Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Hollow
Patent
1992-08-21
1994-03-29
Look, Edward K.
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Hollow
416 96A, 416232, F01D 518
Patent
active
052979377
ABSTRACT:
A hollow rotor blade of a gas turbine includes a shaped core accommodated within a hollow space formed between two skins and joined to the skins. The fatigue strength at a portion where the skins are joined to the core is enhanced. More specifically, the portions of the skins joined with the core are in the form of island-shaped protrusions, and the core is joined to these protrusions by solid-phase diffusion bonding, diffusion-brazing, liquid-phase diffusion bonding, and the like.
REFERENCES:
patent: 3222774 (1965-12-01), Kump et al.
patent: 3566493 (1971-03-01), Poucher et al.
patent: 3806276 (1974-04-01), Aspinwall
patent: 3858290 (1975-01-01), Albani
patent: 4043498 (1977-08-01), Conn
patent: 4208222 (1980-06-01), Barlow et al.
patent: 4583914 (1986-04-01), Craig et al.
patent: 4604780 (1986-08-01), Metcalfe
patent: 4768700 (1988-09-01), Chen
Makita Haruomi
Umetani Masahiko
Look Edward K.
Mitsubishi Jukogyo Kabushiki Kaisha
Sgantzos Mark
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