Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Tined or irregular periphery
Patent
1988-11-18
1989-10-24
Garrett, Robert E.
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Tined or irregular periphery
416224, F04D 2938
Patent
active
048758310
ABSTRACT:
A blade of a compressor rotor has its tip provided with at least one discontinuous sealing lip formed by two half lips arranged on opposite sides of the blade asymmetrically with respect to a transverse sectional plane of the blade tip, either with or without overlap of the half lips in the direction of the chord of the blade.
REFERENCES:
patent: 2459850 (1949-01-01), Stine
Garrett Robert E.
Kwon John T.
Societe Nationale d'Etude et de Construction de Moteurs d'Aviati
LandOfFree
Compressor rotor blade having a tip with asymmetric lips does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Compressor rotor blade having a tip with asymmetric lips, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Compressor rotor blade having a tip with asymmetric lips will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1586018