F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 25/12 (2006.01) F01D 25/18 (2006.01) F02C 9/18 (2006.01) F28D 1/06 (2006.01)
Patent
CA 2661707
A cooling apparatus for cooling a fluid in a bypass gas turbine engine comprises a heat exchanger (34) disposed within a bypass duct (30) and accommodated by a sub passage (50) defined by a flow divider (48) affixed to an annular wall of the bypass duct (30). The sub-passage (50) defines an open upstream end (52) and an open downstream end (54) to direct a portion of the bypass air flow to pass therethrough.
L'invention concerne un appareil de refroidissement destiné au refroidissement d'un fluide dans un moteur à double flux, comprenant un échangeur de chaleur (34) disposé dans un canal de flux secondaire (30), complété d'un passage secondaire (50) défini par un diviseur de débit (48) fixé à une paroi annulaire du canal de flux secondaire (30). Ce passage secondaire (50) comprend une extrémité amont ouverte (52) et une extrémité aval ouverte (54) permettant de diriger une partie du flux secondaire dans le passage secondaire (50).
Bernard Martin
Ciampa Alessandro
Germain Patrick
Lamarre Sylvain
Marrano Roberto
Norton Rose Or S.e.n.c.r.l.,s.r.l./llp
Pratt & Whitney Canada Corp.
LandOfFree
Turbofan bypass duct air cooled fluid cooler installation does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Turbofan bypass duct air cooled fluid cooler installation, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbofan bypass duct air cooled fluid cooler installation will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1375464