Power plants – Reaction motor – Interrelated reaction motors
Reexamination Certificate
2011-06-28
2011-06-28
Kim, Ted (Department: 3741)
Power plants
Reaction motor
Interrelated reaction motors
C060S268000, C060S039162
Reexamination Certificate
active
07966806
ABSTRACT:
A turbofan engine assembly includes a core gas turbine engine including a high-pressure compressor, a combustor, and a high-pressure turbine, a low-pressure turbine coupled to said core gas turbine engine, a counter-rotating booster compressor comprising a first rotor section configured to rotate in a first direction and a second rotor section configured to rotate in an opposite second direction, and a gearbox comprising an input and an output, said gearbox output coupled to at least one of said first and second rotor sections, said gearbox input coupled to said low-pressure turbine. A method of assembling the turbofan engine assembly described herein is also provided.
REFERENCES:
patent: 3673802 (1972-07-01), Krebs et al.
patent: 3729957 (1973-05-01), Petrie et al.
patent: 4751816 (1988-06-01), Perry
patent: 4790133 (1988-12-01), Stuart
patent: 4827712 (1989-05-01), Coplin
patent: 6158210 (2000-12-01), Orlando
patent: 6339927 (2002-01-01), DiPietro, Jr.
patent: 6684626 (2004-02-01), Orlando et al.
patent: 6739120 (2004-05-01), Moniz et al.
patent: 6763652 (2004-07-01), Baughman et al.
patent: 6763653 (2004-07-01), Orlando et al.
patent: 6763654 (2004-07-01), Orlando et al.
patent: 7186073 (2007-03-01), Orlando et al.
patent: 7334392 (2008-02-01), Moniz et al.
patent: 0558769 (1992-02-01), None
Henry John Leslie
Moniz Thomas Ory
Orlando Robert Joseph
Andes Esq. William Scott
Armstrong Teasdale LLP
General Electric Company
Kim Ted
LandOfFree
Turbofan engine assembly and method of assembling same does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Turbofan engine assembly and method of assembling same, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbofan engine assembly and method of assembling same will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-2740475