Circumferentially grooved shroud liner

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Means to seal radial flow pump runner inlet from outlet

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Details

415170R, F01D 1108, F01D 520

Patent

active

044667728

ABSTRACT:
A turbine is provided with a stationary shroud surrounding a rotor provided with a plurality of radially extending blades. The stationary shroud includes a plurality of spaced-apart lands defining therebetween openings to deflect the flow leakage from the high pressure side of each blade to the low pressure side of the respective blade.

REFERENCES:
patent: 1651855 (1924-06-01), Warren
patent: 1708044 (1924-09-01), Baumann
patent: 3843278 (1974-10-01), Torell
patent: 3854842 (1974-12-01), Caudill
patent: 3867061 (1975-02-01), Moskowitz
patent: 4055041 (1977-10-01), Adamson et al.
patent: 4239452 (1980-12-01), Roberts
Aircraft Propulsion-NASA SP-259-NASA Lewis Research Center, Cleveland, Ohio, Nov. 18-19, 1970, Scientific & Technical Information Office, 1971.

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