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Honeycomb structure 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • E04B-001/82
  • F01N-001/02
출원번호 US-0414746 (1982-09-03)
발명자 / 주소
  • Bourland
  • Jr. Gordon (Arlington TX) Price Howard M. (Burleson TX)
출원인 / 주소
  • LTV Aerospace and Defense Company (Dallas TX 02)
인용정보 피인용 횟수 : 33  인용 특허 : 3

초록

A septum (18) is installed at a desired depth within a section of honeycomb core (12) for use in a sound attenuation panels, the septum is sandwiched between two layers (20, 24) of support material having a melting temperature intermediate between the fusing and curing temperatures of the septum mat

대표청구항

A honeycomb structure formed by inserting a honeycomb core through a septum material and one or more layers of meltable support material, employed to precisely position the septum material relative to said honeycomb core comprising: a honeycomb core having a plurality of cells therethrough, a plural

이 특허에 인용된 특허 (3)

  1. Harp Marlyn F. (Winfield KS) Diepenbrock ; Jr. James L. (Wichita KS) Nelsen M. Dean (Wichita KS), Honeycomb core with internal septum and method of making same.
  2. Schindler Guenter M. (Palos Verdes CA), Multi-layered acoustic liner.
  3. Shuttleworth Richard G. (South Windsor CT) Snyder Gene R. (Vernon CT), Sound absorbing structure.

이 특허를 인용한 특허 (33)

  1. Peiffer, Alexander; Maier, Rudolf, Acoustic absorber for aircraft engines.
  2. Syed Asif A., Acoustic liner manufacture.
  3. Nampy, Sreenivas Narayanan; Biset, Charles Michael; Soria, Christian, Acoustic structural panel with herringbone core.
  4. Kuan-Hong Lo (8-3 Fl. ; No. 1 ; Lane 535 ; Minchuan E. Rd. Taipei TWX), Assembled sound-muffling thermal insulation board.
  5. Niemerski Michael C., Deformable impact test barrier.
  6. Niemerski Michael C., Deformable impact test barrier.
  7. Niemerski Michael C. (Jenison MI) Schoeb Gerald J. (Holland MI) Huebner Fritz (Holland MI), Deformable impact test barrier.
  8. Harper, Cedric B.; Humphries, Neil, Fan section.
  9. Olsen,Ronald F.; Breer,Marlin D., Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods.
  10. Gilson, Jonathan; Cicon, Dennis; Atassi, Oliver V., Gas turbine engine with noise attenuating variable area fan nozzle.
  11. Gilson, Jonathan; Cicon, Dennis; Atassi, Oliver V., Gas turbine engine with noise attenuating variable area fan nozzle.
  12. Johnson, Jeffrey Don, Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture.
  13. Strunk,John, Integrated inlet attachment.
  14. Whalen, John; Hagemann, John J.; Yunger, Robert J.; Henning, Peter H.; Hurt, Thomas; Myre, Jake, Inverted cell honeycomb structure shelving.
  15. Breer, Marlin D.; Olsen, Ronald F.; Kunze, Jr., Robert K.; Riedel, Brian L., Method and apparatus for aircraft inlet ice protection.
  16. Marlin D. Breer ; Ronald F. Olsen ; Robert K. Kunze, Jr. ; Brian L. Riedel, Method and apparatus for aircraft inlet ice protection.
  17. Marlin D. Breer ; Ronald F. Olsen ; Robert K. Kunze, Jr. ; Brian L. Riedel, Method and apparatus for aircraft inlet ice protection.
  18. Shah, Anil D.; Gupta, Alankar, Method and apparatus for detecting conditions conducive to ice formation.
  19. Shah,Anil D.; Gupta,Alankar, Method and apparatus for detecting conditions conducive to ice formation.
  20. Eilert,Theodore J.; Harkins,Henry D.; Kornfeld,Roger E.; Breer,Marlin D., Method and apparatus for forming complex contour structural assemblies.
  21. Friddell,Stephen D.; Prichard,Alan K., Method and apparatus for liquid containment, such as for aircraft fuel vessels.
  22. Clarke James A. ; Kunze ; Jr. Robert K., Method of forming acoustic attenuation chambers using laser processing of multi-layered polymer films.
  23. Clarke James A. ; Kunze ; Jr. Robert K., Method of forming acoustic attenuation chambers using laser processing of multi-layered polymer films.
  24. Eilert, Theodore J.; Harkins, Henry D.; Kornfeld, Roger E.; Breer, Marlin D., Preform for forming complex contour structural assemblies.
  25. Porte, Alain, Process for de-icing by forced circulation of a fluid, an air intake cowling of a reaction motor and device for practicing the same.
  26. Moore, Charles H.; Sutton, Matthew T.; Willham, John E. C., Resin panels with embedded structured-cores and methods of making the same.
  27. Yang,Zhi Yu; Wen,Weijia; Sheng,Ping; Zhang,Xixiang, Sound attenuating structures.
  28. Gao, Zhenyan; Akhlaque-e-rasul, Shaikh; Luo, Cheng; Sherwood, William Moore, Stepped honeycomb rocker insert.
  29. Nye Theodore W. ; Baker Jeffrey L., Structure having low acoustically-induced vibration response.
  30. Brewster, M. Hoyt; Moore, Charles H.; Willham, John E. C., Structured-core laminate panel.
  31. Brewster, M. Hoyt; Moore, Charles H.; Willham, John E. C., Structured-core laminate panels and methods of forming the same.
  32. Brewster, M. Hoyt; Moore, Charles H.; Willham, John E. C., Structured-core laminate panels and methods of forming the same.
  33. Sjogren,John F.; Eilert,Theodore J.; Harkins,Henry D., System and method for processing a preform vacuum vessel to produce a structural assembly.
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