Pressure control system

Fluid handling – Flow affected by fluid contact – energy field or coanda effect – Means to regulate or vary operation of device

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Details

137 81, B64D 1300

Patent

active

039747522

ABSTRACT:
A cabin pressure control system for an aircraft in which the controller provides control signals to an outflow valve by way of a pneumatic amplifier relay means, has the memory or rate chamber of the controller providing the pneumatic signal to the relay instead of the usual case where the signal comes from the reference pressure chamber. Any one of several forms of relays may be used in this novel system. One form of relay includes a feedback signal from the outflow valve.

REFERENCES:
patent: 2513332 (1950-07-01), Kemper
patent: 2556159 (1951-06-01), Arthur
patent: 2669175 (1954-02-01), Fischer
patent: 2873661 (1959-02-01), Fischer
patent: 2900890 (1959-08-01), Fischer et al.
patent: 3376802 (1968-04-01), Emmons
patent: 3650197 (1972-03-01), Voronin et al.

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