이 특허를 인용한 특허 (44)

1. Hurwitz, Wayne; Ochs, Stuart S., Active flow control for nacelle inlet.

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2. Rolston Stephen C.,GBX ; Ashford Edward M.,GB5, Aerodynamic low drag structure.

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3. Namgoong, Howoong, Aircraft engine nacelle.

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4. Skoog Andrew J. ; Murphy Jane A. ; Stowell William R., Article with a diffuse reflective barrier coating and a low-emissity coating thereon, and its preparation.

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5. Sawyers-Abbott, Nigel David, Combined inlet laminar and thrust reverser cascade efflux flow control system.

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6. Boudebiza, Tewfik; Eichstadt, Frederic; Tesniere, Marc, Engine cowl incorporating an equipment ventilation circuit.

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7. Arcas Noe ; Hutto Frederick M. ; Parente Charles A., Extended reaction acoustic liner for jet engines and the like.

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8. Blevio, Sr., Henry L., Five-piece fuselage, including engines and wings, for a aerodynamically stable, high-lift, vertical takeoff aircraft.

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9. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.

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10. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.

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11. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.

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12. Morford, Stephen A.; Larkin, Michael J., Gas turbine engine having slim-line nacelle.

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13. Winter, Michael; Jain, Ashok K., Gas turbine engine providing simulated boundary layer thickness increase.

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14. Winter, Michael; Jain, Ashok K., Gas turbine engine system providing simulated boundary layer thickness increase.

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15. Rodgers Leonard J,GBX, Ice protection for porous structure.

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16. Binks, Alan; James, Norman John; Layland, Michael John, Inlet section of an aircraft engine nacelle.

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17. Binks, Alan; James, Norman John; Layland, Michael John, Inlet section of an aircraft engine nacelle.

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18. Binks, Alan; James, Norman John; Layland, Michael John, Inlet section of an aircraft engine nacelle.

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19. Blackner Anthony M., Jet engine and method for reducing jet engine noise by reducing nacelle boundary layer thickness.

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20. Meyer,Pascal J, Laminar flow nacelle for an aircraft engine.

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21. Crouch Jeffrey D. ; Ng Lian L., Method and apparatus using localized heating for laminar flow.

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22. Kestler, Steven M.; Sundar, Prithvi; Li, Yuan, Method of controlling boundary layer flow.

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23. Bennett,Joseph M., Mitigating ignition of fluids by hot surfaces.

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24. Brown, Keith T., Modular plenum and duct system for controlling boundary layer airflow.

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25. Ortiz Del Cerro, Álvaro; Gallego Pleite, Joaquín; Rubio García, Luis; Ponce Borrero, Sofía, Monolithic fan cowl of an aircraft engine and a manufacturing method thereof.

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26. Brown, Keith T.; Byrne, Stuart J.; Kestler, Steven M., Multi-zone active laminar flow control system for an aircraft propulsion system.

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27. Jain, Ashok K.; Winter, Michael, Nacelle assembly having inlet airfoil for a gas turbine engine.

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28. Haas, Martin, Nacelle assembly having inlet bleed.

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29. Haas, Martin, Nacelle assembly with turbulators.

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30. Jain, Ashok K., Nacelle flow assembly.

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31. Jain, Ashok K., Nacelle flow assembly.

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32. Jain, Ashok K., Nacelle flow assembly.

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33. Olver, Bryan W.; Vrljes, Ljubisa, Nacelle inlet lip.

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34. Brown, Keith T.; Fowler, Frank J.; Byrne, Stuart J.; Stein, Adam, Nacelle inlet with extended outer barrel.

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35. Atassi, Oliver V., Nacelle with porous surfaces.

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36. Khidekel, Ann E., Optimized nacelle profile and plenum shape for boundary layer ingestion active laminar flow control.

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37. Pfennig Juergen,DEX ; Meister Juergen,DEX, Suction device for boundary layer control in an aircraft.

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38. Malmuth, Norman; Fedorov, Alexander, Surface plasma discharge for controlling leading edge contamination and crossflow instabilities for laminar flow.

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39. Duane C. McCormick ; Daniel L. Gysling, Tangentially directed acoustic jet controlling boundary layer.

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40. Jain, Ashok K.; Winter, Michael, Variable contour nacelle assembly for a gas turbine engine.

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41. Jain, Ashok K.; Winter, Michael, Variable contraction ratio nacelle assembly for a gas turbine engine.

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42. Jain, Ashok K., Variable geometry nacelle assembly for a gas turbine engine.

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43. Jain, Ashok K.; Chaudhry, Zaffir A., Variable shape inlet section for a nacelle assembly of a gas turbine engine.

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44. Miller Robin Mihekun ; Tunkel Roman N., Vibration-driven acoustic jet controlling boundary layer separation.

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