Damped gas turbine engine airfoil row

Details Damped gas turbine engine airfoil row Damped gas turbine engine airfoil row

F - Mech Eng,Light,Heat,Weapons

01

D

26/150, 170/72,

F01D 5/10 (2006.01) B23P 15/00 (2006.01) B23P 15/02 (2006.01) F01D 5/22 (2006.01) F01D 9/04 (2006.01)

Patent

CA 1312828

13DV 9529 DAMPED GAS TURBINE ENGINE AIRFOIL ROW ABSTRACT OF THE DISCLOSURE Disclosed is a vibration damped gas turbine engine airfoil row. The airfoil row, comprising first and second coaxial, circular spools and airfoils extending radially therebetween, is cast in at least one piece and then the second or inner spool is cut between adjacent airfoils. Damping inserts are held in place adjacent the inner surface of the second spool by a retaining means.

611425

Affiliated with

Also associated with

Rating

Damped gas turbine engine airfoil row does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Damped gas turbine engine airfoil row, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Damped gas turbine engine airfoil row will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1310775