$\require{mediawiki-texvc}$

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.

Leading edge for an aircraft 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-003/44
출원번호 US-0525535 (2000-03-14)
발명자 / 주소
  • Gruensfelder Cynthia Ann
  • Brase
  • Jr. Lawrence O.
출원인 / 주소
  • The Boeing Company
대리인 / 주소
    Harness Dickey & Pierce PLC
인용정보 피인용 횟수 : 51  인용 특허 : 20

초록

A leading edge (50) for an aircraft has a hard durometer elastomer tip (52). An elastomer panel (54) has a first end attached to the hard durometer elastomer tip (52) and has a plurality of reinforcing members capable of freely sliding inside the elastomer panel (54). A rigid block (58) is attached

대표청구항

[ What is claimed is:] [1.]1. An edge for a portion of an aircraft comprising:a hard durometer elastomer tip having first and second ends;a first elastomer panel having a first end attached to the first end of the hard durometer elastomer tip, a second end and a plurality of reinforcing members capa

이 특허에 인용된 특허 (20)

  1. Geiger Michael Watson ; Gruensfelder Cynthia Ann ; Jacobs Jack Howard, Active reinforced elastomer system.
  2. Maclean Brian J. (Daniel WY) Carpenter Bernard F. (Littleton CO) Misra Mohan S. (Golden CO), Adaptive control surface using antagonistic shape memory alloy tendons.
  3. Orrison William W. (900 NE. Loop 410 ; Suite E-103 San Antonio TX 78209), Air foil with reversible camber.
  4. Austin Fred (Commack NY) Knowles Gareth J. (Smithtown NY) Rossi Michael J. (Huntington NY), Apparatus and method for controlling the shape of structures.
  5. Burbridge Thomas Edward ; Tomko Harvey John ; Wille Robert Henry, Blade seal for an aircraft.
  6. Geiger Michael Watson ; Waldrop ; III John Cleveland,ESX ITX 28223, Continuous moldline technology system.
  7. Diller Joseph B. ; Miller ; Jr. Nicholas F., Elastomeric transition for aircraft control surface.
  8. Geiger Michael Watson, Environmental coating for an elastomer panel.
  9. Gruensfelder Cynthia Ann ; Wille Robert Henry, Expandable aircraft bay and method.
  10. Geders Paul Francis ; Groeneveld John David ; Wille Robert Henry, Expandable fuel cell.
  11. Cameron Dean Emory, Fairing for an expandable bay.
  12. Pierce ; Donald, Flexible aerofoils.
  13. Wille Robert Henry, Hinge line skin system for an aircraft.
  14. Covey James H. (Snohomish WA), Method for plating one side of a woven fabric sheet.
  15. Beier Theodor Harry ; Haake John Martin ; Wille Robert Henry ; Jacobs Jack Howard, Reinforced elastomer panel with embedded strain and pressure sensors.
  16. Wille Robert Henry, Tail for an aircraft.
  17. Brown Stephen T. (Bellevue WA) Statkus Frank D. (Woodinville WA), Variable camber aircraft wing tip.
  18. Ball William Henderson (Mercer Island WA) Ishimitsu Kichio Keith (Mercer Island WA), Variable camber inlet for supersonic aircraft.
  19. Albach Walter C. (Dallas TX) Fewel Kenneth J. (Nacogdoches TX), Variable control aircraft control surface.
  20. Kahara Bryan D. ; Priestley Richard T. ; Seho Kenneth E., Variable displacement fuel tank for aircraft.

이 특허를 인용한 특허 (51)

