Converging pin cooled airfoil

Details Converging pin cooled airfoil Converging pin cooled airfoil

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/18 (2006.01) F02C 7/18 (2006.01)

Patent

CA 2477402

A turbine airfoil (12) includes pressure and suction sidewalls (18,20) extending in chord between leading and trailing edges (22,24) and in span between a root (26) and a tip (28). A septum (30) is spaced between the sidewalls to define two cooling circuits (32,34) on opposite sides of the septum which converge between the leading and trailing edges. An array of pins (44,46) extends inwardly from the pressure sidewall (18) at a discharge end of the circuits, and the pins decrease in length to conform with the converging circuit.

Affiliated with

Also associated with

Rating

Converging pin cooled airfoil does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Converging pin cooled airfoil, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Converging pin cooled airfoil will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-2038026