이 특허를 인용한 특허 (49)

1. Thies, Robert; Buchholz, Carsten; Staudte, Andreas, Accessory mounting for a gas turbine.

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2. Luo, Huageng; Young, Craig Douglas, Active cancellation and vibration isolation with feedback and feedforward control for an aircraft engine mount.

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3. Rossetti Dino J. ; Ivers Douglas E. ; Norris Mark A. ; Heath Michael C. ; Southward Steve C., Active structural control system and method including active vibration absorbers (AVAS).

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4. Jamshidiat, Hamid; Elias, Laila M.; Kosanchick, III, Melvin, Active vibration control system.

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5. Cazenave, Olivier; Lalanne, Clement; Dionne, Luc, Adjustable engine suspension for positioning the engine relative to the mount thereof.

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6. Sanz Martinez, Pablo Timoteo; Folch Cortes, Diego, Aircraft engine supporting pylon.

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7. Hindle, Timothy; Barber, Tim Daniel; Buchele, Paul, Annular bearing support dampers, gas turbine engines including the same, and methods for the manufacture thereof.

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8. Llamas Sandín, Raúl Carlos, Arrangement for mounting an engine on the airframe of an aircraft.

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9. Mulcaire, Thomas G, Assembly comprising a gas turbine engine and a supporting pylon.

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10. Ewens, David; Blanc, Jonathan, Assembly for an aircraft, comprising an engine attachment body equipped with at least one shackle support fitting that passes into the box section of the attachment pylon.

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11. Ewens, David; Blanc, Jonathan, Assembly for an aircraft, comprising an engine attachment body partially produced in one piece with an internal stiffening rib of an attachment pylon box section.

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12. Jamshidiat, Hamid; Jones, Michael D.; Elias, Laila M., Bracket for mounting/removal of actuators for active vibration control.

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13. Rock, Eugene F., Coaxial helicopter.

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14. Seeley Charles E. ; Ramakrishnan Ramanath I. ; Wang Weiping ; Claeys James ; McCallum Al, Computerized method for positioning support jacks underneath industrial gas turbines.

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15. Lafont, Laurent; Magnin, Herve; Rogero, Jean-Michel, Device for measuring a pattern of forces and moments generated by an aircraft propulsion system.

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16. Marche, Herve, Device for mounting an aircraft turboprop engine comprising hydraulic attachments.

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17. Boock, Klaus, Device for reducing hydraulic-fluid oscillation in a hydraulic system.

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18. Antypas, Jerome, Engine attachment pylon.

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19. Combes, Stephane; Lafont, Laurent, Engine mounting structure interposed between an aircraft wing system and said engine.

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20. Schwab, Robert B.; Klingman, Jan Donald; Pham, Giang, Engine vibration and engine trim balance test system, apparatus and method.

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21. Guillemaut, Julien; Gallant, Guillaume, Fish joint device having an improved mechanical hold.

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22. Hindle, Timothy; Hadden, Steven; Davis, Torey, Gas turbine engines including broadband damping systems and methods for producing the same.

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23. Elwood G. Norris, Helicopter propulsion and control system.

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24. Smedresman, Adam G.; Von Berg, Kaleb, Integral centering spring and bearing support and method of supporting multiple damped bearings.

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25. Brochard, Wolfgang; Terral, Romain, Lateral propulsion unit for aircraft comprising a turbine engine support arch.

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26. West, Colin John; Sutton, David Alistair, Method and apparatus for controlling an elastomeric damper.

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27. Udall, Kenneth F, Mounting arrangement for a gas turbine engine.

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28. Beardsley, Peter K, Mounting system for use in mounting a gas turbine engine.

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29. Marche,Herv챕, Mounting system inserted between an aircraft engine and a rigid structure of an attachment strut fixed under a wing of this aircraft.

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30. Jensen Sam C., Paddle fitting tool.

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31. Brochard, Wolfgang; Alby, Sébastien; Ewens, David, Primary structure for an attachment pylon with firewall and thermal layers.

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32. Coraboeuf, Yohann; Dutheil, Jean-Philippe, Propulsion unit for reusable launch vehicle.

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33. Lafont, Laurent; Journade, Frederic, Rear part of an aircraft comprising a structure for supporting engines, connected to the fuselage by at least one blocking element under compression loading.

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34. Lafont, Laurent, Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rod.

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35. Lafont, Laurent; Journade, Frederic; Jalbert, Delphine; Bardou, Etienne, Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rod.

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36. Lafont, Laurent; Saucray, Jean-Michel; Quiroz-Hernandez, Esteban; Antypas, Jerome; Bonnet, Mathieu; Journade, Frederic, Rear part of an aircraft including an engine support structure assembled so as to oscillate on the fuselage.

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37. Marche, Jacques Hervé, Rigid aircraft pylon fitted with a rib extension for taking up the moment in the lengthways direction.

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38. Marche, Jacques Hervé, Rigid aircraft pylon structure in contact with a fuselage lateral extension for attachment.

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39. Machado,Stephane; Cassagne,Jerome; Del Blanco,Anthony; Martin,Yvon; Chambreuil,Arnaud, Structure for mounting a turboprop under an aircraft wing.

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40. Meacham, Walter Lee; Bridges, Eric; Margolis, Alan, Three parameter damper anisotropic vibration isolation mounting assembly.

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41. Schnelz James R. ; Powell Donald T., Tuned engine mounting system for jet aircraft.

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42. Phelps, III,Arthur E.; Barnes,Dwaine R.; Norris,Elwood G.; Rock,Eugene F.; Wallace,Emitt, Ultralight coaxial rotor aircraft.

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43. Maine,Scott T., Vibration engine monitoring neural network object monitoring.

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44. Bachmeyer, Paul J.; Blewett, Michael R.; Ohme, Marvin D., Vibration isolation device with load dependent stiffness.

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45. von Flotow, Andreas H.; Horton, Tyler Patrick, Vibration isolation devices and associated systems and methods.

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46. von Flotow, Andreas Hubertus; Horton, Tyler Patrick, Vibration isolation devices and associated systems and methods.

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47. Whiteford Gerald P. (Waterford PA) Herbst Paul T. (Erie PA), Vibration isolation system including a passive tuned vibration absorber.

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48. Paul T. Herbst, Vibration isolator.

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49. Yamada Naohisa,JPX, Vibration-proof system for a model-craft engine.

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