$\require{mediawiki-texvc}$

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.

Elastomeric transition for aircraft control surface 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-003/52
출원번호 US-0059725 (1998-01-09)
발명자 / 주소
  • Diller Joseph B.
  • Miller
  • Jr. Nicholas F.
출원인 / 주소
  • Northrop Grumman Corporation
대리인 / 주소
    Anderson
인용정보 피인용 횟수 : 43  인용 특허 : 12

초록

Elastomeric transition sections (118, 124) are mounted between the upper and lower portions of a wing (100) and a control surface (102) hinged thereto. The elastomeric transition sections include elastomeric material (126) having a plurality of holes (128) formed therethrough. Flexible rods (134, 13

대표청구항

[ What is claimed is:] [1.] An aircraft wing assembly, comprising:a main wing portion;a control surface having a forward end, an inboard edge and an outboard edge, the forward end being attached to the main wing portion for movement of the control surface relative to the main wing portion; anda sing

이 특허에 인용된 특허 (12)

  1. Kunz Rdiger (Munich DEX), Apparatus for closing an air gap between a flap and an aircraft.
  2. Gar Konrad (Haus Nr. 30 8078 Nettelhofen DT), Flapping wing aircraft.
  3. Thompson Harold L. (Okmulgee OK), Land, water and air craft.
  4. Turris Fabrizio R. S. (Pomigliano ITX) Pagliuso Salvatore (Arzano ITX), Method for the controlled curing of composites.
  5. Clark Frank B. (Glastonbury CT), Method of making a hollow airfoil.
  6. Harder Isaac E. (Grand Prairie TX), Method of making carbon/carbon composites.
  7. Whitener Philip C. (Seattle WA), Method of making composite aircraft wing.
  8. Tanaka Shoichi (Shizuoka JA), Method of vacuum-pressure injection moulding.
  9. Dunahoo Edmond O. (Long Beach CA), Multi-chambered cellular structure and method for manufacture.
  10. Johnson Jay (3225 N. Verdugo Glendale CA 91208), Process for manufacturing resin-impregnated, reinforced articles without the presence of resin fumes.
  11. Brown Stephen T. (Bellevue WA) Statkus Frank D. (Woodinville WA), Variable camber aircraft wing tip.
  12. Albach Walter C. (Dallas TX) Fewel Kenneth J. (Nacogdoches TX), Variable control aircraft control surface.

이 특허를 인용한 특허 (43)

  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. Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F., Aerospace vehicle flow body systems and associated methods.
  4. Jones,Kelly T., Aircraft control surface drive system and associated methods.
  5. Casse, Christophe, Aircraft hinge arranged between a movable panel and a load-bearing structure.
  6. Rampton,Scott N.; Amorosi,Stephen R., Aircraft leading edge apparatuses and corresponding methods.
  7. Lacy,Douglas S.; Wyatt,Greg H., Aircraft leading edge device systems and corresponding sizing methods.
  8. 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.
  9. 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.
  10. 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.
  11. 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.
  12. Good,Mark S.; Viigen,Paul M.; Gitnes,Seth E.; Thomas,Glynn Michael, Aircraft wing systems for providing differential motion to deployable lift devices.
  13. Phillips, Warren F., Apparatus and method for reducing induced drag on aircraft and other vehicles.
  14. Phillips, Warren F., Apparatus and method for twisting a wing to increase lift on aircraft and other vehicles.
  15. Birkenstock, David, Apparatus, system and method for drag reduction.
  16. Stewart, David Mark, Bridging seal.
  17. Dittrich, Kay W., Cover skin for a variable-shape aerodynamic area.
  18. Khorrami, Mehdi R.; Lockard, David P.; Moore, James B.; Su, Ji; Turner, Travis L.; Lin, John C.; Taminger, Karen M.; Kahng, Seun K.; Verden, Scott A., Elastically deformable side-edge link for trailing-edge flap aeroacoustic noise reduction.
  19. Arata, Allen A., Elastomeric transition.
  20. Wildman, Eric, Flight surface seal.
  21. Schlipf, Bernhard; Hue, Xavier, High lift component for an aircraft, high lift system, method for adjusting the high lift characteristics of an aircraft and aircraft.
  22. Loyet, Jessica; Pitt, Dale M., Mitigation of surface discontinuities between flight control surfaces and an airframe of an aircraft.
  23. Burgos Gallego, Francisco de Paula; Maroto De Hoyos, Manuel, Mobile surfaces for aircraft with sealed slots.
  24. Etling, Keith A., Morphing control surface transition.
  25. 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.
  26. Young Kendall Gardner ; Pauletti Steven Louis, Rotor driven edge.
  27. Wilson, James; West, Colin John; Sutton, David Alistair; Hadley, Paul, Seal.
  28. Martin Hernandez, Agustin Mariano, Sealing system for the gap existing between the fuselage and the elevator of an aircraft with orientable horizontal stabilizer.
  29. Wigley, Alexander T., Shape shifting foils.
  30. Manley, David J.; Grip, Robert E., Shape-changing control surface.
  31. Da Rocha-Schmidt, Luiz, Shape-variable gap covering between control surfaces and adjacent structural components on aircrafts.
  32. Conway, Jr., George Louis; Young, Kendall G.; Stroud, Ron L., Single aperture conformal aircraft bays.
  33. McCallum, Brent N.; Young, Kendall G., Subdermally-reinforced elastomeric transitions.
  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. Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V., Trailing edge device catchers and associated systems and methods.
  39. Speer,Thomas E., Vehicle control systems and corresponding sizing methods.
  40. Hancock, Mark, Wind turbine blade with device for changing the aerodynamic surface or shape.
  41. Karem, Abe, Wing and blade structure using pultruded composites.
  42. Karem, Abe, Wing and blade structure using pultruded composites.
  43. Dyckrup, Werner, Wing for an 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