Turbine vane of a gas turbine

Details Turbine vane of a gas turbine Turbine vane of a gas turbine

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/18 (2006.01) F01D 5/28 (2006.01) F01D 9/04 (2006.01)

Patent

CA 2665544

The invention relates to a vane (10) of a gas turbine, especially a gas turbine aircraft engine, comprising a base body (11) provided with an outer surface forming a suction side (13) and a pressure side (12), said outer surface of the base body being at least partially coated with a heat insulating layer (16). According to the invention, the heat insulating layer (16) extends continuously at least mostly over the suction side (13) and mostly over the pressure side (12) of the surface of the base body (11) of the vane, the layer thickness of the heat insulating layer (16) being variable.

L'invention concerne une aube (10) d'une turbine à gaz, en particulier d'un turboréacteur. Cette aube (10) comprend un corps de base (11) présentant une surface extérieure qui forme l'extrados (13) et l'intrados (12) de l'aube (10), cette surface extérieure étant recouverte au moins partiellement d'une couche calorifuge (16). Selon l'invention, ladite couche calorifuge (16) s'étend de façon continue au moins en majeure partie sur l'extrados (13) et en majeure partie sur l'intrados (12) de la surface du corps de base (11) de l'aube (10), l'épaisseur de cette couche calorifuge (16) étant variable.

Affiliated with

Also associated with

Rating

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

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1398490