$\require{mediawiki-texvc}$

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.

Apparatus for closing an air gap between a flap and an aircraft 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-001/38
출원번호 US-0444861 (1982-11-26)
우선권정보 DE-3149629 (1981-12-15)
발명자 / 주소
  • Kunz Rdiger (Munich DEX)
출원인 / 주소
  • Messerschmitt-Boelkow-Blohm Gesellschaft mit beschraenkter Haftung (Munich DEX 03)
인용정보 피인용 횟수 : 42  인용 특허 : 3

초록

An air gap between a main flap and an adjacent aircraft portion is closed by an auxiliary flap. The auxiliary flap (8) has a hinging axis (9) extending substantially in parallel to the aerodynamic flow along aircraft portions adjacent to the auxiliary flap. With the aid of the auxiliary flap an aero

대표청구항

An apparatus for aerodynamically closing an air gap between a trailing edge wing flap and an adjacent side portion of an aircraft body defining an aerodynamic flow direction, comprising auxiliary flap means (8) for aerodynamically closing said air gap, said auxiliary flap means having a given length

이 특허에 인용된 특허 (3)

  1. Pauly, Bernard; Ciprian, Danilo, Aircraft wing provided with a high-lift system in its leading edge.
  2. Ridley ; Jr. Thomas R. (Kent WA) Simmons Gerald C. (Kirkland WA), Assembly for sealing the mounting opening for a flying horizontal stabilizer on a vertical stabilizer.
  3. Cole James B. (Mercer Island WA), Extendable aerodynamic fairing.

이 특허를 인용한 특허 (42)

  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. Fol, Thierry; Jimenez, Philippe; Namer, Arnaud, Aircraft comprising a central fairing that adjusts the pressure on the wing structures by means of local geometric deformations.
  7. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  8. Rampton,Scott N.; Amorosi,Stephen R., Aircraft leading edge apparatuses and corresponding methods.
  9. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  10. 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.
  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.; 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.
  13. 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.
  14. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  15. Kelley-Wickemeyer, Robert H.; Seidel, Gerhard E.; Anast, Peter Z.; McLean, James Douglas, Airplane with unswept slotted cruise wing airfoil.
  16. Flaig Axel,DEX ; Schwetzler Detlev,DEX ; Stache ; deceased Ulrich,DEXITX by Ronald Seiler ; legal representative, Apparatus for influencing a wing root airflow in an aircraft.
  17. Birkenstock, David, Apparatus, system and method for drag reduction.
  18. Burbridge Thomas Edward ; Tomko Harvey John ; Wille Robert Henry, Blade seal for an aircraft.
  19. Diller Joseph B. ; Miller ; Jr. Nicholas F., Elastomeric transition for aircraft control surface.
  20. Diller Joseph B. ; Miller ; Jr. Nicholas F., Elastomeric transition for aircraft control surface.
  21. Ellis James R. ; Diller Joseph B., Expandable aircraft section.
  22. Poppe, Bernd; Auhagen, Kurt, Flap interconnection system for aircraft.
  23. Opsahl Allan W. (Renton WA), Flap torque tube slot seal.
  24. Wheaton, James M.; Amorosi, Stephen R., Leading edge flap apparatuses and associated methods.
  25. Loyet, Jessica; Pitt, Dale M., Mitigation of surface discontinuities between flight control surfaces and an airframe of an aircraft.
  26. Etling, Keith A., Morphing control surface transition.
  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. Young Kendall Gardner ; Pauletti Steven Louis, Rotor driven edge.
  29. Wilson, James; Quayle, Alan; Hadley, Paul, Seal assembly.
  30. Martin Hernandez, Agustin Mariano, Sealing system for the gap existing between the fuselage and the elevator of an aircraft with orientable horizontal stabilizer.
  31. Martin Hernandez, Agustín Mariano, Sealing system for the gap existing between the fuselage and the elevator of the orientable horizontal stabiliser of an aircraft, extended with an aerodynamic fairing for sealing of the opening existing between the fuselage and the orientable horizontal stabiliser.
  32. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  33. Da Rocha-Schmidt, Luiz, Shape-variable gap covering between control surfaces and adjacent structural components on aircrafts.
  34. Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  35. Huynh,Neal V.; Bleeg,Robert J.; Pepper,Ralph Scott; Standley,John A.; Bocksch,Brian L., Systems and methods for controlling aircraft flaps and spoilers.
  36. Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael, Systems and methods for providing differential motion to wing high lift device.
  37. Tobin, James Robert; Gobeli, William Max; Herr, Stefan, Tip extension assembly for a wind turbine rotor blade.
  38. Ross James C. ; Storms Bruce L., Tip fence for reduction of lift-generated airframe noise.
  39. Bleazard, Mark, Torque tube door.
  40. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  41. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
  42. Orazi Paul, Wing assemblies for aircraft.
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