Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Hollow
Patent
1994-04-14
1995-04-18
Look, Edward K.
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Hollow
416232, F01D 518
Patent
active
054073260
ABSTRACT:
A hollow blade for a turbomachine includes a unitary body having a multiplicity of transverse cavities in at least the aerofoil shaped portion of the blade, and plugs disposed within the cavities for restoring the surface continuity of the intrados and extrados faces of the aerofoil shaped portion, the plugs being rigidly secured to the unitary body, such as by welding.
REFERENCES:
patent: 1380431 (1921-06-01), Smith
patent: 1718061 (1929-06-01), Miller
patent: 1778340 (1930-10-01), Reed
patent: 1855589 (1932-04-01), Reed
patent: 2221722 (1940-11-01), Reynolds
patent: 2862686 (1958-12-01), Bartlett
patent: 2882974 (1959-04-01), Boegehold
patent: 3628226 (1971-12-01), Nelson
patent: 3761201 (1973-09-01), Silverstein et al.
patent: 4882823 (1989-11-01), Weisert et al.
Abstract of Japanese Patent 56 88902, Jul. 18, 1981.
Larson James A.
Look Edward K.
Societe Nationale d'Etude et de Construction de Moteurs d'Aviati
LandOfFree
Hollow blade for a turbomachine does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Hollow blade for a turbomachine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Hollow blade for a turbomachine will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-63653