A bleed structure for a bleed passage in a gas turbine engine

Details A bleed structure for a bleed passage in a gas turbine engine A bleed structure for a bleed passage in a gas turbine engine

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 3/075 (2006.01) F02K 3/02 (2006.01)

Patent

CA 2598983

The invention relates to a bleed structure (17) for a bleed passage in a gas turbine engine. The structure comprises a first wall portion (18) defining a first side of an opening for the passage, and a second wall portion (19) defining a second side, opposite the first side of the opening. The first and second wall portions (18; 19) end at different positions in an extension direction of the opening.

L'invention porte sur une structure de ventilation (17) pour un passage de ventilation dans un moteur à turbine à gaz. Cette structure comprend une première partie de paroi (18) définissant un premier côté d'une ouverture pour le passage, et une seconde partie de paroi (19) définissant un second côté, opposé au premier côté de l'ouverture. La première et la seconde partie de paroi (18, 19) se terminent sur des positions différentes dans le sens d'extension de l'ouverture.

Affiliated with

Also associated with

Rating

A bleed structure for a bleed passage in a gas turbine engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with A bleed structure for a bleed passage in a gas turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and A bleed structure for a bleed passage in a gas turbine engine will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1593212