Method and apparatus for balancing gas turbine engines

Details Method and apparatus for balancing gas turbine engines Method and apparatus for balancing gas turbine engines

F - Mech Eng,Light,Heat,Weapons

16

F

F16F 15/34 (2006.01) F01D 25/04 (2006.01)

Patent

CA 2519687

A system for balancing a rotating assembly (50) including a gas turbine engine (10) is provided that includes a plurality of couplers (100) configured to couple the engine to a rotating load (12) such that torque from the engine is transmitted to the rotating load through the plurality of couplers. Each coupler includes a head portion (106), an elongated shank portion (110) extending from the head portion along a longitudinal axis (112) of the coupler, and a threaded stud (120) extending from the head portion along the longitudinal axis and opposite the shank portion. A balance weight (122) is configured to be coupled to each of the plurality of couplers.

Affiliated with

Also associated with

Rating

Method and apparatus for balancing gas turbine engines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method and apparatus for balancing gas turbine engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method and apparatus for balancing gas turbine engines will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1430945