Shroud and vane segment edge notches for compensation for...

Details Shroud and vane segment edge notches for compensation for... Shroud and vane segment edge notches for compensation for...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/28 (2006.01) F01D 25/24 (2006.01) F02C 7/20 (2006.01)

Patent

CA 2509791

Random air flow leakage between a shroud assembly and a stator vane assembly into the gas path of a gas turbine engine due to manufacturing tolerance stack-up is reduced by providing notches to inhibit interference caused by misalignment and/or mismatch of adjacent segments.

Affiliated with

Also associated with

Rating

Shroud and vane segment edge notches for compensation for... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Shroud and vane segment edge notches for compensation for..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Shroud and vane segment edge notches for compensation for... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-2066973