$\require{mediawiki-texvc}$

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

Fluidic propulsive system and thrust and lift generator for aerial vehicles

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-021/04
  • B64D-029/02
  • B64C-039/02
  • B64D-027/18
  • B64D-033/02
  • B64D-033/04
  • B64C-009/38
  • B64C-015/00
  • B64C-021/00
  • B64D-027/10
출원번호 US-0256178 (2016-09-02)
등록번호 US-10207812 (2019-02-19)
발명자 / 주소
  • Evulet, Andrei
출원인 / 주소
  • JETOPTERA, INC.
대리인 / 주소
    Born, P. G. Scott
인용정보 피인용 횟수 : 0  인용 특허 : 85

초록

A vehicle includes a main body and a gas generator producing a gas stream. At least one fore conduit and tail conduit are fluidly coupled to the generator. First and second fore ejectors are fluidly coupled to the at least one fore conduit. At least one tail ejector is fluidly coupled to the at leas

대표청구항

1. A vehicle, comprising: a main body having a fore portion, a tail portion, a starboard side and a port side;a gas generator coupled to the main body and producing a gas stream;at least one fore conduit fluidly coupled to the generator;at least one tail conduit fluidly coupled to the generator;firs

이 특허에 인용된 특허 (85)

  1. Eigenbrode Daniel E. ; Field Robert E., Aerodynamically controlled ejector.
  2. Todorovic, Predrag, Air ejector nozzle tube for an oil heat exchanger of an aircraft engine.
  3. Garreau, Oliver, Aircraft.
  4. Morgan, Brian Herman; Hagen, David LeRoy, Aircraft attitude control configuration.
  5. Parham, Dean Leon, Aircraft engine nozzle.
  6. Sokhey Jack (Jagdish) Singh ; Crook Andrew James ; Snyder Philip Harold ; Vittal Baily R., Aircraft thrust vectoring system.
  7. Deńning, Ralph Murch; Woodward, Clifford Stanley, Aircraft with improved lift.
  8. Arnason Kristjan,ISX, Aircraft with jet flap propulsion.
  9. Capuani Alfredo (Torino ITX), Aircraft with jet propulsion.
  10. Szuminski Gary F. (Cincinnati OH) Ward Benjamin D. (Marietta GA), Aircraft with stowable vectorable nozzle and ejector thrust augmentation.
  11. Schmetzer William M. (15740 Sherman Way Van Nuys CA 91406), Aircraft with thrust and lift augmenting airfoil.
  12. Cummings, Darold B.; Kutzmann, Aaron J.; Droney, Christopher K., Aircraft with thrust vectoring for switchably providing upper surface blowing.
  13. Hapke Donald William (Issaquah WA), Articulated nozzle for upper surface blown aircraft.
  14. Viets Hermann (Dayton OH), Automatic boundary layer control in an ejector wing aircraft.
  15. Wilkinson, Todd; Pederson, Darrell, Automatic takeoff thrust management system.
  16. Alperin Morton (Woodland Hills CA) Wu Jiunn-Jenq (Sierra Madre CA), Axially-symmetric, jet-diffuser ejector.
  17. Reznick Steven G. (Dayton OH) Franke Milton E. (Dayton OH), Axisymmetric thrust augmenting ejector with discrete primary air slot nozzles.
  18. Swanson ; Everts W. ; Wehrman ; Marvin D., Boundary layer control system for aircraft.
  19. Poe, Roger L.; Wilkins, James; Claxton, Michael G., Coanda gas burner apparatus and methods.
  20. Poe, Roger L.; Wilkins, James; Claxton, Michael G., Coanda gas burner apparatus and methods.
  21. Kelber Charles C. (2081 Snowden Ave. Long Beach CA 90815), Combination lift thrust device.
  22. Lair, Jean-Pierre, Confluent variable exhaust nozzle.
  23. Murphy,Michael J.; Cowan,Curtis C.; Paul,Stephen A.; Allore,James P.; Harris,Meggan, Convergent/divergent nozzle with modulated cooling.
