$\require{mediawiki-texvc}$
  • 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"
쳇봇 이모티콘
안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

Free flyable structure

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/42   
미국특허분류(USC) 244/13 ; 244/90R ; 244/46 ; 244/45R
출원번호 US-0617091 (1984-05-23)
국제출원번호 PCT/GB83/00242 (1983-09-28)
§371/§102 date 1984May2 (1984May2)
국제공개번호 WO-8401346 (1984-04-12)
발명자 / 주소
인용정보 피인용 횟수 : 19  인용 특허 : 3
초록

A free flyable structure includes a wing formation (2) including an inflatable container of such form that when it is inflated the container (2) has an aerofoil shaped cross-section whereby relative displacement between the container and surrounding air enables free flight conditions. A substantially rigid means (19) carries the pay load from the wing formation (2). Flight path control of the flyable structure includes producing relative displacement between the load and wing formation. Additional flight path controls may be used. A canard wing assembly ...

대표
청구항

A flyable structure comprising: wing formation including an air inflatable elongate container having a leading edge region and a trailing edge region, the container being of such form that when inflated it provides an airfoil cross-section whereby relative displacement between the container and surrounding air produces aerodynamic lift; elongate means for supporting and maintaining the leading edge region in an extended condition while leaving the trailing edge region unsupported; a king-post arrangement for supporting a load below the wing formation, th...

이 특허를 인용한 특허 피인용횟수: 19

  1. Kendall, Greg T.; Lisoski, Derek L.; Morgan, Walter R.; Griecci, John A.. Active dihedral control system for a torisionally flexible wing. USP2015099120555.
  2. Kendall, Greg T.; Lisoski, Derek L.; Morgan, Walter R.; Griecci, John A.. Active dihedral control system for a torsionally flexible wing. USP2017099764819.
  3. Chutter, Richard. Aerodynamically buoyant sailcraft. USP2017039598144.
  4. Nolan, Robert. Air-ground vehicle with integrated fuel tank frame. USP2017069682620.
  5. Bertelsen, William D.. Aircraft and convertible wing assembly. USP2017059637230.
  6. Cox, Earl C.; Swanson, Kyle D.. Aircraft control method. USP2005086931247.
  7. Kendall, Greg T.; Morgan, Walter R.. Aircraft control system. USP2010097802756.
  8. Lisoski,Derek L.; Kendall,Greg T.. Aircraft control system. USP2007047198225.
  9. James H. Yim. Airwing structure. USP2002046364251.
  10. Farley, Rodger; MacCallum, Taber Kyle; Lee, G. Ryan; Padilla, Sebastian. Continuous multi-chamber super pressure balloon. USP20181110124875.
  11. Fisher Jeffrey A. ; Miller Edward V.. Deployable wing with propulsion for range extension. USP2001116322021.
  12. Nolan, Robert. Ground vehicle with flight capability. USP2017059656526.
  13. Hodgson Frank L. (223 Hedge Rd. Menlo Park CA 94025). Hybrid wing assembly. USP1990024901945.
  14. Flynn John P. P. (Hereford GB2). Light aircraft with parachute wing. USP1989104875642.
  15. Smith, John J.; Witkowski, Allen C.. Method and apparatus for parachute reefing control. USP2010047703720.
  16. Smith, John J.; Witkowski, Allen C.. Method for parachute reefing control. USP2011017871043.
  17. Leidich, Jared; MacCallum, Taber Kyle; Bowen, Ty. Rigidized assisted opening system for high altitude parafoils. USP2017029561858.
  18. Asseline, Jean; De Noni, George. Small-sized radio-controlled flying device. USP2004016676084.
  19. Bertelsen,William D.; Bertelsen,William R.. Wing assembly and aircraft. USP2009037510143.