F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
170/79
F01D 5/30 (2006.01) F01D 11/08 (2006.01)
Patent
CA 1158563
Abstract of the Disclosure A turbine engine is provided with a stationary shroud surrounding a rotor provided with a plurality of radially extending blades. The stationary shroud includes a plurality of spaced-apart lands defining therebetween openings to deflect the flow leakage from the high pressure side of each blade to the low pressure side of the respective blade.
387536
Okapuu Ulo
Patel Kiritkumar V.
Pratt & Whitney Aircraft Of Canada Limited
Swabey Ogilvy Renault
LandOfFree
Circumferentially grooved shroud liner does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Circumferentially grooved shroud liner, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Circumferentially grooved shroud liner will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-802638