Radial turbines

Fluid reaction surfaces (i.e. – impellers) – Rotor having flow confining or deflecting web – shroud or... – Radially extending web or end plate

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Details

415213R, F01D 108, F01D 504

Patent

active

042048079

ABSTRACT:
A radial turbine having rotor blades, each positioned against the exit surface of the turbine at an angle equal to the angle of the relative velocity, between a gas flow pattern simulating the actual velocity of combustion gas flow through a space between two adjacent turbine blades and a rotating turbine rotor blade, against the turbine exit surface.

REFERENCES:
patent: 2965287 (1960-12-01), Schug
Journal of Engineering for Power-Jan. 1971, Trans. A.S.M.E., vol. 93, No. 1, pp. 81-102.

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