Fluid-stream driven aircraft

Details Fluid-stream driven aircraft Fluid-stream driven aircraft

1974-07-10

1977-03-01

Blix, Trygve M.

Aeronautics and astronautics

Aircraft power plants

B64D 3100

Patent

active

040098494

ABSTRACT:
An aircraft body has a pair of hydraulic fluid operated motors mounted on it, a pair of stream-creating devices driven by the motors and symmetrically arranged on opposite sides of the axis of symmetry of the body. One or more hydraulic fluid-flow producing devices has at least a pair of separate fluid-handling chambers each connected to one of a pair of separate outlets, and including arrangements for fluid-tight separation of the chambers and outlets, so that fluid from each chamber passes through only one of the outlets. A pair of displacement units is associated with the fluid-handling chambers, respectively, and an equally acting actuator arrangement cooperates equally with both of the two displacement units for maintaining equal movements of the two displacement units so that fluid flows in the outlets at proportionate and equal flow rates. A pair of delivery passages connects each of the outlets with a different one of the motors, respectively.

REFERENCES:
patent: 1827438 (1931-10-01), Rauch
patent: 1939156 (1933-12-01), Wright
patent: 2212490 (1940-08-01), Adler
patent: 2349286 (1944-05-01), Kreitner et al.
patent: 2454138 (1948-11-01), Delzer
patent: 2514822 (1950-07-01), Wolfe
patent: 2804016 (1957-08-01), Moore

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