  24. Viets Hermann (144 Scenery Dr. Morgantown WV 26505), Directional control of engine exhaust thrust vector in a STOL-type aircraft.
  25. Thayer Edward B. (Jupiter FL), Divergent flap actuation system for a two-dimensional exhaust nozzle.
  26. Rogers,Ernest O.; Imber,Robin D.; Abramson,Jane S.; Donnelly,Martin J., Dual jet emerging lift augmentation system for airfoils and hydrofoils.
  27. Bulman Melvin J. (Folsom CA), Ejector ramjet.
  28. Lackey Jesse R. ; Catt Jeffrey A., Exhaust induced ejector nozzle system and method.
  29. Bratkovich Thomas E. ; Williams Kevin E. ; Bussing Thomas R. A. ; Lidstone Gary L. ; Hinkey John B., Exhaust nozzle for multi-tube detonative engines.
  30. Hammond Mark H. ; Presz ; Jr. Walter M., Exhaust nozzle for suppressing infrared radiation.
  31. Garreau, Oliver, Five-wing aircraft to permit smooth transitions between vertical and horizontal flight.
  32. Smith, Jesse Walter, Fixed nozzle thrust augmentation system.
  33. Sweeney Roy O. (Cincinnati OH), Fluid amplifier with improved operating range using tapered shim.
  34. Cossairt Keith R. (150 Oak Ridge Pl. ; Apartment 7B Greenville SC 29615), Fluid dynamic pump.
  35. John Michael Koshoffer, Fluidic nozzle control system.
  36. Mueller John H., Fluidic throat exhaust nozzle.
  37. Khalid, Syed Jalaluddin, Gas turbine engine with ejector.
  38. Betts Edward E. (Escondido CA), High lift aircraft.
  39. Koenig David G. (Sunnyvale CA) Aoyagi Kiyoshi (Mountain View CA) Dudley Michael R. (Los Altos CA) Schmidt Susan B. (Pensacola FL), High performance forward swept wing aircraft.
  40. Horike Masanori (Tokyo JPX) Ebi Yutaka (Tokyo JPX), Ink jet printing apparatus.
  41. Alperin Morton (6000 Lockhurst Dr. Woodland Hills CA 91364), Jet diffuser ejector.
  42. Seiner John M. ; Gilinsky Mikhail M., Jet nozzle having centerbody for enhanced exit area mixing.
  43. Capuani Alfredo (Turin ITX), Jet-propelled aircraft.
  44. Garreau, Oliver F., Joined-wing tilt-wing aircraft.
  45. Sakamoto Yujiro (Akashi JPX) Kurosaka Toshio (Takarazuka JPX) Fukumoto Hirohiko (Kobe JPX) Miyake Toshiya (Kakogawa JPX) Tokunaga Hirohiko (Kakogawa JPX), Lift generating apparatus, in aircraft employing the lift generating apparatus, and a lift generating method.
  46. Presz, Jr., Walter M.; Werle, Michael J., Lobed convergent/divergent supersonic nozzle ejector system.
  47. Wygnanski Israel (Herzlia ILX) Fiedler Heinrich (Berlin DEX), Method and apparatus for controlling the mixing of two fluids.
  48. Shmilovich, Arvin; Yadlin, Yoram; Gregg, III, Robert D.; Clark, Roger W., Method and apparatus for enhancing engine-powered lift in an aircraft.
  49. Shumate,James, Method and apparatus for thrust augmentation for rocket nozzles.
  50. Cerretelli,Ciro; Kirtley,Kevin Richard, Method and system for flow control with fluidic oscillators.
  51. Novikov-Kopp, Ivan, Method for comprehensively increasing aerodynamic and transport characteristics, a wing-in-ground-effect craft for carrying out said method (variants) and a method for realizing flight.
  52. Hirt William J. (Bellevue WA) Grotz Charles A. (Seattle WA), Method of and apparatus for enhancing Coanda flow attachment over a wing and flap surface.
  53. Horii Kiyoshi (5-8-15-501 Kamimeguro ; Meguro-ku ; Tokyo JPX), Method of generating spiral fluid flow and the device therefor.
  54. Shmilovich, Arvin; Yadlin, Yoram, Methods and apparatus for robust lift generation.
