Fluid reaction surfaces (i.e. – impellers) – With fluid passage in working member communicating with... – Air and watercraft propellers
Reexamination Certificate
2007-07-10
2007-07-10
Edgar, Richard A. (Department: 3745)
Fluid reaction surfaces (i.e., impellers)
With fluid passage in working member communicating with...
Air and watercraft propellers
C416S09700R, C415S115000, C244S199100
Reexamination Certificate
active
10983654
ABSTRACT:
An arrangement for reducing vorticity downstream of a turbine nozzle guide vane34in a gas turbine engine. The arrangement including directing cooling air through the guide vane34and out through outlets40in directions to counteract the wave vorticity produced downstream of the guide vane34.
REFERENCES:
patent: 3039736 (1962-06-01), Pon
patent: 3776363 (1973-12-01), Kuethe
patent: 5503529 (1996-04-01), Anselmi et al.
patent: 6004095 (1999-12-01), Waitz et al.
patent: 2003/0143075 (2003-07-01), Fleck
Edgar Richard A.
Manelli Denison & Selter PLLC
Rolls-Royce plc
Taltavull W. Warren
LandOfFree
Vorticity control 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 Vorticity control in a gas turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Vorticity control in a gas turbine engine will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-3779287