Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Coating – specific composition or characteristic
Patent
1982-09-28
1991-09-24
Kwon, John T.
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Coating, specific composition or characteristic
416188, F01D 528
Patent
active
050510622
ABSTRACT:
A radial flow turbine rotor comprises a trunconical shaft and a plurality of blades provided on the periphery of the shaft and inclined to the axis of the shaft. The shaft and the blades are integrally formed of ceramics. The profile of the cross section of each blade, taken along a line perpendicular to the axis of the shaft, is straight between the tip and base of the blade. The tip of each blade is 1.2 to 2.0 mm thick, and each blade grows thicker from the tip toward the base.
REFERENCES:
patent: 4011295 (1977-03-01), Tree et al.
patent: 4076456, Tree et al.
patent: 4123199 (1978-10-01), Shimizu et al.
patent: 4125344 (1978-11-01), Tiefenbacher
patent: 4176519 (1979-12-01), Kronogard
patent: 4272954 (1981-06-01), Kronogard
patent: 4279576 (1981-07-01), Okano et al.
patent: 4408959 (1983-10-01), Long et al.
patent: 4653976 (1987-03-01), Blair et al.
Keramische Bauteile fur Fahrzeug-Gasturbinen 687 Mofortechnische Zeitschfft; vol. 39, No. 10 (1978,10).
Ando Akio
Inoue Koichi
Nakanishi Masae
Okada Syozi
Kwon John T.
Tokyo Shibaura Denki Kabushiki Kaisha
LandOfFree
Radial flow turbine rotor does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Radial flow turbine rotor, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Radial flow turbine rotor will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1693868