Gas distribution system in an airplane

Aeronautics and astronautics – Aircraft structure – Passenger or crew accommodation

Reexamination Certificate

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Details

C137S110000, C137S899200

Reexamination Certificate

active

06935593

ABSTRACT:
A gas distribution system in an airplane has improved reliability of operation with a first supply line (7) and a second supply line (9) for pressurized gas connected to a pressurized gas source (2) via a branching site (6) with a second shut-off valve (10). The pressure in the supply lines (7, 9) is determined with a pressure-measuring means (24). An evaluating device (24) for the measured pressure signal is provided for sending a closing signal to the shut-off valve (8, 10) of the supply line (7, 9) in which a pressure drop of consequence occurs.

REFERENCES:
patent: 2934293 (1960-04-01), Boehme et al.
patent: 3903729 (1975-09-01), Covington
patent: 4197868 (1980-04-01), Carson
patent: 4355654 (1982-10-01), Levesque et al.
patent: 4507128 (1985-03-01), Werner
patent: 4651559 (1987-03-01), Horigome et al.
patent: 195 31 916 (1997-03-01), None
patent: 1 577 943 (1980-10-01), None
patent: WO 99/04858 (1999-02-01), None

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