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Aircraft engine mount with single thrust link

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B54D-027/00
출원번호 US-0185922 (2002-06-28)
발명자 / 주소
  • Manteiga, John Alan
  • Wilusz, Christopher James
  • Dykhuizen, Cornelius Harm
출원인 / 주소
  • General Electric Company
대리인 / 주소
    Herkamp, Nathan D.Atwood, Pierce
인용정보 피인용 횟수 : 57  인용 특허 : 8

초록

A mount for mounting an aircraft engine to an aircraft includes a mounting frame having first and second flanges spaced apart a predetermined distance. Each of the first and second flanges has a bolt hole formed therein. A single thrust link is connected at one end to the mounting frame and at anoth

대표청구항

A mount for mounting an aircraft engine to an aircraft includes a mounting frame having first and second flanges spaced apart a predetermined distance. Each of the first and second flanges has a bolt hole formed therein. A single thrust link is connected at one end to the mounting frame and at anoth

이 특허에 인용된 특허 (8)

  1. Dunstan Kent W., Aircraft engine thrust mount.
  2. Hey Kenneth E., Aircraft engine thrust mount.
  3. Ellis Joe E. ; Stuart Alan R., Integrated failsafe engine mount.
  4. Manteiga John Alan ; Dykhuizen Cornelius Harm ; Joseph Thomas Peter ; Wilusz Christopher James ; Troup Robert Eugene ; Boger Ethan ; Franceschelli Anthony John, Link component for aircraft engine mounting systems.
  5. Murphy Patrick (Bellevue WA), Mounting apparatus for fan jet engine having mixed flow nozzle installation.
  6. Rodgers Leonard J.,GB2 ; Newton Arnold C.,GB2 ; Berry James P.,GB2 ; Farrar Peter G. G.,GB2 ; Udall Kenneth F.,GB2, Mounting for coupling a turbofan gas turbine engine to an aircraft structure.
  7. White John L. (Bellevue WA), System for mounting a jet engine.
  8. Dunstan Kent W. ; Hey Kenneth E., Three link failsafe engine mount.

이 특허를 인용한 특허 (57)

