Gas turbine moving blade

Details Gas turbine moving blade Gas turbine moving blade

F - Mech Eng,Light,Heat,Weapons

01

D

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

Patent

CA 2255230

Disclosed is a gas turbine moving blade assembly comprising a leading edge confronting a combustion gas flow, and a trailing edge, a cooling passage defined in an interior of the leading edge for causing cooling air to flow from a proximal end portion of the blade to a tip end of the blade, and a plurality of turbulators arranged in a direction transverse to a flow of the cooling air and slanted relative to the combustion gas flow. The plurality of turbulators includes long turbulators and short turbulators, both the long turbulators and the short turbulators being provided on facing inner wall surfaces of the cooling passage, and wherein the long turbulators and the short turbulators are slanted from the leading edge, in a direction into the flow of the cooling air, toward a downstream side of the combustion gas flow.

Affiliated with

Also associated with

Rating

Gas turbine moving blade does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas turbine moving blade, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine moving blade will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1488103