$\require{mediawiki-texvc}$

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.

Active system for early destruction of trailing vortices

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-023/06
  • B64C-009/00
  • B64C-013/16
출원번호 US-0964941 (1997-11-05)
발명자 / 주소
  • Crouch Jeffrey D.
  • Spalart Philippe R.
출원인 / 주소
  • The Boeing Company
대리인 / 주소
    Christensen O'Connor Johnson & Kindness
인용정보 피인용 횟수 : 39  인용 특허 : 10

초록

An active control method and apparatus for encouraging the early destruction of trailing vortices formed by a lifting body having at least two control surfaces on each side and creating multiple vortex pairs is provided. The method includes actuating the control surfaces in a manner leading to the d

대표청구항

[ The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:] [1.] A method of encouraging the early destruction of trailing vortices formed by a lifting body with left and right lifting surfaces which produce at least two trailing vortex pairs, t

이 특허에 인용된 특허 (10)

  1. Taylor Robert M. (Vienna VA), Aerodynamic surface tip vortex attenuation system.
  2. Haney William R. (6507 Foxboro Dr. Mayfield Village OH 44143), Air foil providing vortex attenuation.
  3. Gratzer Louis B. (Seattle WA), Laminar flow control airfoil.
  4. Nosenchuck Daniel M. (Mercerville NJ) Brown Garry L. (Princeton NJ), Lifting body with reduced-strength trailing vortices.
  5. Erwin John R. (Paradise Valley AZ), Method and apparatus for controlling tip vortices.
  6. Wygnanski Israel (4559 N. Placita de las Charcras Tucson AZ 85718), Method and apparatus for delaying the separation of flow from a solid surface.
  7. Griswold ; II Roger W. (Ben Franklin Rd. Old Lyme CT 06371), Vortex alleviating wing tip.
  8. Finch ; Reginald Vernon, Vortex reducing wing tip.
  9. Ransick Thomas F. (Rockford IL), Wingtip turbine.
  10. Patterson ; Jr. James C. (Newport News VA), Wingtip vortex turbine.

이 특허를 인용한 특허 (39)

  1. Shmilovich, Arvin; Yadlin, Yoram; Clark, Roger W., Active systems and methods for controlling an airfoil vortex.
  2. Good,Mark S.; Huynh,Neal V.; Jones,Kelly T.; Sakurai,Selya, Actuation device positioning systems and associated methods, including aircraft spoiler droop systems.
  3. Breitsamter, Christian; Allen, Alexander, Aerodynamic element and wing with aerodynamic element, actuator-activation module, computer, computer program and method of influencing wake eddies.
  4. Voogt, Nicolaas, Aerospace vehicle fairing systems and associated methods.
  5. Voogt,Nicolaas, Aerospace vehicle fairing systems and associated methods.
  6. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F., Aerospace vehicle flow body systems and associated methods.
  7. Konings,Christopher A., Aerospace vehicle leading edge slat devices and corresponding methods.
  8. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  9. Rampton,Scott N.; Amorosi,Stephen R., Aircraft leading edge apparatuses and corresponding methods.
  10. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  11. 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.
  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.; 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.
  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. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  17. Roland Stuff DE; Heinrich Vollmers DE, Aircraft with means for a premature breakdown of the wing vortex pair.
  18. Shmilovich, Arvin; Yadlin, Yoram; Clark, Roger; Leopold, Donald, Apparatus and method for the control of trailing wake flows.
  19. Wheaton, James M.; Amorosi, Stephen R., Leading edge flap apparatuses and associated methods.
  20. Wheaton,James M.; Amorosi,Stephen R., Leading edge flap apparatuses and associated methods.
  21. Fox, Stephen J.; Sakurai, Seiya, Link mechanisms for gapped rigid krueger flaps, and associated systems and methods.
  22. 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.
  23. Huenecke, Klaus, Method and apparatus for reducing trailing vortices in the wake of an aircraft.
  24. Journade, Jerome, Method and device for reducing the induced speeds in vortices in the wake of an aircraft.
  25. Laporte, Florent; Hansen, Heinz, Method of controlling an aircraft in flight, especially to reduce wake vortices.
  26. Laporte, Florent; Hansen, Heinz, Method of controlling an aircraft in flight, especially to reduce wake vortices.
  27. 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.
  28. Ingo Borchers DE; Roger Drobietz DE; Michael Gruenewald DE; Knut Mau DE; Johann Reichenberger DE, Noise reducing vortex generators on aircraft wing control surfaces.
  29. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  30. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  31. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  32. Shmilovich, Arvin; Yadlin, Yoram; Clark, Roger W.; Leopold, Donald H., Systems and methods for destabilizing an airfoil vortex.
  33. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael, Systems and methods for providing differential motion to wing high lift device.
  34. Lewis, Michael S.; Meserole, Jere S.; Dunn, Michael J.; Tillotson, Brian J., Systems and methods for tracing aircraft vortices.
  35. Lewis, Michael S.; Meserole, Jere S.; Dunn, Michael J.; Tillotson, Brian J., Systems and methods for tracing aircraft vortices.
  36. Lewis, Michael S.; Meserole, Jere S.; Dunn, Michael J.; Tillotson, Brian J., Systems and methods for tracing aircraft vortices.
  37. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  38. Eaton, John K.; Matalanis, Claude, Translating active Gurney flap to alleviate aircraft wake vortex hazard.
  39. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
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