Turbine blade with improved aerodynamic performance

Details Turbine blade with improved aerodynamic performance Turbine blade with improved aerodynamic performance

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/14 (2006.01)

Patent

CA 2740030

According to the invention, one or more projections (25) are formed on the turbine blade on the suction side (21) thereof in the vicinity of the trailing edge (17) thereof. Such protrusions reduce the separation area in the vicinity of the blade surface, which is responsible for the interference affecting the turbine yield.

Selon l'invention, une ou plusieurs protubérances (25) sont prévues sur l'aube de turbine, côté extrados (21) au voisinage de son bord de fuite (17). De telles protubérances permettent de réduire la zone de décollement au voisinage de la surface de l'aube, responsable de perturbations affectant le rendement de la turbine.

Affiliated with

Also associated with

Rating

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

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1886541