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Unidirectional, multi-head fiber placement 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B65H-081/00
출원번호 US-0646316 (2003-08-22)
발명자 / 주소
  • Clark,Randall R.
  • Engwall,Dwight L.
  • Yonash,Mark G.
  • New,Jeffrey A.
출원인 / 주소
  • The Boeing Company
대리인 / 주소
    Shimokaji &
인용정보 피인용 횟수 : 50  인용 특허 : 5

초록

An aircraft part manufacturing device for automated composite lay up includes a mandrel tool having a an interior mandrel surface that conforms to an outside mold line (OML) of a part: to be manufactured. One or more circular rings surround the mandrel and are attached to the mandrel. The circular r

대표청구항

We claim: 1. A device for automated composite lay-up, comprising: a tool having an axis of rotation and an outside mold surface inside of a mandrel; and a circular ring surrounding said tool and said mandrel and concentric with said axis of rotation wherein said tool is rotated about said axis of r

이 특허에 인용된 특허 (5)

  1. Murray William J. (Midlothian TX), Apparatus for forming concave tape wrapped composite structures.
  2. Barr Roy L. ; Bloch Daniel D. ; Mallow Andrew R. ; Rhodes Charles A., Fiber placement mid-span redirect.
  3. Alenskis Brian A. (Bountiful UT) Geil Gerald L. (Diamond Bar CA) Gill Dee R. (Sandy UT) Moloney Brian N. (West Valley City UT), Filament winding system.
  4. Walker ; Grant W., Method of forming a tubular container.
  5. Koury James L., Multiple fiber placement head arrangement for placing fibers into channels of a mold.

이 특허를 인용한 특허 (50)

  1. Biornstad, Robert D.; Blankinship, Bruce C.; George, Terry J.; Ingram, William H., Composite barrel sections for aircraft fuselages and other structures.
  2. 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.
  3. 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.
  4. 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.
  5. Velicki, Alexander; Thrash, Patrick J., Composite fabric with rigid member structure.
  6. Nelson, Paul E.; Kramp, Jr., Robert A.; Lum, Matthew K., Composite lamination using array of parallel material dispensing heads.
  7. Nelson, Paul E.; Kramp, Jr., Robert Alan; Lum, Matthew K., Composite lamination using array of parallel material dispensing heads.
  8. 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.
  9. 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.
  10. 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.
  11. Hamlyn, Alexander; Hardy, Yvan, Device for using fibers with flexible fiber-routing tubes.
  12. Hamlyn, Alexander; Hardy, Yvan, Fiber application machine.
  13. Hamlyn, Alexander; Hardy, Yvan, Fiber application machine comprising a flexible compacting roller with a thermal regulation system.
  14. Hagman, Thomas J.; Bunker, Mark S., Graphite tape supply and backing paper take-up apparatus.
  15. Koon, Robert; Engelstad, Stephen P.; Tatting, Brian; Gurdal, Zafer, Highly tailored stiffening for advanced composites.
  16. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim, In-process vision detection of flaw and FOD characteristics.
  17. Englebart, Roger W.; Hannebaum, Reed; Pollock, Tim, In-process vision detection of flaw and FOD characteristics.
  18. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim, In-process vision detection of flaws and FOD by back field illumination.
  19. Engelbart, Roger W.; Hannebaum, Reed; Pollock, Tim, In-process vision detection of flaws and FOD by back field illumination.
  20. Wampler, Robert Ray; Zia Ullah, Muhammad, Material placement method and apparatus.
  21. Wampler, Robert Ray; Zia Ullah, Muhammad, Material placement method and apparatus.
  22. Hamlyn, Alexander, Method and apparatus for making structures of composite material, in particular airplane fuselage sections.
  23. Anderson, Patrick L.; Estrada, Leonard P., Method and apparatus for measuring the width of composite tape.
  24. Kisch, Robert A., Method and apparatus for placing short courses of composite tape.
  25. McCowin, Peter D.; Boberg, Mark C.; Nelson, Paul E., Method and apparatus for producing composite structures.
  26. Schuermann, Klaus; Sebastian, Lothar, Method and device for producing large cylindrical structures.
  27. Munaux, Olivier; Cappelle, Hervé ; Hamlyn, Alexander, Method and machine for applying a band of fibers on convex surfaces and/or with edges.
  28. Anderson,Donald A.; Johnson,Brice A.; Spoon,Stephen S., Method of transferring large uncured composite laminates.
  29. Brennan, Joseph Daniel; Atsebha, Solomon T.; Dorsey Palmateer, John W.; Anderson, Patrick L., Methods and systems for automated ply boundary and orientation inspection.
  30. Engelbart, Roger W.; Hannebaum, Reed; Schrader, Steve, Methods for determining inconsistency characteristics of a composite structure.
  31. 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.
  32. Johnson, Kent E.; Ulvin, Mark A., Methods of manufacturing structural panels.
  33. Tsotsis, Thomas K., Nanotube-enhanced interlayers for composite structures.
  34. Tsotsis, Thomas K., Nanotube-enhanced interlayers for composite structures.
  35. McCowin, Peter D., Reduced complexity automatic fiber placement apparatus and method.
  36. McCowin, Peter D., Reduced complexity automatic fiber placement apparatus and method.
  37. McCowin, Peter D., Simplified fiber tensioning for automated fiber placement machines.
  38. McCowin, Peter D., Simplified fiber tensioning for automated fiber placement machines.
  39. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  40. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  41. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  42. Stulc, Jeffrey F.; Chan, Wallace C.; Clapp, Brian C.; Rolfes, Neal G., Splice joints for composite aircraft fuselages and other structures.
  43. Johnson, Kent E.; Ulvin, Mark A., Structural panels for use in aircraft fuselages and other structures.
  44. Engelbart, Roger W.; Hannebaum, Reed; Rector, Eric; Haywood, Jeffrey, System and method for determining cumulative tow gap width.
  45. Engelbart, Roger W; Hannebaum, Reed; Schrader, Steve, Systems and methods for determining inconsistency characteristics of a composite structure.
  46. Engelbart, Roger W; Hannebaum, Reed; Schrader, Steve, Systems and methods for determining inconsistency characteristics of a composite structure.
  47. Engelbart,Roger W.; Speno,Frank G., Systems and methods for using light to indicate inconsistency locations on a composite structure.
  48. Slyne, William J., Tape laying apparatus and method.
  49. Slyne, William J., Tape laying apparatus and method.
  50. Hagman, Thomas J., Tape removal apparatus and process.
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