  1. Good,Mark S.; Huynh,Neal V.; Jones,Kelly T.; Sakurai,Selya, Actuation device positioning systems and associated methods, including aircraft spoiler droop systems.
  2. Voogt, Nicolaas, Aerospace vehicle fairing systems and associated methods.
  3. Voogt,Nicolaas, Aerospace vehicle fairing systems and associated methods.
  4. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F., Aerospace vehicle flow body systems and associated methods.
  5. Konings,Christopher A., Aerospace vehicle leading edge slat devices and corresponding methods.
  6. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
  7. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.
  8. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  9. Couffignal, Jean-Pierre; Vinches, Frederic, Aircraft horizontal stabilizer.
  10. Rampton,Scott N.; Amorosi,Stephen R., Aircraft leading edge apparatuses and corresponding methods.
  11. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  12. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V., Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods.
  13. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V., Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods.
  14. Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V., Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods.
  15. Lacy, Douglas S.; Beyer, Kevin W.; Brown, Stephen T.; Dees, Paul W.; Huynh, Neal V.; Kordel, Jan A.; Prow, Clayton A.; Sakurai, Seiya, Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods.
  16. Lacy,Douglas S.; Beyer,Kevin W.; Brown,Stephen T.; Dees,Paul W.; Huynh,Neal V.; Kordel,Jan A.; Prow,Clayton A.; Sakurai,Seiya, Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods.
  17. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  18. Arata,Allen A.; Graham,David H., Aircraft with articulated leading edge of fuselage and wings.
  19. Arata,Allen A., Aircraft with extendable leading edge of fuselage and wings.
  20. Arata,Allen A., Aircraft with rotatable leading edge of fuselage and wings.
  21. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas, Airplane with unswept slotted cruise wing airfoil.
  22. Dunne, James P.; Pitt, Dale M.; Kilian, Kevin J.; White, Edward V., Apparatus for variation of a wall skin.
  23. Hetrick, Joel A.; Kota, Sridhar; Ervin, Gregory F., Compliant structure design for varying surface contours.
  24. Bak, Dan Christian; Buhl, Thomas; Fuglsang, Peter; Madsen, Helge Aagaard; Rasmussen, Flemming, Control of power, loads and/or stability of a horizontal axis wind turbine by use of variable blade geometry control.
  25. Eveker, James V.; Young, Roger K., Hinge cover integration into door seal edges.
  26. Eveker, James V.; Young, Roger K., Hinge cover integration into door seal edges.
  27. Eveker, James V.; Young, Roger K., Hinge cover integration into door seal edges.
  28. Chang-Yuan Lin TW, Lamp holder for decorative lighting device.
  29. Wheaton, James M.; Amorosi, Stephen R., Leading edge flap apparatuses and associated methods.
  30. Wheaton,James M.; Amorosi,Stephen R., Leading edge flap apparatuses and associated methods.
  31. Fox, Stephen J.; Sakurai, Seiya, Link mechanisms for gapped rigid krueger flaps, and associated systems and methods.
  32. Beyer,Kevin W.; Fox,Stephen J.; Lacy,Douglas S.; Meredith,Paul T.; Prow,Clayton A.; Sakurai,Seiya; Wells,Stephen L., Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface.
  33. Dun, Roy, Methods and apparatuses for controlling airflow proximate to engine/airfoil systems.
  34. Grip, Robert E.; Brown, John J.; Harrison, Neal A.; Rawdon, Blaine K.; Vassberg, John C., Morphing airfoil leading edge.
  35. Sakurai,Seiya; Fox,Stephen J.; Beyer,Kevin W.; Lacy,Douglas S.; Johnson,Paul L.; Wells,Stephen L.; Noble,Jack S.; Meredith,Paul T.; Huynh,Neal V.; Christianson,Russell R.; Vijgen,Paul M.; Fitzpatrick, Multi-function trailing edge devices and associated methods.
  36. Wilson, James; West, Colin John; Sutton, David Alistair; Hadley, Paul, Seal.
  37. Kordel, Jan A.; Sakurai, Seiya; Bowers, Bret A.; Glassmoyer, Christopher G.; Williams, Darren B., Seal assemblies for use with drooped spoilers and other control surfaces on aircraft.
  38. Jasklowski, Christopher T., Shape memory alloy actuation system for variable area fan nozzle.
  39. Madsen, Casey Lyn, Shape memory alloy rods for actuation of continuous surfaces.
  40. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  41. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  42. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  43. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael, Systems and methods for providing differential motion to wing high lift device.
  44. Huynh,Neal V., Systems, apparatuses, and methods for moving aircraft control surfaces.
  45. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  46. Ambrose,David R., Unitized rotary actuator hinge fitting.
  47. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
  48. Hancock, Mark, Wind turbine blade.
  49. Hancock, Mark; Loh, Wuh Ken; Chang, Yun Chong Gabriel, Wind turbine blade.
  50. Loh, Wuh Ken; Ning, Ying, Wind turbine rotor blade.
  51. Irving,Jan; Davies,Robert, Wing tip device.
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