., Rib support for wing panels.
  71. Blankinship,Bruce C., Segmented flexible barrel lay-up mandrel.
  72. Peter Brinck DE; Wilfried Mueller DE; Klaus P. Sanmann DE; Joerg Spitzner DE, Shell component for an aircraft fuselage and method of manufacturing the same.
  73. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  74. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  75. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  76. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  77. Stulc,Jeffrey F.; Chan,Wallace C.; Clapp,Brian C.; Rolfes,Neal G., Splice joints for composite aircraft fuselages and other structures.
  78. Meyer, Cedric, Splice plate for stringers and orbital joining device.
  79. Woodard, Patrick; Kismarton, Max; Andrews, Francis E., Split resistant composite laminate.
  80. Gross, Claus-Peter; Haack, Cord; Humfeldt, Dirk; Thomaschewski, Oliver, Structural element of an aircraft fuselage.
  81. Stephen R. Early, Structural panel system.
  82. 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.
  83. Johnson, Kent E.; Ulvin, Mark A., Structural panels for use in aircraft fuselages and other structures.
  84. Johnson,Kent; Ulvin,Mark A., Structural panels for use in aircraft fuselages and other structures.
  85. Engelbart, Roger W.; Hannebaum, Reed; Rector, Eric; Haywood, Jeffrey, System and method for determining cumulative tow gap width.
  86. 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.
  87. 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.
  88. Engelbart, Roger W; Hannebaum, Reed; Schrader, Steve, Systems and methods for determining inconsistency characteristics of a composite structure.
  89. Engelbart, Roger W; Hannebaum, Reed; Schrader, Steve, Systems and methods for determining inconsistency characteristics of a composite structure.
  90. Engelbart,Roger W.; Hannebaum,Reed; Schrader,Steve, Systems and methods for determining inconsistency characteristics of a composite structure.
  91. Engelbart,Roger W.; Speno,Frank Gregory, Systems and methods for using light to indicate defect locations on a composite structure.
  92. Engelbart,Roger W.; Speno,Frank G., Systems and methods for using light to indicate inconsistency locations on a composite structure.
  93. Marin, Yannick; Luche, Emilie, Tool for simultaneously holding several attachment clips in contact with an aircraft fuselage frame element.
  94. Marin, Yannick; Guilloteau, Damien, Tool to hold several mounting clamps simultaneously against an aircraft fuselage frame element.
  95. Stephen R. Early, Web core structural panel.
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트

맨위로