Dual-entry centrifugal compressor

Rotary kinetic fluid motors or pumps – Axially opposed working fluid paths to or from runner – Pump impeller means

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Details

415102, 415211, 416184, F01D 302, F04D 2938

Patent

active

045306397

ABSTRACT:
The improved dual-entry radial compressor rotor of the present invention has two sets of alternating full length and partial length blades on a symmetrical hub, with the partial length blades on one hub side terminating at the rotor high velocity exit coincident with the full length blades on the other hub side, to smooth the gas velocity profile in the tangential direction. Aerodynamically shaped sawtooth-profiled reliefs are provided in the hub radial portion between the blade tips to allow induced pressure differentials between the flow paths to smooth the axial velocity profile.

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patent: 1674543 (1928-06-01), Clifton
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patent: 2465671 (1949-03-01), Van Millingen et al.
patent: 3430921 (1969-03-01), Dewey
patent: 3625003 (1971-12-01), Liddle et al.
patent: 3642062 (1972-02-01), Edmaier et al.
patent: 3953150 (1976-04-01), Onal
Johnson, D. and Mowill, R. J., "Aegidius Elling--A Norwegian Gas Turbine Pioneer", Norsk Teknisk Museum, Oslo 1968.
Mowill, R. J. and Strom, S., "New Radial Engine Technology from Kongsburg", ASME, 83-Gt-221, Mar. 1983.
Thomassen Holland b.N. publication.
AiResearch GT-85 publication.

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