Angled cooling divider wall in blade attachment

Details Angled cooling divider wall in blade attachment Angled cooling divider wall in blade attachment

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/30 (2006.01) F01D 5/18 (2006.01)

Patent

CA 2547172

A rotor blade of a gas turbine engine includes a blade root defining a cooling airflow entry cavity therein, in fluid communication with internal cooling air passages through the blade. The cavity includes opposed side walls and at least one divider wall extending therebetween. At least one end portion of the divider walls adjoins one of the side walls in an angled direction relative to a perpendicular direction of the side walls.

Affiliated with

Also associated with

Rating

Angled cooling divider wall in blade attachment does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Angled cooling divider wall in blade attachment, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Angled cooling divider wall in blade attachment will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1890193