$\require{mediawiki-texvc}$

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.

Retractable vortex generator 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-023/06
출원번호 US-0477806 (2006-06-30)
등록번호 US7878457 (2011-01-18)
발명자 / 주소
  • Narramore, Jimmy Charles
출원인 / 주소
  • Bell Helicopter Textron, Inc.
대리인 / 주소
    Pillsbury Winthrop Shaw Pittman LLP
인용정보 피인용 횟수 : 19  인용 특허 : 27

초록

A flow control device is disclosed including a flow control surface over which fluid is designed to flow in a predetermined direction. Vortex generators are associated with the flow control surface. Each respective vortex generator has a pivot axis that forms an acute angle with respect to the prede

대표청구항

What is claimed is: 1. A flow control device comprising:vortex generators associated with a flow control surface of an aircraft over which fluid is designed to flow in a predetermined direction, each respective vortex generator having a pivot axis that forms an acute angle with respect to the predet

이 특허에 인용된 특허 (27)

  1. Maestrello Lucio (Newport News VA), Active control of boundary layer transition and turbulence.
  2. McKillip ; Jr. Robert M., Actuating device with multiple stable positions.
  3. Spillman John J. (Bedford GB2), Aerofoil bodies.
  4. Clark, Walter Dennis, Aircraft with forward opening inlay spoilers for yaw control.
  5. Nelson Wilbur C. (1540 Cedar Bend Drive Ann Arbor MI 48103), Airfoil tip vortex control.
  6. Cox Ronald A. (Norman OK), Concealable flap-actuated vortex generator.
  7. Michael Campbell, Controllable vortex generator.
  8. Maxworthy Tony (Culver City CA), Delta wing with lift enhancing flap.
  9. Lisy Frederick J. ; Schmidt Robert N., Deployable flow control device.
  10. Burnham Robert W. (Seattle WA), Directional control device for aircraft.
  11. Narramore Jimmy C. (Bedford TX), Flaperon system for tilt rotor wings.
  12. Schmidt Robert N. ; Shaw Greg S., Fluid flow control devices.
  13. Kayser Lyle D. ; Brown T. Gordon, Fold-out fin.
  14. Wake Brian E. ; Egolf T. Alan ; Lorber Peter F. ; Landgrebe Anton J., Half-plow vortex generators for rotor blades for reducing blade-vortex interaction noise.
  15. Wake Brian E. ; Lorber Peter F. ; Landgrebe Anton J., Half-plow vortex generators for rotorcraft blades for reducing blade-vortex interaction noise.
  16. Bauer Andrew B. (Orange CA), Hidden vortex generators.
  17. Codina George, Method and apparatus for countering asymmetrical aerodynamic process subjected onto multi engine aircraft.
  18. Wygnanski Israel (4559 N. Placita de las Charcras Tucson AZ 85718), Method and apparatus for delaying the separation of flow from a solid surface.
  19. King, David W.; Shultz, Peter M., Multi-mode tiltrotor nacelle control system with integrated envelope protection.
  20. Liu John ; McVeigh Michael A. ; Mayer Robert J., Pivoting spanwise-flow redirector for tiltrotor aircraft.
  21. Jordan Heinz (Wlfnitz bei Klagenfurt ATX), Rigid wing flying craft.
  22. Jacot Arthur Dean ; Julien Gerald J. ; Clingman Dan J., Shape memory rotary actuator.
  23. Russell ; Jr. William F. (Westport CT) Roncz John (Elkhart IN), Spoiler system for ground effect vehicles.
  24. Vess Robert J. (Raleigh NC) Rao Dhanvada (Hampton VA), Strake fence flap.
  25. Farokhi Saeed (Lawrence KS) Taghavi Ray R. (Lawrence KS), Supersonic vortex generator.
  26. Bruce D. Charles ; Ahmed A. Hassan ; Hormoz Tadghighi ; Ram D. JanakiRam, Tapered/segmented flaps for rotor blade-vortex interaction (BVI) noise and vibration reduction.
  27. McCarthy Peter T. (134 Park St. #5 Buffalo NY 14201), Tip vortex generation technology for creating a lift enhancing and drag reducing upwash effect.

이 특허를 인용한 특허 (19)

  1. Ireland, Peter, Application of elastomeric vortex generators.
  2. Lee, Yee-Chun, Boundary layer propulsion airship with related system and method.
  3. Bonnaud, Cyril; Stevens, Thomas; Roche, Frédéric; Dostes, Stéphane, Device for generating aerodynamic disturbances so as to protect the outer surface of an aircraft against elevated temperatures.
  4. Hutcheson, Florence V.; Brooks, Thomas F., Flow disruption devices for the reduction of high lift system noise.
  5. Dixon, Kristian R.; Mayda, Edward A., Method and apparatus for reduction of fatigue and gust loads on wind turbine blades.
  6. Beckman, Brian C.; Kimchi, Gur; Ko, Allan, Propeller blade indentations for improved aerodynamic performance and sound control.
  7. Beckman, Brian C.; Kimchi, Gur; Ko, Allan, Propeller blade leading edge serrations for improved sound control.
  8. Beckman, Brian C.; Kimchi, Gur; Ko, Allan, Propeller blade trailing edge fringes for improved sound control.
  9. Beckman, Brian C.; Kimchi, Gur; Ko, Allan, Propeller surface area treatments for sound dampening.
  10. Barrett, Ronald M., Radar energy absorbing deformable low drag vortex generator.
  11. Barrett, Ronald M., Radar energy absorbing deformable low drag vortex generator.
  12. Sclafani, Anthony J.; Konings, Christopher A., Retractable nacelle chine.
  13. Ikeda, Tadashige, Smart vortex generator, and aircraft, vessel, and rotary machine being equipped with the same.
  14. Sutton, Drew, System and method for reducing rotor blade noise.
  15. Hegenbart, Matthias; Eilken, Wolfgang; Paul, Erich; Stefes, Bruno; Duken, Lena, Vortex generator arrangement.
  16. Tobin, James Robert; Herr, Stefan; Riddell, Scott Gabell; Booth, Michael Christopher, Vortex generator for a rotor blade.
  17. Shivashankara, Belur N.; Mabe, James H.; Clingman, Dan J., Vortex generator using shape memory alloys.
  18. Bordoley, Anat; Tillotson, Brian J.; Wang, Michael Chih-Huan; Clingman, Dan J., Vortex generators responsive to ambient conditions.
  19. Xiong, Wei, Wind turbine blades with controllable aerodynamic vortex elements.
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