Bladed member, in particular for an axial turbine of an...

Details Bladed member, in particular for an axial turbine of an... Bladed member, in particular for an axial turbine of an...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/14 (2006.01)

Patent

CA 2411873

A bladed member, particularly for an axial turbine of an aircraft engine; the bladed member having at least one aerodynamic profile defined by a back face and an underside face connected to each other along a leading edge and a trailing edge and defining respective nozzles for a stream of gas; the underside face having a projecting rib elongated in a direction crosswise to the leading and trailing edges.

Affiliated with

Also associated with

Rating

Bladed member, in particular for an axial turbine of an... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Bladed member, in particular for an axial turbine of an..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Bladed member, in particular for an axial turbine of an... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1766955