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특허 상세정보

Jet actuators for aerodynamic surfaces

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-027/04   
미국특허분류(USC) 416/090A; 244/130; 244/204; 417/412; 417/427
출원번호 US-0742489 (2000-12-22)
발명자 / 주소
  • Ahmed A. Hassan
  • David B. Domzalski
출원인 / 주소
  • The Boeing Company
대리인 / 주소
    Stout, Uxa, Buyan & Mullins, LLP
인용정보 피인용 횟수 : 47  인용 특허 : 11
초록

A jet actuator positioned within a hollow space in an aerodynamic structure for controlling the flow over an aerodynamic surface thereof includes a movable member linearly displaced by a voice coil mechanism and a flexible diaphragm defining a compression chamber open to the exterior of the aerodynamic surface through an orifice. Reciprocal displacement of the movable member changes the shape of the flexible diaphragm to alternately expel fluid (e.g., air) from and pull fluid into the compression chamber through the orifice. The movable member includes a...

대표
청구항

1. A jet actuator for control of an aerodynamic structure, comprising:an aerodynamic structure having an aerodynamic surface and a hollow space adjacent the surface; an orifice opening through the aerodynamic surface adjacent to the hollow space; a substantially rigid movable member sized to fit within the hollow space, the movable member having a pair of pistons connected by an elongated cross element defining an axis, the movable member being substantially symmetric in terms of its mass about a plane extending perpendicularly through the mid-point of t...

이 특허를 인용한 특허 (47)

  1. Hassan, Ahmed A.; Madsen, Casey L.; Billman, Garrett M, Active flow control for transonic flight.
  2. Shmilovich, Arvin; Yadlin, Yoram; Clark, Roger W., Active systems and methods for controlling an airfoil vortex.
  3. Shmilovich, Arvin; Yadlin, Yoram, Aircraft wing structure and associated method for addressing lift and drag.
  4. Shmilovich, Arvin; Yadlin, Yoram; Clark, Roger; Leopold, Donald, Apparatus and method for the control of trailing wake flows.
  5. Zientek, Thomas A.; Birchette, Terrence S.; Straub, Friedrich K., Apparatus, system, and method for pitching and twisting a blade of a rotorcraft.
  6. Wang, An Bang; Trávní{hacek over (c)}ek, Zden{hacek over (e)}k; Wang, Yi Hua; Hsu, Ming Chang, Double-acting device for generating synthetic jets.
  7. Wang, An-Bang; Travnicek, Zdenek; Wang, Yi-Hua; Hsu, Ming-Chang, Double-acting device for generating synthetic jets.
  8. Smith, Brian R.; Saddoughi, Seyed, Dual bimorph synthetic pulsator.
  9. Hassan, Ahmed A.; Osborne, Bradley A.; Schwimley, Scott; Billman, Garry; Billman, legal representative, Mary, Dynamic bumps for drag reduction at transonic-supersonic speeds.
  10. Reichenbach, Robert T.; Booth, John Stanley, Electronics package for synthetic jet ejectors.
  11. Hartman,Peter A.; Meadowcroft,Edward T., Engine inlet air particle separator with active flow control.
  12. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.
  13. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.
  14. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.
  15. Winter, Michael; Jain, Ashok K., Gas turbine engine system providing simulated boundary layer thickness increase.
  16. Shmilovich, Arvin; Yadlin, Yoram; Clark, Roger W., Lift augmentation system and associated method.
  17. Hassan,Ahmed A.; Billman,Garry, Method and apparatus for controlling a vehicle.
  18. Hassan, Ahmed A.; JanakiRam, Ram D., Method and device for altering the separation characteristics of air-flow over an aerodynamic surface via intermittent suction.
  19. Hassan, Ahmed A.; JanakiRam, Ram D.; Cerchie, Dino A., Method and device for altering the separation characteristics of flow over an aerodynamic surface via hybrid intermittent blowing and suction.
  20. Hassan, Ahmed A.; Domzalski, David B.; JanakiRam, Ram D., Method and device for low-noise underwater propulsion.
  21. Hassan, Ahmed A.; Domzalski, David B., Method and device for low-noise underwater propulsion and for reducing hull drag.
  22. Clingman, Dan John; Whalen, Edward Andrew, Multi-stage flow control actuation.
  23. Jain, Ashok K.; Winter, Michael, Nacelle assembly having inlet airfoil for a gas turbine engine.
  24. Haas, Martin, Nacelle assembly having inlet bleed.
  25. Haas, Martin, Nacelle assembly with turbulators.
  26. Jain, Ashok K., Nacelle flow assembly.
  27. Jain, Ashok K., Nacelle flow assembly.
  28. Jain, Ashok K., Nacelle flow assembly.
  29. Filter, Evan J., Rotorcraft rotor including primary pitch horns and secondary horns.
  30. Baruzzini, Dan J.; Miller, Daniel N.; Domel, Neal D.; Hakes, Jeff G., Suprression of shock-induced airflow separation.
  31. Griffin, Steven F., Synthetic jet muffler.
  32. Griffin, Steven F.; Shurilla, Christopher R., Synthetic vacuum generator.
  33. Shmilovich, Arvin; Yadlin, Yoram; Clark, Roger W.; Manley, David J., System for aerodynamic flows and associated method.
  34. Shmilovich, Arvin; Yadlin, Yoram; Clark, Roger W.; Leopold, Donald H., Systems and methods for destabilizing an airfoil vortex.
  35. Lewis, Michael S.; Meserole, Jere S.; Dunn, Michael J.; Tillotson, Brian J., Systems and methods for tracing aircraft vortices.
  36. Lewis, Michael S.; Meserole, Jere S.; Dunn, Michael J.; Tillotson, Brian J., Systems and methods for tracing aircraft vortices.
  37. Lewis, Michael S.; Meserole, Jere S.; Dunn, Michael J.; Tillotson, Brian J., Systems and methods for tracing aircraft vortices.
  38. Arik, Mehmet; Wolfe, Charles Franklin; Utturkar, Yogen Vishwas; Seeley, Charles Erklin; Slaton, David Shannon; Lueckenbach, William Henry, Thermal management system for embedded environment and method for making same.
  39. Durham, Zachary B.; Megarity, William M.; Nickerson, Matthew L.; Totten, Brian C., Transversely actuated piezoelectric bellows heatsink.
  40. Birchette, Terrence S., Ultra-low friction air pump for creating oscillatory or pulsed jets.
  41. Birchette, Terrence S., Ultra-low friction air pump for creating oscillatory or pulsed jets.
  42. Jain, Ashok K.; Chaudhry, Zaffir A., Variable shape inlet section for a nacelle assembly of a gas turbine engine.
  43. Boldrin, Clete M.; Hassan, Ahmed A., Vernier active flow control effector.
  44. Boldrin,Clete M.; Hassan,Ahmed A., Vernier active flow control effector.
  45. McVeigh, Michael A.; Maciolek, Robert F., Vortex generators on rotor blades to delay an onset of large oscillatory pitching moments and increase maximum lift.
  46. Tadayon, Saied; Tadayon, Bijan; Martin, David, Wind turbine blade system with air passageway.
  47. Ferguson, Stanley D.; Fialho, Ian J.; Potter, Richard C., Wing aerial refueling system.