Turbine airfoil for gas turbine engine

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

F01D 5/14 (2006.01) F01D 5/18 (2006.01)

Patent

CA 2398502

A hollow cooled turbine airfoil (18) is provided having pressure and suction side walls (20, 22) and a plurality of trailing edge cooling passages (46) that feed cooling air bleed slots (28) at the trailing edge (26). The trailing edge (26) is selectively thickened in the root (34) portion so as to allow shortened trailing edge slots (28), thereby improving trailing edge (26) cooling and reducing mechanical and thermal stresses.

LandOfFree

Say what you really think

Search LandOfFree.com for Canadian inventors and patents. Rate them and share your experience with other people.

Rating

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

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

Rate now

     

Profile ID: LFCA-PAI-O-1469183

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.