Method of producing and assembling a cooling device inside...

Details Method of producing and assembling a cooling device inside... Method of producing and assembling a cooling device inside...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/18 (2006.01) F01D 5/14 (2006.01) F01D 17/16 (2006.01)

Patent

CA 2435070

A method of producing and assembling a cooling device inside an axial-flow gas turbine blade; the airfoil profile of the blade has an inner surface defining a chamber, and is connected to a supporting structure by two opposite end pins having respective openings for the passage of cooling air and which come out inside the chamber; the method provides for forming an insert having a number of holes and defined by a first and at least a second body separate from each other, and each of a size approximating but no larger than that of at least one of the openings; the bodies are inserted successively through the openings in the pins, and, are positioned inside the chamber to direct a relative stream of air through each hole on to the inner surface of the airfoil profile.

Affiliated with

Also associated with

Rating

Method of producing and assembling a cooling device inside... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method of producing and assembling a cooling device inside..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method of producing and assembling a cooling device inside... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1914458