  55. Johnson ; Jr. Virgil E. (Gaithersburg MD) Etter Robert J. (Ellicott City MD) Lain Horton W. (Severna Park MD) Stephens Larry K. (Glenelg MD) Van Dyke Peter (Baltimore MD), Movable ramp inlet for water jet propelled ships.
  56. Gilbertson Frederick L. (Toronto CAX) Garland Douglas B. (Toronto CAX) Whittley Donald C. (Toronto CAX), Nozzle structure with notches.
  57. Bevilaqua Paul M. (Dublin OH) Dehart John H. (Powell OH), Nozzle system.
  58. Baker, Von David; Vittal, Baily Ramachandra, Nozzle with an adjustable throat.
  59. Urruela Jose R. (Las Arenas ESX), Orientable axisymmetric nozzle of variable geometry of gas turbine propulsors.
  60. Shmilovich, Arvin; Yadlin, Yoram; Clark, Roger W.; Gregg, III, Robert D., Propulsion system and method for efficient lift generation.
  61. Nozaki Yoshio (No. 89 ; Saiwai-cho Inazawa-shi ; Aichi-ken JPX), STOL aircraft.
  62. Garland Douglas (Rexdale CAX), Segmented rotatable nozzles.
  63. Ladharam, Mahendra, Slotted injection nozzle and low NOx burner assembly.
  64. Markowski Stanley J. (East Hartford CT) Reilly Richard S. (Lake Park FL), Swirler assembly for a vorbix augmentor.
  65. Kampe, Robert F., Thrust augmentation technique and apparatus.
  66. Stewart Derwent G. (Upper Beaconsfield AUX) Fisher Samuel A. (Ashburton AUX), Thrust augmentor.
  67. Nichols ; Jr. James H. (Hyattsville MD) Furey Roger J. (Vienna VA) Englar Robert J. (Derwood MD) Lee David G. (Reston VA), Thrust deflector and force augmentor.
  68. Barcza W. Kevin (Stuart FL) Anders Larry E. (West Palm Beach FL), Thrust vectoring ejector nozzle.
  69. David Levi Sutterfield ; Von David Baker ; Jagdish Singh Sokhey, Thrust vectoring mechanism.
  70. Ulanoski Michael S. ; Sokhey Jagdish S., Thrust vectoring system.
  71. Kawai, Ronald Tatsuji, Thrust vectoring system and method.
  72. Ulanoski Michael S. ; Sokhey Jagdish S. ; Vittal Baily R. ; Baker Von D., Thrust vectoring techniques.
  73. Sutton Richard C. (Bellevue WA), Tilt wing short takeoff aircraft and method.
  74. Billig Frederick S. (Rockville MD) VanWie David M. (Brookeville MD), Translating cowl inlet with retractable propellant injection struts.
  75. Gerhardt Heinz A. (Redondo Beach CA), Transverse thrust lift augmentation system.
  76. Dacre, Mike, Turbofan engine for stol aircraft.
  77. Seiner John M. ; Gilinsky Mikhail M., Undulated nozzle for enhanced exit area mixing.
  78. Kress Robert W. (4308 Ulster Landing Rd. Saugerties NY 12477) Stump Joseph W. (42 Derby Pl. Smithtown NY 11787), Unmanned aerial aircraft having a single engine with dual jet exhausts.
  79. Oliver, Garreau, VTOL aircraft.
  80. Garreau, Oliver, VTOL/STOL tilt-prop flying wing.
  81. Szuminski Gary F. (Marietta GA) Nightingale Douglas J. (Jonesboro GA), Vectorable nozzles for aircraft.
  82. Boulton Donald G. (Henry County TN) Arcangeli Gerald T. (St. Louis County MO), Vented cowl variable geometry inlet for aircraft.
  83. Willis Mark T. (San Diego CA), Venturi enhanced airfoil.
  84. Belloso Gregorio M. (Rte. 1 ; Box 9323 ; Cullen Pkwy. Crisfield MD 21817), Vertical take-off and landing aircraft.
  85. Lendriet William C. (8814 Sylmar Ave. Panorama City CA 91402), Vertical/short takeoff or landing aircraft having a rotatable wing and tandem supporting surfaces.
섹션별 컨텐츠 바로가기

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

AI-Helper 아이콘
AI-Helper
안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

선택된 텍스트