$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Switchable vortex generator and array formed therewith, and uses of the same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/38    B64C-005/10    B64C-009/00    B64C-019/00    B64C-021/00   
미국특허분류(USC) 244/099.12; 244/201; 244/204; 244/204.1
출원번호 US-0436616 (2009-05-06)
등록번호 US-8616494 (2013-12-31)
우선권정보 DE-10 2008 022 504 (2008-05-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Global IP Counselors, LLP
인용정보 피인용 횟수 : 1  인용 특허 : 15
초록

The invention relates to a vortex generator (10), in particular for a model (12) in a fluid-dynamic channel. In order to save time during the development of vehicles, in particular aircraft, in particular to save wind tunnel time, it is suggested to configure the vortex generator (10) switchable. Further, the invention relates to various uses of such a switchable vortex generator (10), in particular on models in fluid-dynamic channels and in fluid-dynamic channel tests.

대표
청구항

1. A switchable vortex generator for arrangement on a flow-dynamic surface comprising a vortex generating element reciprocatingly switchable between at least first and second positions, the vortex generating element being configured to generate vortices in a flow flowing in the area of said flow-dynamic surface, anda support member configured to support the vortex generating element, the support member being moveable to selectively hold the vortex generating element at least in the first position at which the vortex generating element is extended from th...

이 특허에 인용된 특허 (15)

  1. Alan J. Bilanin ; Robert M. McKillip, Jr.. Actuating device with at least three stable positions. USP2002026345792.
  2. McKillip ; Jr. Robert M.. Actuating device with multiple stable positions. USP2001046220550.
  3. DiCocco,Jack; Prince,Troy; Patel,Mehul; Ng,Tsun Ming Terry. Aircraft and missile afterbody flow control device and method of controlling flow. USP2006077070144.
  4. Prince, Troy; Lisy, Frederick J.; Patel, Mehul P.; DiCocco, Jack M.; Carver, Reed; Schmidt, Robert N.. Aircraft and missile forebody flow control device and method of controlling flow. USP2004026685143.
  5. Prince, Troy; Lisy, Frederick J.; Patel, Mehul P.; DiCocco, Jack M.; Carver, Reed; Schmidt, Robert N.. Aircraft and missile forebody flow control device and method of controlling flow. USP2011077977615.
  6. Prince,Troy; Lisy,Frederick J.; Patel,Mehul P.; DiCocco,Jack M.; Carver,Reed; Schmidt,Robert N.. Aircraft and missile forebody flow control device and method of controlling flow. USP2007067226015.
  7. Wygnanski Israel,ILX ; Greenblatt David,ILX ; Seifert Avi,ILX. Airfoil with dynamic stall control by oscillatory forcing. USP2001076267331.
  8. van Namen, Frederik T.. Bistable electro-magnetic mechanical actuator. USP2003016512435.
  9. Lisy, Frederick J.; Modarreszadah, Mohammed; Patel, Mehul P.; DiCocco, Jack M.; Carver, Reed; Schmidt, Robert N.; Prince, Troy. Flow control device and method of controlling flow. USP2005016837465.
  10. Lisy,Frederick J.; Modarreszadah,Mohammed; Patel,Mehul P.; DiCocco,Jack M.; Carver,Reed; Schmidt,Robert N.; Prince,Troy. Flow control device and method of controlling flow. USP2008027334760.
  11. Wygnanski Israel (4559 N. Placita de las Charcras Tucson AZ 85718). Method and apparatus for delaying the separation of flow from a solid surface. USP1993055209438.
  12. Lee,Hak Tae; Bieniawski,Stefan R.; Kroo,Ilan M.. Miniature trailing edge effector for aerodynamic control. USP2008087410133.
  13. Lorkowski, Thomas; Grohmann, Boris. System for reducing aerodynamic noise at a supplementary wing of an aircraft. USP2010087766281.
  14. Lorkowski, Thomas; Grohmann, Boris. System for reducing aerodynamic noise at a supplementary wing of an aircraft. USP2011088006941.
  15. Waring John,CAX ITX K4A 3H5. Wearable article for athlete with vortex generators to reduce form drag. USP1998045734990.