이 특허를 인용한 특허 (41)

1. Kari Appa, Active control surface modal system for aircraft buffet and gust load alleviation and flutter suppression.

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2. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.

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3. Harrigan,Jeffery S.; Beaufrere,Henry L., Aerospace vehicle yaw generating systems and associated methods.

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4. Najmabadi, Kioumars; Tran, Chuong B.; Ho, John Koon-Hung, Aircraft multi-axis modal suppression system.

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5. Najmabadi,Kioumars; Tran,Chuong B.; Ho,John Koon Hung, Aircraft multi-axis modal suppression system.

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6. Kubica, Fran.cedilla.ois, Aircraft with electric flight controls provided with a fuselage able to deform and vibrate.

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7. Charles Bruce D. ; Hassan Ahmed A. ; Tadghighi Hormoz ; JanakiRam Ram D. ; Sankar Lakshmi N., Blade vortex interaction noise reduction techniques for a rotorcraft.

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8. Volk, John A., Control system for alleviating a gust load on an aircraft wing.

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9. Charron, Richard, Control system for ornithopter.

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10. Sobotta, Gerald; Bosch, Dieter, Device for measuring pressure, sound and vibration and method of analyzing flow on surfaces of structural parts.

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11. Becker, Juergen, Flight control device for improving the longitudinal stability of an automatically controlled airplane and method of operating same.

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12. Prince, Troy S; Kolacinski, Richard; Patel, Mehul, Hierarchical closed-loop flow control system for aircraft, missiles and munitions.

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13. Prince, Troy S; Kolacinski, Richard; Patel, Mehul, Hierarchical closed-loop flow control system for aircraft, missiles and munitions.

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14. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.

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15. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A., Isentropic compression inlet for supersonic aircraft.

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16. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.

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17. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.

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18. Conners, Timothy R., Low shock strength inlet.

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19. Conners, Timothy R., Low shock strength inlet.

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20. Conners, Timothy R., Low shock strength propulsion system.

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21. Conners, Timothy R., Low shock strength propulsion system.

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22. Grinits, Erick Vile; de Oliveira Alves Junior, Marco Antonio; Gangsaas, Dagfinn; Negrao, Roberto Garcia; Trotta, Bianca Prazim; Silva, Fabiano Prieto; de Almeida Filho, Mauricio Martins; Coccolin, Marco Antonio; Garcia, Karina Sanches; de Campos, Daniel Carmona; Saracho, Cristina Minioli; de Oliveira Moreira, Fernando Jose, Low-frequency flight control system oscillatory faults prevention via horizontal and vertical tail load monitors.

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23. Berthereau, Mathieu; Mazet, Michel, Method and device for an aircraft buffet reduction.

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24. Jenaro Rabadan, Guillermo; Havas, Juliane; Soumillon, Stéphane; Despre-Flachard, Carole, Method and device for determining critical buffeting loads on a structure of an aircraft.

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25. Kubica, François; Le Garrec, Christophe, Method and device for reducing the vibratory motions of the fuselage of an aircraft.

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26. Kubica, Francois, Method for controlling the flight of an aircraft.

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27. Ross, Anthony, Methods and apparatus for aircraft turbulence detection.

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28. Hassan Ahmed A. ; Straub Friedrich K. ; Domzalski David B., Oscillating air jets for helicopter rotor aerodynamic control and BVI noise reduction.

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29. Hassan, Ahmed A.; Straub, Friedrich K.; Domzalski, David B., Oscillating air jets for implementing blade variable twist, enhancing engine and blade efficiency, and reducing drag, vibration, download and ir signature.

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30. Hassan Ahmed A. ; Tadghighi Hormoz ; Janakiram Ram D., Oscillating air jets for reducing HSI noise.

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31. Domzalski David B. ; Hassan Ahmed A. ; Kennedy Dennis K., Oscillating air jets on aerodynamic surfaces.

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32. Kubica,Fran챌ois; Briere,Dominique, Process for countering the vibrations induced in an aircraft by the windmilling of a fan and system of electric flight controls implementing this process.

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33. Gratzer, Louis B., Split blended winglet.

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34. Gratzer, Louis B., Split blended winglet.

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35. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Supersonic aircraft jet engine installation.

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36. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L., Supersonic aircraft with spike for controlling and reducing sonic boom.

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37. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L., Supersonic aircraft with spike for controlling and reducing sonic boom.

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38. Juergen Becker DE, System and method for compensating structural vibrations of an aircraft caused by outside disturbances.

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39. Miller,Daniel N.; Truax,Philip P.; Yagle,Patrick J., System and method to control flowfield vortices with micro-jet arrays.

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40. Bruce D. Charles ; Ahmed A. Hassan ; Hormoz Tadghighi ; Ram D. JanakiRam, Tapered/segmented flaps for rotor blade-vortex interaction (BVI) noise and vibration reduction.

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41. Ngo Hieu Thien, Tip vortex reduction system.

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