• 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
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

Large dimension aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/00   
미국특허분류(USC) 244/013 ; 244/035R ; 244/045R
출원번호 US-0574364 (1995-12-18)
우선권정보 EP-0120021 (1994-12-16)
발명자 / 주소
대리인 / 주소
    Browdy and Neimark
인용정보 피인용 횟수 : 40  인용 특허 : 9

A large transport aircraft, for more than 400 passengers, with a first wing (3) extending from an intermediate point on the fuselage (1) and a second wing (4) extending from the rear of the fuselage, in proximity to the fin (2). The first wing comprises two halfwings (3a, 3b) swept backward, while the two halfwings (4a, 4b) of the second wing (4) are swept forward. The first and second wings lie on two vertically spaced planes and are connected to one another by respective aerodynamic surfaces (5a, 5b) rigid in their plane in correspondence with the resp...


[ I claim:] [1.] A large transport aircraft having a maximum take-off weight greater than 400,000 kg, comprising a fuselage (1) having multiple passenger decks with a fin (2), a first wing (3) extending from an intermediate point on said fuselage (1) and a second wing (4) extending from the rear of said fuselage in proximity to said fin (2), an entire length of each of said first wing and second wing respectively lying on two vertically spaced apart and substantially parallel planes so that each of two end tips of said first wing respectively lie vertica...

이 특허를 인용한 특허 피인용횟수: 40

  1. Guida, Nicholas R.. Active winglet. USP2014048684315.
  2. Guida, Nicholas R.. Active winglet. USP2017099764825.
  3. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.. Aircraft configuration. USP2011098016233.
  4. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.; Lan, Justin. Aircraft configuration. USP2014018628040.
  5. Carr, Robert Jonathan; Higgins, James Michael. Aircraft design. USP200908D598838.
  6. Llamas Sandin, Raul Carlos. Aircraft having a lambda-box wing configuration. USP2012058186617.
  7. Gall, Pierre-Emmanuel; Cros, Christophe. Aircraft having a reduced environmental impact. USP2012118313055.
  8. Carr, Robert Jonathan. Aircraft internal wing and design. USP2005016840478.
  9. Carr,Robert Jonathan; Higgins,James Michael. Aircraft internal wing and design. USP2007087258302.
  10. Manuel Munoz Saiz ES. Aircraft lift arrangement. USP2002096446908.
  11. Cazals, Olivier; Genty de la Sagne, Jaime. Aircraft presenting two pairs of wings and fuel tanks in fluid communication. USP2013058439310.
  12. McGinnis, John William. Aircraft stability and efficient control through induced drag reduction. USP2017019545993.
  13. Peters ; Jr. Spence E.. Aircraft structure to improve directional stability. USP2000086098923.
  14. Cazals, Olivier. Aircraft with jet engines arranged at the rear. USP2012038128023.
  15. Moore, Matthew D.; Boren, Kelly L.; Marques, Edward C.. Airplane configuration. USP2012018087607.
  16. August, Henry. Arch wing and forward steering for an advanced air vehicle. USP2003126659396.
  17. Alford, Jr., Lionel D.; Clayman, Jr., Gary J.. Blended winglet. USP2010017644892.
  18. Chandler, Jesse M.; Suciu, Gabriel L.. Box wing with angled gas turbine engine cores. USP2017029567062.
  19. Suciu, Gabriel L.; Merry, Brian D.. Conjoined reverse core flow engine arrangement. USP2017129845159.
  20. Guida, Nicholas R.. Controllable airflow modification device periodic load control. USP2017029567066.
  21. Hernadi, Andras. Decagonal box-wing aircraft. USP201904D844538.
  22. Hernadi, Andras. Decagonal boxed-wing for aircraft. USP201903D843920.
  23. McGinnis, John William. Efficient control and stall prevention in advanced configuration aircraft. USP2014028657226.
  24. Suokas, Aki. Flying device and a wing construction for the same. USP2016049308984.
  25. Branly,Rolando M.. Folded wing rocket aircraft. USP200809D576098.
  26. Garreau, Oliver F.. Joined-wing tilt-wing aircraft. USP201503D724001.
  27. Carr,Robert Jonathan; Higgins,James Michael. Lift system for an aerial crane and propulsion system for a vehicle. USP2006127147183.
  28. Saiz, Manuel Munoz. Lifting arrangement for aircraft fuselages. USP2005106957792.
  29. Houck, II, Ronald G.. Lifting foil. USP2013038387912.
  30. Houck, II,Ronald G.. Lifting foil. USP200608D526951.
  31. Houck, II,Ronald G.. Lifting foil. USP2006097100867.
  32. Jerry E. Carlow. Mobius-like joining structure for fluid dynamic foils. USP2002116474604.
  33. Guida, Nicholas R.. Multiple controllable airflow modification devices. USP2015109162755.
  34. Guida, Nicholas R.. Multiple controllable airflow modification devices. USP2018059969487.
  35. August, Henry. Survivable and reusable launch vehicle. USP2004066749153.
  36. Morgenstern, John M.. Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom. USP2004056729577.
  37. Dong, Lawrence Y.; Sankrithi, Mithra M. K. V.. Tandem wing aircraft and method for manufacturing and operating such aircraft. USP2004036705567.
  38. Churchman, Charles Gilpin. V/STOL biplane. USP2005126974106.
  39. Wood, Ryan S.; Cummings, Darold B.; Hall, David W.. VTOL aerial vehicle. USP2012078220737.
  40. Ronald G. Meschino CA. Wing combination for drag reduction, aircraft including such a wing, and a method of reducing the drag of an existing aircraft. USP2002016340134.