$\require{mediawiki-texvc}$
  • 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

Systems and methods for control of engine exhaust flow

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/50   
미국특허분류(USC) 244/215; 244/213; 244/198
출원번호 UP-0927257 (2007-10-29)
등록번호 US-7823840 (2010-11-22)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Tung & Associates
인용정보 피인용 횟수 : 16  인용 특허 : 9
초록

Coanda Effect and lift produced along a surface of an airfoil are increased by ducting compressed fluid from the engine to the surface of the airfoil. An engine produces exhaust gases that are predominantly directed toward an aft end of the aircraft by a cowling or other structure as an exhaust plume. One or more internal ducts extend from the engine to the surface of the airfoil to thereby transmit a compressed fluid from the engine to the surface in order to suppress flow separation along the surface, thereby causing the engine exhaust flow to remain a...

대표
청구항

What is claimed is: 1. An aircraft comprising: an airfoil having a cowling extending outwardly from a surface of the airfoil, said surface comprising an upper surface of said airfoil; an engine coupled to the airfoil and configured to produce exhaust gases that are predominantly directed over the air foil toward an aft end of the aircraft by the cowling as an exhaust plume; and a duct extending from the engine to an opening in the surface of the airfoil that is configured to transmit a compressed fluid from the engine to the surface of the airfoil witho...

이 특허를 인용한 특허 피인용횟수: 16

  1. Manley, David J.; Kutzmann, Aaron J.; Gregg, III, Robb; Vassberg, John C.; Gonzales, Antonio B.; Hollowell, Steve; Harrison, Neal; Lawson, Edward; Kismarton, Max; Lutke, Kevin. Aircraft configuration utilizing fuselage, wing, empennage, and exhaust flow control devices. USP2011118061655.
  2. Kismarton, Max; Kutzmann, Aaron J.; Lutke, Kevin. Blended wing aircraft. USP2012078226035.
  3. Kismarton, Max; Kutzmann, Aaron J.; Lutke, Kevin. Blended wing aircraft. USP2013018353478.
  4. Kismarton, Max; Kutzmann, Aaron J.; Lutke, Kevin. Blended wing aircraft. USP2012118302908.
  5. Harrison, Neal; Vassberg, John C.. Controllable upper surface blown nozzle. USP2012058167249.
  6. Bernhardt, Roger D.. Flow control structure and associated method for controlling attachment with a control surface. USP2015119193436.
  7. Hamilton, Terry Wayne. Hamilton H.N2 laminar flow diskette wing. USP2013028382040.
  8. Shmilovich, Arvin; Yadlin, Yoram. Method and apparatus for robust lift generation. USP2015089108725.
  9. Shmilovich, Arvin; Yadlin, Yoram. Method and apparatus for robust lift generation. USP2017029573680.
  10. Shmilovich, Arvin; Yadlin, Yoram. Methods and apparatus for robust lift generation. USP2017079714082.
  11. Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
  12. Gregg, III, Robert D.; Kutzmann, Aaron J.; Manley, David J.; Vassberg, John C.; Harrison, Neal; Kismarton, Max. Swept-wing powered-lift aircraft. USP2013108567711.
  13. Gregg, III, Robert D; Kutzmann, Aaron J.; Manley, David J.; Vassberg, John C.; Harrison, Neal; Kismarton, Max. Swept-wing powered-lift aircraft. USP2013038403256.
  14. Kismarton, Max; Kutzmann, Aaron J.; Lutke, Kevin. Twin-boom empennage. USP2012128322655.
  15. Kismarton, Max; Kutzmann, Aaron J.; Lutke, Kevin. Twin-boom empennage. USP2014058720817.
  16. Lawson, Edward; Kutzmann, Aaron J.. Universal convergent nozzle and distinct nozzle aperture. USP2012118317129.