Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Hollow
Reexamination Certificate
2006-09-12
2006-09-12
Nguyen, Ninh H. (Department: 3745)
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Hollow
C416S248000
Reexamination Certificate
active
07104762
ABSTRACT:
The control stage buckets for a steam turbine have airfoils which are hollowed out to form an interior cavity within the airfoil. The cavity opens through the radial inner platform of the bucket and terminates short of the tip of the bucket. The buckets are therefore of reduced weight. This reduced weight causes reduced creep damage in the axially extending dovetails along the rotor rim.
REFERENCES:
patent: 2639119 (1953-05-01), Greenwald
patent: 4142824 (1979-03-01), Andersen
patent: 5062769 (1991-11-01), Ortolano
patent: 6923616 (2005-08-01), McRae et al.
Dausacker Paul Walter
Deallenbach Robert Edward
Holliday Allyn Keith
General Electric Company
Nguyen Ninh H.
Nixon & Vanderhye P.C.
LandOfFree
Reduced weight control stage for a high temperature steam... does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Reduced weight control stage for a high temperature steam..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Reduced weight control stage for a high temperature steam... will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-3570907