Devices for controlling gas flows

• US 4,336,590 A
• Filed: 05/01/1980
• Issued: 06/22/1982
• Est. Priority Date: 05/02/1979
• Status: Expired due to Term

• Current Assignee: Intertechnique SA (Safran SA)
• Original Assignee: Intertechnique SA (Safran SA)
• Inventors: Jacq, Georges, Damico, Pierre
• Primary Examiner(s): Wise, Edward J.
• Application Number:
  US06/145,844
• Time in Patent Office: 782 Days
• Field of Search: 364/413, 364/418, 364/510, 128/204.21, 128/204.22, 128/205.11, 128/205.24, 128/205.25, 128/1 A, 73/3, 73/23, 73/199
• US Class Current: 128/204.21
• CPC Class Codes: A62B 9/027 pilot operated, i.e. controlled by valve means sensitive to a reduced downstream pressure
• CPC Class Codes: B64D 10/00 Flight suits helmets in general A42B3/00; breathing helmets A62B18/00

Abstract

A regulating apparatus for supplying a receiving unit with gas from a pressurized source comprises a valve piloted by a two-position solenoid valve controlled by a computer which receives data from pressure sensors. When used as a demand breathing regulator, the apparatus has a main valve for connecting a source of pressurized breathing gas and a breathing mask and a pilot diaphragm subjected to the pressure in the mask. A sensor senses the movements of a diaphragm or the pressure in the mask. A solenoid valve controls the pressure in a pilot chamber of the main valve.

Claims

1. In a transportation aircraft, an apparatus for distributing oxygen to passenger breathing masks, comprising:

a source of oxygen under pressure;

an oxygen distribution line;

a first gas flow control device having an inlet connected to said source and an outlet connected to said distribution line;

a pressure reducer having an inlet connected to said source and adapted to deliver oxygen at a predetermined reduced pressure at an outlet;

a second gas flow control device having an inlet connected to the outlet of said pressure reducer and an outlet connected to said line;

each of said gas flow control devices having a servo-valve controlling communication between the inlet and the outlet thereof and a pilot two-position solenoid valve for controlling said servo-valve in response to a control signal;

sensor means for sensing the pressure in the cabin of the aircraft and delivering a signal responsive of said pressure; and

computer control means connected to receive said pressure responsive signal for delivering a control signal to the solenoid valve of said first gas flow control device in response to said pressure responsive signal being lower than a threshold corresponding to a first predetermined altitude and for delivering a temporary control signal to the solenoid valve of said first gas flow control device and then a continuous control signal to the solenoid valve of said second gas flow control device in response to said pressure responsive signal being comprised between said first threshold and a second threshold corresponding to a second altitude lower than the first altitude.

2. Demand breathing regulator apparatus for controlling a respiratory gas flow to an inhalation mask from a respiratory gas source, comprising:

a gas flow control device having a housing provided with an inlet for connection to the gas source and an outlet for connection with the mask;

a servo valve controlling communication between said inlet and said outlet and defining a control chamber in said housing, said servo valve being controlled by pressure variations in said control chamber;

first sensor means arranged to deliver an electrical signal representative of the pressure variations at said outlet; and

second sensor means arranged to deliver an electric signal representative of the pressure at said outlet;

electrically controlled valve means operatively associated with said control chamber to control the pressure prevailing in said chamber;

and computer means connected to receive electrical input signals from said sensor means and to deliver electric control signals to said electrically controlled valve means in accordance with a stored program responsive to the input signals.

3. Demand breathing regulator apparatus according to claim 2, wherein said electrically controlled valve means comprises a first solenoid valve controlling communication between said control chamber and said outlet and a second solenoid valve controlling communication between said control chamber and said gas source.

4. Apparatus according to claim 2 or 3, wherein said servo valve comprises a diaphragm separating said control chamber from a space in said housing and a seat which separates said space into a zone receiving the pressure from the source and a zone connected to the mask by a dilution nozzle emerging into a chamber connected to the ambient atmosphere by a proportional electrically controlled valve controlled by said computer means.

5. Apparatus according to claim 2, wherein said computer means is arranged to further control g-valve means and to maintain a minimum output pressure of the g-valve.

6. Apparatus as in claim 2, wherein said electrically controlled valve means comprises an ON-OFF solenoid valve and said computer means is arranged to deliver electric control signals in the form of square pulses having a variable duty ratio.

7. Apparatus as in claim 2, further comprising a dilution nozzle in the gas path between said servo-valve and said outlet and an electrically controllable dilution control valve located on an airflow path from atmosphere to a location in said gas path immediately downstream of said dilution nozzle, wherein said computer means is arranged to deliver a control current to said dilution control valve which opens said dilution control valve by an amount in relation to the signal from said second sensor means which is in compliance with a stored program.

8. Apparatus according to claims 2 or 7, wherein said first sensor means comprises a control compartment formed in said housing, diaphragm means between said control compartment and said outlet, electrically controlled valve means operatively associated with said control compartment to meter the pressure prevailing therein, third sensor means arranged to deliver an electric signal representative of the pressure in said control compartment, and a capacitor probe for delivering an electric signal representative of the movements of said diaphragm responsive to demand and wherein said computer means are arranged to control the pressure in said control compartment responsive to the signal delivered by said third sensor means.

9. A g-valve apparatus for controlling a gas flow to a g-suit from a pressurized gas source, comprising:

a gas flow control device having a housing provided with an inlet for connection to the gas source and an outlet for connection with the g-suit and formed with an inner chamber in permanent communication with said outlet;

servo exhaust valve means controlling communication between said chamber and atmosphere and piloted by the pressure which prevails in a control compartment connected by a calibrated leak orifice to said chamber;

a first two-position solenoid valve located to control communication between said inlet and said chamber;

a second two-position solenoid valve controlling communication between the control compartment and the ambient atmosphere;

acceleration sensor means carried by the housing and arranged to deliver electrice signals representative of the acceleration impressed to the housing in a predetermined direction; and

pressure sensor means carried by the housing and arranged to deliver electric signals representative of the pressure in said chamber;

and computer means connected to receive the signals from said sensors and arranged to deliver control signal to said solenoid valves as a function of the signals from said sensors and a stored program.

10. An apparatus according to claim 9, wherein said computer means is arranged for connection with a sensor mounted on the joy-stick of the aircraft equipped with the apparatus and for establishing an output pressure in said chamber as soon as the position of the joy stick of the aircraft anticipates an acceleration.