$\require{mediawiki-texvc}$
  • 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"

과학기술 지식인프라 ScienceON

상세검색 다국어 입력
도움말도움말

특허 상세정보

MyON담기
내보내기

Joined wing aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/00   
미국특허분류(USC) 244/13 ; 244/16 ; 244/45R ; 244/87
출원번호 US-0482226 (1974-06-24)
발명자 / 주소
인용정보 피인용 횟수 : 16  인용 특허 : 0
초록
▼

An aircraft of the Canard type in which a first airfoil is attached to an aft fin portion of the fuselage at a higher elevation than a second airfoil which is attached to the fore portion of the fuselage. The second airfoil extends outwardly and rearwardly to meet the first airfoil whereby a triangular configuration is formed in plan view and in front elevation view. The airfoils may be flexible; simple cable controls may be provided to control the aircraft so that even inexperienced pilots can easily operate the aircraft. The triangular configuration en...

대표
청구항
▼

An aircraft comprising: a fuselage having fore and aft portions; a first airfoil connected to said aft portion of said fuselage, and said airfoil extending outwardly therefrom; a second airfoil connected to said fuselage at a location spaced forwardly from said first airfoil and at an elevation different from said first airfoil, said second airfoil extending rearwardly away from said fuselage and having extended ends connected to said first airfoil, said first and second airfoils forming a triangular configuration in front elevation view wherein said fir...

이 특허를 인용한 특허 피인용횟수: 16

  1. O'Shea, Hank. Aerial vehicle with variable aspect ratio deployable wings. USP2010117841559.
  2. Shepshelovich, Michael; Sletean, Mario; Steinbuch, Moshe; Levy, David Eli. Aircraft configuration for micro and mini UAV. USP2012028123160.
  3. Carr, Robert Jonathan. Aircraft internal wing and design. USP2005016840478.
  4. Carr,Robert Jonathan; Higgins,James Michael. Aircraft internal wing and design. USP2007087258302.
  5. Peters ; Jr. Spence E.. Aircraft structure to improve directional stability. USP2000086098923.
  6. Adkins Gordon V. (Wimborne GBX) McDonald John R. (Wimborne GBX) Sivertsen Olav N. (Isswich GBX). Aircraft with paired aerofoils. USP1989084856736.
  7. Sommer, Geoffrey S.; Cote, Kenneth A.. Canard-locked oblique wing aircraft. USP2015079079663.
  8. Hall Eric B. (135 ; Spring Grove Crescent Hounslow Middlesex TW3 4DA GB2). Compound wing aircraft. USP1982064336913.
  9. Radebold Reinhart (Quastenhornweg 14a 1000 Berlin 22 DEX). Concentrating reflector for solar radiation of low aerodynamic friction force and high aerodynamic buoyancy force. USP1984034438760.
  10. Russom,Jeffery D.; White,Lawrence R.; Greenwood,James. Control surface assemblies with torque tube base. USP2008087410120.
  11. Ferman,Marty Allen. Device and method of control of fixed and variable geometry rhomboid wings. USP2006117131611.
  12. Shmoldas John D. (Thousand Oaks CA) Hutchings Michael B. (Westlake Village CA) Barlow Christopher W. (Newbury Park CA). Extendable wing for guided missles and munitions. USP1997045615846.
  13. Van Ruymbeke, Edwin. Flying toy able to move by the flapping of wings. USP2013028382546.
  14. Tracy, Richard R.; Chase, James D.; Kroo, Ilan. Highly swept canard with low sweep wing supersonic aircraft configuration. USP2005026857599.
  15. Carr,Robert Jonathan; Higgins,James Michael. Lift system for an aerial crane and propulsion system for a vehicle. USP2006127147183.
  16. Morgenstern, John M.. Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom. USP2004056729577.

이 특허와 함께 이용한 콘텐츠

IPC 상위 출원인