Gas turbine engine rotor and balance weight therefor

Details Gas turbine engine rotor and balance weight therefor Gas turbine engine rotor and balance weight therefor

F - Mech Eng,Light,Heat,Weapons

16

F

F16F 15/34 (2006.01) F01D 5/10 (2006.01) F16F 15/28 (2006.01)

Patent

CA 2680645

A balance weight (62, 162) for a rotor includes: (a) an arcuate body including a front wall and a rear wall interconnected by an end wall (68, 168), the front, rear, and end walls collectively defining a generally U-shaped cross-sectional shape; and (b) a projection (70, 170) extending outwardly from the rear wall, the projection (70, 170) being adapted to engage an aperture (54) extending through a flange (46) of the rotor.

Affiliated with

Also associated with

Rating

Gas turbine engine rotor and balance weight therefor does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas turbine engine rotor and balance weight therefor, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine engine rotor and balance weight therefor will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1914605