$\require{mediawiki-texvc}$
  • 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

Thrust generating apparatus

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-029/00   
미국특허분류(USC) 244/023.C; 244/012.2; 244/034.0A
출원번호 UP-0909524 (2006-03-23)
등록번호 US-7857256 (2011-02-24)
우선권정보 GB-0505956.3(2005-03-23)
국제출원번호 PCT/GB2006/050064 (2006-03-23)
§371/§102 date 20070924 (20070924)
국제공개번호 WO06/100523 (2006-09-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Fleit, Martin
인용정보 피인용 횟수 : 8  인용 특허 : 14
초록

There have been past proposals for air vehicles employing the Coanda effect. In these proposals, a jet of fluid, usually air, is made to flow radially outwardly over 5 a dome-shaped canopy to create lift. A cross-section through the canopy is curved to follow a segment of a circle or it may have a radius of curvature that increases in the direction of flow. In the invention, the radius (r) of the canopy curve decreases towards the downstream direction (x) in a way that is related to the decrease in the width of 10 the jet as it flows over the surface. Th...

대표
청구항

The invention claimed is: 1. A vertical take-off aircraft, comprising: means for causing fluid to flow radially outwardly from a central position over a canopy having a surface with double convex curvature about an axis, this surface serving to divert the radial flow towards an axial direction by operation of the Coanda effect and having a radius of curvature which decreases progressively less rapidly with increasing distance from the axis to a point close to but separated from a peripheral edge of the canopy; and a peripheral portion extending from the...

이 특허에 인용된 특허 (14)

  1. del Castillo Gilbert (10803 Hazen Rd. Houston TX 77072). Amphibious discoidal aircraft. USP1987064674708.
  2. Day Terence R. (9 Wolfram Court Anula ; Northern Territory AUX 0812). Annular body aircraft. USP1993045203521.
  3. Michael Amitay ; Ari Glezer. Apparatus and method for enhancement of aerodynamic performance by using pulse excitation control. USP2002076412732.
  4. Lowe ; Jr. Charles S.. Blown air lift generating rotating airfoil aircraft. USP2001086270036.
  5. Langley Lawrence W. (910 Cardinal Dr. Christiansburg VA 24073) Moses Hal L. (Rte. 1 ; Box 78 Newport VA 24128). Circular airplane. USP1991105054713.
  6. Vass Gabor I. (118-10221 133A Street Surrey ; B.C. CAX V3T 5J8). Circular wing aircraft. USP1996045503351.
  7. Bill Holben. Counter rotating circular wing for aircraft. USP2002096450446.
  8. Walter William C.. Lift augmented ground effect platform. USP1998095803199.
  9. Walter William C. ; Johnson Marshel Thomas. Lift augmented ground effect platform. USP2000076082478.
  10. Cunningham John T. (3559 High Mesa Dallas TX 75234). Lift-producing machine or device. USP1991075031859.
  11. Lurz Werner (Hamburg DEX). Method of and apparatus for controlling the boundary layer flow over the surface of a body. USP1985054516747.
  12. Ari Glezer ; Mark G. Allen. Micromachined synthetic jet actuators and applications thereof. USP2002106457654.
  13. Hassan Ahmed A. ; Tadghighi Hormoz ; Janakiram Ram D.. Oscillating air jets for reducing HSI noise. USP2001056234751.
  14. Beck ; Jr. August H. (San Antonio TX). VTOL aircraft. USP1992125170963.