Turbine blade, manufacturing method of turbine blade, and...

Details Turbine blade, manufacturing method of turbine blade, and... Turbine blade, manufacturing method of turbine blade, and...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/18 (2006.01) C23C 4/00 (2006.01) C23C 4/02 (2006.01) C23C 28/00 (2006.01) F01D 5/28 (2006.01)

Patent

CA 2385932

There is disclosed a turbine blade comprising a turbine blade main body 10 with a blade-shaped section and a thermal barrier coat 20 as an insulating layer. The turbine blade main body 10 includes an internal air gap 12 disposed inside so that a coolant gas passes and a plurality of coolant gas ports 13 connected to the internal air gap and disposed in the outer peripheral surface. The thermal barrier coat 20 is coated with the outer peripheral surface of the turbine blade main body. The thermal barrier coat fills in at least some of the coolant gas ports. Thereby, a temperature of a high-temperature gas is raised and the turbine blade can be run.

Affiliated with

Also associated with

Rating

Turbine blade, manufacturing method of turbine blade, and... 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 blade, manufacturing method of turbine blade, and..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine blade, manufacturing method of turbine blade, and... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-2046074