Ram air turbines

Rotary kinetic fluid motors or pumps – Resilient or movably mounted blade portion or axially... – Yieldingly or pivotedly mounted or flexible blade

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Details

415 25, 416186A, 416 45, F01D 702

Patent

active

045403376

ABSTRACT:
A cup shaped disc (13) consisting of a central portion (20) having radially extending blades (18) is attached with its central portion to the protruding hub portion (12) of a radial flow turbine wheel (2) consisting of a backing plate (10) extending transversely to its rotational axis (7) and having axially protruding turbine blades (11) in addition to the protruding hub. At high rotational speeds this disc (13) will tend to straighten out, whereby the effective portion of the turbine blades will be reduced and the increase in the rotational speed restricted. This is of importance in ram air turbines for missiles.

REFERENCES:
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patent: 1186289 (1916-06-01), Dalen
patent: 2459815 (1949-01-01), Hammell
patent: 2766964 (1956-10-01), Almquist et al.
patent: 3069137 (1962-12-01), Barr
patent: 3128989 (1964-04-01), Allingham
patent: 3352536 (1967-11-01), Almquist
patent: 3733143 (1973-05-01), Theis
patent: 3856432 (1974-12-01), Campagnuolo et al.
patent: 4161371 (1979-07-01), Sheppa

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