  1. Sandy, David F; Zheng, Zhijun, Adjustable engine mount.
  2. Rossi, Frédéric; Alcala, Laurent, Aerofoil portion of an aircraft comprising an attachment support of a connecting device mounted in translation.
  3. Whiteford, Gerald P.; Zameroski, Daniel, Aircraft engine mounting system and method of mounting aircraft engines.
  4. Whiteford, Gerald P.; Zameroski, Daniel, Aircraft engine mounting system and method of mounting aircraft engines.
  5. Whiteford, Gerald P.; Zameroski, Daniel, Aircraft engine mounting system and method of mounting aircraft engines.
  6. Binks, Alan J.; Penda, Allan R., Assembly for mounting a turbine engine to a pylon.
  7. Sandy, David F.; Zheng, Zhijun; Dailey, Stephen P.; Foster, Joseph P., Assembly for mounting a turbine engine to a pylon.
  8. Foster, Lawrence D., Catcher pin assembly.
  9. Gallagher, Edward J.; Monzon, Byron R., Efficient, low pressure ratio propulsor for gas turbine engines.
  10. Pautis, Olivier; Rogero, Jean Michel, Engine assembly for an aircraft comprising a primary structure of a mounting pylon equipped with a box extension comprising two parts in the overall shape of an arch.
  11. West, Randall Ray, Fail-safe aircraft engine mounting apparatus.
  12. Manteiga, John Alan; Wilusz, Christopher James; Dykhuizen, Cornelius Harm, Fail-safe aircraft engine mounting system.
  13. McCune, Michael E.; Husband, Jason, Flexible support structure for a geared architecture gas turbine engine.
  14. Gallagher, Edward J.; Monzon, Byron R.; Liu, Ling; Li, Linda S.; Whitlow, Darryl; Ford, Barry M., Gas turbine engine airfoil.
  15. Gallagher, Edward J.; Monzon, Byron R.; Liu, Ling; Li, Linda S.; Whitlow, Darryl; Ford, Barry M., Gas turbine engine airfoil.
  16. McCune, Michael E.; Portlock, Lawrence E.; Schwarz, Frederick M., Gas turbine engine gear train.
  17. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  18. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  19. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  20. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  21. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  22. Kohlenberg, Gregory A.; Zamora, Sean P., Gas turbine engine with axial movable fan variable area nozzle.
  23. McCune, Michael E.; Portlock, Lawrence E.; Schwarz, Frederick M., Gas turbine engine with geared architecture.
  24. Suciu, Gabriel L.; Schwarz, Frederick M.; Ackermann, William K.; Kupratis, Daniel Bernard, Gas turbine engine with high speed low pressure turbine section.
  25. Schwarz, Frederick M.; Suciu, Gabriel L.; Ackermann, William K.; Kupratis, Daniel Bernard; McCune, Michael E., Gas turbine engine with high speed low pressure turbine section and bearing support features.
  26. Sheridan, William G., Gear system architecture for gas turbine engine.
  27. McCune, Michael E.; Husband, Jason; Schwarz, Frederick M.; Kupratis, Daniel Bernard; Suciu, Gabriel L.; Ackermann, William K., Geared architecture for high speed and small volume fan drive turbine.
  28. Houston, David P.; Kupratis, Daniel Bernard; Schwarz, Frederick M., Geared turbofan gas turbine engine architecture.
  29. Houston, David P.; Kupratis, Daniel Bernard; Schwarz, Frederick M., Geared turbofan gas turbine engine architecture.
  30. Kupratis, Daniel Bernard; Schwarz, Frederick M., Geared turbofan gas turbine engine architecture.
  31. Brefort, François; Huet, Patrick; Pasquer, Félix, Jet engine suspension.
  32. Topol, David A.; Morin, Bruce L., Low noise compressor rotor for geared turbofan engine.
  33. Sheridan, William G.; Hasel, Karl L., Method for setting a gear ratio of a fan drive gear system of a gas turbine engine.
  34. Schwarz, Frederick M.; Sheridan, William G., Monitoring system for non-ferrous metal particles.
  35. Udall, Kenneth F, Mounting arrangement for a gas turbine engine.
  36. Hill, James D.; Suciu, Gabriel L.; Chandler, Jesse M., Mounting systems for gas turbine engines.
  37. Sheridan, William G., Oil loss protection for a fan drive gear system.
  38. Pasquer,F챕lix; Loewenstein,Philippe; Tesniere,Marc, Rear fastening device for aircraft engine.
  39. McCune, Michael E.; Portlock, Lawrence E., Ring gear mounting arrangement with oil scavenge scheme.
  40. McCune, Michael E.; Portlock, Lawrence E., Ring gear mounting arrangement with oil scavenge scheme.
  41. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M., Shared flow thermal management system.
  42. Guillou, Pierrot, Suspension for a turbine engine.
  43. Cabeen, Jack Harvey; Estevez, III, Manuel; Sieveking, Edward William; Struck, Bruno Enriquez, System and method for aligning a gas turbine engine.
  44. Tiemon, Jorg Arrien, Systems and methods for mounting a rotatable machine.
  45. Suciu, Gabriel L.; Merry, Brian D.; Dye, Christopher M., Thermal management system integrated pylon.
  46. Sabnis, Jayant, Thrust efficient turbofan engine.
  47. Sabnis, Jayant, Thrust efficient turbofan engine.
  48. Sabnis, Jayant, Thrust efficient turbofan engine.
  49. Sabnis, Jayant, Thrust efficient turbofan engine.
  50. Sabnis, Jayant, Thrust efficient turbofan engine.
  51. Hurst, Kenneth; Sieveking, Edward; Tse, Kwok-Kwong Ben; Blankenship, Eric, Turbine engine mounting system and method.
  52. Adams, Paul R.; Magge, Shankar S.; Staubach, Joseph Brent; Lord, Wesley K.; Schwarz, Frederick M.; Suciu, Gabriel L., Turbine section of high bypass turbofan.
  53. Upton, Daniel E.; Gruhn, Joel D., Wind turbine rotor blade components and machine for making same.
  54. Gruhn, Joel D.; Franklin, Ethan; Narasimhan, Kameshwaran, Wind turbine rotor blade components and methods of making same.
  55. Gruhn, Joel D.; Franklin, Ethan; Narasimhan, Kameshwaran, Wind turbine rotor blade components and methods of making same.
  56. Gruhn, Joel D.; Franklin, Ethan; Narasimhan, Kameshwaran, Wind turbine rotor blade components and methods of making same.
  57. Gruhn, Joel D.; Franklin, Ethan; Narasimhan, Kameshwaran, Wind turbine rotor blade components and methods of making same.

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