Diffuser/ejector system for a very high vacuum environment

Measuring and testing – Vehicle chassis – Steering

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417159, G01M 1500

Patent

active

044547536

ABSTRACT:
A system for testing space engines at sea level under a very low pressure environment. The system includes a space simulation chamber connected to a diffuser which has two variable area ratio ejectors connected to it in tandem. Each of the ejectors is driven by a jet engine, preferably a turbo jet. The system is capable of providing a low pressure environment of about three or four millimeters of mercury for testing of engines mounted in the space simulation chamber. The system also may be used for other purposes requiring very high vacuum, such as evaporation and dehydration of food products or drugs.

REFERENCES:
patent: 2939316 (1960-06-01), Beecher et al.
patent: 3015231 (1962-01-01), Ganahl

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