Contoured supersonic nozzle

Details Contoured supersonic nozzle Contoured supersonic nozzle

1978-07-12

1981-08-25

Marbert, James B.

Fluid sprinkling, spraying, and diffusing

Combined or convertible

415216, 415181, B05B 1500, B05B 1700

Patent

active

RE0307203

ABSTRACT:
A convergent-divergent nozzle for supersonic expansion of turbine motive fluid is presented wherein the major part of contouring of the flow paths between adjacent nozzles is in the direction between top and bottom walls between adjacent nozzle side walls, the contouring being accomplished by contoured top and bottom nozzle walls which are asymmetrically contoured in an axial direction to define a symmetric flow path therebetween.

REFERENCES:
patent: 767689 (1904-08-01), Hedlund
patent: 2735612 (1956-02-01), Hausmann
patent: 2910005 (1959-10-01), Angell et al.
patent: 3804335 (1974-04-01), Sohre

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